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b BYRON UNIT 2 PRESSURE TEMPERATURE LIMITS REPORT (PTLR)
e b
BYRON UNIT 2 PRESSURE TEMPERATURE LIMITS REPORT (PTLR)
(Revised November 3,1997)
(Revised November 3,1997)
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    *~                                                                                                                     '
*~
BYRON UNIT 2
BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT-Table of Contents -
    -*.                                              PRESSURE AND TEMPERATURE LIMITS REPORT-Table of Contents -
Section Page i
Section                                                                                                                             Page       I l
1.0
i 1.0         Introductions                                                                                                         1 s
 
1 2.0         Operating Limits                                                                                                     1
===Introductions===
                                                                                                                                                                                ]
1 s
2.1   RCS Pressure and Temperature (P/T) Limits                                                                       1 2.2   Low Temperature Overpressure Protection (LTOP) System Setpoints                                               2       l 2.3   LTOP Enable Temperature ~                                                                                     2-2.4   Reactor Vessel Boltup Temperature                                                                             3         .
1 2.0 Operating Limits 1
2.5   Reactor Vessel Minimum Pressurization Temperature                                                             3         l
]
                                - 3.0         Reactor Vessel Material Surveillance Progiam                                                                         9 4.0           Supplemental Data Tables                                                                                           11 i
2.1 RCS Pressure and Temperature (P/T) Limits 1
5.0           References                                                                                                         18 Attacluner*
2.2 Low Temperature Overpressure Protection (LTOP) System Setpoints 2
WCAP 14824, Revision 2 " Byron Unit 1 Heatup and Cooldown Limit Curves for Norr-Operation and Surveillance Weld Metal Integration for Byron and Braidwood," Novemv.r,                                                           !
l 2.3 LTOP Enable Temperature ~
1997.
2-2.4 Reactor Vessel Boltup Temperature 3
2.5 Reactor Vessel Minimum Pressurization Temperature 3
l
- 3.0 Reactor Vessel Material Surveillance Progiam 9
4.0 Supplemental Data Tables 11 i
5.0 References 18 Attacluner*
WCAP 14824, Revision 2 " Byron Unit 1 Heatup and Cooldown Limit Curves for Norr-Operation and Surveillance Weld Metal Integration for Byron and Braidwood," Novemv.r, 1997.
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i BYRONo UNIT 2
{
{
5 PRESSURE AND TEMI ERATURE LIMITS REPORT                                                                                                         {
PRESSURE AND TEMI ERATURE LIMITS REPORT
i List of Figures
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5 i
List of Figures
[
[
t Figure                                                                                                                                                     Page         {
t Figure Page
        ' 2.1         Byron Unit 2 Reactor Coolant System Heatup Limitadons (Heatup Rates up to                                                                   4 100' F/hr) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix 0 Methodology) 2.2         Byron Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates                                                                     5             '
{
' 2.1 Byron Unit 2 Reactor Coolant System Heatup Limitadons (Heatup Rates up to 4
100' F/hr) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix 0 Methodology) 2.2 Byron Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates 5
up to 100 'F/le) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors: Using 1996 Appendix G Methodology)
up to 100 'F/le) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors: Using 1996 Appendix G Methodology)
        - 2.3       Byron Unit 2 Maximum Allowable Nominal PORY Setpoints for the Low                                                                             7 Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY s
- 2.3 Byron Unit 2 Maximum Allowable Nominal PORY Setpoints for the Low 7
iii                                                                                       '
Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY s
iii


                                            .._ _ _ . _                                    . _ . _ . - . ~ . _ _
. _. _. -. ~. _ _
BYRON. UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT List of Tables Table                                                                                               Page                     ;
BYRON. UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT List of Tables Table Page 2.1 Byron Unit 2 Heatup and Cooldown Data Points at 12 EFPY 6
2.1 Byron Unit 2 Heatup and Cooldown Data Points at 12 EFPY                                             6                   i (Without Margins for Instrumentation Errors) 2.2 Data Points from Byron Unit 2 PORY Setpoints for the LTOP System                                   8 3.1 Byron Unit 2 Capsule Withdrawal Schedule                                                       10-4.1 ~ Byron Unit 2 Calculation of Chemistry Factors Using Surveillance Capsule Data                 12 L4.2 Byron Unit 2 Reactor Vessel Material Properties                                                 13 4.3 Summary of Byron Unit 2 Adjusted Reference Temperatures (ARTS) at the 1/4T                                               i 14 and 3/4T Locations for 12 EFPY 4.4 Byror. Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at                         15 12 EFPY at the Limiting Reactor Vessel Material Weld Metal (Based on Surveillance Capsule Data)                   ,
i (Without Margins for Instrumentation Errors) 2.2 Data Points from Byron Unit 2 PORY Setpoints for the LTOP System 8
't 4.5 RTns Values for Byron Unit 2 for 32 EFPY                                                                                 '
3.1 Byron Unit 2 Capsule Withdrawal Schedule 10-4.1
16 4.6 RTns Values for Byron Unit 2 for 48 EFPY                                                       17 1
~ Byron Unit 2 Calculation of Chemistry Factors Using Surveillance Capsule Data 12 L4.2 Byron Unit 2 Reactor Vessel Material Properties 13 4.3 Summary of Byron Unit 2 Adjusted Reference Temperatures (ARTS) at the 1/4T 14 i
and 3/4T Locations for 12 EFPY 4.4 Byror. Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 15 12 EFPY at the Limiting Reactor Vessel Material Weld Metal (Based on Surveillance Capsule Data)
't 4.5 RTns Values for Byron Unit 2 for 32 EFPY 16 4.6 RTns Values for Byron Unit 2 for 48 EFPY 17 1
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BYRON UNIT 2                                                 :
BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 1.0 Reactor Coolant System (RCS) Pressure and Temperature Limits Report (PTLR)
PRESSURE AND TEMPERATURE LIMITS REPORT 1.0   Reactor Coolant System (RCS) Pressure and Temperature Limits Report (PTLR)                             '
Reference to Technical Specifications (TS) numbers are given in both the Byron Station current Technical Specifications (CTS) and improved Technical Specifications (ITS). The CTS number is presented first, followed by the ITS number in brackets [ ).
Reference to Technical Specifications (TS) numbers are given in both the Byron Station current Technical Specifications (CTS) and improved Technical Specifications (ITS). The CTS number is presented first, followed by the ITS number in brackets [ ).
l This PTLR for Unit I has been prepared in accordance with the requirements of                           .
l This PTLR for Unit I has been prepared in accordance with the requirements of TS 6.9.1.1liilTS 5.6.6). Revisions to the PTLR shall be provided to the NRC after issuance.
TS 6.9.1.1liilTS 5.6.6). Revisions to the PTLR shall be provided to the NRC after issuance.             l l
l l
The Technical Specifications addressed in this report are listed below:
The Technical Specifications addressed in this report are listed below:
l LCO 3.4.9.1 Pressure / Temperature Limits; and                                                         ;
l LCO 3.4.9.1 Pressure / Temperature Limits; and LCO 3.4.9.3 Overpressure Protection Systems.
LCO 3.4.9.3 Overpressure Protection Systems.                                                           !
[ITS LCO 3.4.3 RCS Pressure and Temperature (P/T) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System).
[ITS LCO 3.4.3 RCS Pressure and Temperature (P/T) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System).
2.0   Operating Limits The PTLR limits were developed using a methodology specified in the Technical Specifications. The methodology listed in WCAP 14040 NP A (Reference 1) was used with four exceptions:
2.0 Operating Limits The PTLR limits were developed using a methodology specified in the Technical Specifications. The methodology listed in WCAP 14040 NP A (Reference 1) was used with four exceptions:
: a. Un of ENDF/B IV neutron transport cross section library and ENDF/B V dosimeter                       :
Un of ENDF/B IV neutron transport cross section library and ENDF/B V dosimeter a.
reaction cross s~ections,                       *                                                  '
reaction cross s~ections,
: b. Optional use of ASME Code Section XI, Appendix G, Article G 2000,1996 Addenda,
: b. Optional use of ASME Code Section XI, Appendix G, Article G 2000,1996 Addenda,
: c. Use of ASME Code Case N 514, and
: c. Use of ASME Code Case N 514, and
: d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.                                                                                    .
: d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.
WCAP-14824, Revision 2, is included as an attachment for reference. WCAP 14824, Rev. 2 contains the P/T cunts for Byron Unit 1, along with the weld metal data integration for Byron and Braidwood Units 1 and 2 and the Byron /Biaidwood fluence methodologyjustification for ENDF/B-VI cross sections. WCAP 14940 (Ref.14) contains the Byron Unit 2 Heatup and Cooldown Limit Curves applicable to 12 EFPY.
WCAP-14824, Revision 2, is included as an attachment for reference. WCAP 14824, Rev. 2 contains the P/T cunts for Byron Unit 1, along with the weld metal data integration for Byron and Braidwood Units 1 and 2 and the Byron /Biaidwood fluence methodologyjustification for ENDF/B-VI cross sections. WCAP 14940 (Ref.14) contains the Byron Unit 2 Heatup and Cooldown Limit Curves applicable to 12 EFPY.
2.1     RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [ITS LCO 3.4.3))
2.1 RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [ITS LCO 3.4.3))
2.1.1 The RCS temperature rate of-change limits defined in Reference 14 are:
2.1.1 The RCS temperature rate of-change limits defined in Reference 14 are:
: a. A maximum heatup of 100'F in any 1-hour period,
: a. A maximum heatup of 100'F in any 1-hour period,
Line 86: Line 103:
: c. A maximum temperature changt ofless than or equal to 10'F in any 1-bour period during inservice hydrostatic and leak testing operations above the heatup and cooldown limit cunes.
: c. A maximum temperature changt ofless than or equal to 10'F in any 1-bour period during inservice hydrostatic and leak testing operations above the heatup and cooldown limit cunes.
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IlYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2.1.2 The RCS P/T limits for '.catup, insenice hydrostatic and leak testing, and criticality are specified by Figure 2.. and Table 2.1. The RCS P/T limits for cooldown are shown in       j Figuie 2.2 and Table 2.1. These limits are defined in Reference 14. Consistent with the   l methodology described in Reference 1, the RCS P/T limits for heatup and cooldown shown in Figures 2.1 and 2.2 are provided without margins for instrument error. These limits were developed using ASME Code Section XI, Appendix 0, Article G 2000,1996 Addenda. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, mstrument uncertainties need not be con >ldered since appropriate station operating procedures ensure that the limits contained in the figures rnd table are not exceeded. The criticality limit curve specifies pressure temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix 0.
IlYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2.1.2 The RCS P/T limits for '.catup, insenice hydrostatic and leak testing, and criticality are specified by Figure 2.. and Table 2.1. The RCS P/T limits for cooldown are shown in j
Figuie 2.2 and Table 2.1. These limits are defined in Reference 14. Consistent with the methodology described in Reference 1, the RCS P/T limits for heatup and cooldown shown in Figures 2.1 and 2.2 are provided without margins for instrument error. These limits were developed using ASME Code Section XI, Appendix 0, Article G 2000,1996 Addenda. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, mstrument uncertainties need not be con >ldered since appropriate station operating procedures ensure that the limits contained in the figures rnd table are not exceeded. The criticality limit curve specifies pressure temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix 0.
The P/T limits for core operation (excep for low power physics testing) are that the reactor vessel must be at a temperature equal to or higher than the minimum temperature required for the inservice hydrostatic test, and at least 40*F higher than the minimum permissible temperature in the corresponding P/T curve for heatup and cooldown.
The P/T limits for core operation (excep for low power physics testing) are that the reactor vessel must be at a temperature equal to or higher than the minimum temperature required for the inservice hydrostatic test, and at least 40*F higher than the minimum permissible temperature in the corresponding P/T curve for heatup and cooldown.
2.2   Low Temperature Overpressure Protection (LTOP) System Setpoints (l.CO 3.4.9.3/
2.2 Low Temperature Overpressure Protection (LTOP) System Setpoints (l.CO 3.4.9.3/
[lTS LCO 3.4.12]).
[lTS LCO 3.4.12]).
The power operated relief valves (PORVs) shall each have lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13 and 15.
The power operated relief valves (PORVs) shall each have lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13 and 15.
The LTOP setpoints are based on P/T limits which were established in accordance .vith 10 CFR 50, Appendix G without ailowance for instmmentation error and in accordance with the methodology described in Reference 1. The LTOP PORV maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.
The LTOP setpoints are based on P/T limits which were established in accordance.vith 10 CFR 50, Appendix G without ailowance for instmmentation error and in accordance with the methodology described in Reference 1. The LTOP PORV maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.
2.3   LTOP Enable Temperature The as analyzed LTOP enable temperature is 200*F (Reference 16).
2.3 LTOP Enable Temperature The as analyzed LTOP enable temperature is 200*F (Reference 16).
The TS required enable temperature for the PORVs shall be 2 350'F RCS temperature.
The TS required enable temperature for the PORVs shall be 2 350'F RCS temperature.
(Byron Unit 2 procedures goveming the heatup and cooldown of the RCS require the arming of the LTOP System for RCS temperature of 350'F and below and disarming of LTOP for RCS temperature above 350'F).
(Byron Unit 2 procedures goveming the heatup and cooldown of the RCS require the arming of the LTOP System for RCS temperature of 350'F and below and disarming of LTOP for RCS temperature above 350'F).
Line 100: Line 122:
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      ..                                                                                                                                                                        -4                                                                                     !
-4 BYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2,4 Reactor Vessel Boltup Temperature (Non Technical Specification)
BYRON - UNIT 2                                                                                                                                   .
The minimum boltup teraperature for the Reactor Vessel Flange shall be h 60'F. Boltop is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and with the RCS vented to atmosphere (Reference 2).
PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2,4 Reactor Vessel Boltup Temperature (Non Technical Specification)
2.5 Reactor Vessel Minimum Pressuriution Temperature (Non-Technical SpecMication)-
The minimum boltup teraperature for the Reactor Vessel Flange shall be h 60'F. Boltop                                                                                                 !
The minimum temperature at which the Reactor Vessel may be pressurized (i.e., in an unvented condition) shall be 2 60'F, plus an allowance for the uncertainty of the temperature instrument, determined using a technique consistent with ISA S67.04-1994.
is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and with the RCS vented to atmosphere (Reference 2).
2.5 Reactor Vessel Minimum Pressuriution Temperature (Non-Technical SpecMication)-
The minimum temperature at which the Reactor Vessel may be pressurized (i.e., in an unvented condition) shall be 2 60'F, plus an allowance for the uncertainty of the temperature instrument, determined using a technique consistent with ISA S67.04-1994.                                                                                                   !
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~ -. -. -. -
BYRON . UMT 2 s
BYRON. UMT 2 s
4, PRESSURE AND TEMPERATURE LIMITS REPORT MATERIAL PROPERTY BASIS i
PRESSURE AND TEMPERATURE LIMITS REPORT 4,
LIMITING MATERIAL: CIRCUMFERENTIAL WELD iusing eurv. capsule data)                                                                                                                                                                                                                                         !
MATERIAL PROPERTY BASIS i
LIMITING ART VALUES AT 12 EFPY:                                                                                           ./ IT, 87,6'F                                                                                                                                                                   i 3s4T. 71.S'F 2500                                                                         . .                                ;                  ,.                          ,
LIMITING MATERIAL: CIRCUMFERENTIAL WELD iusing eurv. capsule data)
                        ,                            : is...                   ....                        , , .                        .                            i       ..                    ,.        .      .:, ..                        . . .                      .
LIMITING ART VALUES AT 12 EFPY:
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e i                          s ~' I~I's                          s 750            lll'                            l                       ,                                                  :                                                        ;                                                                              '
250 e;3 Boitup x
g                            ie i a               e <      t                        t ll:'                    :
Terr'p.
I 8 i                                                 i                                                  ee                    .
c R a t i,c a t a t y t wit inson ser synnostaticsass,o o,r i
i                                                               ,                                     ; 6 g                  g m                              l                4              l
(j ftWPERATUS8 (345 F)0 FOR TRE I f f f I I I
                                                                                            #          f                I                                          (
388?let PERIOD UP 7
                                                                        '                  '                                                                                                                                                                l i a f 4                ie *
It.e IFPY 8 ' '
                        "            500                                                                                                                          '                                    '
0 1 I i i J f e
a
i-0 50 160 150 200 250 3$0 3$0 400 4$0 500 Moderator Temperature (Deg.F)
                                                +                                                                                                                  la                                              ,
Figure 2.1 Byron Unit 2 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/br)
ll          l i            x                                                                                                  i,          . .            .
Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors) l 4
                      ~                                                                                                                                         6                # %                                                                                              **          , . . .
l
e;3 250          ,                                        Boitup                                                             :
                                                                                                                                                                                  '              x                                                                                 ' '          '      - -
Terr'p.                                                                           cinson                                        t        wit R a t i ,c     ser   ata    synnostaticsass,o ty                                                    o ,r i
(j                       .-                                                                                                              '
                                                                                                                                                                '                                                                                        FOR TRE I f f f I I 1 I i i J f I
ftWPERATUS8 388?let                         PERIOD             (345  UP F)0  7             It.e IFPY                               8 ' '
0                                                                                       e                             i-0                         50                 160                         150                     200                             250                       3$0                       3$0                 400                         4$0                     500 Moderator Temperature                                                                                                                                                                   (Deg.F)
Figure 2.1
"                    Byron Unit 2 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/br) l Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors)
!                                                                                                                                                4 l


                  .  .        -. - -                            .                    .      --                            - - _ -                                      -                        _~             .                    -                    .                              .- . .
_~
BYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT MATERIAL PROPERTY BASIS LIMITING MATERIAL: CIRCUMFERENTIAL WELD (using sury. capsule cata)
BYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT MATERIAL PROPERTY BASIS LIMITING MATERIAL: CIRCUMFERENTIAL WELD (using sury. capsule cata)
LIMITING ART VALUES AT 12 EFPY:                                                                       1/4T. 87.6'F 3/47, 71.5'F 2500                               ,.                    .
LIMITING ART VALUES AT 12 EFPY:
: ii........                                   ,  , ,            ,.                  .          ..                    4 4 .                    . . . .                    . . .                                        .
1/4T. 87.6'F 3/47, 71.5'F 2500
i       6         e                                       I     I             6i                  i i t                       I e .
: ii........
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4 4.
no 2250 l
i 6
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e I
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I 6 i i i t I e.
                                                              .l.
A i a.
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t t
                                                                                                                                                                                                                                              . 4 s .
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m                                 .          . .            ,                              i _                       , .i                                                 . . r                 . . i             .      . . . .                  .                  .
.I 1 e t.
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                                          . . . .                            !            .                                          ei      -
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                                              .#     .     i         i i        !        4                      e                   i                      ii                                                  i a . ,                       .            .      .
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La                    E.,            OPERATloH                                                                      /                                            e                                e          *              * * . .                    t          . '
6' 4
                                                                                                                                ,                                                                                #          #              #        ; i              eiie g                        . i 4 i + t e              i
/
                                                                                                                              /
4 I e s
6 e 4              t          i t
6 1 4 i e m
                                                                                                                                                                                                                                            . # 8 1 a . , .
4 i.
                                                                                                                                                                                                                                                                        .f
I
                                                                      !                                                    /                                                                                    1    i
/
(/)                      t      t .4      1                                                            i                                              e                  a    i              l                         I i f .                   . I e . 6'         4                                                         /                                                 4                   I e                 s                         614                      i e               .
e i
m                        4 i .             I                                                       /                                                                             e               i                         i 1 3                     4 f         .
i 1 3 4 f e
                                        . ,                e                                                    p                                                                               .              n                         , ss                       , e U                             6             ,                                                f                                                                                                                                   . . .
p n
1250
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              ,                        . .              .                                              .                                                AcCEPTAstE                                                             .      . .              .      .
, e U
                                        .e                '                                      '
6 f
I                                                   OPERATION                                                       l             ' ' ' '                  ' '
1250 AcCEPTAstE
L                           t a t             i                                       j                                                                                                                       t               l . i.                   i4
' I OPERATION l
                                        . t i             6                                     /                                                                     . .          .          , i           e           i             e ! e e                   i     .
. e L
f                                                                     64                                                                6 t i.                    .*s
t a t i
                                                                                                                                      , 'I ,
j t
i      a    6                                                                                                                          . I i 6                 e           a 100O                , ,        ,    ,                                                                                          ,                , ,          .          ,            , ,,.                      . ,              ,        .          .
l. i.
                                            ...          .                                                                                1                           6 '         4 . 4                     l t i e                     e i .                     l .
i 4
U ll CC0L00VN                                                               ,                                                    ,    l                 , ,                                                  l                                 ,
. t i 6
750 -: UnM                                           ,                                            ,                                              ::                ,    ::                      ',l'             ':''                      ;;;
/
ra                   -
, i e
O      m,-                                                       l                                                           'll
i e ! e e i
                                                                                                                                                                                                                      ,:                ,l                 l               :::
i a
c-     500         7 noU V ll                 ll                 :              :
6 f
u         .
I 6 4
m       250             .
. I i 6 e
Botrup                                                                                                                                                                                     .'
a 6 t i.
o                         ,
.*s 100O 1
4
6 '
                                                    #                          Temp.
4. 4 l t i e e i.
i r     . .
l.
0 0                    50                 100           .150                         200                         250                     300                     350                         400                       4$0-                       500 M6derator Temperature                                                                                                                                                           (Deg.F)
U
" CC0L00VN l
l ll 750 -: UnM
',l' ra O
m,-
l
'll
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c-500 7 U V ll ll no u
m 250 Botrup o
Temp.
4 i
r 0
0 50 100
.150 200 250 300 350 400 4$0-500 M6derator Temperature (Deg.F)
Figure 2.2,
Figure 2.2,
        - Byron Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to 100 *F/hr)
- Byron Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to 100 *F/hr)
Applicable for the First 12 EFPY (Without Margios for Instrumentation Errors)
Applicable for the First 12 EFPY (Without Margios for Instrumentation Errors)
I
I m.-%...
* m.-%...                           - , , , , - , ,                    -n           ,-.e ,--              + ,+- -                       --r                               ---r                                           ,    w   w -
-n
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--r
---r w
w


  - . _ -                        - - -                . _            _ _ .                        _ . - -                  . . _ _ .        -                  _ ~ _ - . - _ - -
_ ~ _ -. - _ - -
1 BYRON . UNIT 2
1 BYRON. UNIT 2 l
                                                                                                                                                          .                                                                        l l
PRESSURE AND TEM 7ERATURE LIMITS REPORT 4
l 4 g PRESSURE AND TEM 7ERATURE LIMITS REPORT                                                                                                                   ;
g l
l
. Table 2,1 -
                                                                                                              . Table 2,1 -
Byron Unit 2 Heatup and Cooldown* Data Points at 12 EFPY" (Without margins for instrumentation errors)
Byron Unit 2 Heatup and Cooldown* Data Points at 12 EFPY" (Without margins for instrumentation errors)
HEATUP CURVES                             ,m                             COOLDOWN CURVES                                                                                          i 180 F HeetvP                           Test Curve       Cettecemy Unit Limit                                 stee8f State               25 000 F           SO 000 F         180 000 F T           P         T     -P       T           P                   T           P             T l P               T     I P       T           P 40           0     212       0       191       2000                 60             0           80       0         80           0   to           0 80         821     212     849     212         2485                 80           821         80       See         to         $38   to           437 SS         821     212     692                                       SS           821         SS     801         SS         551   SS           452                     ,
HEATUP CURVES COOLDOWN CURVES
70         821     212     878                                       70           821         70     814         70         885   70                                   '
,m i
488 75         821     212     889                                       75           421         75     821       . 75         881   75       488                         f 80 -       $21     212     882                                       80           821         40     $21         80         597   80         SOS SS          821    212      858                                        85          821          85      821        -85          814
180 F HeetvP Test Curve Cettecemy Unit Limit stee8f State 25 000 F SO 000 F 180 000 F T
P T
-P T
P T
P T l P T
I P T
P 40 0
212 0
191 2000 60 0
80 0
80 0
to 0
80 821 212 849 212 2485 80 821 80 See to
$38 to 437 SS 821 212 692 SS 821 SS 801 SS 551 SS 452 70 821 212 878 70 821 70 814 70 885 70 488 75 821 212 889 75 421 75 821
. 75 881 75 488 f
80 -
$21 212 882 80 821 40
$21 80 597 80 SOS
{
{
85       528 90         421     212     457                                       90           821         to       821         90         821   90       548                         !
SS 821 212 858 85 821 85 821
95         821     212     859                                       95           821         95       421         95         421   95       572                         l 100         821     212     883                                       100         821         100       821         100         821   100       599 105         821     212     870                                       108         821         105     821         10!         821   105       821 110         821     212       679                                       110         821         110     821         110       821   110       $21 115         821     212       890                                       115         421         115     421         115         421   its       821 120         821     212       703                                       120         821         120     821         120         821   120
-85 814 85 528 90 421 212 457 90 821 to 821 90 821 90 548 95 821 212 859 95 821 95 421 95 421 95 572 l
                                                                                                            ,                                                                                        821 125         821     212       719                                       125         821         128     421         125         421   125 821 130         821     212     738                                       130         $1. I 1             821         130       821   130       821                         '
100 821 212 883 100 821 100 821 100 821 100 599 105 821 212 870 108 821 105 821 10!
135         821     212     758                                       135         821       135       821         135       i't21 135       : .?                         (
821 105 821 110 821 212 679 110 821 110 821 110 821 110
140         821     212     781                                       140         821       140       821         140       821   140       821 145         821     212     807                                       145         821         145       821         145       821   145       821 150         821     212     435                                       150         821         150       821         150 -     $21   150       821 150         738     215       888                                       150         1045       150     1028       150       tote   150       1008
$21 115 821 212 890 115 421 115 421 115 421 its 821 120 821 212 703 120 821 120 821 120 821 120 821 125 821 212 719 125 821 128 421 125 421 125 821 130 821 212 738 130
.                                                155         758     220       900             1 155       41087         155     1074       155       1088   155     1088                           >
$1. I 1 821 130 821 130 821 135 821 212 758 135 821 135 821 135 i't21 135
180         781     225       937           l                         150         1132         180     1123       100       1120   180     1131 185
:.?
                                                                                                                                                                                                        ~
(
807 ,   230       977           i                         185         1180         185     1177       185       1177 170         438     235     1021           l                           170         1232 175 !       088     240     1088                                       175         1248 180 1 900           245     1119                                       180       1349                                                       l 185         937     250     1174                                       185       1413 190         977     255                                                 190       1483 12ja 195         1021   280       1297                                     195         1558 200         1088   285       1308                                     200         1838 205         1119   270       1441                                     205         1725 210         1174   275     1521                                       U0         1818 215         1233   280     1807                                       til         1918 220         1297     285     1899                                       220       2028 225         1388     290     1798                                       225       2141 230         1441     295     1905                                       230       2288 235       ~1521     300     2020                                       235       2400 240         1807     30$     2143 245         1899     310     2275 250         1794     315     2417 255         190$
140 821 212 781 140 821 140 821 140 821 140 821 145 821 212 807 145 821 145 821 145 821 145 821 150 821 212 435 150 821 150 821 150 -
280         2020 285         2143 270         2275
$21 150 821 150 738 215 888 150 1045 150 1028 150 tote 150 1008 155 758 220 900 1
                                                                                        ~
155 41087 155 1074 155 1088 155 1088 180 781 225 937 l
275          2417 Heatup and Conidown data includes vessel flange requirements of 150 F and 621 psig per 10CFR50, Appeaduc G.
150 1132 180 1123 100 1120 180 1131 185 807,
                                        ** For each cooldown rate, the steady state pre 55ure values shell govern the temperature where no allowable pressure values are provided
230 977 i
185 1180 185 1177 185 1177
~
170 438 235 1021 l
170 1232 175 !
088 240 1088 175 1248 180 1 900 245 1119 180 1349 l
185 937 250 1174 185 1413 190 977 255 12ja 190 1483 195 1021 280 1297 195 1558 200 1088 285 1308 200 1838 205 1119 270 1441 205 1725 210 1174 275 1521 U0 1818 215 1233 280 1807 til 1918 220 1297 285 1899 220 2028 225 1388 290 1798 225 2141 230 1441 295 1905 230 2288 235
~1521 300 2020 235 2400 240 1807 30$
2143 245 1899 310 2275 250 1794 315 2417 255 190$
280 2020 285 2143 270 2275 275 2417
~
Heatup and Conidown data includes vessel flange requirements of 150 F and 621 psig per 10CFR50, Appeaduc G.
** For each cooldown rate, the steady state pre 55ure values shell govern the temperature where no allowable pressure values are provided


BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT
BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT
        <so j
<so j
                                                                                                        .6
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l     I ACCEPTABkE.
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t         I i' I
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l l                                                                           l                         1 400 0           80       100             150               200           250             300       354           400 AUCTIONEERED LOW RCS TEMPERATURE (DEG, F)
x tt
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80 100 150 200 250 300 354 400 AUCTIONEERED LOW RCS TEMPERATURE (DEG, F)
Figure 2.3 Byron Unit 2 Maximum Allowable Nominal PORV Setpoints for the Low Teniperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY 7
Figure 2.3 Byron Unit 2 Maximum Allowable Nominal PORV Setpoints for the Low Teniperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY 7


t HYRON o UNIT 3                                                                                         +
t HYRON o UNIT 3
PRESSURE AND TEMPERATURE LIMITS REPORT                                                                                                       !
+
I Table 2.2                                                                                       !
PRESSURE AND TEMPERATURE LIMITS REPORT I
Data Points for Byron Uniti Mksimum Allowable PORY Setpoints for the LTOP System Applicable for the First 12 EFPY'
Table 2.2 Data Points for Byron Uniti Mksimum Allowable PORY Setpoints for the LTOP System Applicable for the First 12 EFPY' PCV-455A PCV-456
<                PCV-455A                                                                             PCV-456                                                                               :
*~
                                                                                  *~
(2TY 0413M)
(2TY 0413M)                                                                           (2TY-0413P)
(2TY-0413P)
AUCTIONEERED LOW                 RCS PRESSURE                                         AUCTIONEERED LOW                                     RCS PRESSURE RCS TEMP. (DEG. F)                   (PSIG)                                           RCS TEMP. (DEG. F)                                             (PSIG)       ~~
AUCTIONEERED LOW RCS PRESSURE AUCTIONEERED LOW RCS PRESSURE RCS TEMP. (DEG. F)
50                           497                                                               50                                             514 70                           497                                                               70                                             514 100                           497                                                             100                                             514 120                           446                                                             120                                             462 150                           446                                                             150                                               462 200                           446                                                             200                                               462 250                           587                                                             250                                               004 300                           587                                                             300                                             6 04 350                           587                                                             350                                               604 450                         2350                                                             450                                             2350 Note: To determine maximum allowable lift setpoints for RCS Pressure and RCS                                                                                             '
(PSIG)
Temperatures greater than 350'F, linearly interpolate between the 350'F and 450*F data points shown above.'
RCS TEMP. (DEG. F)
(PSIG)
~~
50 497 50 514 70 497 70 514 100 497 100 514 120 446 120 462 150 446 150 462 200 446 200 462 250 587 250 004 300 587 300 6 04 350 587 350 604 450 2350 450 2350 Note: To determine maximum allowable lift setpoints for RCS Pressure and RCS Temperatures greater than 350'F, linearly interpolate between the 350'F and 450*F data points shown above.'
* 8
* 8
      ,-            . .. _.            ..      ._    ,- __ _ . _ . . . _ , _                          . _ _ _ - - _ _              .-    ~ . _ . - _ . . . , _ _ _       __.,__-_:
~. _. - _..., _ _ _


BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0 Reactor Vessel Material S trveillance Program The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determiae changes in material properties. He removal schedule is provided in Table 3.1. Also,                                                   !'
BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0 Reactor Vessel Material S trveillance Program The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determiae changes in material properties. He removal schedule is provided in Table 3.1. Also, ine results of these analyses shall be used to update Figures 2.1 and 2.2, and Table 2.1. The time of specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns most closely approaching the withdrawal schedule.
ine results of these analyses shall be used to update Figures 2.1 and 2.2, and Table 2.1. The time of specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns most closely approaching the withdrawal schedule.
The pressure vessel material surveillance program (Reference 6)is in compliance with Appendix H to 10 CFR 50,"Reactot Vessel Radiation Surveillance Program." he material test requirements and the acceptance standard utilize the reference nil-ductility temperature, RTu, which is determined in accordance with ASME Section III, ND 2331. The empirical relationship between RTm and the fracture teughness of the reactor vessel ste:1 is developed in accordance with Appendix 0," Protection Against Non Ductile Failure," to Section XI of the ASME Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM El85 82.
The pressure vessel material surveillance program (Reference 6)is in compliance with Appendix H to 10 CFR 50,"Reactot Vessel Radiation Surveillance Program." he material test requirements and the acceptance standard utilize the reference nil-ductility temperature, RTu, which is determined in accordance with ASME Section III, ND 2331. The empirical relationship between RTm and the fracture teughness of the reactor vessel ste:1 is developed in accordance with Appendix 0," Protection Against Non Ductile Failure," to Section XI of the ASME Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM El85 82.
h t-9 1-
h t-9 1 -
_._,,-,.____,,.__.,,,....._.mm..                                    , , _ _ . , . _ . . . - . _ . -      , -.
_._,,-,.____,,.__.,,,....._.mm..


~
~
BYRON o UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 3.1 Byron Unit 2 Capsule Withdrawal Schedule Capsule         Vessel Location         Capsule Lead     Removal Time ("       Estimated Capsule (Degrees)                 Factor             (EFPY)             Fluence (n/cm')
BYRON o UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 3.1 Byron Unit 2 Capsule Withdrawal Schedule Capsule Vessel Location Capsule Lead Removal Time ("
U                 58.5'                   3.96       1.15 (Removed)             3.996 x 10" W                 121.5*                   3.89       4.634 (Removed)             1.211 x 10" X                 238.5'                   3.89       8.23 (EOL Wall)           2.192 x 10"N 12.34(1.5 EOL Z                 301.5*                   3.89             Wall (*?)           3.288 x 10" V                 61.0'                   3.64             Standby                   ---
Estimated Capsule (Degrees)
l        Y                 241.0'                   3.64             Standby                   ---
Factor (EFPY)
(a) Effective Full Power Years (EFPY) from plar I stanup.
Fluence (n/cm')
(b) Maximum end oflicense (32 EFPY) inner vessel wall Duence.           ,
U 58.5' 3.96 1.15 (Removed) 3.996 x 10" W
121.5*
3.89 4.634 (Removed) 1.211 x 10" X
238.5' 3.89 8.23 (EOL Wall) 2.192 x 10"N 12.34(1.5 EOL Z
301.5*
3.89 Wall (*?)
3.288 x 10" V
61.0' 3.64 Standby l
Y 241.0' 3.64 Standby (a) Effective Full Power Years (EFPY) from plar I stanup.
(b) Maximum end oflicense (32 EFPY) inner vessel wall Duence.
(c) Derived from Tabe C 2 of WCAP 14824, Rev. 2 (Reference 2, which is the Anachment to this repon).
(c) Derived from Tabe C 2 of WCAP 14824, Rev. 2 (Reference 2, which is the Anachment to this repon).
10
10


  ..                                                                                                                                      .,                                                    j BYRON. UNIT 2                                                               ;
j BYRON. UNIT 2
  "                                                                                                                                                                                      ^
^
PRI'SSURE AND TEMPERA'l URE LIMITS REPORT                                                                               f i
PRI'SSURE AND TEMPERA'l URE LIMITS REPORT f
4.0             Supplemental Data Tables                                                                                                                                   !
i 4.0 Supplemental Data Tables t
t
~
~
The following tables provide supplemental information on reactor vessel material properties and are provided to be consistent with Generic Letter 96 03. Some cd the material property                                                                 ,
The following tables provide supplemental information on reactor vessel material properties and are provided to be consistent with Generic Letter 96 03. Some cd the material property values shown were used as inputs to the P/T limits.
values shown were used as inputs to the P/T limits.
Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance i
Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance                                                         i capsule data.                                                                                                                                               ,
capsule data.
Table 4.2 provides the reactor vessel material properties table.
Table 4.2 provides the reactor vessel material properties table.
Table 4.3 provides a summary of the Byron Unit 2 adjusted reference temperature (ARTS) at the 1/4T and 3/4T locations for 12 EFPY.
Table 4.3 provides a summary of the Byron Unit 2 adjusted reference temperature (ARTS) at the 1/4T and 3/4T locations for 12 EFPY.
Table 4.4 shows the calculation of ARTS at 12 EFPY for the limiting Byron Unit 2 reactor                                                                   ,
Table 4.4 shows the calculation of ARTS at 12 EFPY for the limiting Byron Unit 2 reactor vessel material weld metal (Based on Surveillance Capsule Data).
vessel material weld metal (Based on Surveillance Capsule Data).
Table 4.5 provides RTns values for Byron Unit 2 for 32 EFPY.
Table 4.5 provides RTns values for Byron Unit 2 for 32 EFPY.                                                                                               l Table 4.6 provides RTnsvalues for Byron Unit 2 for 48 EFPY.
l Table 4.6 provides RTnsvalues for Byron Unit 2 for 48 EFPY.
t I
t I
I1
I1


BYRON o UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.1 Calculation of Chemistry Factors Using Surveillance Capsule Data Fluence Material               Capsule               (n/cm',                           FFW                         Measured FF*ARTm               (FF)2 E>1.0                                                       ARTm Mev), f Lower Shell Forging 49D330/                     U         3.996x10"                           0.746                           0                 0         0.556 49C298 1-1 (Tangential)
BYRON o UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.1 Calculation of Chemistry Factors Using Surveillance Capsule Data Fluence Material Capsule (n/cm',
W           l.211x10"                           1.053                           5         5.267           1.110 Lower Shell Forging 49D330/                       U         3.996x10"                           0.727                           25           18.65           0.556 49C298 1 -1 (Axial)
FFW Measured FF*ARTm (FF)2 E>1.0 ARTm Mev), f Lower Shell Forging 49D330/
W         l.211x10"                           1.053                           40         32.73             1.110 Sum: 66.037             3.332 Chemistry Factor (0 = 66.037 + 3.332 = 19.8'F Byron 1 Weld Metal WF 336*                         U         3.72x10"                           0.727                         0     0       0.00           0.529 X           1.39x10"                         1.091                       35     105") 114.56             1.190 Byron 2 Weld Metal WF-447("                         U       3.996x10"                           0.746                         0       0           0           0.557 W         l.211x10"                           1.053                     30       90"'   94.77             1.110 Sum:   209.33             3.386 Chemistry Factor (* = 209.33+3.386= 61.8'F (a) FF = FRence Factor a- f"*** 0 (b) B> ton Unit 1 ARTm values were obtained from the surveillance Capsule X analysis (WCAP 13880, Reference 10).
U 3.996x10" 0.746 0
The ByTon Uni tI capsule fluence values were recalculated using the ENDF/B V scattering cross sections in 1994 and are documented in WCAP 14044 (Reference 8).
0 0.556 49C298 1-1 (Tangential)
W l.211x10" 1.053 5
5.267 1.110 Lower Shell Forging 49D330/
U 3.996x10" 0.727 25 18.65 0.556 49C298 1 -1 (Axial)
W l.211x10" 1.053 40 32.73 1.110 Sum:
66.037 3.332 Chemistry Factor (0 = 66.037 + 3.332 = 19.8'F Byron 1 Weld Metal WF 336*
U 3.72x10" 0.727 0
0 0.00 0.529 X
1.39x10" 1.091 35 105")
114.56 1.190 Byron 2 Weld Metal WF-447("
U 3.996x10" 0.746 0
0 0
0.557 W
l.211x10" 1.053 30 90"'
94.77 1.110 Sum:
209.33 3.386 Chemistry Factor (* = 209.33+3.386= 61.8'F (a) FF = FRence Factor a-f"*** 0 (b) B> ton Unit 1 ARTm values were obtained from the surveillance Capsule X analysis (WCAP 13880, Reference 10).
The ByTon Uni I capsule fluence values were recalculated using the ENDF/B V scattering cross sections in 1994 and t
are documented in WCAP 14044 (Reference 8).
(c) Dyron Unit 2 capsule fluence FF, and ARTm values were obtained from the surveillance Capsule W analysis of WCAP 14064 (Reference 3) using the ENDF/B.V scattering cross sections.
(c) Dyron Unit 2 capsule fluence FF, and ARTm values were obtained from the surveillance Capsule W analysis of WCAP 14064 (Reference 3) using the ENDF/B.V scattering cross sections.
(d) Chemistry Factor = E (FF'ARTm)/I((FF)')
(d) Chemistry Factor = E (FF'ARTm)/I((FF)')
(c) Adjusted ARTm per Ratio Procedure of Regulatory Guide 1.99, Rev. 2 (Ref.12). Ratio = 3.0. See Table 2 of WCAP 14824, Rev. 2, (Ref. 2). Actual ratio is 2.5 (68.007.0 = 2.5); However, for conservatism, ratio of 3.0 was used.
(c) Adjusted ARTm per Ratio Procedure of Regulatory Guide 1.99, Rev. 2 (Ref.12). Ratio = 3.0. See Table 2 of WCAP 14824, Rev. 2, (Ref. 2). Actual ratio is 2.5 (68.007.0 = 2.5); However, for conservatism, ratio of 3.0 was used.
12
12
_ .. _ _ _ _                . _ _ _ _            - _ _              . . . . - - . - _                          - _ _ ~ . _ . - - _              _ _ _ _ . _ _ _ .        -.
~.


DYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT                                                               !
DYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.2 Byron Unit 2 Reactor Vessel Material Properties Material Description Cu(%)N Ni (%)(*)
Table 4.2 Byron Unit 2 Reactor Vessel Material Properties Material Description             Cu(%)N     Ni (%)(*) Chemistry                       Initial FactorM                     RT m ('F)N Closure Head Flange                 Not       0.74           --                -
Chemistry Initial FactorM RT m ('F)N Closure Head Flange Not 0.74 OM Reponed Vessel Flange Not 0.73 30M heported Inter. Shell Forging 0.01 0.70 20.0
OM Reponed Vessel Flange                   Not       0.73           --                        30M heported Inter. Shell Forging               0.01       0.70       20.0                       -20 49D329/49C2971-1 Lower Shell Forging                 0.0a       0.72       32.2                         -20 49D330/49C2981-1 Circumferential Weld                 0.05       0.62       68.0                         10 WF-447 I
-20 49D329/49C2971-1 Lower Shell Forging 0.0a 0.72 32.2
a) Chemistry Factors are calculated from Cu and Ni values per Regulatory Guide 1.99, Rev. 2 (Reference 12).
-20 49D330/49C2981-1 Circumferential Weld 0.05 0.62 68.0 10 WF-447 a) Chemistry Factors are calculated from Cu and Ni values per Regulatory Guide 1.99, Rev. 2 (Reference I
12).
b) Initial RT,et values are measured, WCAP 14063 (Reference 7) c) Closure head and vessel flange Initial RT,,, values are used for considering flange requirements for the heatup/cooldown curve'., WCAP 14940 (Reference 14).
b) Initial RT,et values are measured, WCAP 14063 (Reference 7) c) Closure head and vessel flange Initial RT,,, values are used for considering flange requirements for the heatup/cooldown curve'., WCAP 14940 (Reference 14).
13
13
_ _ _ - ~ _ -                    _
- ~
~.


                              . -      - - -                                  - . . -  .                - - . - - . _ - - ~ . .                 - -            - - - .. _-
- -. - -. _ - - ~..
HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3                                                                                         :
HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3 I
I Summary of Hyron Unit 2 Adjusted Reference Temp:istures (ARTS'y                                                                                             ,
Summary of Hyron Unit 2 Adjusted Reference Temp:istures (ARTS'y at 1/4T and 3/4T Locations for 12 EFPY F
at 1/4T and 3/4T Locations for 12 EFPY F
12 EFPY Material Description 1/4T ART ('F) 3/4T ART ('F)
12 EFPY Material Description                                       1/4T ART ('F)                           3/4T ART ('F)
Intermediate Shell Forging 12.1 1.7 49D329/49C2971-1 (R.G.1.99 Position 1 ('')
Intermediate Shell Forging                                                 12.1                               1.7 49D329/49C2971-1 (R.G.1.99 Position 1 ('')
Using credible surveillance 31.7 14.9 capsule data (RG Position 2(*))
Using credible surveillance                                               31.7                               14.9 capsule data (RG Position 2(*))
Lower Shell Fo ging 11.8 1.5 49D330/49C2981 1 (RG Position l''))
Lower Shell Fo ging                                                   11.8                               1.5 49D330/49C2981 1 (RG Position l''))
Circumfriential Weld 131.9 98.9 bi-447 (RG Position 1(*)
Circumfriential Weld                                                 131.9                               98.9 bi-447 (RG Position 1(*)
Using credible surveillance 87.6*)
Using credible surveillance                                             87.6*)                             71.5*)
71.5*)
capsule data (RG Position 2('))
capsule data (RG Position 2('))
(a) Calculated using a chemistry factor based on Regulatory Guide (RG) 1.99, Positions I and 2 (Reference 12).
(a) Calculated using a chemistry factor based on Regulatory Guide (RG) 1.99, Positions I and 2 (Reference 12).
(b) These ART values were used to generate the Byron Unit 2 Heatup and Cooldown Curves, WCAP-14940 (Reference 14).
(b) These ART values were used to generate the Byron Unit 2 Heatup and Cooldown Curves, WCAP-14940 (Reference 14).
14
14
_ _ _ _ _ . ~ . . . _ - _ _ _                  . . . - _ . . _ - - . ~ _ _ _              _ _ - _ . . _ - .                .      . . . - _          _ _ _ _ . -          ._    . - _ . . . _ . .
. ~...
- -. ~


BYRON UNIT 2                                                             l t
BYRON UNIT 2 l
PRESSURE AND TEMPERATURE LIMITS REPORT l
t PRESSURE AND TEMPERATURE LIMITS REPORT l
Table 4.4 Byron Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 12 EFPY at the Limiting Reactor Vessel Material Weld Metal (Based on Surveillance Capsule Data)
Table 4.4 Byron Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 12 EFPY at the Limiting Reactor Vessel Material Weld Metal (Based on Surveillance Capsule Data)
Parameter                                     Values                                             ,
Parameter Values Operating Time 12 EFPY '
Operating Time                                   12 EFPY '
l LocationN 1/4T ART 3/4T ART i
l LocationN                     1/4T ART                     3/4T ART i
-}
                                                                                                                                                        -}
Chemistry Factor, CF (*F) 68.0 68,0 Fluence (f), n/cm' 4.94x10" 1.78x10"
Chemistry Factor, CF (*F)                   68.0                           68,0 Fluence (f), n/cm'                   4.94x10"                     1.78x10"                             [
[
(E>l.0 Mev)*
(E>l.0 Mev)*
Fluence Factor, FF                     0.803                         0.542 ARTum= CFxFF(*F)                         49.63                         33.50
Fluence Factor, FF 0.803 0.542 ARTum= CFxFF(*F) 49.63 33.50 Initial lit ym,1('F) 10 10
                                                                                  ~
~
Initial lit ym,1('F)                     10                             10 Margin, M (*F)                       28.00                         28.00 ART = I+(CF*FF)+M,'F                       87.6                           71.5 per RG 1.99, Revision 2 (a) Fluence, f, is based upon fs(E>l.0 Mev) = 8.22x10'' at 12 EFPY, WCAP 14940 (Reference 14).
Margin, M (*F) 28.00 28.00 ART = I+(CF*FF)+M,'F 87.6 71.5 per RG 1.99, Revision 2 (a) Fluence, f, is based upon fs(E>l.0 Mev) = 8.22x10'' at 12 EFPY, WCAP 14940 (Reference 14).
(b) The Byron Unit 2 reactor vessel wall thickness is 8.5 inches at the beltline region.
(b) The Byron Unit 2 reactor vessel wall thickness is 8.5 inches at the beltline region.
I E
I E
t                     -                                  -
t


1                                                                                                                 ,
1 HYRON UNIT 2 PRESSURE AND TEMPERATURE 1.lMITS REPORT Table 4.5 RTna Valuer for flyron Unit 2 for 32 EFPY M
HYRON UNIT 2 PRESSURE AND TEMPERATURE 1.lMITS REPORT Table 4.5 RTna Valuer for flyron Unit 2 for 32 EFPY CF                       p.i                             pp,        M    l RTune ARTns RTn, Material                 ('F)                                                               ('F)     (*F) ('F) (*F)
l RTune ARTns
Lower Shell Forging                 32.2           2.192                                     1.213     34.0       -20 39.1 53.1 MK 24 3 4
: RTn, CF p.i pp, Material
Using Surveillance                 19.8           2.192                                     1.213     34.0       -20 24.0 38.0 Capsule Data"'
('F)
intennediate Shell Forging             20.0           2.192                                     1.213     24.3       20 24.3 28.6 MK 24 2 Circurnference Weld                 68.0             2.192                                   1.21 I   56.0       10 82.5 148.5 Metal WF447 Using Surveillance                 61.3             2.192                                   1.213     28.0       10 75.0 113.0 Capsule Data (3) 2.192x10'' n/cm (Epl.0 Mev) for 32 EFPY from flyron 2 P t s report. WCAP 14054 (Reference 9) 3 (b) FF (Fluence Factor) = l'"'*'''**
('F)
0 (c) Cakulated using a CF based on suncillance capsule data per RG l.99. Position 2 (Reference 12).
(*F)
('F)
(*F)
Lower Shell Forging 32.2 2.192 1.213 34.0
-20 39.1 53.1 MK 24 3 4
Using Surveillance 19.8 2.192 1.213 34.0
-20 24.0 38.0 Capsule Data"'
intennediate Shell Forging 20.0 2.192 1.213 24.3 20 24.3 28.6 MK 24 2 Circurnference Weld 68.0 2.192 1.21 I 56.0 10 82.5 148.5 Metal WF447 Using Surveillance 61.3 2.192 1.213 28.0 10 75.0 113.0 Capsule Data (3) 2.192x10'' n/cm (Epl.0 Mev) for 32 EFPY from flyron 2 P t s report. WCAP 14054 (Reference 9) 3 (b) FF (Fluence Factor) = l'"'*'''** 0 (c) Cakulated using a CF based on suncillance capsule data per RG l.99. Position 2 (Reference 12).
(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation.
(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation.
16
16
_    _    _        ._-____=.___-_.-_m_---____-._-___------_---_.2_-
._-____=.___-_.-_m_---____-._-___------_---_.2_-


4 HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.6 RTn, Yalues for Ilyron Unit 2 for 48 EFPY CF        p.,        pp63              M                                         RTm,mn ARTns RTn, Material                   ('F)                               ('F)-                                           (*F)   ('F) (*F)
4 HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.6 RTn, Yalues for Ilyron Unit 2 for 48 EFPY M
Lower Shell Forging               32.2     3.288       1.312       34.0                                             -20   42.2 56.2 MK 24 3 d
RTm,mn ARTns
Using Surveillar.cc               19.8     3.288       1.312       34.0                                             -20   26.0 40.0 Capsule Data"'
: RTn, CF p.,
Intermediate Shell Forging             20.0     3.288       1.312       26.2                                               20   26.2 32.4 MK 24 2 Circumference Weld                 68.0     3.288       1.312       56.0                                             10   89.2 155.2 Metal WF447 Using Surveillance               61.f,     3.288       1.312       28.0                                             10   81.1 119.1 Capsule Data (a) 2.192x10" n/cm (E>l.0 8
pp63 Material
Mev) for 32 ETPY from Dyron 2 PTS report. WCAP 14054 (Reference 9). The following calculation provides the 48 F/PY Oueni e value:
('F)
2.192x10" + ((2.19.!x10".3 tkx10"y32 4.634 EFPY)) * (48 32 EFPY) = 3.288x10" n/cm 8 (b) FF (Fluence Factor) = f* 8"'''** 0 (c) Calculated using a CF based on w.c ihnce capsule data per RO 1.99, Position 2 (Reference 12).
('F)-
(*F)
('F)
(*F)
Lower Shell Forging 32.2 3.288 1.312 34.0
-20 42.2 56.2 MK 24 3 d
Using Surveillar.cc 19.8 3.288 1.312 34.0
-20 26.0 40.0 Capsule Data"'
Intermediate Shell Forging 20.0 3.288 1.312 26.2 20 26.2 32.4 MK 24 2 Circumference Weld 68.0 3.288 1.312 56.0 10 89.2 155.2 Metal WF447 Using Surveillance 61.f, 3.288 1.312 28.0 10 81.1 119.1 Capsule Data (a) 2.192x10" n/cm (E>l.0 Mev) for 32 ETPY from Dyron 2 PTS report. WCAP 14054 (Reference 9). The following 8
calculation provides the 48 F/PY Oueni e value:
8 2.192x10" + ((2.19.!x10".3 tkx10"y32 4.634 EFPY)) * (48 32 EFPY) = 3.288x10" n/cm (b) FF (Fluence Factor) = f* 8"'''** 0 (c) Calculated using a CF based on w.c ihnce capsule data per RO 1.99, Position 2 (Reference 12).
(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation.
(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation.
17
17


HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 5.0 References
HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 5.0 References 1.
: 1. WCAP-14040 NP A, Revision 2," Methodology Used to Develop Cold Overpressure Mitigating System Setpoints and RCS Heatup and Cooldown Limit Curves," Andrachek, J.D., et. al., January 1996.
WCAP-14040 NP A, Revision 2," Methodology Used to Develop Cold Overpressure Mitigating System Setpoints and RCS Heatup and Cooldown Limit Curves," Andrachek, J.D., et. al., January 1996.
: 2. WCAP-14824, Revision 2 " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"
2.
WCAP-14824, Revision 2 " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"
November,1997.
November,1997.
: 3. WCAP-14064," Analysis of Capsule W from the Commonwealth Edison Company Byron Unit 2 Reactor Vessel Radiation Surveillance Program," Malone, M.J., et al., -
3.
WCAP-14064," Analysis of Capsule W from the Commonwealth Edison Company Byron Unit 2 Reactor Vessel Radiation Surveillance Program," Malone, M.J., et al.,
July 1994.
July 1994.
: 4. WCAP-12431," Analysis of Capsule U from the Commonwealth Edison Company Byron Unit 2 Reactor Vessel Radiation Surveillance Prvgram," Terek, E., et al.,
4.
WCAP-12431," Analysis of Capsule U from the Commonwealth Edison Company Byron Unit 2 Reactor Vessel Radiation Surveillance Prvgram," Terek, E., et al.,
October 1989.
October 1989.
: 5. Westinghouse Letter to Commonwealth Edison Company, CAE 96-106," Byron Unit I and 2 LTOPS Setpoints Based on 10 and 12 EFPY P/T Limits," January 17,1996.
5.
: 6. WCAP-10398," Commonwealth Edison Company, Byron Station Unit 2 Reactor Vessel Radiation Surveillance Program," Singer,IlR., December 1983.
Westinghouse Letter to Commonwealth Edison Company, CAE 96-106," Byron Unit I and 2 LTOPS Setpoints Based on 10 and 12 EFPY P/T Limits," January 17,1996.
: 7. WCAP-14063," Commonwealth Edison Company, Byron Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," Peter, P.A., November 1994.
6.
: 8. WCAP-14044," Westinghouse Surveillance Capsule Neutron Fluence Reevaluation,"
WCAP-10398," Commonwealth Edison Company, Byron Station Unit 2 Reactor Vessel Radiation Surveillance Program," Singer,IlR., December 1983.
Lippencott, E.P., April 1994,
7.
: 9. WCAP-14054," Evaluation of Pressurized Thermal Shoch for Byron Unit 2," Peter, P.A., August 1994.
WCAP-14063," Commonwealth Edison Company, Byron Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," Peter, P.A., November 1994.
8.
WCAP-14044," Westinghouse Surveillance Capsule Neutron Fluence Reevaluation,"
Lippencott, E.P., April 1994, 9.
WCAP-14054," Evaluation of Pressurized Thermal Shoch for Byron Unit 2," Peter, P.A., August 1994.
: 10. 10 CFR Part 50, Appendix 0," Fracture Toughness Requirements," Federal Register, Volume 60, No. 243, dated December 19,1995.
: 10. 10 CFR Part 50, Appendix 0," Fracture Toughness Requirements," Federal Register, Volume 60, No. 243, dated December 19,1995.
I1. 10 CFR 50.61," Fracture Toughness Requirements for Protection Against Pressurized Thennal Shock Events,"(PTS Rule) May 15,1991.
I1. 10 CFR 50.61," Fracture Toughness Requirements for Protection Against Pressurized Thennal Shock Events,"(PTS Rule) May 15,1991.
Line 459: Line 702:
I8
I8


HYRON - UNIT 2 l
HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT
PRESSURE AND TEMPERATURE LIMITS REPORT
: 13. Comed Calculation BRW 96 9071/BYR 96-294," Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 2 Original Steam Generators)" Revision 0.
: 13. Comed Calculation BRW 96 9071/BYR 96-294," Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 2 Original Steam Generators)" Revision 0.
: 14. Wr AP-14940,"11yron Unit 2 ileatup and Cooldown Limit Curves for Normal Ope.ation," Laubham, T. J., et al., October,1997.
: 14. Wr AP-14940,"11yron Unit 2 ileatup and Cooldown Limit Curves for Normal Ope.ation," Laubham, T. J., et al., October,1997.
Line 467: Line 709:
19
19


i
.. o,
  .. o ,                                                           \
\\
ATTACHMENT WCAP -24824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD
ATTACHMENT WCAP -24824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD w
r ma


BRAIDWOOD - UNIT I                                       -
BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table of Contents Section _
    ,                            PRESSURE AND TEMPERATURE LIMITS REPORT Table of Contents Section _                                                                           Page 1.0     Introduction                                                               1 2.0     Operating Limits                                                           I k                           2.1   RCS Pressure and Temperature (P/T) Limits                           1 2.2   Low Temperature Overpresure Protection (LTOP) System Setpoints     2 2.3   LTOP Enable Temperature                                             2 2.4   Reactor Vessel Boltup Tempe:ature                                   3 2.5   Reactor Vessel Minimum Pressurization Temperature                   3 3.0     Reactor Vessel Material Surveillance Program                               9 4.0     Supplemental Data Tables                                                 11 5.0     References                                                               18 M               Attachment WCAP-14824, " Byron Unit i Heatup and Cooldown Limit Curves for Normal Operation and Sune!!!ance Weld Metal Integration for Byron and Braidwood," Revision 2, Novembo.1997.
Page 1.0 Introduction 1
2.0 Operating Limits I
k 2.1 RCS Pressure and Temperature (P/T) Limits 1
2.2 Low Temperature Overpresure Protection (LTOP) System Setpoints 2
2.3 LTOP Enable Temperature 2
2.4 Reactor Vessel Boltup Tempe:ature 3
2.5 Reactor Vessel Minimum Pressurization Temperature 3
3.0 Reactor Vessel Material Surveillance Program 9
4.0 Supplemental Data Tables 11 5.0 References 18 M
Attachment WCAP-14824, " Byron Unit i Heatup and Cooldown Limit Curves for Normal Operation and Sune!!!ance Weld Metal Integration for Byron and Braidwood," Revision 2, Novembo.1997.
i-
i-


s BRAIDWOOD - UNIT 1
s BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITT, REPORT List of Figures Figure Page 2.1 Braidwood Unit 1 Reactor Coolant System Heatup Limitations (Heatup Rates up to 4
      ,                                                  PRESSURE AND TEMPERATURE LIMITT, REPORT List of Figures Figure                                                                                               Page 2.1   Braidwood Unit 1 Reactor Coolant System Heatup Limitations (Heatup Rates up to       4
{
{                                                 100'F/hr) Applicable for the First 16 EFPY (Without Margins for Instrementation Errors) 2.2   Braidwood Unit 1 Reactor Coolant System Cooldown Limitations (Cooldown Rates up 5 to 100 *F/hr) Applicable for the First 16 EFPY (Without Margins for Instrumentation Errors)
100'F/hr) Applicable for the First 16 EFPY (Without Margins for Instrementation Errors) 2.2 Braidwood Unit 1 Reactor Coolant System Cooldown Limitations (Cooldown Rates up 5 to 100 *F/hr) Applicable for the First 16 EFPY (Without Margins for Instrumentation Errors)
\
\\
2,3  Braidwood Unit 1 Maximum Allowable Nominal PORY Setpoints for the Low                  7
}
}
F                                               Temperature Overpressure Protection (LTOP) System App::pW for the First 16 EFPY
2,3 Braidwood Unit 1 Maximum Allowable Nominal PORY Setpoints for the Low 7
\
F Temperature Overpressure Protection (LTOP) System App::pW for the First 16 EFPY
\\
L k
L k
r
r


            =-                           .
=-
BRAIDWOOD - UNIT I
BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT.
,-                    PRESSURE AND TEMPERATURE LIMITS REPORT.
List of Tables Table Page 2.1 Braidwood Unit 1 Hntup and Cooldown Data Points at 16 EFPY 6
List of Tables Table                                                                             Page 2.1   Braidwood Unit 1 Hntup and Cooldown Data Points at 16 EFPY                 6 (Without Margins for Instrumentation Errors) 2.2   Data Points for Braidwood Unit 1 Maximum Allowable PORV Setpoints           8 for the LTOP System Applicable for the First 16 EFPY 3.1   Braidwood Unit 1 Capsule Withdrawal Schedule                               10 4.)   Braidwood Unit 1 Calculation of Chemistry Factors Using Surveillance       12 Capsule Data 4.2   Braidwood Unit 1 Reactor Vessel Material Properties                       13 4.3   Summary of Braidwood Unit 1 Adjusted Reference Temperatures (ARTri) at     14 the 1/4T and 3/4T Locations for 16 EFPY-4.4   Braidwood Unit 1 Calculation of Adjusted Reference Temperatures (ARTS) at   15 16 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on
(Without Margins for Instrumentation Errors) 2.2 Data Points for Braidwood Unit 1 Maximum Allowable PORV Setpoints 8
        'Survei: lance Capsule Data) 4.5   RTns Values for Braidwood Unit I for 32 EFPY                               16   -
for the LTOP System Applicable for the First 16 EFPY 3.1 Braidwood Unit 1 Capsule Withdrawal Schedule 10 4.)
4.6   RTns Values for Braidwood Unit I for 48 EFPY                               17 iiF
Braidwood Unit 1 Calculation of Chemistry Factors Using Surveillance 12 Capsule Data 4.2 Braidwood Unit 1 Reactor Vessel Material Properties 13 4.3 Summary of Braidwood Unit 1 Adjusted Reference Temperatures (ARTri) at 14 the 1/4T and 3/4T Locations for 16 EFPY-4.4 Braidwood Unit 1 Calculation of Adjusted Reference Temperatures (ARTS) at 15 16 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on
'Survei: lance Capsule Data) 4.5 RTns Values for Braidwood Unit I for 32 EFPY 16 4.6 RTns Values for Braidwood Unit I for 48 EFPY 17 iiF


    - .              .    -                      -            .-.        -    ~ . -       - -                .
~. -
BRAIDWOOD - UNIT 1 PRESSURE AND TEMI'EP.ATURE LIMITS REPORT 1.0   Introduction Reference to Technical Specifications (TS) numbers are given in both the Braidwooc' Station current Technical Specifications (CTS) and Improved Tect nical Specifications (ITS). The CTS number ir, presented fir:1, followed by the ITS number in brackets [ ).
BRAIDWOOD - UNIT 1 PRESSURE AND TEMI'EP.ATURE LIMITS REPORT 1.0 Introduction Reference to Technical Specifications (TS) numbers are given in both the Braidwooc' Station current Technical Specifications (CTS) and Improved Tect nical Specifications (ITS). The CTS number ir, presented fir:1, followed by the ITS number in brackets [ ).
This PTLR for Unit I has been prepared in accordance with the requirements of TS 6.9.1.11/[ITS-5.6.6]. Revisions to the PTLR shall be provided to the NRC after issuance.
This PTLR for Unit I has been prepared in accordance with the requirements of TS 6.9.1.11/[ITS-5.6.6]. Revisions to the PTLR shall be provided to the NRC after issuance.
The Technical Specifications addressed in this report are listed below:
The Technical Specifications addressed in this report are listed below:
LCO 3.4.9.1 Pressure / Temperature Limits; and LCO 3.4.9.3 Overpressure Protection Systems.
LCO 3.4.9.1 Pressure / Temperature Limits; and LCO 3.4.9.3 Overpressure Protection Systems.
[ITS LCO 3.4.3 RCS Pressure and Temperature (P/T) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System).
[ITS LCO 3.4.3 RCS Pressure and Temperature (P/T) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System).
2.0   Operating Limits The PTLR limits were developed using a methodology specified in the Technical Specifications.
2.0 Operating Limits The PTLR limits were developed using a methodology specified in the Technical Specifications.
The methodology listed in WCAP-14040-NP-A (Reference 1) was used with four exceptions:
The methodology listed in WCAP-14040-NP-A (Reference 1) was used with four exceptions:
: a. Use of ENDF/B-IV neutron transpcrt cross-section library and ENDF/B-V dosimeter reaction cross-sections,
: a. Use of ENDF/B-IV neutron transpcrt cross-section library and ENDF/B-V dosimeter reaction cross-sections,
Line 505: Line 758:
: c. Use of ASME Code Case N-514, and
: c. Use of ASME Code Case N-514, and
: d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.
: d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.
WCAP-14824, Revision 2, is included as an attachment for reference. WCAP-14824, Rev. 2 contains the P/T curves for Byron Unit 1, along with the weld metal data integratior ir Byron and Braidwood Units 1 and 2 and the Byron /Braidwood fluence methodologyjustifica z. lor ENDF/B-VI cross sections.
WCAP-14824, Revision 2, is included as an attachment for reference. WCAP-14824, Rev. 2 contains the P/T curves for Byron Unit 1, along with the weld metal data integratior ir Byron and Braidwood Units 1 and 2 and the Byron /Braidwood fluence methodologyjustifica
2.1   RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [iTS-LCO 3.4.3])
: z. lor ENDF/B-VI cross sections.
2.1 RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [iTS-LCO 3.4.3])
2.1.1 The RCS temperature rate-of-change limits defined in Reference 7 are:
2.1.1 The RCS temperature rate-of-change limits defined in Reference 7 are:
: a. A raaximum heatup of 100 F ir, any 1-hour period,
: a. A raaximum heatup of 100 F ir, any 1-hour period,
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p
p


BRAIDWOOD - UNIT I
BRAIDWOOD - UNIT I P.RESSURE AND TEMPERATURE LIMITS REPORT
,                      P.RESSURE AND TEMPERATURE LIMITS REPORT
- Operating Limits (Continued) 2.1.2 The RCS Pff limits for heatup, inservice hydrostatic and leak testing, and criticality are specified by Figure 2.1 and Table 2.1. The RCS P/T limits for cooldown are shown in Figure 2.2 and Table 2.1. These limits are defined in Reference 7. Consistent with the methodology described in Reference 1, the RCS P/T limits for heatup and cooldown showm in Figures 2.1 and 2.2 are provided without margins for instrumeat error. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, instrument uncertainties need not be considered since appropriate station operating procedures ensure that the limits contained in the figures and table are not exceedea. The criticality limit curve specifies pressure-temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix G.
  - Operating Limits (Continued) 2.1.2 The RCS Pff limits for heatup, inservice hydrostatic and leak testing, and criticality are specified by Figure 2.1 and Table 2.1. The RCS P/T limits for cooldown are shown in Figure 2.2 and Table 2.1. These limits are defined in Reference 7. Consistent with the methodology described in Reference 1, the RCS P/T limits for heatup and cooldown showm in Figures 2.1 and 2.2 are provided without margins for instrumeat error. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, instrument uncertainties need not be considered since appropriate station operating procedures ensure that the limits contained in the figures and table are not exceedea. The criticality limit curve specifies pressure-temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix G.
The Pff limits for core operation (except for low power physics testing) are that the reactor vi.ssel must be at a temperature equal to or higher than the minimum temperature required for the inservice hydrostatic test, and at least 40'F higher than the minimum permissible temperature in the corresponding P/T curve for heatup and cooldown.
The Pff limits for core operation (except for low power physics testing) are that the reactor vi.ssel must be at a temperature equal to or higher than the minimum temperature required for the inservice hydrostatic test, and at least 40'F higher than the minimum permissible temperature in the corresponding P/T curve for heatup and cooldown.
2.2       Low Temperature Overpressure Protection (LTOP) System Setpoints (LCO 3.4.9.3/
2.2 Low Temperature Overpressure Protection (LTOP) System Setpoints (LCO 3.4.9.3/
[ITS-LCO 3.4.12]).
[ITS-LCO 3.4.12]).
The power operated relief valves (PORVs) shall e .ch have maximum lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13, and 14.
The power operated relief valves (PORVs) shall e.ch have maximum lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13, and 14.
The LTOP setpoints are based on P/T limits which were established by 10 CFR 50, Appendix G without allowance for instrumentation erroi in accordance with the methodology described in Reference 1. The LTOP PORY maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.
The LTOP setpoints are based on P/T limits which were established by 10 CFR 50, Appendix G without allowance for instrumentation erroi in accordance with the methodology described in Reference 1. The LTOP PORY maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.
2.3       LTOP Enable Temperature The as analyzed LTOP enable temperature is 200*F (Reference 15).
2.3 LTOP Enable Temperature The as analyzed LTOP enable temperature is 200*F (Reference 15).
The TS required enable temperature for the PORVs shall be 2 350 F RCS temperature (Braidwood Unit 1 procedures governing the heatup and cooldown of the RCS require the arming of the LTOP System for RCS r mperature of 350*F and below and disarming of LTOP for RCS temperatu:e above 350'F).
The TS required enable temperature for the PORVs shall be 2 350 F RCS temperature (Braidwood Unit 1 procedures governing the heatup and cooldown of the RCS require the arming of the LTOP System for RCS r mperature of 350*F and below and disarming of LTOP for RCS temperatu:e above 350'F).
          - Note that the last LTOP PORV segment in Table 2.2 extends to 450*F where the pressure setpoint is 2350 psig. This is intended to prohibit PORV lift for an inadvertent LTOP system arming at power.
- Note that the last LTOP PORV segment in Table 2.2 extends to 450*F where the pressure setpoint is 2350 psig. This is intended to prohibit PORV lift for an inadvertent LTOP system arming at power.
2
2


BRAIDWOOD - UNIT 1
BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT Operating Lhnits (Continued) 2.4 Reactor Vessel Boltup Temperature (Non-Technical Specification)_
,--                                PRESSURE AND TEMPERATURE LIMITS REPORT Operating Lhnits (Continued) 2.4     Reactor Vessel Boltup Temperature (Non-Technical Specification)_
The minimum boltup temperature for the Reactor Vessel Flange shall be 2 60 F. Boltup is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and the RCS vented to atmosphere (Reference 7).
The minimum boltup temperature for the Reactor Vessel Flange shall be 2 60 F. Boltup is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and the RCS vented to atmosphere (Reference 7).
2.5 - Reactor Vessel Minimum Pressurization Temperature (Non-Technical Specification)
2.5 - Reactor Vessel Minimum Pressurization Temperature (Non-Technical Specification)
Line 533: Line 785:
3
3


.'                                                                              BRAIDWOOD - UNIT 1 l
BRAIDWOOD - UNIT 1 l
PRESSURE AND TEMPERATURE LIMITS REPORT                                                                                                                                               l MATERIAL PROPERTY BA315 LIMTTING MATERIAL WELD METAL LIMITING ART VALUES AT 16 EFPY:                                             1/4 76.6*F 3/4 65.4*F 2500             .          ,,                                                                    ,                                  .
PRESSURE AND TEMPERATURE LIMITS REPORT l
                                                                                                                                                                                                -                          4 I
MATERIAL PROPERTY BA315 LIMTTING MATERIAL WELD METAL LIMITING ART VALUES AT 16 EFPY:
i                                 1 Ic e
1/4 76.6*F 3/4 65.4*F 2500 4
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                                                                                                                                                                                                                              ~
/
as                          ,,        , , , ,              ,                                /                                                        l. l 2000                 ,'
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g                                            i.                                                                               I                   (
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/
1750                 ,                  UNACCEPTABLE                                                             ;                      ;
: l. l
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~
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/ " '
                                                                                                                                              /                                               l m                         ;                                                                                ~                       ,
=
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                                                                                                  /
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IM5ERVICE HYDROET& TIC TEST                                                                           i i          *'            '              ' ''              ''''                            TEMPERATURE late FI FOR THE
1250 ll' UP TO 400 t/Hr.
                        ! a i!                   i             e it i           e e **                           SERVICE PERIOD UP 70                                                 1. 0 EFPY
/
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/
0                 5'O             Id0                   150             200                   2$0                         380                       3$0         480     4$0                     500 Indicated Temperature                                                                                                                     (Deg.F)
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0 EFPY l
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0 5'O Id0 150 200 2$0 380 3$0 480 4$0 500 Indicated Temperature (Deg.F)
Figure 2.1 Braidwood Unit 1 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/hr) Applicable for the First 16 EFPY (Without Margins for Instrumentation Errors)
Figure 2.1 Braidwood Unit 1 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/hr) Applicable for the First 16 EFPY (Without Margins for Instrumentation Errors)
                                                                                                          '4
'4


BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT -
BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT -
MATERIAL PROPERTY BASIS LIMITING MATERIAL WELD METAL                                                                                                                                                                       ...
MATERIAL PROPERTY BASIS LIMITING MATERIAL WELD METAL I,IMITING ART VALUES AT 16 EFPY:
I,IMITING ART VALUES AT 16 EFPY:                                                               . t/4.t. 76.6*F
. t/4.t. 76.6*F
: 3/4-t, 65.4*F
: 3/4-t, 65.4*F
                        .2500                 ,,,,,,,,,,,                                                                                                                  ,                            ,                                          ,      ,          .
.2500 l
sessessessase                                                                                                                                           8 l
}
                                                                                                                                                                                                                                                                                }
sessessessase 8
4!                                   ,                                                                                                                                                          '
4!
l                                                                                 J               ,
l J
2250.
2250.
j'     '
j' l ;'
l 1
1 m
m                         ,                                                            ,                ,                      ,
- ing._
                                                      '                                  ,                !
J 1
* J                                                      1
2000
                  - ing ._                                                                                                                                                                                                                                       ,,
/
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l f
                  .      2000                                             ,            ,
00 m.
00                                                    $,,,.,      '                                                    f
l
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)
: m.                     ;
i i
l                                 .                      )                                                                                                   i                 i l750 _'_uN A c c r P T A s t r-                                                               i             /                                      ,
/
__        OPrRATioN                                                                         J cu-                                                                                                            I
l750
                                                                                              ,        ,                          /
_'_uN A c c r P T A s t r-i cu-OPrRATioN J
                    ,    1500                                                                                                   /
I
sn                                                                                                       l
/
,                . cc                                                                                                     /
1500
o   1250.                           ,                      ,    ,
/
                                                                                                                      ,,',                                    AccrPTAstr b                                     i                                         .                fl !                                       oPrRATION
l sn
'               1                                                       i                                   r                                                         .,                          , ,        #',h                        ,                  ,
. cc
i
/
: g.     1000              ,' , , ,'                                                2r             ,' ' ,                                                                                                                                i a                                        s,,,                                                     W               e         f
o 1250.
'                                      ~~
AccrPTAstr b
o                                                                         AP                   a         6 C00LDOWN                                   jyj                         ,,,                                                                                                                ,'
i fl !
                ===8                 -
oPrRATION
RATES                    -                                                                    -
#',h 1
                  =       750 --     "
i r
r/ur.                                     7''                        l,'                      l                                                                                                                        ,
1000 i
                                                                                                      ,            it                      i                                                                                                                        6
g.
: g.                                     ,,,,
2r i
                                    ~~
s,,,
o               cx ,-               ,                            ,,
W e
                'e       -500                   'S
f a
                                                '"              ',f l               l,             ,            ll                                 ,                ,,l                       ,                                  ,            ,          ,
~~
q
o AP a
                  =                 -
6
                                                                              ,    ,#            ,            ,,,                                  #                          i             6                                               ,
- C00LDOWN jyj
250           ,,,,                        ,,,            ,,,,                        ,,,                      ,                                  ,                    ,          ,          ,          ,              ,          ,,
 
4,,                        ,  ,,          .,,,                        ,          ,                                          ,,                                  ,            ,
===8
0                                                                             <
- RATES 7''
0                    50                   Id0 150                                           2 d O'               250                       300                       350           400                     450             500 I n d i c a t e-d                                                     Temperature                                                                       (Deg..F)
l,'
Figure 2.2
l
,                        Braidwood Unit 1 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to
=
:                        100 *F/hr) Applicable for the First 16 EFP.Y (Without Margins for Instrumentation Errors)
750 -- r/ur.
                                                                                                                                      ~5 i>
g.
it i
6 o
cx,-
'e
-500
'S
',f l l,
ll
,,l
~~
=
q i
6 250 4,,
0 0
50 Id0 150 2 d O' 250 300 350 400 450 500 I n d i c a t e-d Temperature (Deg..F)
Figure 2.2 Braidwood Unit 1 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to 100 *F/hr) Applicable for the First 16 EFP.Y (Without Margins for Instrumentation Errors)
~5 i>


n m.un www-w.:..            .
n m.un www-w.:..
PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.1 BRAIDWOOD Unit 1 Heatup* and Cooldown* Data Points at 16 EFPY" (Without margins for instrumentation errors)
PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.1 BRAIDWOOD Unit 1 Heatup* and Cooldown* Data Points at 16 EFPY" (Without margins for instrumentation errors)
HEATUP CURVES                                               COOLDOWN CURVES l 100 F Heatup                         Leak Test Criticahty Limit     UmH                   Steady State       26 DEO F       So DEO F       100 DEO F curve I     P   T 4 P                     T I     P       T I       P     T 4 P         T        ,  P T          P    T 80         0 00   210 l 0 00     188l2000                 60 1 0 00       60 1 0 00       60 1 0 00       60 f 0 00 210l2495                 80 ! 620 27     60 l 577 45     80     534 28   60 1 446 98 60        565 09  210 1 611 83 65       565 09 210 l 597.56           I                 65 1 621.00     65 1 590 68     65     548 52   85 i 463 79 70       565 09 210 ! 585 60           i                 70 f 621.00     70 1 605 03     70 1 563 98     70 ' 481.93 75    i  565 09 210 i 576 77           I                 75 l 62100       75 l 620 51     75 1 560 67   75 1 501 49 80         585 09 210 1 570 35           I                 80 ! 621 00     80 i 621 00     80 l 598 51   80 I 522 88 85         84509   210 6 586 61           1                 85 l 621.00     85 l 62100     85 I 617 90   85 6 545 50 90         565 09 210 j 565 09           l                 90 1 621 00     90 1 621 00     90 1 621.00   90 1 570.23 95         585 09 210 1 565.87           l                 95 1 621.00     95     621.00 95 1 621 00   95       i   596 83 100       565 87 210 f 568 89           i                 100 l 62100     100     621 00 100 l 621.00   1{l 621 00 105       568 89 210 i 573 56           l                 105     621.00   105 1 621 00   105 1 621 00   e           621.00 110         573 58 210 i 580 30           i                 110 1 621.00     110 1 621 00   110 1 621.00   110 t 62140 115         580 30 210 1 585 84                             110 I 795 92     110 1 786 92   110 l 739.27   110 l 890 04 120 1 588 84       210 I 599.36     __
HEATUP CURVES COOLDOWN CURVES l 100 F Heatup Leak Test curve Criticahty Limit UmH Steady State 26 DEO F So DEO F 100 DEO F P
115 ! 821 55     115     7e4 59 115 1 769 53   115 l 726.2 125         599 36 210 1 811.78                             120 I 849 00     120     824 45 120 } 801 97   120 1 785 12 130         611.78 210 i 626 07         l                 125 1 818 42     125     856 54 125 1 836 87   125 I 807.07 135         626C7 210 i 64216           l                 130 1 91025     130       890 97 130 1 874 41   130 1 852.23 140         642 16 210 I 860 36           1                 135 l 944 34   135 l 928 00     135 i 915 0", 135 } 900 91 145         660 36 210 1 680 59           l                 140 i 980 89   140 i 967.79     140 l 958 57   '40 1 953.33 150         680 59 210 1 702 80         1                   145 1 1020.15   145 1 1010 84   145 11005 42   145 l 1009 81 155 i 702 80       210 ! 727.33         i                   150 l 1062.35   150 i 1056 88   150 11055 76           l 160  i 727.33 210 1 754 07         i                   155 t 1107.92   155 j 1106.38         l               l 165         754 07 210 t 783 17         !                  160 11156 42           }             I               !
T P
17:         78317 215 I 814 98         i                   165 ! 1208 78           l             !                !
T I
175       814 98 223 I 849 37         I                   170 I 1265 05           .              I               I 180       849 37 225 ! 886 54         '
P T 4 P T I P
175 i1325.37            i              i                i 185                230 ! 926 73         1                   180 1 1390 04           l             l               l 886 f _
T I P
190       926 73 235 i 970 11                             185 l 1459 41           I             I               i 195       970 11 240 1 1016 91                             190 1 1533 55           i             1               I 200       1016 91 245 t 1067.33                             195 i 1613 49           l                             !
T 4 P T
205         1067.33 250 i 1121 63                           200 11699 01             l                             l 210       1121 63 255 1 1180 01                           205 ' 1790.55           l             t               i 215       1180 01 260 l 1242 62                           210 i 1888 81           I             I               i 220       1242 62 285 i 1309 84                           215 619C3 61           I             I               !
80 0 00 210 l 0 00 188l2000 60 1 0 00 60 1 0 00 60 1 0 00 60 f 0 00 60 565 09 210 1 611 83 210l2495 80 ! 620 27 60 l 577 45 80 534 28 60 1 446 98 65 565 09 210 l 597.56 I
225       1309 84 270 ' 1382 03                           220 : 2105 6e           .              ,              i 1382 03 275 1 1459 45                           225 2225.77             '            '                i 230 235       1459 45 280 t 1542.27                           230 ! 2353 75           6             i               i 1542.27 285 : 1630 97                                   '              !              4 240 245       1630 97 290 i 1728 05                                   i               I             i 250       1726 05 295 1 1827 80                                 +                                               ,
65 1 621.00 65 1 590 68 65 548 52 85 i 463 79 70 565 09 210 ! 585 60 i
255       '827 80 300 ' 1936 51                                 >                l              i 260       193651   305 ; 2052 39                                 ,                !              I              i i
70 f 621.00 70 1 605 03 70 1 563 98 70 ' 481.93 565 09 210 i 576 77 I
565       2052 39 310 ! 2176 33                                 i 270       2176 33 315     2308 42                               i               i 275       2308 42 320 ' 2449 09                                 1 280       2449 09                                                                 i
75 l 62100 75 l 620 51 75 1 560 67 75 1 501 49 75 i
80 585 09 210 1 570 35 I
80 ! 621 00 80 i 621 00 80 l 598 51 80 I 522 88 85 84509 210 6 586 61 1
85 l 621.00 85 l 62100 85 I 617 90 85 6 545 50 90 565 09 210 j 565 09 l
90 1 621 00 90 1 621 00 90 1 621.00 90 1 570.23 596 83 95 585 09 210 1 565.87 l
95 1 621.00 95 621.00 95 1 621 00 95 i
100 565 87 210 f 568 89 i
100 l 62100 100 621 00 100 l 621.00 1{l 621 00 105 568 89 210 i 573 56 l
105 621.00 105 1 621 00 105 1 621 00 e
621.00 110 573 58 210 i 580 30 i
110 1 621.00 110 1 621 00 110 1 621.00 110 t 62140 115 580 30 210 1 585 84 110 I 795 92 110 1 786 92 110 l 739.27 110 l 890 04 120 1 588 84 210 I 599.36 115 ! 821 55 115 7e4 59 115 1 769 53 115 l 726.2 125 599 36 210 1 811.78 120 I 849 00 120 824 45 120 } 801 97 120 1 785 12 130 611.78 210 i 626 07 l
125 1 818 42 125 856 54 125 1 836 87 125 I 807.07 135 626C7 210 i 64216 l
130 1 91025 130 890 97 130 1 874 41 130 1 852.23 140 642 16 210 I 860 36 1
135 l 944 34 135 l 928 00 135 i 915 0",
135 } 900 91 145 660 36 210 1 680 59 l
140 i 980 89 140 i 967.79 140 l 958 57
'40 1 953.33 150 680 59 210 1 702 80 1
145 1 1020.15 145 1 1010 84 145 11005 42 145 l 1009 81 155 i 702 80 210 ! 727.33 i
150 l 1062.35 150 i 1056 88 150 11055 76 l
727.33 210 1 754 07 i
155 t 1107.92 155 j 1106.38 l
l 160 i
165 754 07 210 t 783 17 160 11156 42
}
I 17:
78317 215 I 814 98 i
165 ! 1208 78 l
175 814 98 223 I 849 37 I
170 I 1265 05 I
I 175 i1325.37 i
i i
180 849 37 225 ! 886 54 185 886 f _
230 ! 926 73 1
180 1 1390 04 l
l l
190 926 73 235 i 970 11 185 l 1459 41 I
I i
195 970 11 240 1 1016 91 190 1 1533 55 i
1 I
200 1016 91 245 t 1067.33 195 i 1613 49 l
205 1067.33 250 i 1121 63 200 11699 01 l
l 210 1121 63 255 1 1180 01 205 ' 1790.55 l
t i
215 1180 01 260 l 1242 62 210 i 1888 81 I
I i
220 1242 62 285 i 1309 84 215 619C3 61 I
I 225 1309 84 270 ' 1382 03 220 : 2105 6e i
230 1382 03 275 1 1459 45 225 2225.77 i
235 1459 45 280 t 1542.27 230 ! 2353 75 6
i i
240 1542.27 285 : 1630 97 4
245 1630 97 290 i 1728 05 i
I i
250 1726 05 295 1 1827 80
+
l i
255
'827 80 300 ' 1936 51 I
i 260 193651 305 ; 2052 39 565 2052 39 310 ! 2176 33 i
i 270 2176 33 315 2308 42 i
i 275 2308 42 320 ' 2449 09 1
280 2449 09 i
* Heatup and C,ooldown data include vessel flange requirernents of 110 F and 621 psig pr 10CFRSO, Appendix G
* Heatup and C,ooldown data include vessel flange requirernents of 110 F and 621 psig pr 10CFRSO, Appendix G
    " For e8ch cooldown rate, the steady-state pressure values shall govern the ternperature where no allowab 8 pressure values are provided 6-
" For e8ch cooldown rate, the steady-state pressure values shall govern the ternperature where no allowab 8 pressure values are provided 6-


GRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT i i i I i l I Il lII i                                   'l l l 1 III i l i             i i ! I f         -
GRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT i i i I i l I Il lII i
Q ll I
'l l l 1 III i l i i i ! I f Q ll I i i i ! I i i
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i I -l i l /e IN l       i ! l I               !! I i             i                                               l 1 ! I i I i           ! .
1 I I !
        ,        I            i i I                       i     i I i l                   //
I i
I i UNACCEPTABLE i l' !                                         i       i   NIii         IiNI f i ! i I Il I ijif i i iil                                       l       l   f/ l l 1       l l } l l 1 T     ,
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i i
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    !                                                                  ,            !      i i !I     i E             : i I i i i               -
l i i i i i IiiiiiI i i I//
                                                    ! t i           i i i i i ; I i i i                 liI         II l i lii 5       : ! I i i
d pcvjanga l i i i Iil I 'i 5
                                        !          ! i i i ! ; j i ! II I I i                           l       I   i I i liI       ,
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                    .                t                       l                     ! ! ! i iil i i i! ! l l 1 I i i l 0                     so                   100                 160               200         260           300             sao AUCTIONEERED LOW RCS TEMPERATURE (DEG, F)
: ! I i i
! i i i ! ; j i ! II I I i l
I i I i liI 3
l t i i i i i i i i i ! ACCEPTABLE ji' I i !
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t l
! ! ! i iil i i i! ! l l 1 I i i l 0
so 100 160 200 260 300 sao AUCTIONEERED LOW RCS TEMPERATURE (DEG, F)
Figure 2.3 Braidwood Unit 1 Maximum Allowable Nominal PORV Setpoints for the Low Temperature Overpressure Protection (LTOP) System Applicable for the First 16 EFPY 7
Figure 2.3 Braidwood Unit 1 Maximum Allowable Nominal PORV Setpoints for the Low Temperature Overpressure Protection (LTOP) System Applicable for the First 16 EFPY 7


BRAIDWOOD - UNIT 1
BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.2 Data Points for Braidwood Unit ! Maximum Allowable PORV Setpoints for the LTOP Sy5 tem Applicable for the First 16 EFPY PCV-455A PCV-456 (1TY 0413M)
        .                                                            PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.2 Data Points for Braidwood Unit ! Maximum Allowable PORV Setpoints for the LTOP Sy5 tem Applicable for the First 16 EFPY PCV-455A                                                                                             PCV-456 (1TY 0413M)                                                                                         (1TY-0413P) b           AUCTIONEERED LOW                                             RCS PRESSURE                             AUCTIONEERED LOW             RCS PRESSURE RCS TEMP. (DEG. F)                                               (PSIG)                         '
(1TY-0413P) b AUCTIONEERED LOW RCS PRESSURE AUCTIONEERED LOW RCS PRESSURE RCS TEMP. (DEG. F)
8tCS TEMP. (DEG. F)           (PSIG) 50                                                         497                                                         50       513 70                                                         497                                                       70       513 iOO                                                         497                                                       100       513 110                                                         497                                                       110       513
(PSIG) 8tCS TEMP. (DEG. F)
(                   160 200 497 616 160 203 513 634 250                                                         603                                                       250       619 300                                                         588                                                       300       604
(PSIG) 50 497 50 513 70 497 70 513 iOO 497 100 513 110 497 110 513
_                    350                                                         588                                                       350       604 450                                                       2350                                                       450       2350 Note: To determine maximum allowable fift setpoints for RCS Pressure and RCS Temperatures greater than 350 F, linearly interpolate betwetn the 350 F and 450 F data points shown above.
(
160 497 160 513 200 616 203 634 250 603 250 619 300 588 300 604 350 588 350 604 450 2350 450 2350 Note: To determine maximum allowable fift setpoints for RCS Pressure and RCS Temperatures greater than 350 F, linearly interpolate betwetn the 350 F and 450 F data points shown above.
r n
r n
E
E


BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0 - Reactor Vessel Material Sun'e.illance Program
BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0
            ' The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determine changes in material properties. The removal schedule is provided in Table 3.1, The results of these anslyses shall be used to update Figures 2.1 and 2.2 and Table 2.1. The time of
- Reactor Vessel Material Sun'e.illance Program
            - specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns most closely approaching the withdrawal schedule.
' The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determine changes in material properties. The removal schedule is provided in Table 3.1, The results of these anslyses shall be used to update Figures 2.1 and 2.2 and Table 2.1. The time of
The pressure vessel material surveillance program (Reference 6)is in compliance with Appendix H to 10 CFR 50, " Reactor Vessel Radiation Surveillance Program." The material test requirements and the acceptance standards utilize the reference nil-ductility temperature, RTmr ,
- specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns most closely approaching the withdrawal schedule.
which is determined in accordance with ASME Section III Paragraph NB-2331. The empirical relationship between RTer nd a the fracture toughness of the reactor vessel steel is developed in accordance with Appendix G," Protection Against Non-Ductile Failure," to Section XI of the AShE Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM E18F 82.
The pressure vessel material surveillance program (Reference 6)is in compliance with Appendix H to 10 CFR 50, " Reactor Vessel Radiation Surveillance Program." The material test requirements and the acceptance standards utilize the reference nil-ductility temperature, RTmr,
which is determined in accordance with ASME Section III Paragraph NB-2331. The empirical relationship between RTer nd the fracture toughness of the reactor vessel steel is developed in a
accordance with Appendix G," Protection Against Non-Ductile Failure," to Section XI of the AShE Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM E18F 82.
i
i


BRAIDWOOD- UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT Table 3.1 Braidwood Unit 1 Capsule Withdrawal Schedule Capsule       Vessel Location     Capsule Lead     Removal Time'"   Estimated Capsule 2
BRAIDWOOD-UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT Table 3.1 Braidwood Unit 1 Capsule Withdrawal Schedule Capsule Vessel Location Capsule Lead Removal Time'"
(Decrees)             Factor           (EFPY)         Fluence (n/cm )
Estimated Capsule 2
U               58.5*               4.03         1.10 (Removed)       3.814 x 10'8 X               238.5'               4.03       4.234 (Removed)       1.144 x 10''
(Decrees)
W               121.5'             4.03         7.95 (EOL Wall)     2.239 x 10'*
Factor (EFPY)
11.93 (1.5 EOL Z               301.5*             4.03             Wall'4)         3.359 x 10" __
Fluence (n/cm )
V               61.0'               3.73             Standby               -
U 58.5*
Y              241.0*               3.73             Standby               --
4.03 1.10 (Removed) 3.814 x 10'8 X
(a) Effective Full Power Years (EFPY) from plant startup.
238.5' 4.03 4.234 (Removed) 1.144 x 10''
W 121.5' 4.03 7.95 (EOL Wall) 2.239 x 10'*
11.93 (1.5 EOL Z
301.5*
4.03 Wall'4) 3.359 x 10" __
V 61.0' 3.73 Standby Y
241.0*
3.73 Standby (a) Effective Full Power Years (EFPY) from plant startup.
(b) Maximum end oflicense (32 EFPY) inner vessel wall fluence.
(b) Maximum end oflicense (32 EFPY) inner vessel wall fluence.
(c) Derived from Table C-3 of WCAP-14824, Rev. 2 (Reference 2, which is the Attachment to this report).
(c) Derived from Table C-3 of WCAP-14824, Rev. 2 (Reference 2, which is the Attachment to this report).
10
10


BRAIDWOOD - UNIT 1
BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT 4.0 Supplemental Data Tables The following tables provide supplemental information on reactor vessel material properties and are provided to be consistent with Generic Letter 96-03. Some of the material property values shown were used as inputs to the P/T limits.
  .                      PRESSURE AND TEMPERATURE LIMITS REPORT 4.0 Supplemental Data Tables The following tables provide supplemental information on reactor vessel material properties and are provided to be consistent with Generic Letter 96-03. Some of the material property values shown were used as inputs to the P/T limits.
Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance capsule data.
Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance capsule data.
Table 4.2 provides the reactor vessel material properties.
Table 4.2 provides the reactor vessel material properties.
Table 4.3 provides a summary of the Braidwood Unit 1 adjusted referer.ce temperatures (ARTS) at the 1/4T and 3/4T locations for 16 EFPY.
Table 4.3 provides a summary of the Braidwood Unit 1 adjusted referer.ce temperatures (ARTS) at the 1/4T and 3/4T locations for 16 EFPY.
Table 4.4 shows the calculation of ARTS at 16 EFPY for the limiting Braidwood Unit I reactor vessel material -Weld Metal WF562 (Based on Surveillance Capsule Data).
Table 4.4 shows the calculation of ARTS at 16 EFPY for the limiting Braidwood Unit I reactor vessel material -Weld Metal WF562 (Based on Surveillance Capsule Data).
.      Table 4.5 provides the RTns values for Braidwood Unit 1 for 32 EFPY.
Table 4.5 provides the RTns alues for Braidwood Unit 1 for 32 EFPY.
Table 4.6 provides the RTnsvalues for Braidwood Unit i for 48 EFPY.
v Table 4.6 provides the RTns alues for Braidwood Unit i for 48 EFPY.
It
v It


BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.1 Braidwood Unit 1 Calculation of Chemistry Factors Usine Surveillance Capsule Data Fluence Material       Capsule       (ri/cm2 ,     FF")       Measured       FF*ARTmr         (FF)2 E> l . 0                 ARTsm Mev), f Lower Shell Forging               U       3.814 x10"     0.733           5           3.666         0.538 24-3                               ,
BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.1 Braidwood Unit 1 Calculation of Chemistry Factors Usine Surveillance Capsule Data Fluence Material Capsule (ri/cm,
(Tangential)
FF")
X       1.144 x10"     1.038         30           31.127         1.077 Lower Shell Forging                 U       3.814 x10"     0.733           0               0           0.538 24-3 (Axial)               X         1.144x10"       1.038         25           25.939         1.077 Sum:       60.733       3.228 Chemistry Factor d' = 60.733 + 3.228 = 18.8'F Braidwood 1 Weld                   U       3.814x10"       0.733         10")           7.333         0.538 Metal WF562*'
Measured FF*ARTmr (FF)2 2
X       1.144x10"       1.038         25")           25.95         1.077 Braidwood 2 Weld                   U       3.933x10"       0.741           0               0         0.550 Metal WF562")
E> l. 0 ARTsm Mev), f Lower Shell Forging U
X       1.126 x I0"     1.033         20"'           20.66         1.067 Sum:       53.943       3.232 Chemistrv Factor "' = 53.943+ 3.232 = I6.7'F (a) FF = Fluence Factor = f*2" "'*"'
3.814 x10" 0.733 5
3.666 0.538 24-3 (Tangential)
X 1.144 x10" 1.038 30 31.127 1.077 Lower Shell Forging U
3.814 x10" 0.733 0
0 0.538 24-3 (Axial)
X 1.144x10" 1.038 25 25.939 1.077 Sum:
60.733 3.228 Chemistry Factor d' = 60.733 + 3.228 = 18.8'F Braidwood 1 Weld U
3.814x10" 0.733 10")
7.333 0.538 Metal WF562*'
X 1.144x10" 1.038 25")
25.95 1.077 Braidwood 2 Weld U
3.933x10" 0.741 0
0 0.550 Metal WF562")
X 1.126 x I0" 1.033 20"'
20.66 1.067 Sum:
53.943 3.232 Chemistrv Factor "' = 53.943+ 3.232 = I6.7'F (a) FF = Fluence Factor = f*2" "'*"'
(b) Braidwood Unit 1 ARTxor values were obtained from WCAP-14243 (Reference 7).
(b) Braidwood Unit 1 ARTxor values were obtained from WCAP-14243 (Reference 7).
l (c) Braidwood Unit 2 capsule fluence, FF, and ARTxo1 values obtained from WCAP-14970 (Reference 12)-
l (c) Braidwood Unit 2 capsule fluence, FF, and ARTxo1 values obtained from WCAP-14970 (Reference 12)-
Line 739: Line 1,167:
f
f


BRAIDWOOD - UNIT 1 PRESSURE AND TEh!PERATURE LIMITS REPORT Table 4.2 Braidwood Unit 1 Reactor Vessel Material Pro perties Chemistry         Initial Material       Cu (%)")   Ni (%)")   Factor'"     RT mr ('F)'"
BRAIDWOOD - UNIT 1 PRESSURE AND TEh!PERATURE LIMITS REPORT Table 4.2 Braidwood Unit 1 Reactor Vessel Material Pro perties Chemistry Initial Material Cu (%)")
Description Closure Head           -        -              -          -20'"
Ni (%)")
* Flange Vessel Flange          -        -              -          - 10"'
Factor'"
Lower Shell         0.04       0.74         26.0           -20 Forging 24-3 Intermediat- Shell     0.05       0.73       31.0             -30 Forging 24 2 Weld Metal         (i.03     0.67       41.0             40 WF562 (a) Chemist y Factors are calculated from Cu and Ni values per Regulatory Guide 199, Position 1 (Reference 11).
RT mr ('F)'"
v are measured, WCAP-14243 (Reference 7)
Description Closure Head
(b) initial RTer alues (c) Closure head and vessel flange Initial RTer values are used for considering flange requirements for the heatup/cooldown curves, WCAP-14243.
-20'"
Flange
- 10"'
Vessel Flange Lower Shell 0.04 0.74 26.0
-20 Forging 24-3 Intermediat-Shell 0.05 0.73 31.0
-30 Forging 24 2 Weld Metal (i.03 0.67 41.0 40 WF562 (a) Chemist y Factors are calculated from Cu and Ni values per Regulatory Guide 199, Position 1 (Reference 11).
(b) initial RTer alues are measured, WCAP-14243 (Reference 7) v (c) Closure head and vessel flange Initial RTer values are used for considering flange requirements for the heatup/cooldown curves, WCAP-14243.
13 1
13 1


BRAIDWOOD - UNIT I
BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3 Summary of Braidwood Unit 1 Adjusted Reference Temperatures (ARTS) at the 1/4T and 3/471.ocations for 16 EFPY")
    ,            PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3 Summary of Braidwood Unit 1 Adjusted Reference Temperatures (ARTS) at the 1/4T and 3/471.ocations for 16 EFPY")
16 EFPY Material Description 1/4T ART (*F) 3/4T ART (*F)
16 EFPY Material Description                                           1/4T ART (*F)                   3/4T ART (*F)
Lower Shell Forging
Lower Shell Forging                                                           -26.2                 12.1 24-3 Using credible 7
-26.2 12.1 24-3 Using credible surveillance capsule data 13.4*)
surveillance capsule data                                                         13.4*)             3.2*'
3.2*'
(RG Position 2''))
7 (RG Position 2''))
Intermediate Shell                                                           25.1                 8.2 Forgi..g 24-2 (RG Position 1)
Intermediate Shell 25.1 8.2 Forgi..g 24-2 (RG Position 1)
Circumferential Weld                                                           112.9               90.5
Circumferential Weld 112.9 90.5 (RG Position 1)
                                                        ~
~
(RG Position 1)
Using credible 76.6*'
Using credible                                                           76.6*'               65.4*'
65.4*'
surveillance capsule data (RG Position 2''))
surveillance capsule data (RG Position 2''))
(a) Calculated using a chemistry factor based on Pegulatory Guide (RG) 1.99, Position 2 (Reference 11).
(a) Calculated using a chemistry factor based on Pegulatory Guide (RG) 1.99, Position 2 (Reference 11).
(b) These ART values were used to generate the Braidwood Unit I heatup and cooldown curves, WCAP-14243 (Reference 7).
(b) These ART values were used to generate the Braidwood Unit I heatup and cooldown curves, WCAP-14243 (Reference 7).
(c) Based on evaluation of WCAP-14243; however, applicability date has been increased to 27.9 EFPY per evaluation in WCAP-14824, Rev. 2- Appendix D: Weld Mctal Integration for Braidwood Units 1 and 2 (Reference 2).
(c) Based on evaluation of WCAP-14243; however, applicability date has been increased to 27.9 EFPY per evaluation in WCAP-14824, Rev. 2-Appendix D: Weld Mctal Integration for Braidwood Units 1 and 2 (Reference 2).
14                                       l l
14 l
l


l BRAIDWOOD - UNIT 1 1
l BRAIDWOOD - UNIT 1 1
    ,                                          PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.4 Braidwood Unit 1 Calculation of Adjusted Reference Temperatures (ARTa) at 16 EFPi*' at the Limiting Reactor % ssel Mcterial Weld Metal WF562 (Based on Surveillance Capsule Data)
PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.4 Braidwood Unit 1 Calculation of Adjusted Reference Temperatures (ARTa) at 16 EFPi*' at the Limiting Reactor % ssel Mcterial Weld Metal WF562 (Based on Surveillance Capsule Data)
Parameter                               Values                       -
Parameter Values r
r Operating Time                           16 EFPi*'
Operating Time 16 EFPi*'
Location"'                 1/4T ART               3/4T ART fhemistry Factor, CF ('F)               20.6                 20.6 Fluence (f), n/cm'             0.73x10"               2.43x10" (E>1.0 Mev))"'
Location"'
Fluence Factor, FF                 0.889                 0.616 ARTmr= CFxFF ('F)                   18.31                 12.70 Initial RT mr, I (*F)                 40                   40 Margin, M ( F)                   18.31                 12.70 ART = 1+(CF*FF)+M, *F                   76.6                 65.4                 '
1/4T ART 3/4T ART fhemistry Factor, CF ('F) 20.6 20.6 Fluence (f), n/cm' 0.73x10" 2.43x10" (E>1.0 Mev))"'
per RG 1.99. Rwision 2 (a) Fluence, f, is based upon f.s(E>l.0 Mev) = 1.120x10" at 16 EFPY, WCAP-14241 (Reference 3).
Fluence Factor, FF 0.889 0.616 ARTmr= CFxFF ('F) 18.31 12.70 Initial RT mr, I (*F) 40 40 Margin, M ( F) 18.31 12.70 ART = 1+(CF*FF)+M, *F 76.6 65.4 per RG 1.99. Rwision 2 (a) Fluence, f, is based upon f.s(E>l.0 Mev) = 1.120x10" at 16 EFPY, WCAP-14241 (Reference 3).
(b) Based on evaluation of WCAP 14243; however, applicability date has been increased to 27.9 EFPY per evaluation in WCAP-14824, Rev. 2 Appendix B: Weld Metal Integration for Braidwood Units 1 and 2 (Reference 2).
(b) Based on evaluation of WCAP 14243; however, applicability date has been increased to 27.9 EFPY per evaluation in WCAP-14824, Rev. 2 Appendix B: Weld Metal Integration for Braidwood Units 1 and 2 (Reference 2).
(c) The Braidwood Unit I reactor vescel wall thickness is 3.5 inches at the beltline region.
(c) The Braidwood Unit I reactor vescel wall thickness is 3.5 inches at the beltline region.
t 15
t 15


BRAIDWOOD - UNIT 1
BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT T
  ,                                  PRESSURE AND TEMPERATURE LIMITS REPORT T
Table 4.5 RTers Values for Braidwood Unit 1 for 32 EFPY CF p.
Table 4.5 RTers Values for Braidwood Unit 1 for 32 EFPY CF       p.     ppm   M   RTane ARTns     RTns Material                                             (*F)                   (*F) (*F)   (*F)     (*F)
ppm M
Lower Shell Forging                                         26.0   2.239   1.218 31.68 -20   31,68     43.4 MK 24 3 Using Sun'eillance                                         18.8   2.239   1.218 17.0 -20 22.90       19.8 Capsule Data"'
RTane ARTns RTns Material
                                                                                                                                  ~
(*F)
                                                                                                                                    ~
(*F)
Intermediate Shell Forging                                     31.0   2.239   1.218 34.0 -30 37.77       41.8 24 2                                                                                           ,
(*F)
Circumferential Weld                                         41.0   2.239   1.218 49.95   40 49.95 ! 139,9 Metal WF562 Using Sun eillance                                         16.7   2.239   1.218 20.34 40   20.34       80.7 Capsule Data")
(*F)
(*F)
Lower Shell Forging 26.0 2.239 1.218 31.68
-20 31,68 43.4 MK 24 3 Using Sun'eillance 18.8 2.239 1.218 17.0
-20 22.90 19.8 Capsule Data"'
~
Intermediate Shell Forging 31.0 2.239 1.218 34.0
-30 37.77 41.8
~
24 2 Circumferential Weld 41.0 2.239 1.218 49.95 40 49.95 ! 139,9 Metal WF562 Using Sun eillance 16.7 2.239 1.218 20.34 40 20.34 80.7 Capsule Data")
(a) 2.239x10'' n/cm'(E>l 0 Mev) for 32 EFPY from Braidwood 1 PTS report, WCAP-14242 (Reference 8).
(a) 2.239x10'' n/cm'(E>l 0 Mev) for 32 EFPY from Braidwood 1 PTS report, WCAP-14242 (Reference 8).
(b) FF (Fluence Factor) = fo.2w io w,o r
(b) FF (Fluence Factor) = fo.2w io w,o r
Line 788: Line 1,232:
16
16


BRAIDWOOD - UNIT I
BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.6 RTns Values for B aidwood Unit 1 for 48 EFPY CF M
, .                              PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.6 RTns Values for B aidwood Unit 1 for 48 EFPY CF f.>      ppm    M     RTmrrm)   ARTns       RTns Material             ('F)                         ('F)   ('F)       ('F)       ('F)
RTmrrm)
Lower Shell Forging           26.0         3.358     1.317 34.0     -20       34.25       48.3 MK 24 3 Using Surveillance           18.8         3.358     1.317 17.0     -20       24.76     21.8 Capsule Data"'
ARTns RTns f.>
Intermediate Shell Forging       31.0         3.358     1.317 34.0   -30       40.83       44.8 24-2 C'rcumferential Weld         41.0         3.358     1.317 54.00     40       54.00       148.0 Metal WF562 Using Surveillance           16.7         3.358   1.317 21.99     40       21.99       84.0 Capsule Data")
ppm Material
2 (a) 3.358x10'' n/cm (E>l.0 Mev) for 48 EFPY from Braidwood 1 PTS repon, WCAP-14242 (Reference 5).
('F)
('F)
('F)
('F)
('F)
Lower Shell Forging 26.0 3.358 1.317 34.0
-20 34.25 48.3 MK 24 3 Using Surveillance 18.8 3.358 1.317 17.0
-20 24.76 21.8 Capsule Data"'
Intermediate Shell Forging 31.0 3.358 1.317 34.0
-30 40.83 44.8 24-2 C'rcumferential Weld 41.0 3.358 1.317 54.00 40 54.00 148.0 Metal WF562 Using Surveillance 16.7 3.358 1.317 21.99 40 21.99 84.0 Capsule Data")
(a) 3.358x10'' n/cm (E>l.0 Mev) for 48 EFPY from Braidwood 1 PTS repon, WCAP-14242 2
(Reference 5).
(b) FF (Fluence Factor) = f"''#'*80 (c) Calculated with CF based on surveillance capsule data per RG 1.99, Position 2 (Reference 11).
(b) FF (Fluence Factor) = f"''#'*80 (c) Calculated with CF based on surveillance capsule data per RG 1.99, Position 2 (Reference 11).
17
17


BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT.
BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT.
5.0 References
5.0 References 1.
: 1.                             Andrachek, J.D., et al., WCAP-14040-NP-A, " Methodology used to Develop Cold Overpressure Mitigating System Setpoints and RCS Heatup and Cooldown Limit Curves," Revision 2, January 1996.
Andrachek, J.D., et al., WCAP-14040-NP-A, " Methodology used to Develop Cold Overpressure Mitigating System Setpoints and RCS Heatup and Cooldown Limit Curves," Revision 2, January 1996.
: 2.                             Grendys, P.A., WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"
2.
Revision 2, November 1997
Grendys, P.A., WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"
: 3.                             Peter, P.A., et al., WCAP-14241, " Analysis of Capsule X from the Commonwealth Edison Company Braidwood Unit 1 Reactor Vessel Radiation Surveillance Program,"
Revision 2, November 1997 3.
Peter, P.A., et al., WCAP-14241, " Analysis of Capsule X from the Commonwealth Edison Company Braidwood Unit 1 Reactor Vessel Radiation Surveillance Program,"
March 1995.
March 1995.
: 4.                           Terek, E., et al., WCAP-12685, " Analysis of Capsule U from the Commonwealth Edison Company Braidwood Unit 1 Reactor Vessel Radiation Surveillance Program," August 1990.
4.
: 5.                           Westinghouse Letter to Conunonwealth Edison Company, CCE-95 186, "Braidwood Unit 1 LTOPS Setpoints Based on 16 EFPY Pfr Limits," June 5,1995.
Terek, E., et al., WCAP-12685, " Analysis of Capsule U from the Commonwealth Edison Company Braidwood Unit 1 Reactor Vessel Radiation Surveillance Program," August 1990.
: 6.                           Yanichko, S.E., et al., WCAP-9807, " Commonwealth Edison Company, Braidwood Station Unit i Reactor Vesse! Surveillance Program," February 1981.
5.
: 7.                           Peter, P.A , WCAP-14243, "B,raidwood Unit i Heatup and Cooldown Limit Curves for Normal Operation," March 1995.
Westinghouse Letter to Conunonwealth Edison Company, CCE-95 186, "Braidwood Unit 1 LTOPS Setpoints Based on 16 EFPY Pfr Limits," June 5,1995.
: 8.                           Peter, P. A., WCAP-14242, " Evaluation of Pressurized Thermal Shock for Braidwood Unit 1," March 1995.
6.
: 9.                           Lippencott, E.P., WCAP-14044, " Westinghouse Surveillance Capsule Neutron Fluence Reevaluation," April 1994, 10, 10 CFR 50.61, " Fracture Toughaess Requirements for Protection Against Pressurized Thermal Shock Events," (PTS Rule) January 18,1996.
Yanichko, S.E., et al., WCAP-9807, " Commonwealth Edison Company, Braidwood Station Unit i Reactor Vesse! Surveillance Program," February 1981.
7.
Peter, P.A, WCAP-14243, "B,raidwood Unit i Heatup and Cooldown Limit Curves for Normal Operation," March 1995.
8.
Peter, P. A., WCAP-14242, " Evaluation of Pressurized Thermal Shock for Braidwood Unit 1," March 1995.
9.
Lippencott, E.P., WCAP-14044, " Westinghouse Surveillance Capsule Neutron Fluence Reevaluation," April 1994, 10, 10 CFR 50.61, " Fracture Toughaess Requirements for Protection Against Pressurized Thermal Shock Events," (PTS Rule) January 18,1996.
I1. U.S. Nuclear Regulatory Commission, Regulatory Guide 1.99, " Radiation Embrittlement of Reactor Vessel Materials," Revisicn 2, May 1988.
I1. U.S. Nuclear Regulatory Commission, Regulatory Guide 1.99, " Radiation Embrittlement of Reactor Vessel Materials," Revisicn 2, May 1988.
: 12. Laubham, T. J., WCAP-14970,"Braidwood Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," October 1997 and Erratta Sheet (Westinghouse Letter CAE                                       210, CCE 97-289).
: 12. Laubham, T. J., WCAP-14970,"Braidwood Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," October 1997 and Erratta Sheet (Westinghouse Letter CAE 210, CCE 97-289).
18
18


1; i
1; i
I'                                                                   BRAIDWOOD - UNIT l' PRESSURE AND TEMPERATURE LIMITS REPORT References (Continued)
I' BRAIDWOOD - UNIT l' PRESSURE AND TEMPERATURE LIMITS REPORT References (Continued)
: 13. Comed Ca'culation BRW-96-9061/BYR 96-293, " Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 1 Original Steam Generators and Replacement Steam Generators)," Revision 0.
: 13. Comed Ca'culation BRW-96-9061/BYR 96-293, " Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 1 Original Steam Generators and Replacement Steam Generators)," Revision 0.
: 14. Comed Nuclear Fuel Services Department, NDIT No. 960194, " Maximum Allowable LTOPS PORV Setpoints for Braidwood Unit I with RSGs," Revision 2.
: 14. Comed Nuclear Fuel Services Department, NDIT No. 960194, " Maximum Allowable LTOPS PORV Setpoints for Braidwood Unit I with RSGs," Revision 2.
: 15. Westinghouse Letter to Commonwealth Edison Company, CAE 97-211, CCE 290,
: 15. Westinghouse Letter to Commonwealth Edison Company, CAE 97-211, CCE 290,
          " Comed Byron and Braidwood Units 1 and 2 ATmetal Evaluation for Commonwealth Edison ," November 7,1997.
" Comed Byron and Braidwood Units 1 and 2 ATmetal Evaluation for Commonwealth Edison," November 7,1997.
T 4
T 4
19                       i
19 i


ATTACHMENT 1 WCAP-14824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD 20 -
ATTACHMENT 1 WCAP-14824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD 20 -


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N .;                                    - BRAIDWOOD - UNIT 2
N
,.                        PRESSURE AND TEMPERATURE LIMITS REPORT i
- BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT i
Table of Contents
Table of Contents
      - Section                                                                               Page l
- Section Page 1.0 - Introduction 1
1.0 - Introduction                                                                   1
.- 2.0 Operating Limits 1-2.1 RCS Pressure and Temper ture (PR) Limits 1
        .- 2.0   Operating Limits                                                             1-l 2.1   RCS Pressure and Temper ture (PR) Limits                             1 2.2 - Low Temperature Overpressure Protection (LTOP) System Setpoints       2
2.2 - Low Temperature Overpressure Protection (LTOP) System Setpoints 2
                ; 2.3   LTOP Enable Temperature                                             2 2.4   Reactor Vessel Boltup Temperature                                   3 2.5     Reactor Vessel Minimum Pressurization Temperature                   3 3.0     Reactor. Vessel Material Surveillance Program                               9 4.0     Supplemental Data Tables                                                 11 5,0     References                                                               18 Attachment WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron and Braidwood," Revision 2, November 1997.
; 2.3 LTOP Enable Temperature 2
2.4 Reactor Vessel Boltup Temperature 3
2.5 Reactor Vessel Minimum Pressurization Temperature 3
3.0 Reactor. Vessel Material Surveillance Program 9
4.0 Supplemental Data Tables 11 5,0 References 18 Attachment WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron and Braidwood," Revision 2, November 1997.
i-
i-
* i BRAIDWOOD - UNIT 2.l PRESSURE AND TEMPERATURE LIMITS REPORT List of Figures Firure Page 2.1 Braidwood Unit 2 Reactor Coolant System Heatup Limitations (Heatup Rates up to 4
i 100.*F/hr) Applicable for the First 12 EFPY (Without Margins for Instmmentation Errors) 2.2 Braidwoc,d Unit 2 Reactor Coolant System Cooldowa Limitations (Cooldown Rates up 5 to 100 'F/hr) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors) 2.3
_ Braidwood Unit 2 Maximum Allowabic Nominal PORY Setpoints for the Low 7
Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY n


*i .,                                  BRAIDWOOD - UNIT 2.l                                                l 1
'Es _
,.                    PRESSURE AND TEMPERATURE LIMITS REPORT                                              .
CRAIDWOOD. UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT List of Tabler Table -
List of Figures Firure                                                                                            Page 2.1  Braidwood Unit 2 Reactor Coolant System Heatup Limitations (Heatup Rates up to 4
Page 2.1 Braidwood Unit 2 Heatup and Cooldown Data Points at 12 EFPY
100.*F/hr) Applicable for the First 12 EFPY (Without Margins for Instmmentation                i Errors) 2.2  Braidwoc,d Unit 2 Reactor Coolant System Cooldowa Limitations (Cooldown Rates up 5 to 100 'F/hr) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors) 2.3  _ Braidwood Unit 2 Maximum Allowabic Nominal PORY Setpoints for the Low                    7 Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY n
> 6
 
-(Without Margins for Instrumentation Errors) 2.2 Data Points for Braidwood Unit 2 Maximum Allowable PORY Setpoints 8
'Es _    ",-                                CRAIDWOOD . UNIT 2
for the LTOP System Applicable for the First 12 EFPY 3.1 Braidwood Unit 2 Cap.me Withdrawal Schedule 10 4
.,_                          PRESSURE AND TEMPERATURE LIMITS REPORT List of Tabler Table -                                                                               Page 2.1     Braidwood Unit 2 Heatup and Cooldown Data Points at 12 EFPY                 >6
-4.1-Braidwood Unit 2 Calculation of Chemistry Factors Using Surveillance 12 Ct.psule Data 4.2 -
                -(Without Margins for Instrumentation Errors) 2.2       Data Points for Braidwood Unit 2 Maximum Allowable PORY Setpoints             8 for the LTOP System Applicable for the First 12 EFPY 3.1       Braidwood Unit 2 Cap.me Withdrawal Schedule                                 10   4
Braidwood Unit 2 Reactor Vessel Material Properties 13 4.3 Summary ofBraidwood Unit 2 Adjusted Reference Temperatures (ARTS) at 14 the 1/4T and 3/4T Locations for 12 EFPY 4.4 Braidwood Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 15 12 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on Sun eillance Capsule Data) i 4.5 RTus Values for Braidwood Unit 2 for 32 EFPY 16 4.6 RTm Values t'or Braidwood Unit 2 for 48 EFPY 17 tii
      -4.1-       Braidwood Unit 2 Calculation of Chemistry Factors Using Surveillance         12 Ct.psule Data 4.2 -     Braidwood Unit 2 Reactor Vessel Material Properties                         13 4.3       Summary ofBraidwood Unit 2 Adjusted Reference Temperatures (ARTS) at         14 the 1/4T and 3/4T Locations for 12 EFPY 4.4       Braidwood Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at   15 12 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on Sun eillance Capsule Data)                                                       i 4.5       RTus Values for Braidwood Unit 2 for 32 EFPY                                 16 4.6       RTm Values t'or Braidwood Unit 2 for 48 EFPY                                 17 tii
* i HRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 1.0 Introduction Reference to Technical Specifications (TS) numbers are given in both the Braidwood Station current Technical Specifications (CTS) and Improved Technical Specifications (ITS). The CTS number is presented first, followed by the ITS number in brackets [ ].
 
  *i     ,
HRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 1.0     Introduction Reference to Technical Specifications (TS) numbers are given in both the Braidwood Station current Technical Specifications (CTS) and Improved Technical Specifications (ITS). The CTS number is presented first, followed by the ITS number in brackets [ ].
This PTLR for Unit I has been prepared in accordance with the requirements of.
This PTLR for Unit I has been prepared in accordance with the requirements of.
TS 6.9.1.11/[ITS-5.6.6]. Revisions to the PTLR shall be provided to the NRC after issuance.
TS 6.9.1.11/[ITS-5.6.6]. Revisions to the PTLR shall be provided to the NRC after issuance.
The Technical Specifications addressed in this report are listed below:
The Technical Specifications addressed in this report are listed below:
LCO 3.4.9.1 Pressure /femperature Limits; and                                                     -
LCO 3.4.9.1 Pressure /femperature Limits; and LCO 3.4.9.3 Overpressure Protection Systems.
LCO 3.4.9.3 Overpressure Protection Systems.
[ITS-LCO 3,4.3 RCS Pressure and Temperature (Pff) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System].
[ITS-LCO 3,4.3 RCS Pressure and Temperature (Pff) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System].
2.0   Operating Limits The FTLR limits were developed using a methodology specified in the Technical Specifications.
2.0 Operating Limits The FTLR limits were developed using a methodology specified in the Technical Specifications.
The methodolcgy listed in WCAP-14040-NP-A (Reference 1) was used with four exceptions:
The methodolcgy listed in WCAP-14040-NP-A (Reference 1) was used with four exceptions:
a Use of ENDF/B-IV neutron transport cross-section library and ENDF/B-V dosimeter reaction cross-sections,
a Use of ENDF/B-IV neutron transport cross-section library and ENDF/B-V dosimeter reaction cross-sections,
Line 884: Line 1,369:
: d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.
: d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.
WCAP-14824, Revision 2, is included s an attachment for reference. WCAP-14824, Rev,2 contains the D/T curves for Byron Unit 4, along with th: weld metal data integration for Byron and Braidwood Units 1 and 2 and the Byron /Braidwood fluence methodologyjustifica: ion for ENDF/B-VI cross sections.
WCAP-14824, Revision 2, is included s an attachment for reference. WCAP-14824, Rev,2 contains the D/T curves for Byron Unit 4, along with th: weld metal data integration for Byron and Braidwood Units 1 and 2 and the Byron /Braidwood fluence methodologyjustifica: ion for ENDF/B-VI cross sections.
21       RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [ITS-LCO 3.4.3])
21 RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [ITS-LCO 3.4.3])
2.1.1 The RCS temperature rate-of-change limits defined in Reference 7 are:
2.1.1 The RCS temperature rate-of-change limits defined in Reference 7 are:
: a. A maximum heatup of 100"F in any 1-hour period,
: a. A maximum heatup of 100"F in any 1-hour period,
                      - b A maximum cooldown of 100*F in any 1-hour period, and c A maximum temperature change ofless than or equal to 10 F in any 1-hour period during
- b A maximum cooldown of 100*F in any 1-hour period, and c A maximum temperature change ofless than or equal to 10 F in any 1-hour period during j.
: j.                         inseivice hydrostatic and leak testing operations above the heatup and cooldown limit curves.
inseivice hydrostatic and leak testing operations above the heatup and cooldown limit curves.
I-
I-


1 BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2.1.2 The RCS P/T limits for heatup, insenice hydrostatic and leak testing, and criticality are specified by Figure 2.1 and Table 2.1. The RCS P/T limits for cooldown are shown in Figure 2.2 and Table 2.1. These limits are defmed in Reference 7. Consistent with the methodology described in Reference 1, the RCS P/T limits for heatup and cooldown shown in Figures 2.1 and 2.2 are provided without margins for instrument error. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, instrument uncertainties need not be considered since appropriate station operating procedures ensure that the limits contained in the figures and table are not exceeded. The criticality limit curve specifies pressure-temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix G.
BRAIDWOOD - UNIT 2 1
The P/T limits for core operation (except for low power physics testing) are that the reactor vessel must be at a temperature equal to or higher than the minimum temperature required for the insenice hydrostatic test, and at least 40'F higher than the minimum permissible         ,
PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2.1.2 The RCS P/T limits for heatup, insenice hydrostatic and leak testing, and criticality are specified by Figure 2.1 and Table 2.1. The RCS P/T limits for cooldown are shown in Figure 2.2 and Table 2.1. These limits are defmed in Reference 7. Consistent with the methodology described in Reference 1, the RCS P/T limits for heatup and cooldown shown in Figures 2.1 and 2.2 are provided without margins for instrument error. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, instrument uncertainties need not be considered since appropriate station operating procedures ensure that the limits contained in the figures and table are not exceeded. The criticality limit curve specifies pressure-temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix G.
temperature in the corresponding P/T curve for heatup and cooldown.
The P/T limits for core operation (except for low power physics testing) are that the reactor vessel must be at a temperature equal to or higher than the minimum temperature required for the insenice hydrostatic test, and at least 40'F higher than the minimum permissible temperature in the corresponding P/T curve for heatup and cooldown.
2.2   Low Temperature Overpressure Protection (LTOP) System Setpoir.ts (LCO 3.4.9.3/
2.2 Low Temperature Overpressure Protection (LTOP) System Setpoir.ts (LCO 3.4.9.3/
[ITS-LCO 3.4.12]).
[ITS-LCO 3.4.12]).
The power operated relief valves (PORVs) shall each have maximum lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13 and 14.
The power operated relief valves (PORVs) shall each have maximum lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13 and 14.
The LTOP setpoints are based on P/T limits which were established by 10 CFR 50, Appendix G without allowance for instrumentation error in accordance with the methodology described in Reference 1. The LTOP PORY maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.
The LTOP setpoints are based on P/T limits which were established by 10 CFR 50, Appendix G without allowance for instrumentation error in accordance with the methodology described in Reference 1. The LTOP PORY maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.
2.3   LTOP Enable Temperature The as taalyzed LTOP enable temperature is 200 F (Reference 15)
2.3 LTOP Enable Temperature The as taalyzed LTOP enable temperature is 200 F (Reference 15)
The TS required enable temperature for the PORVs shall be 2 350*F RCS temperature.
The TS required enable temperature for the PORVs shall be 2 350*F RCS temperature.
(Braidwood Unit 2 procedures governing tne heatup and cooldown of the RCS require the arming of the LTOP System for RCS temperature of 350*F and below and disarming of LTOP for RCS temperature above 350*F).
(Braidwood Unit 2 procedures governing tne heatup and cooldown of the RCS require the arming of the LTOP System for RCS temperature of 350*F and below and disarming of LTOP for RCS temperature above 350*F).
Line 904: Line 1,389:
t 2
t 2


's *;                                  BRAIDWOOD - UNIT 2
's BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Op: rating Limits (Continued) 2.4 Reactor Vessel Boltup Temperature (Non-Technical Specification)
,-                      PRESSURE AND TEMPERATURE LIMITS REPORT Op: rating Limits (Continued) 2.4   Reactor Vessel Boltup Temperature (Non-Technical Specification)
The minimum boltup temperature for the Reactor Vessel Flange shall be 2 60'F, Boltup is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and with the RCS vented to atmosphere (Reference 7).
The minimum boltup temperature for the Reactor Vessel Flange shall be 2 60'F, Boltup is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and with the RCS vented to atmosphere (Reference 7).
2.5   Reactor Vessel Minimum Pressurization Temperature (Non-Technical Specification)
2.5 Reactor Vessel Minimum Pressurization Temperature (Non-Technical Specification)
The minimum temperature at which the Resctor Vessel may be pressurized (i.e., in an unvented concDion) shall be 2 60*F, plus an allowance for the uncertainty of the temperature instrument, determined using a technique consistent with ISA-S67.04-1994.
The minimum temperature at which the Resctor Vessel may be pressurized (i.e., in an unvented concDion) shall be 2 60*F, plus an allowance for the uncertainty of the temperature instrument, determined using a technique consistent with ISA-S67.04-1994.
3
3


BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Material Property Basis LIMITING MATERIAL: CIRCUMFREtGIAL WELD (using sun'. capsule data)
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Material Property Basis LIMITING MATERIAL: CIRCUMFREtGIAL WELD (using sun'. capsule data)
LIMITING ART VALUES AT 12 EFPY:                                                                                                 1/4T,66.9'F 3/4T, 58.I'F 2500                                                                                                     ,              .
LIMITING ART VALUES AT 12 EFPY:
:      i.,......                                                                              ,              . . .                                                                  .                          ,          -                        .
1/4T,66.9'F 3/4T, 58.I'F 2500 i.,......
t                       .                    I                     i g                           '      '          '''
t I
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          ._              ~
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gn             -      LEAK TEST LIMIT                                                     7I                 '            '                      />                     V i
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1250                                                                                                                                                                                                                                              . . .
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' n.',
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UP To 300 r/Er.
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l, l
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i      -                                                              ' B I"'P                                               '                        ^'                                '
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250                                                                                                                                                                                             '                                          ' '
i..
m                                                  .          .
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TemE'                                             crit:Cativt t wit e49to OR                                                                                                         ,          ,
1250 f,
e                                                    '                                                                    INSERVICE RYDROST4"lC TEST                                                                                                   '
if i.
f TEMPERaTURS dIst F                                                                 i FOR TWE                                                   '
1 l
I SERVICE PER!dD UP PO 88.0 EFPY                                                                                               ' '
i I
: 0.                          ,                      ,                  .                            .                              ,                          ,                        ,                          .              .
i ACCEPTABLE g
0                   50                         100               150                   200                               250                     300                           350                   400                 450                     500 Moderator Temperature                                                                                                                                                                         (Deg.F) l                                                                                                                                 Figure 2.I Braidwood Unit 2 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/hr)
,i
Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix G Methodolgy)
,i
!                                                                                                                                            4
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e TemE' crit:Cativt t wit e49to OR m
INSERVICE RYDROST4"lC TEST TEMPERaTURS dIst F i FOR TWE f
I SERVICE PER!dD UP PO 88.0 EFPY 0.
0 50 100 150 200 250 300 350 400 450 500 Moderator Temperature (Deg.F) l Figure 2.I Braidwood Unit 2 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/hr)
Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix G Methodolgy) 4


BRAIDWOOD - UNIT 2 I
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Material Property Basis LIMIT!NG MATERIAL: CIRCUMFRENTIAL WELD (using sury capsule data)
PRESSURE AND TEMPERATURE LIMITS REPORT Material Property Basis LIMIT!NG MATERIAL: CIRCUMFRENTIAL WELD (using sury capsule data)
LIMITING ART VALUES AT 12 EFPY:
LIMITING ART VALUES AT 12 EFPY:                                                                                                           1/4T. 66.9'F 3/4T, 58.I'F 2500                                                                           ,                                                                                          .
1/4T. 66.9'F 3/4T, 58.I'F 2500
u...-
.,. 4 u...-
                                      ,,,,,,,,,                          i              ,                  i            . ...                                          ,          . . .                        . . ..                                                                    .
                                                                          ,                    ..                                  ..                  . ,... 4                     . . ,                        ,                                                        .              .
          -=                                                                                                                                            gi                                                        . .                          .                                                                        .
                                    ,            ,                , ,                  i...                            . ...                                    .                i i .                                        .
                                    , ;;i                ;        ,j                  ,..                              . .              .          ,..                          . . .                          i i ,i                                                                    .        .      8  . .
te-2250                    ,
                                                                                                                                    ..              i.
                                                                                                                                                                                    . , i 4        ..                  .                            .                        .          . .
      -                                                                                                                i ..                    ,,                    ,          . . . .                      . . ,                        .            .                      .
6 .,                  ,        , ,                        ..
                                                        .'4                                          ''                ' '              '      ''                    '          ' ' '                        ' '                                                                                                    '
U2                        1 '*'                                4
        = 2000
                                                                                                                                          ./                                      .
i i                                                  ,
                                                                                                                                          .i v                              i        . .        ,          , ,              .              .                                     v                                        .                             .
f c      1750 -- UNaccEPristE                                                                                                : <'                          .                                                                  .
                          ~
6                  "          OPERATION                                                                        ',/i
                                                                                                                                                                                    , i . i                      ,      . ..
1      .                i - i
                                                                                                                      ; /. ,                        ,..                          . . s .                      4 . ..                      .      .                      ...                      . . ! .
        -                          4 ,,.                ,          , ,              ....                              .                              ....                          . , . .                    . . ,,                        ...                      ....                          . . . t m      1500                        , ,        . . . ,                      ,,,                              , ,v i                                                      . . .                        , .              .          .
                                  ,          . ,      , . , ,                      ,              ..                      f.          .                        ..                      . i .                . , ,i                        ..                                          ,
u3                        iii.                i i .                        ..                  .            f.        .                        . ..                  ' ' i e                    i          ..                i...                      ..ii                          i i              ._
i          . .      . i i i                                      i              /              .                        . ..                  . . .                      . i ..                      .      . .              .,..                          . . .
c)                              .,,          ..i,                          .                    ,
fi          .        .            ..                                                                                                    .              .              ,          i i . .
6 1250              .                                .                                            ,    .
ACCEPTABLE                                                                                                          .
i...                '          .                          .          i/          i..
OFERATION                                                                                      ..
                                ..i.
i i
i i
                                                                                                                                                                ..i..i, 1
i...
                                                                                                                                                                                                              ; i ..
gi i i.
                                                                                                                                                                                                                                            .' ' . ... .''6...'
-=
i i,i 8
, ;;i
,j te-2250 i.
., i 4
6.,
i..
U2 1 '*'
.'4 4
= 2000 '.
./
i
i
                                                                                                                                                                                                                                                                                                    , , i .
.i i
1000                    .,.           .
v v
                                                                                                                                  .                                           i....                           ,                            ,                        ....                                   .       ,
i f
w                      .i               .               .                                                   .                         ,                            ii                 , .         . .               .           .,,                      .           ,                , , . .
~
                                                                                                                    . .               .           ,                              , , . .                   . .               .         ,                        ,...                                 i , a 0                -
1750 -- UNaccEPristE c
e00LDDVN                                                                                  . ,,                          , ,                          , , ,                . , ,,                      i,                      ,,,                                    ,
6
a RATES                                                    .,                                                             , ,                        ,                                      ,                                                  ,.               . . . .
" OPERATION
750 --
',/i 1
r/ar.                                                                                                      .                                                .                                        .                              .                        . . . .
i - i
e:               -
, i. i
                              .                0           y,               ,                  .                                                                              , , ,                    ,                            ,                              ,,                        . ,              .
; /.,
      =
.. s.
y 500 7 '-*-
4...
                        '"1" 100 50
1500
                                                      ^
,,v i 4,,.
                                                                                                                                .            i
... t m
                                                                                                                                                                                                                                                                                                  , . i .
f.
                                                            ,         .          .              ..               ,                          i           .                     . . .                    ,          ,
. i.
: m.             ,                    .                      .            ,            .                                  ,                                                      .                        .            .                . .              ,
.,,i u3 iii.
                                          . .            x.,                                                                               i                       .        . .                .    .                            ..              .        ,            ..                . . .
i i.
88       250~,                                         N               Boltup                                                     .                                  .            .                      .                                          ..                              . .              .
f.
g                        .            .
' ' i e i
                                              .            ..i
i...
                                                            .        6 g P.                                                       4 i...
..ii i i i
0 0                         5'O                 Id0                               150                           20                             2$0                           300                     3$0                         4 0                         480                           500 Moderator                                                                               Temperature                                                                                                         (Deg.F)
. i i i i
/
. i..
c)
..i, i i..
fi 1250 ACCEPTABLE 6
i/
i..
OFERATION i...
. '6...'
..i.
i i
1
..i..i,
; i..
,, i.
i 1000 i....
w
.i ii i, a 0
- e00LDDVN i,
- RATES a
750 -- r/ar.
e:
0 y,
=
500 7 50
^
100 y
i
'"1" i
,. i.
m.
x.,
i 88 250~,
N Boltup 4
..i g
g P.
6 i...
0 0
5'O Id0 150 20 2$0 300 3$0 4 0 480 500 Moderator Temperature (Deg.F)
Figure 2.2 Braidwood Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to 100*F/hr)
Figure 2.2 Braidwood Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to 100*F/hr)
              . Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix G methodolgy) 5
. Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix G methodolgy) 5


                                          ~         ~     ~                                                           ~~                                     ~ ' ~
~
orwvvvi.ivuivivu e PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.1 BRAIDWOOD Unit 2 Hestup* and Cooldown* Data Points at 12 EFPY"
~
                ; (Using 1996 Appendix G Methodolgy Without margins for instrumentation errors)
~
HEATUP CURVES                                                   ' COOLDOWN CURVES                                                         _
orwvvvi.ivuivivu e
100 F Heat 4                           Leek Test curve         CatacelHy Lindt         Undt                 Stee8y 8tste     28 D80 F           88 DSO F           100 080F T           P       T     1 P         T I P                       T i P         T i P               T i P             T + P 80           C     192 1 0           17012000                   80 1 0       to 1 0               80 i- 0           80 1 0 to         821     1 92       708   192i2485                   80 l 821     to i 821             to I 801           80 ' 511 85         821     192       741               f               85 . 821     85 t 821             85 ! 819           85 i 532 70         821-     192       729               1               70 I 821     70 l 821             70 1 821           70 1 555
~~
                    -75           821     192 I 720                     I               75     821   75 i 821           - 75       1 821   75 1 579 80    '
~ '
821     192 I 715                   l                 80     821   80 l 821             80         821   80 { 805 85         821     192 4 713                   1                 85     821   85 i 821             85         821   85 l 821 90 i 821           192 1 114                                     20     821   to           821     to         821   90 1 821 95         f'71     192 1 719                                     95 l 821     95         821     95 I 821           95 i 821 100         821     192 i 728                   6               100 l 821     100         421     100 I 821         100 i 821 105         821     192 1 735                   1               105 1 821     -105 I 821           105! 821         -105 1 821
~
                  '110           821     192         748             i               '10 1 821
PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.1 BRAIDWOOD Unit 2 Hestup* and Cooldown* Data Points at 12 EFPY"
                                                                                        ,              110 l 821           110         821   110 4 821 115 : 821           192       783             f               115 i 821       115 l 821           1151 821           115           821 120 ; $21           192       700             1               120       821   120 l 821           120- 821           120           821 125         821     192 I 801                   l               125       821   125         821     125         821   125           821 130 i - 821         192 1 824                   1               130       821   130         821     130         821   130 1 821 135         821     195 ! 850                 1                 135       821   135         821   135         821   135 I 821 140         821     200 1 879                 !
; (Using 1996 Appendix G Methodolgy Without margins for instrumentation errors)
140 i 821       140 1 821           140 1 821                       f 140         700   _.205       911           l                 140 1 1138     140 ! 1131         140 l 1128                     1 145 1 801           210 [ 948                 1                 145 l 1187     145 ! 1184         145         1188               i 150  '
HEATUP CURVES
824     215 l 984                 i                 150 ! 1240               (-                                       i 155         850     220 ' 1028               6                   155 i 1297               l                                       !
' COOLDOWN CURVES 100 F Heat 4 Leek Test curve CatacelHy Lindt Undt Stee8y 8tste 28 D80 F 88 DSO F 100 080F T
180         879     225 i 1071               1                   180 6 1357               L                   I                   i 185         911     230 1 1120               l                   185 1 1423               I                   i                   l 170         948     235 t 1174                                   170 l 1493               I                   I                   i 175         984     240 t 1231               .
P T
1F5 l 1589               I                   i                   l 180         1028     245 1 1294               i                   180 f 1850               f                   I                   i 185         1071     250       1381         i                   185 i 1738               i                   l                   i 190         1120     255 l 1433                                   190 1 1832               l                   l                   t 195         1174     280 ; 1511                                   195 1 1933             I                   I                   t 200         1231     285 ! 1595                                   200 ? 2041             i                   I                 1 205         1294     270       1886                               205 i 2158             i                   i                   1 210         1381     27f       1783                               210 1 2284             i                                       I 215         1433     280       1888                               215 2419               i                                     !
1 P T I P T i P T i P T i P T + P 80 C
220         1511     285 ' 2000                                           i             t                   i                   i 225         1595     290       2121                                       t             I                   !
192 1 0 17012000 80 1 0 to 1 0 80 i- 0 80 1 0 to 821 1 92 708 192i2485 80 l 821 to i 821 to I 801 80 ' 511 85 821 192 741 f
* 230         1886     295       2251                                       i             i                   i 235         1783     300 ' 2391             i                             i             t                   l                 l 240       -1888               6                                           1                                 i                 !
85. 821 85 t 821 85 ! 819 85 i 532 70 821-192 729 1
245         2000             '                                            '                                '
70 I 821 70 l 821 70 1 821 70 1 555
i 250         2121'             .                                                                                                4 255         2251                                                         1             4                   !                  l 280         2391                                                         I                                 i                 i i
-75 821 192 I 720 I
i
75 821 75 i 821
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- 75 1 821 75 1 579 821 192 I 715 l
80 821 80 l 821 80 821 80 { 805 80 85 821 192 4 713 1
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100 l 821 100 421 100 I 821 100 i 821 105 821 192 1 735 1
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821
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'110 821 192 748 i
'10 1 821 110 l 821 110 821 110 4 821 115 : 821 192 783 f
115 i 821 115 l 821 1151 821 115 821 120 ; $21 192 700 1
120 821 120 l 821 120-821 120 821 125 821 192 I 801 l
125 821 125 821 125 821 125 821 130 i - 821 192 1 824 1
130 821 130 821 130 821 130 1 821 135 821 195 ! 850 1
135 821 135 821 135 821 135 I 821 140 821 200 1 879 140 i 821 140 1 821 140 1 821 f
140 700
_.205 911 l
140 1 1138 140 ! 1131 140 l 1128 1
145 1 801 210 [ 948 1
145 l 1187 145 ! 1184 145 1188 i
824 215 l 984 i
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180 879 225 i 1071 1
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* HeStup and C00100wn data inclu0e vessel flange requirements of 140 F Snd 621 psig per 10CFR50. Appendix G l         " For each c00ldOwn rate, the steady-state pressure values shall govern the temperature where no ellowable pressure values are provided.
* HeStup and C00100wn data inclu0e vessel flange requirements of 140 F Snd 621 psig per 10CFR50. Appendix G l
l:                                                                             6 l
" For each c00ldOwn rate, the steady-state pressure values shall govern the temperature where no ellowable pressure values are provided.
l:
6 l


GRAIDWOOD - UNIT 2                                                                                     l 4
GRAIDWOOD - UNIT 2 4
L                                       PRESSURE AND TEMPERATURE LIMITS REPORT
L PRESSURE AND TEMPERATURE LIMITS REPORT
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t ' i: it i I II I i l l                                           1II             !I I II I O                 M                   100                 1H                         200               2H               300             3M AUCTIONEERED LOW RCS TEMPERATURE (DEG, F)
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Figure 2.3 Braidwood Unit 2 Maximum Allowable Nominal PORV Setpoints for the Low Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY
Figure 2.3 Braidwood Unit 2 Maximum Allowable Nominal PORV Setpoints for the Low Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY
'(
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s  ,-                                        BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.2 Data Points for Braidwood Unit 2 Madmum Allowable PORV Setpoints for the LTOP System Applicable for the First 12 EFPY PCV-455A '                                                   PCV-456 (2TY-0413M)                                                 (2TY-0413P)-
BRAIDWOOD - UNIT 2 s
AUCTIONEERED LOW           RCS PRESSURE                     AUCTIONEERED LOW   RCS PRESSURE RCS TEMP. (DEG. F)             (PalG)                       RCS TEMP. (DEG. F)       (PSIG) 50                     497                                 50             513 70                     497                                 70             513 100-                   497                                 100             513
PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.2 Data Points for Braidwood Unit 2 Madmum Allowable PORV Setpoints for the LTOP System Applicable for the First 12 EFPY PCV-455A '
          ,          120                     452                                 120             469 170                     451                                 170             468 200                     614                                 200             630 250                     599                                 250             615 300                     584                                 300             600 350                     584                                 350             600 450                     2350                                 450             2350 Note: To determine maximum allowable lift setpoints for RCS Pressure and RCS Temperatures greater than 350*F, linearly interpolate between the 350'F and 450 F data points shown above.
PCV-456 (2TY-0413M)
(2TY-0413P)-
AUCTIONEERED LOW RCS PRESSURE AUCTIONEERED LOW RCS PRESSURE RCS TEMP. (DEG. F)
(PalG)
RCS TEMP. (DEG. F)
(PSIG) 50 497 50 513 70 497 70 513 100-497 100 513 120 452 120 469 170 451 170 468 200 614 200 630 250 599 250 615 300 584 300 600 350 584 350 600 450 2350 450 2350 Note: To determine maximum allowable lift setpoints for RCS Pressure and RCS Temperatures greater than 350*F, linearly interpolate between the 350'F and 450 F data points shown above.
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BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0   Reactor Vesse! Material Surveillance Program The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determine changes in material properties. Tne removal schedule is provided in Table 3.1. The results of these analyses shall be used to update Figures 2.1 and 2.2 and Table 2.1.' The time of specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns rnost closely approaching the withdrawal schedule.
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0 Reactor Vesse! Material Surveillance Program The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determine changes in material properties. Tne removal schedule is provided in Table 3.1. The results of these analyses shall be used to update Figures 2.1 and 2.2 and Table 2.1.' The time of specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns rnost closely approaching the withdrawal schedule.
The pressure vessel material surveillance program (Reference 6) is in compliance with Appendix H to 10 CFR 50, " Reactor Vessel Radiation Surveillance Program." The material test requirements and the acceptance standards ntilize the reference nil-ductility temperature, RTr,w ,
The pressure vessel material surveillance program (Reference 6) is in compliance with Appendix H to 10 CFR 50, " Reactor Vessel Radiation Surveillance Program." The material test requirements and the acceptance standards ntilize the reference nil-ductility temperature, RTr,w,
which is determined in accordance with ASME Section III Paragraph NB 2331. The empirical relationship between RTum and the fracture toughness of the reactor vessel steel is developed in accordance with Appendix G, " Protection Against Non Ductile Failure," to Section XI of the ASME Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM E185 82.
which is determined in accordance with ASME Section III Paragraph NB 2331. The empirical relationship between RTum and the fracture toughness of the reactor vessel steel is developed in accordance with Appendix G, " Protection Against Non Ductile Failure," to Section XI of the ASME Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM E185 82.
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          ,                                          BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORf Table 3.1 Braidwood Unit 2 Capsule Withdrawal Schedule Capsule         Vessel Location       Capsule La.ad     Removal Time"'   Estimated Capsule 2
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORf Table 3.1 Braidwood Unit 2 Capsule Withdrawal Schedule Capsule Vessel Location Capsule La.ad Removal Time"'
(Degrees)               Factor             (EFPY)       Fluence (n/cm )
Estimated Capsule 2
U                   58.5'               4.00           1.15 (Removed)     3.933 x 10" X                   238.5*               4.02         4.215 (Removed)       1.126 x 10" W                   121.5*             4.02         7.97 (EOL Wall)     2.199 x 10"N 11,95 (1.5 EOL Z                   301.5'               4.02               Wall'")         3.299 x 10" V                   61.0*               3.70               Standby               -
(Degrees)
Y          t     241.0*               3.70               Standby               --
Factor (EFPY)
(a) Effective Full Power Years (EFPY) from plant startup.
Fluence (n/cm )
U 58.5' 4.00 1.15 (Removed) 3.933 x 10" X
238.5*
4.02 4.215 (Removed) 1.126 x 10" W
121.5*
4.02 7.97 (EOL Wall) 2.199 x 10"N 11,95 (1.5 EOL Z
301.5' 4.02 Wall'")
3.299 x 10" V
61.0*
3.70 Standby Y
t 241.0*
3.70 Standby (a) Effective Full Power Years (EFPY) from plant startup.
(b) Maximum end oflicense (32 EFPY) inner vessel wall fluence.
(b) Maximum end oflicense (32 EFPY) inner vessel wall fluence.
(c) Derived from Table C-4 of WCAP-14824, Rev. 2 (Reference 2, which is the Attachment to this report).
(c) Derived from Table C-4 of WCAP-14824, Rev. 2 (Reference 2, which is the Attachment to this report).
10
10


      '.                                    BRAIDWOOD - UNIT 2
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 4.0
  ,                        PRESSURE AND TEMPERATURE LIMITS REPORT 4.0 . Suppicmental Data Tables The following tables provide supplemental information on reactor vessel material propenies and are provided to be consistent with Geaeric Letter 96-03. Some of the material property values shown were used as inputs to the P/T limits.
. Suppicmental Data Tables The following tables provide supplemental information on reactor vessel material propenies and are provided to be consistent with Geaeric Letter 96-03. Some of the material property values shown were used as inputs to the P/T limits.
Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance capsule data.
Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance capsule data.
Table 4.2 provides the reactor vessel material properties.
Table 4.2 provides the reactor vessel material properties.
Table 4.3 provides a summary of the Brsidwood Unit 2 adjusted reference temperatures (ARTS) at     I the 1/4T and 3/4T locations for 12 EFPY.
Table 4.3 provides a summary of the Brsidwood Unit 2 adjusted reference temperatures (ARTS) at I
the 1/4T and 3/4T locations for 12 EFPY.
Table 4.4 shows the calculation of ARTS at 12 EFPY for the limiting Braidwood Unit 2 reactor vessel material -Weld Metal WF562 (Based on Surveillance Capsule Data).
Table 4.4 shows the calculation of ARTS at 12 EFPY for the limiting Braidwood Unit 2 reactor vessel material -Weld Metal WF562 (Based on Surveillance Capsule Data).
Table 4.5 provides the RTns values for Braidwood Unit 2 for 32 EFPY.                               !
Table 4.5 provides the RTns values for Braidwood Unit 2 for 32 EFPY.
i Table 4.6 provides the RTnsvalues for Braidwood Unit 2 for 48 EFPY, l
i Table 4.6 provides the RTns alues for Braidwood Unit 2 for 48 EFPY, v
Il i                                                   _    ._  __
l Il i


2-    *
BRAIDWOOD - UNIT 2 2-PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.1 Braidwood Unit 2 Calculation of Chemistry Factors Using Surveillance Capsule Data Fluence Material Capsule (n/cm',
        ,                                                          BRAIDWOOD - UNIT 2                                                                             l l
FF"' -
PRESSURE AND TEMPERATURE LIMITS REPORT                                                                                       ,
- Measured FF*ARTm1
l Table 4.1                                     ,
- (FF)2 E>l.0 ARTet Mev). f Lower Shell Forging U
Braidwood Unit 2 Calculation of Chemistry Factors Using Surveillance Capsule Data Fluence Material           Capsule           (n/cm',                 FF"' -               - Measured             FF*ARTm1                   - (FF)2 E>l .0                                         ARTet                                                     ,
3.933 x10''
Mev). f Lower Shell Forging                   U             3.933 x10''             O.741                           0                     0.000                 0.550 50D102/50C97                                                                                                         ._ .
O.741 0
(Tangential)
0.000 0.550 50D102/50C97 (Tangential)
X             1.126 x10''             l.033                         2                     3.099                 1.067 Lower Shell Forging                   U             3.933 x10''             O.741                         5                     3.707                 0.550 50D102/50C97 (Axial)                   X             1.126x10''             l.033                         35                     36.160                 1.067 Sum:               42.996                 3.234 Chemistry Factord' = 42.996 + 3.234 = 13.3*F Braidwood 1 Weld                     U             3.814x10''             O.733                         10"'                   7.333                 0,538 Metal WF562*'
X 1.126 x10''
_X                 1.144x10''             l.038                         25")                   25.95                   1.077 Braidwood 2 Weld                       U             3.933 x 10''           O.741                           0                           0               0.550 Metal WF562"'
l.033 2
X             l.126 x10''             l.033                         20'"                   2066                   1.067 Sum:               53.943                   3.232 Chemistry Factor d' = 53.943+ 3.232= 16.7'F (a) FF = Fluence Factor = fo.2a innn (b) Braidwood Unit 1 ARTer alues         v were obtained from WCAP-14243. (Reference 12).
3.099 1.067 Lower Shell Forging U
(c) Braidwood Unit 2 capsule fluence, FF, and ARTm1 values were obtained from WCAP-14970 (Reference 7).
3.933 x10''
O.741 5
3.707 0.550 50D102/50C97 (Axial)
X 1.126x10''
l.033 35 36.160 1.067 Sum:
42.996 3.234 d
Chemistry Factor ' = 42.996 + 3.234 = 13.3*F Braidwood 1 Weld U
3.814x10''
O.733 10"'
7.333 0,538 Metal WF562*'
_X 1.144x10''
l.038 25")
25.95 1.077 Braidwood 2 Weld U
3.933 x 10''
O.741 0
0 0.550 Metal WF562"'
X l.126 x10''
l.033 20'"
2066 1.067 Sum:
53.943 3.232 Chemistry Factor d' = 53.943+ 3.232= 16.7'F (a) FF = Fluence Factor = fo.2a innn (b) Braidwood Unit 1 ARTer alues were obtained from WCAP-14243. (Reference 12).
v (c) Braidwood Unit 2 capsule fluence, FF, and ARTm1 values were obtained from WCAP-14970 (Reference 7).
(d) Chemistry Factor = I (FF* ARTmT) / I ((FF) 2),
(d) Chemistry Factor = I (FF* ARTmT) / I ((FF) 2),
(e) ARTer per Ratio Procedure of 10 CFR 50.61 (Reference 10) is not affected, since Ratio = 1.0.
(e) ARTer per Ratio Procedure of 10 CFR 50.61 (Reference 10) is not affected, since Ratio = 1.0.
See Table E.-4 ofWCAP 14824, Rev. 2 (Reference 2)
See Table E.-4 ofWCAP 14824, Rev. 2 (Reference 2)
                                                                          ,12
,12


    ,                                BRAIDWOOD - UNIT 2 PRESStJRE AND TEMPERATURE LIMITS REPORT Table 4.2 Braidwood Unit 2 Reactor Vessel Material Pro perties Chemistry           Initial Material       Cu (%)"' Ni (%)"'     Factor"'     RT er ('F)*'
BRAIDWOOD - UNIT 2 PRESStJRE AND TEMPERATURE LIMITS REPORT Table 4.2 Braidwood Unit 2 Reactor Vessel Material Pro perties Chemistry Initial Material Cu (%)"'
Description Closure Head         Not         0.75       -                20"'
Ni (%)"'
* Flange       Reported Vessel Flange         0.07       0.70       -                20"'
Factor"'
Lower Shell         0.06       0.77     37.0               -30 Forging Upper Shell         0.03       0.71       20.0               -30 Forging Weld Metal         0.03       0.67       41.0               40 WF562 (a) Chemistry Factors are calculated from Cu and Ni values per Regulatory Guide 1.99, Position 1 (Reference 11).
RT er ('F)*'
Description Closure Head Not 0.75 20"'
Flange Reported Vessel Flange 0.07 0.70 20"'
Lower Shell 0.06 0.77 37.0
-30 Forging Upper Shell 0.03 0.71 20.0
-30 Forging Weld Metal 0.03 0.67 41.0 40 WF562 (a) Chemistry Factors are calculated from Cu and Ni values per Regulatory Guide 1.99, Position 1 (Reference 11).
(b) Initial RTervalues are measured, WCAP-14970 (Ref:rence 7).
(b) Initial RTervalues are measured, WCAP-14970 (Ref:rence 7).
(c) Closure head and vessel Dange Initial RTervalues are used for considering Dange requirements for the heatup/cooldown curves, WCAP-14970.
(c) Closure head and vessel Dange Initial RTervalues are used for considering Dange requirements for the heatup/cooldown curves, WCAP-14970.
13
13


      ,                              BRAIDWOOD - UNIT 2
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3 Summary of Braidwood Unit 2 Adjusted Reference Temperatures (ARTS) at the 1/4T and 3/4T Locations for 12 EFPY 12 EFPY Material Description 1/4T ART (*F) 3/4T ART ('F)
,                  PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3 Summary of Braidwood Unit 2 Adjusted Reference Temperatures (ARTS) at the 1/4T and 3/4T Locations for 12 EFPY 12 EFPY Material Description           1/4T ART (*F)         3/4T ART ('F)
Lower Shell Forging 29.5 10.1 Using credible surveillance capsule datt.
Lower Shell Forging                 29.5                   10.1 Using credible surveillance capsule datt.
(RG Position 2'")
(RG Position 2'")                 -8.6                   -15.6 Upper Shell Forging                 2.2                   -8.3 (RG Position l'")
-8.6
Weld Metal                   105 o                   84.4 (RG Position l'")
-15.6 Upper Shell Forging 2.2
Using credible                 66.9*                   58.l*
-8.3 (RG Position l'")
Weld Metal 105 o 84.4 (RG Position l'")
Using credible 66.9*
58.l*
surveillance capsule data (RG Position 2'")
surveillance capsule data (RG Position 2'")
(a) Calculated using a chemistry factor based on Regulatory Guide (RG) 1.99, Position 1 and Position 2 (Reference 11).
(a) Calculated using a chemistry factor based on Regulatory Guide (RG) 1.99, Position 1 and Position 2 (Reference 11).
Line 1,155: Line 1,837:
14
14


t
BRAIDWOOD - UNIT 2 t
  '.                              BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.4 Braidwood Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 12 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on Surveillance Capsule Data)
PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.4 Braidwood Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 12 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on Surveillance Capsule Data)
Parameter                               Values Operating Time                           12 EFPY Location")               1/4T ART                       3/4T ART f.
Parameter Values Operating Time 12 EFPY Location")
Chemistry Factor, CF ('F)             16.7                             16.7 Fluence (f), n/cm 2          4.95x10"                       1.78x10" (E>1.0 Mev)i')
1/4T ART 3/4T ART f.
Fluence Factor, FF             0.804                       _ 0.542 ARTmn= CFxFF('F)                 13.43                             9.05 Initial RTm . I('F)               40                               40 Margia, M(*F)                 13.43                             9.05 ART = 1+(CF'FF)+M, 'F               66.9                               58.1 per RG 1.99. Revision 2 (a) Fluence, f, is based upon f r(E>l.0 Mev) = 1.100x10'* at 16 EFPY, WCAP 14228 (Reference 3).
Chemistry Factor, CF ('F) 16.7 16.7 2
Fluence (f), n/cm 4.95x10" 1.78x10" (E>1.0 Mev)i')
Fluence Factor, FF 0.804
_ 0.542 ARTmn= CFxFF('F) 13.43 9.05 Initial RTm. I('F) 40 40 Margia, M(*F) 13.43 9.05 ART = 1+(CF'FF)+M, 'F 66.9 58.1 per RG 1.99. Revision 2 (a) Fluence, f, is based upon f r(E>l.0 Mev) = 1.100x10'* at 16 EFPY, WCAP 14228 (Reference 3).
(b) The Braidwood Unit 2 reactor vessel wall thickness is 8.5 inches at the beltline region.
(b) The Braidwood Unit 2 reactor vessel wall thickness is 8.5 inches at the beltline region.
15
15


BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.5 RTru Values for 13raidwood Unit 2 for 32 EFPY CF       p.> . pgi         .M   RTsum   ARTeis- RTers Material-               ('F)                           (*F)   ('F)       ('F)   ('F)-
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.5 RTru Values for 13raidwood Unit 2 for 32 EFPY CF p.>.
Upper Shell Forging             20.0     2.199   1.214       24.28     -30     24.28   18.6 MK 24 3 Lower Shell Forging             37.0     2 199   1.214       34,0     -30     44.92   48.9 Using Surveillance Capsule                                                                               ,
pgi
Data                   13.3     2.199   1214       34.0")     30     16.15   20.2 Circumferential Weld           41.0     2.199   1.214       49.77     40     49.77   139.5 Metal WF562 Using Surveillance             16.7     2.199   1.214       20.27     40     20.27   80.5 Capsule Data")
.M RTsum ARTeis-RTers Material-('F)
(*F)
('F)
('F)
('F)-
Upper Shell Forging 20.0 2.199 1.214 24.28
-30 24.28 18.6 MK 24 3 Lower Shell Forging 37.0 2 199 1.214 34,0
-30 44.92 48.9 Using Surveillance Capsule Data 13.3 2.199 1214 34.0")
30 16.15 20.2 Circumferential Weld 41.0 2.199 1.214 49.77 40 49.77 139.5 Metal WF562 Using Surveillance 16.7 2.199 1.214 20.27 40 20.27 80.5 Capsule Data")
(a) 2.199x10" n/cm' (E>l.0 Mev) for 32 EFPY from Braidwood 2 PTS report WCAP-14229 (Reference 8)
(a) 2.199x10" n/cm' (E>l.0 Mev) for 32 EFPY from Braidwood 2 PTS report WCAP-14229 (Reference 8)
(b) FF (Fluence Factor) = fa2:en n (c) Calculated using CF based on surveillance capsule data per RG 1.99, Position 2 (Refaence 1l)
(b) FF (Fluence Factor) = fa2:en n (c) Calculated using CF based on surveillance capsule data per RG 1.99, Position 2 (Refaence 1l)
Line 1,171: Line 1,864:
16
16


BRAIDWOOD - UNIT 2                           -
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4 6 RTns Values for Braidwood Unit 2 for 48 EFPY CF p.>
PRESSURE AND TEMPERATURE LIMITS REPORT Table 4 6 RTns Values for Braidwood Unit 2 for 48 EFPY CF         p.>     pp     M     RTsortv)   ARTns       RTns Matenal                 ("F)                       (*F)     (*F)       ('F)     ('F)
pp M
Upper Shell Forging           20.0     3.298   1.313 26.26       -30       26.26     22.5 Lower Shell Forging             37.0     3.298   1.313   34.0       -30       48.58     52.6 Using Surveillance           13.3     3.298   1.313 34.0N)     -30       17.46     21.5 Capsule Data (*)
RTsortv)
Circumferential Weld           41.0     3.298   1.313 53.83       40       53.83-     147.7 Metal WF562 Using Surveillance           16.7     3.298   1.313 21.93       40       21.93     83.9 Capsule Data'*)
ARTns RTns Matenal
(a) 3.298x10" rt/ cm2 (E>l.0 Mev) for 48 EFPY from Braidwood 2 PTS report WCAP-14229 (Reference 8).
("F)
(*F)
(*F)
('F)
('F)
Upper Shell Forging 20.0 3.298 1.313 26.26
-30 26.26 22.5 Lower Shell Forging 37.0 3.298 1.313 34.0
-30 48.58 52.6 N
Using Surveillance 13.3 3.298 1.313 34.0 )
-30 17.46 21.5 Capsule Data (*)
Circumferential Weld 41.0 3.298 1.313 53.83 40 53.83-147.7 Metal WF562 Using Surveillance 16.7 3.298 1.313 21.93 40 21.93 83.9 Capsule Data'*)
(a) 3.298x10" rt cm (E>l.0 Mev) for 48 EFPY from Braidwood 2 PTS report WCAP-14229
/
2 (Reference 8).
(b) FF (Fluence Factor) = f*2'#'*"*'O (c) Calculated using a CF based on surveillance capsule data per RG 1.99, Position 2 (Reference 11).
(b) FF (Fluence Factor) = f*2'#'*"*'O (c) Calculated using a CF based on surveillance capsule data per RG 1.99, Position 2 (Reference 11).
(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation. See WCAP-14824 Rev. 2 (Reference 2).
(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation. See WCAP-14824 Rev. 2 (Reference 2).
Line 1,181: Line 1,887:
l 17
l 17


      '.                                    BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 5.0   References
BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 5.0 References 1.
: 1. Andracheck, J.D., et al., WCAP-14040-A. " Methodology used to Develop Cold Overpressure / Mitigating System Setpoints and RCS Heatup and Cooldown Limit         l Curves," Revision 2 January 1996.                                                   ;
Andracheck, J.D., et al., WCAP-14040-A. " Methodology used to Develop Cold Overpressure / Mitigating System Setpoints and RCS Heatup and Cooldown Limit Curves," Revision 2 January 1996.
1
2.
: 2.   ' Grendys, P.A., WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for       ;
' Grendys, P.A., WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"
Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"     l Revision 2, November 1997.
Revision 2, November 1997.
i
i 3.
: 3.     Peter, P.A., et al., WCAP-14228, " Analysis of Capsule X from the Commonwealth Edison Company Braidwood Unit 2 Reactor Vessel Radiation Surveillance Program,"
Peter, P.A., et al., WCAP-14228, " Analysis of Capsule X from the Commonwealth Edison Company Braidwood Unit 2 Reactor Vessel Radiation Surveillance Program,"
March 1995.                                                                         i
March 1995.
: 4. Terek, E., et al., WCAP-12845, " Analysis of Capsule U from the Commonwealth Edison Company Braidwood Unit 2 Reactor Vessel Radiation Surveillance Program,"
i 4.
Terek, E., et al., WCAP-12845, " Analysis of Capsule U from the Commonwealth Edison Company Braidwood Unit 2 Reactor Vessel Radiation Surveillance Program,"
March 1991.
March 1991.
: 5. Westinghouse Letter to Commonwealth Edison Company, CCE-96-104, "Braidwood Unit 2 LTOPS Setpoints Based on 16 EFPY P/T Limits," January 24,1996.
5.
: 6.     Singer, L.R., WCAP-11188, " Commonwealth Edison Company, Braidwood Station Unit 2 Reactor Vessel Surveillance Program," December 1986.
Westinghouse Letter to Commonwealth Edison Company, CCE-96-104, "Braidwood Unit 2 LTOPS Setpoints Based on 16 EFPY P/T Limits," January 24,1996.
: 7.     Laubham, T. J., WCAP-14970, "Braidwood Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," October 1997 and Erratta Sheet (Westinghouse Letter CAE-97 210, CCE-97 289).
6.
: 8. Peter, P. A., WCAP 14229, " Evaluation of Pressurized Thermal Shock for Braidwood Unit 2," March 1995.
Singer, L.R., WCAP-11188, " Commonwealth Edison Company, Braidwood Station Unit 2 Reactor Vessel Surveillance Program," December 1986.
: 9. Lippencott, E.P. WCAP-14044, " Westinghouse Surveillance Capsule Neutron Fluence Reevaluation," April 1994.
7.
: 10. 10 CFR 50.61, " Fracture Tou'ghness Requirements for Protection Against Pressurized Thermal Shock Events,"(PTS Rule) January 18,1996.
Laubham, T. J., WCAP-14970, "Braidwood Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," October 1997 and Erratta Sheet (Westinghouse Letter CAE-97 210, CCE-97 289).
: 11. U.S. Nuclear Regulatory Commission, Regulatory Guide 1.99, "Radation Embrittlement of Reactor Vessel Materials," Revision 2, May 1988.
8.
: 12. Peter, P.A., WCAP-14243, "Braidwood Unit i Heatup and Cooldown Limit Curves for Normal Operation," March 1995.
Peter, P. A., WCAP 14229, " Evaluation of Pressurized Thermal Shock for Braidwood Unit 2," March 1995.
9.
Lippencott, E.P. WCAP-14044, " Westinghouse Surveillance Capsule Neutron Fluence Reevaluation," April 1994.
10.
10 CFR 50.61, " Fracture Tou'ghness Requirements for Protection Against Pressurized Thermal Shock Events,"(PTS Rule) January 18,1996.
11.
U.S. Nuclear Regulatory Commission, Regulatory Guide 1.99, "Radation Embrittlement of Reactor Vessel Materials," Revision 2, May 1988.
12.
Peter, P.A., WCAP-14243, "Braidwood Unit i Heatup and Cooldown Limit Curves for Normal Operation," March 1995.


ERAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT References (Continued)
ERAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT References (Continued) 13.
: 13. Comed Calculation BRW 96-9061/BYR 96-293," Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 2 Origimd Steam Generators)," Revision O.
Comed Calculation BRW 96-9061/BYR 96-293," Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 2 Origimd Steam Generators)," Revision O.
: 14. Westinghouse Letter to Commonwealth Edison Company, CCE-97-278, "CemEd Braidwood Unit 2 COMMS Setpoint for 12 EFPY," October 23,1997.
14.
: 15. Westinghouse Letter to Commonwealth Edison Company, CAE-97-211, CCE-97 290,
Westinghouse Letter to Commonwealth Edison Company, CCE-97-278, "CemEd Braidwood Unit 2 COMMS Setpoint for 12 EFPY," October 23,1997.
                  " Comed Byron and Braidwood Units 1 and 2 ATmetal Evaluation for Commonwealth Edison," November 7,1997, 1
15.
Westinghouse Letter to Commonwealth Edison Company, CAE-97-211, CCE-97 290,
" Comed Byron and Braidwood Units 1 and 2 ATmetal Evaluation for Commonwealth Edison," November 7,1997, 1
19
19


e, ,
e, ATTACHMENT I WCAP-14824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD 20-
ATTACHMENT I WCAP-14824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD 20-
,}}
,}}

Latest revision as of 07:52, 10 December 2024

Revised Byron Unit 2 Pressure Temperature Limits Rept (PTLR)
ML20199E880
Person / Time
Site: Byron  Constellation icon.png
Issue date: 11/03/1997
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BYRON UNIT 2 PRESSURE TEMPERATURE LIMITS REPORT (PTLR)

(Revised November 3,1997)

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BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT-Table of Contents -

Section Page i

1.0

Introductions

1 s

1 2.0 Operating Limits 1

]

2.1 RCS Pressure and Temperature (P/T) Limits 1

2.2 Low Temperature Overpressure Protection (LTOP) System Setpoints 2

l 2.3 LTOP Enable Temperature ~

2-2.4 Reactor Vessel Boltup Temperature 3

2.5 Reactor Vessel Minimum Pressurization Temperature 3

l

- 3.0 Reactor Vessel Material Surveillance Progiam 9

4.0 Supplemental Data Tables 11 i

5.0 References 18 Attacluner*

WCAP 14824, Revision 2 " Byron Unit 1 Heatup and Cooldown Limit Curves for Norr-Operation and Surveillance Weld Metal Integration for Byron and Braidwood," Novemv.r, 1997.

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i BYRONo UNIT 2

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PRESSURE AND TEMI ERATURE LIMITS REPORT

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5 i

List of Figures

[

t Figure Page

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' 2.1 Byron Unit 2 Reactor Coolant System Heatup Limitadons (Heatup Rates up to 4

100' F/hr) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix 0 Methodology) 2.2 Byron Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates 5

up to 100 'F/le) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors: Using 1996 Appendix G Methodology)

- 2.3 Byron Unit 2 Maximum Allowable Nominal PORY Setpoints for the Low 7

Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY s

iii

. _. _. -. ~. _ _

BYRON. UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT List of Tables Table Page 2.1 Byron Unit 2 Heatup and Cooldown Data Points at 12 EFPY 6

i (Without Margins for Instrumentation Errors) 2.2 Data Points from Byron Unit 2 PORY Setpoints for the LTOP System 8

3.1 Byron Unit 2 Capsule Withdrawal Schedule 10-4.1

~ Byron Unit 2 Calculation of Chemistry Factors Using Surveillance Capsule Data 12 L4.2 Byron Unit 2 Reactor Vessel Material Properties 13 4.3 Summary of Byron Unit 2 Adjusted Reference Temperatures (ARTS) at the 1/4T 14 i

and 3/4T Locations for 12 EFPY 4.4 Byror. Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 15 12 EFPY at the Limiting Reactor Vessel Material Weld Metal (Based on Surveillance Capsule Data)

't 4.5 RTns Values for Byron Unit 2 for 32 EFPY 16 4.6 RTns Values for Byron Unit 2 for 48 EFPY 17 1

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BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 1.0 Reactor Coolant System (RCS) Pressure and Temperature Limits Report (PTLR)

Reference to Technical Specifications (TS) numbers are given in both the Byron Station current Technical Specifications (CTS) and improved Technical Specifications (ITS). The CTS number is presented first, followed by the ITS number in brackets [ ).

l This PTLR for Unit I has been prepared in accordance with the requirements of TS 6.9.1.1liilTS 5.6.6). Revisions to the PTLR shall be provided to the NRC after issuance.

l l

The Technical Specifications addressed in this report are listed below:

l LCO 3.4.9.1 Pressure / Temperature Limits; and LCO 3.4.9.3 Overpressure Protection Systems.

[ITS LCO 3.4.3 RCS Pressure and Temperature (P/T) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System).

2.0 Operating Limits The PTLR limits were developed using a methodology specified in the Technical Specifications. The methodology listed in WCAP 14040 NP A (Reference 1) was used with four exceptions:

Un of ENDF/B IV neutron transport cross section library and ENDF/B V dosimeter a.

reaction cross s~ections,

b. Optional use of ASME Code Section XI, Appendix G, Article G 2000,1996 Addenda,
c. Use of ASME Code Case N 514, and
d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.

WCAP-14824, Revision 2, is included as an attachment for reference. WCAP 14824, Rev. 2 contains the P/T cunts for Byron Unit 1, along with the weld metal data integration for Byron and Braidwood Units 1 and 2 and the Byron /Biaidwood fluence methodologyjustification for ENDF/B-VI cross sections. WCAP 14940 (Ref.14) contains the Byron Unit 2 Heatup and Cooldown Limit Curves applicable to 12 EFPY.

2.1 RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [ITS LCO 3.4.3))

2.1.1 The RCS temperature rate of-change limits defined in Reference 14 are:

a. A maximum heatup of 100'F in any 1-hour period,
b. A maximum cooldown of 100*F in any 1-hour period, and
c. A maximum temperature changt ofless than or equal to 10'F in any 1-bour period during inservice hydrostatic and leak testing operations above the heatup and cooldown limit cunes.

I

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IlYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2.1.2 The RCS P/T limits for '.catup, insenice hydrostatic and leak testing, and criticality are specified by Figure 2.. and Table 2.1. The RCS P/T limits for cooldown are shown in j

Figuie 2.2 and Table 2.1. These limits are defined in Reference 14. Consistent with the methodology described in Reference 1, the RCS P/T limits for heatup and cooldown shown in Figures 2.1 and 2.2 are provided without margins for instrument error. These limits were developed using ASME Code Section XI, Appendix 0, Article G 2000,1996 Addenda. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, mstrument uncertainties need not be con >ldered since appropriate station operating procedures ensure that the limits contained in the figures rnd table are not exceeded. The criticality limit curve specifies pressure temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix 0.

The P/T limits for core operation (excep for low power physics testing) are that the reactor vessel must be at a temperature equal to or higher than the minimum temperature required for the inservice hydrostatic test, and at least 40*F higher than the minimum permissible temperature in the corresponding P/T curve for heatup and cooldown.

2.2 Low Temperature Overpressure Protection (LTOP) System Setpoints (l.CO 3.4.9.3/

[lTS LCO 3.4.12]).

The power operated relief valves (PORVs) shall each have lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13 and 15.

The LTOP setpoints are based on P/T limits which were established in accordance.vith 10 CFR 50, Appendix G without ailowance for instmmentation error and in accordance with the methodology described in Reference 1. The LTOP PORV maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.

2.3 LTOP Enable Temperature The as analyzed LTOP enable temperature is 200*F (Reference 16).

The TS required enable temperature for the PORVs shall be 2 350'F RCS temperature.

(Byron Unit 2 procedures goveming the heatup and cooldown of the RCS require the arming of the LTOP System for RCS temperature of 350'F and below and disarming of LTOP for RCS temperature above 350'F).

Note that the last LTOP PORV segment in Table 2.2 extends to 450*F where the pressure setpoint is 2350 psig. This is intended to prohibit PORV lift for an inadvertent LTOP system arming at power.

l 2

t

-4 BYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2,4 Reactor Vessel Boltup Temperature (Non Technical Specification)

The minimum boltup teraperature for the Reactor Vessel Flange shall be h 60'F. Boltop is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and with the RCS vented to atmosphere (Reference 2).

2.5 Reactor Vessel Minimum Pressuriution Temperature (Non-Technical SpecMication)-

The minimum temperature at which the Reactor Vessel may be pressurized (i.e., in an unvented condition) shall be 2 60'F, plus an allowance for the uncertainty of the temperature instrument, determined using a technique consistent with ISA S67.04-1994.

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BYRON. UMT 2 s

PRESSURE AND TEMPERATURE LIMITS REPORT 4,

MATERIAL PROPERTY BASIS i

LIMITING MATERIAL: CIRCUMFERENTIAL WELD iusing eurv. capsule data)

LIMITING ART VALUES AT 12 EFPY:

./ IT, 87,6'F i

3s4T. 71.S'F 2500

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Figure 2.1 Byron Unit 2 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/br)

Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors) l 4

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BYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT MATERIAL PROPERTY BASIS LIMITING MATERIAL: CIRCUMFERENTIAL WELD (using sury. capsule cata)

LIMITING ART VALUES AT 12 EFPY:

1/4T. 87.6'F 3/47, 71.5'F 2500

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- Byron Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to 100 *F/hr)

Applicable for the First 12 EFPY (Without Margios for Instrumentation Errors)

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1 BYRON. UNIT 2 l

PRESSURE AND TEM 7ERATURE LIMITS REPORT 4

g l

. Table 2,1 -

Byron Unit 2 Heatup and Cooldown* Data Points at 12 EFPY" (Without margins for instrumentation errors)

HEATUP CURVES COOLDOWN CURVES

,m i

180 F HeetvP Test Curve Cettecemy Unit Limit stee8f State 25 000 F SO 000 F 180 000 F T

P T

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P T

P T l P T

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P 40 0

212 0

191 2000 60 0

80 0

80 0

to 0

80 821 212 849 212 2485 80 821 80 See to

$38 to 437 SS 821 212 692 SS 821 SS 801 SS 551 SS 452 70 821 212 878 70 821 70 814 70 885 70 488 75 821 212 889 75 421 75 821

. 75 881 75 488 f

80 -

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$21 80 597 80 SOS

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100 821 212 883 100 821 100 821 100 821 100 599 105 821 212 870 108 821 105 821 10!

821 105 821 110 821 212 679 110 821 110 821 110 821 110

$21 115 821 212 890 115 421 115 421 115 421 its 821 120 821 212 703 120 821 120 821 120 821 120 821 125 821 212 719 125 821 128 421 125 421 125 821 130 821 212 738 130

$1. I 1 821 130 821 130 821 135 821 212 758 135 821 135 821 135 i't21 135

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140 821 212 781 140 821 140 821 140 821 140 821 145 821 212 807 145 821 145 821 145 821 145 821 150 821 212 435 150 821 150 821 150 -

$21 150 821 150 738 215 888 150 1045 150 1028 150 tote 150 1008 155 758 220 900 1

155 41087 155 1074 155 1088 155 1088 180 781 225 937 l

150 1132 180 1123 100 1120 180 1131 185 807,

230 977 i

185 1180 185 1177 185 1177

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170 438 235 1021 l

170 1232 175 !

088 240 1088 175 1248 180 1 900 245 1119 180 1349 l

185 937 250 1174 185 1413 190 977 255 12ja 190 1483 195 1021 280 1297 195 1558 200 1088 285 1308 200 1838 205 1119 270 1441 205 1725 210 1174 275 1521 U0 1818 215 1233 280 1807 til 1918 220 1297 285 1899 220 2028 225 1388 290 1798 225 2141 230 1441 295 1905 230 2288 235

~1521 300 2020 235 2400 240 1807 30$

2143 245 1899 310 2275 250 1794 315 2417 255 190$

280 2020 285 2143 270 2275 275 2417

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Heatup and Conidown data includes vessel flange requirements of 150 F and 621 psig per 10CFR50, Appeaduc G.

    • For each cooldown rate, the steady state pre 55ure values shell govern the temperature where no allowable pressure values are provided

BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT

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80 100 150 200 250 300 354 400 AUCTIONEERED LOW RCS TEMPERATURE (DEG, F)

Figure 2.3 Byron Unit 2 Maximum Allowable Nominal PORV Setpoints for the Low Teniperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY 7

t HYRON o UNIT 3

+

PRESSURE AND TEMPERATURE LIMITS REPORT I

Table 2.2 Data Points for Byron Uniti Mksimum Allowable PORY Setpoints for the LTOP System Applicable for the First 12 EFPY' PCV-455A PCV-456

  • ~

(2TY 0413M)

(2TY-0413P)

AUCTIONEERED LOW RCS PRESSURE AUCTIONEERED LOW RCS PRESSURE RCS TEMP. (DEG. F)

(PSIG)

RCS TEMP. (DEG. F)

(PSIG)

~~

50 497 50 514 70 497 70 514 100 497 100 514 120 446 120 462 150 446 150 462 200 446 200 462 250 587 250 004 300 587 300 6 04 350 587 350 604 450 2350 450 2350 Note: To determine maximum allowable lift setpoints for RCS Pressure and RCS Temperatures greater than 350'F, linearly interpolate between the 350'F and 450*F data points shown above.'

  • 8

~. _. - _..., _ _ _

BYRON UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0 Reactor Vessel Material S trveillance Program The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determiae changes in material properties. He removal schedule is provided in Table 3.1. Also, ine results of these analyses shall be used to update Figures 2.1 and 2.2, and Table 2.1. The time of specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns most closely approaching the withdrawal schedule.

The pressure vessel material surveillance program (Reference 6)is in compliance with Appendix H to 10 CFR 50,"Reactot Vessel Radiation Surveillance Program." he material test requirements and the acceptance standard utilize the reference nil-ductility temperature, RTu, which is determined in accordance with ASME Section III, ND 2331. The empirical relationship between RTm and the fracture teughness of the reactor vessel ste:1 is developed in accordance with Appendix 0," Protection Against Non Ductile Failure," to Section XI of the ASME Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM El85 82.

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BYRON o UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 3.1 Byron Unit 2 Capsule Withdrawal Schedule Capsule Vessel Location Capsule Lead Removal Time ("

Estimated Capsule (Degrees)

Factor (EFPY)

Fluence (n/cm')

U 58.5' 3.96 1.15 (Removed) 3.996 x 10" W

121.5*

3.89 4.634 (Removed) 1.211 x 10" X

238.5' 3.89 8.23 (EOL Wall) 2.192 x 10"N 12.34(1.5 EOL Z

301.5*

3.89 Wall (*?)

3.288 x 10" V

61.0' 3.64 Standby l

Y 241.0' 3.64 Standby (a) Effective Full Power Years (EFPY) from plar I stanup.

(b) Maximum end oflicense (32 EFPY) inner vessel wall Duence.

(c) Derived from Tabe C 2 of WCAP 14824, Rev. 2 (Reference 2, which is the Anachment to this repon).

10

j BYRON. UNIT 2

^

PRI'SSURE AND TEMPERA'l URE LIMITS REPORT f

i 4.0 Supplemental Data Tables t

~

The following tables provide supplemental information on reactor vessel material properties and are provided to be consistent with Generic Letter 96 03. Some cd the material property values shown were used as inputs to the P/T limits.

Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance i

capsule data.

Table 4.2 provides the reactor vessel material properties table.

Table 4.3 provides a summary of the Byron Unit 2 adjusted reference temperature (ARTS) at the 1/4T and 3/4T locations for 12 EFPY.

Table 4.4 shows the calculation of ARTS at 12 EFPY for the limiting Byron Unit 2 reactor vessel material weld metal (Based on Surveillance Capsule Data).

Table 4.5 provides RTns values for Byron Unit 2 for 32 EFPY.

l Table 4.6 provides RTnsvalues for Byron Unit 2 for 48 EFPY.

t I

I1

BYRON o UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.1 Calculation of Chemistry Factors Using Surveillance Capsule Data Fluence Material Capsule (n/cm',

FFW Measured FF*ARTm (FF)2 E>1.0 ARTm Mev), f Lower Shell Forging 49D330/

U 3.996x10" 0.746 0

0 0.556 49C298 1-1 (Tangential)

W l.211x10" 1.053 5

5.267 1.110 Lower Shell Forging 49D330/

U 3.996x10" 0.727 25 18.65 0.556 49C298 1 -1 (Axial)

W l.211x10" 1.053 40 32.73 1.110 Sum:

66.037 3.332 Chemistry Factor (0 = 66.037 + 3.332 = 19.8'F Byron 1 Weld Metal WF 336*

U 3.72x10" 0.727 0

0 0.00 0.529 X

1.39x10" 1.091 35 105")

114.56 1.190 Byron 2 Weld Metal WF-447("

U 3.996x10" 0.746 0

0 0

0.557 W

l.211x10" 1.053 30 90"'

94.77 1.110 Sum:

209.33 3.386 Chemistry Factor (* = 209.33+3.386= 61.8'F (a) FF = FRence Factor a-f"*** 0 (b) B> ton Unit 1 ARTm values were obtained from the surveillance Capsule X analysis (WCAP 13880, Reference 10).

The ByTon Uni I capsule fluence values were recalculated using the ENDF/B V scattering cross sections in 1994 and t

are documented in WCAP 14044 (Reference 8).

(c) Dyron Unit 2 capsule fluence FF, and ARTm values were obtained from the surveillance Capsule W analysis of WCAP 14064 (Reference 3) using the ENDF/B.V scattering cross sections.

(d) Chemistry Factor = E (FF'ARTm)/I((FF)')

(c) Adjusted ARTm per Ratio Procedure of Regulatory Guide 1.99, Rev. 2 (Ref.12). Ratio = 3.0. See Table 2 of WCAP 14824, Rev. 2, (Ref. 2). Actual ratio is 2.5 (68.007.0 = 2.5); However, for conservatism, ratio of 3.0 was used.

12

~.

DYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.2 Byron Unit 2 Reactor Vessel Material Properties Material Description Cu(%)N Ni (%)(*)

Chemistry Initial FactorM RT m ('F)N Closure Head Flange Not 0.74 OM Reponed Vessel Flange Not 0.73 30M heported Inter. Shell Forging 0.01 0.70 20.0

-20 49D329/49C2971-1 Lower Shell Forging 0.0a 0.72 32.2

-20 49D330/49C2981-1 Circumferential Weld 0.05 0.62 68.0 10 WF-447 a) Chemistry Factors are calculated from Cu and Ni values per Regulatory Guide 1.99, Rev. 2 (Reference I

12).

b) Initial RT,et values are measured, WCAP 14063 (Reference 7) c) Closure head and vessel flange Initial RT,,, values are used for considering flange requirements for the heatup/cooldown curve'., WCAP 14940 (Reference 14).

13

- ~

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- -. - -. _ - - ~..

HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3 I

Summary of Hyron Unit 2 Adjusted Reference Temp:istures (ARTS'y at 1/4T and 3/4T Locations for 12 EFPY F

12 EFPY Material Description 1/4T ART ('F) 3/4T ART ('F)

Intermediate Shell Forging 12.1 1.7 49D329/49C2971-1 (R.G.1.99 Position 1 ()

Using credible surveillance 31.7 14.9 capsule data (RG Position 2(*))

Lower Shell Fo ging 11.8 1.5 49D330/49C2981 1 (RG Position l))

Circumfriential Weld 131.9 98.9 bi-447 (RG Position 1(*)

Using credible surveillance 87.6*)

71.5*)

capsule data (RG Position 2('))

(a) Calculated using a chemistry factor based on Regulatory Guide (RG) 1.99, Positions I and 2 (Reference 12).

(b) These ART values were used to generate the Byron Unit 2 Heatup and Cooldown Curves, WCAP-14940 (Reference 14).

14

. ~...

- -. ~

BYRON UNIT 2 l

t PRESSURE AND TEMPERATURE LIMITS REPORT l

Table 4.4 Byron Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 12 EFPY at the Limiting Reactor Vessel Material Weld Metal (Based on Surveillance Capsule Data)

Parameter Values Operating Time 12 EFPY '

l LocationN 1/4T ART 3/4T ART i

-}

Chemistry Factor, CF (*F) 68.0 68,0 Fluence (f), n/cm' 4.94x10" 1.78x10"

[

(E>l.0 Mev)*

Fluence Factor, FF 0.803 0.542 ARTum= CFxFF(*F) 49.63 33.50 Initial lit ym,1('F) 10 10

~

Margin, M (*F) 28.00 28.00 ART = I+(CF*FF)+M,'F 87.6 71.5 per RG 1.99, Revision 2 (a) Fluence, f, is based upon fs(E>l.0 Mev) = 8.22x10 at 12 EFPY, WCAP 14940 (Reference 14).

(b) The Byron Unit 2 reactor vessel wall thickness is 8.5 inches at the beltline region.

I E

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1 HYRON UNIT 2 PRESSURE AND TEMPERATURE 1.lMITS REPORT Table 4.5 RTna Valuer for flyron Unit 2 for 32 EFPY M

l RTune ARTns

RTn, CF p.i pp, Material

('F)

('F)

(*F)

('F)

(*F)

Lower Shell Forging 32.2 2.192 1.213 34.0

-20 39.1 53.1 MK 24 3 4

Using Surveillance 19.8 2.192 1.213 34.0

-20 24.0 38.0 Capsule Data"'

intennediate Shell Forging 20.0 2.192 1.213 24.3 20 24.3 28.6 MK 24 2 Circurnference Weld 68.0 2.192 1.21 I 56.0 10 82.5 148.5 Metal WF447 Using Surveillance 61.3 2.192 1.213 28.0 10 75.0 113.0 Capsule Data (3) 2.192x10 n/cm (Epl.0 Mev) for 32 EFPY from flyron 2 P t s report. WCAP 14054 (Reference 9) 3 (b) FF (Fluence Factor) = l'"'*'** 0 (c) Cakulated using a CF based on suncillance capsule data per RG l.99. Position 2 (Reference 12).

(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation.

16

._-____=.___-_.-_m_---____-._-___------_---_.2_-

4 HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.6 RTn, Yalues for Ilyron Unit 2 for 48 EFPY M

RTm,mn ARTns

RTn, CF p.,

pp63 Material

('F)

('F)-

(*F)

('F)

(*F)

Lower Shell Forging 32.2 3.288 1.312 34.0

-20 42.2 56.2 MK 24 3 d

Using Surveillar.cc 19.8 3.288 1.312 34.0

-20 26.0 40.0 Capsule Data"'

Intermediate Shell Forging 20.0 3.288 1.312 26.2 20 26.2 32.4 MK 24 2 Circumference Weld 68.0 3.288 1.312 56.0 10 89.2 155.2 Metal WF447 Using Surveillance 61.f, 3.288 1.312 28.0 10 81.1 119.1 Capsule Data (a) 2.192x10" n/cm (E>l.0 Mev) for 32 ETPY from Dyron 2 PTS report. WCAP 14054 (Reference 9). The following 8

calculation provides the 48 F/PY Oueni e value:

8 2.192x10" + ((2.19.!x10".3 tkx10"y32 4.634 EFPY)) * (48 32 EFPY) = 3.288x10" n/cm (b) FF (Fluence Factor) = f* 8"** 0 (c) Calculated using a CF based on w.c ihnce capsule data per RO 1.99, Position 2 (Reference 12).

(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation.

17

HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 5.0 References 1.

WCAP-14040 NP A, Revision 2," Methodology Used to Develop Cold Overpressure Mitigating System Setpoints and RCS Heatup and Cooldown Limit Curves," Andrachek, J.D., et. al., January 1996.

2.

WCAP-14824, Revision 2 " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"

November,1997.

3.

WCAP-14064," Analysis of Capsule W from the Commonwealth Edison Company Byron Unit 2 Reactor Vessel Radiation Surveillance Program," Malone, M.J., et al.,

July 1994.

4.

WCAP-12431," Analysis of Capsule U from the Commonwealth Edison Company Byron Unit 2 Reactor Vessel Radiation Surveillance Prvgram," Terek, E., et al.,

October 1989.

5.

Westinghouse Letter to Commonwealth Edison Company, CAE 96-106," Byron Unit I and 2 LTOPS Setpoints Based on 10 and 12 EFPY P/T Limits," January 17,1996.

6.

WCAP-10398," Commonwealth Edison Company, Byron Station Unit 2 Reactor Vessel Radiation Surveillance Program," Singer,IlR., December 1983.

7.

WCAP-14063," Commonwealth Edison Company, Byron Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," Peter, P.A., November 1994.

8.

WCAP-14044," Westinghouse Surveillance Capsule Neutron Fluence Reevaluation,"

Lippencott, E.P., April 1994, 9.

WCAP-14054," Evaluation of Pressurized Thermal Shoch for Byron Unit 2," Peter, P.A., August 1994.

10. 10 CFR Part 50, Appendix 0," Fracture Toughness Requirements," Federal Register, Volume 60, No. 243, dated December 19,1995.

I1. 10 CFR 50.61," Fracture Toughness Requirements for Protection Against Pressurized Thennal Shock Events,"(PTS Rule) May 15,1991.

12. U.S. Nuclear Regulatory Commission, Regulatory Guide 1.99," Radiation Embrittlement of Reactor Vessel Materials," Revision 2, May 1988.

I8

HYRON - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT

13. Comed Calculation BRW 96 9071/BYR 96-294," Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 2 Original Steam Generators)" Revision 0.
14. Wr AP-14940,"11yron Unit 2 ileatup and Cooldown Limit Curves for Normal Ope.ation," Laubham, T. J., et al., October,1997.
15. Westinghouse Letter to Comed, CAE 97 202," Byron Unit 2 COMS Setpoints for 12 EFPY," October 23,1997,
16. Westinghouse Letter to Comed, CAE 97 211/CCE 97-290," Byron and Braidwood Units 1 and 2 ATmetal Evaluation," November 7,1997.

19

.. o,

\\

ATTACHMENT WCAP -24824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD w

r ma

BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table of Contents Section _

Page 1.0 Introduction 1

2.0 Operating Limits I

k 2.1 RCS Pressure and Temperature (P/T) Limits 1

2.2 Low Temperature Overpresure Protection (LTOP) System Setpoints 2

2.3 LTOP Enable Temperature 2

2.4 Reactor Vessel Boltup Tempe:ature 3

2.5 Reactor Vessel Minimum Pressurization Temperature 3

3.0 Reactor Vessel Material Surveillance Program 9

4.0 Supplemental Data Tables 11 5.0 References 18 M

Attachment WCAP-14824, " Byron Unit i Heatup and Cooldown Limit Curves for Normal Operation and Sune!!!ance Weld Metal Integration for Byron and Braidwood," Revision 2, Novembo.1997.

i-

s BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITT, REPORT List of Figures Figure Page 2.1 Braidwood Unit 1 Reactor Coolant System Heatup Limitations (Heatup Rates up to 4

{

100'F/hr) Applicable for the First 16 EFPY (Without Margins for Instrementation Errors) 2.2 Braidwood Unit 1 Reactor Coolant System Cooldown Limitations (Cooldown Rates up 5 to 100 *F/hr) Applicable for the First 16 EFPY (Without Margins for Instrumentation Errors)

\\

}

2,3 Braidwood Unit 1 Maximum Allowable Nominal PORY Setpoints for the Low 7

F Temperature Overpressure Protection (LTOP) System App::pW for the First 16 EFPY

\\

L k

r

=-

BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT.

List of Tables Table Page 2.1 Braidwood Unit 1 Hntup and Cooldown Data Points at 16 EFPY 6

(Without Margins for Instrumentation Errors) 2.2 Data Points for Braidwood Unit 1 Maximum Allowable PORV Setpoints 8

for the LTOP System Applicable for the First 16 EFPY 3.1 Braidwood Unit 1 Capsule Withdrawal Schedule 10 4.)

Braidwood Unit 1 Calculation of Chemistry Factors Using Surveillance 12 Capsule Data 4.2 Braidwood Unit 1 Reactor Vessel Material Properties 13 4.3 Summary of Braidwood Unit 1 Adjusted Reference Temperatures (ARTri) at 14 the 1/4T and 3/4T Locations for 16 EFPY-4.4 Braidwood Unit 1 Calculation of Adjusted Reference Temperatures (ARTS) at 15 16 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on

'Survei: lance Capsule Data) 4.5 RTns Values for Braidwood Unit I for 32 EFPY 16 4.6 RTns Values for Braidwood Unit I for 48 EFPY 17 iiF

~. -

BRAIDWOOD - UNIT 1 PRESSURE AND TEMI'EP.ATURE LIMITS REPORT 1.0 Introduction Reference to Technical Specifications (TS) numbers are given in both the Braidwooc' Station current Technical Specifications (CTS) and Improved Tect nical Specifications (ITS). The CTS number ir, presented fir:1, followed by the ITS number in brackets [ ).

This PTLR for Unit I has been prepared in accordance with the requirements of TS 6.9.1.11/[ITS-5.6.6]. Revisions to the PTLR shall be provided to the NRC after issuance.

The Technical Specifications addressed in this report are listed below:

LCO 3.4.9.1 Pressure / Temperature Limits; and LCO 3.4.9.3 Overpressure Protection Systems.

[ITS LCO 3.4.3 RCS Pressure and Temperature (P/T) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System).

2.0 Operating Limits The PTLR limits were developed using a methodology specified in the Technical Specifications.

The methodology listed in WCAP-14040-NP-A (Reference 1) was used with four exceptions:

a. Use of ENDF/B-IV neutron transpcrt cross-section library and ENDF/B-V dosimeter reaction cross-sections,
b. Optional use of ASME Code Section XI, Appendix G, Article G-2000,1996 Addenda (not used for Braidwood Unit 1 P-T curves),
c. Use of ASME Code Case N-514, and
d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.

WCAP-14824, Revision 2, is included as an attachment for reference. WCAP-14824, Rev. 2 contains the P/T curves for Byron Unit 1, along with the weld metal data integratior ir Byron and Braidwood Units 1 and 2 and the Byron /Braidwood fluence methodologyjustifica

z. lor ENDF/B-VI cross sections.

2.1 RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [iTS-LCO 3.4.3])

2.1.1 The RCS temperature rate-of-change limits defined in Reference 7 are:

a. A raaximum heatup of 100 F ir, any 1-hour period,
b. A maximum cooldown of 100*F in any 1-hour period, and
c. A maximum temperature change ofless t.'en or equal to 10 F in any 1-hour period during inservice hydrostatic and leak testing operations above the heatup and cooldown limit curves.

p

BRAIDWOOD - UNIT I P.RESSURE AND TEMPERATURE LIMITS REPORT

- Operating Limits (Continued) 2.1.2 The RCS Pff limits for heatup, inservice hydrostatic and leak testing, and criticality are specified by Figure 2.1 and Table 2.1. The RCS P/T limits for cooldown are shown in Figure 2.2 and Table 2.1. These limits are defined in Reference 7. Consistent with the methodology described in Reference 1, the RCS P/T limits for heatup and cooldown showm in Figures 2.1 and 2.2 are provided without margins for instrumeat error. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, instrument uncertainties need not be considered since appropriate station operating procedures ensure that the limits contained in the figures and table are not exceedea. The criticality limit curve specifies pressure-temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix G.

The Pff limits for core operation (except for low power physics testing) are that the reactor vi.ssel must be at a temperature equal to or higher than the minimum temperature required for the inservice hydrostatic test, and at least 40'F higher than the minimum permissible temperature in the corresponding P/T curve for heatup and cooldown.

2.2 Low Temperature Overpressure Protection (LTOP) System Setpoints (LCO 3.4.9.3/

[ITS-LCO 3.4.12]).

The power operated relief valves (PORVs) shall e.ch have maximum lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13, and 14.

The LTOP setpoints are based on P/T limits which were established by 10 CFR 50, Appendix G without allowance for instrumentation erroi in accordance with the methodology described in Reference 1. The LTOP PORY maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.

2.3 LTOP Enable Temperature The as analyzed LTOP enable temperature is 200*F (Reference 15).

The TS required enable temperature for the PORVs shall be 2 350 F RCS temperature (Braidwood Unit 1 procedures governing the heatup and cooldown of the RCS require the arming of the LTOP System for RCS r mperature of 350*F and below and disarming of LTOP for RCS temperatu:e above 350'F).

- Note that the last LTOP PORV segment in Table 2.2 extends to 450*F where the pressure setpoint is 2350 psig. This is intended to prohibit PORV lift for an inadvertent LTOP system arming at power.

2

BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT Operating Lhnits (Continued) 2.4 Reactor Vessel Boltup Temperature (Non-Technical Specification)_

The minimum boltup temperature for the Reactor Vessel Flange shall be 2 60 F. Boltup is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and the RCS vented to atmosphere (Reference 7).

2.5 - Reactor Vessel Minimum Pressurization Temperature (Non-Technical Specification)

The minimum temperature at which the Reactor Vessel may be pressurized (i.e., in an unvented condition) shall be 2 60'F, plus an allowance for the uncertainty of the temperature instrument, determined using a technique consistent with ISA-S67.04 1994.

3

BRAIDWOOD - UNIT 1 l

PRESSURE AND TEMPERATURE LIMITS REPORT l

MATERIAL PROPERTY BA315 LIMTTING MATERIAL WELD METAL LIMITING ART VALUES AT 16 EFPY:

1/4 76.6*F 3/4 65.4*F 2500 4

l i

1 e

I Ic i'

ii, i e t

  • I f

I

/

l' 2250 m

m LEAK TEST L1MIT I

J l

t

/

/

l. l

~

as 2000 ll'

/

/ " '

=

.i i.

I

(

g l t f

f f I

I w

I

/

1750 UNACCEPTABLE OPERATION I

I' CJ I

i i

f f

y a

1500

/

/

l m

~

m s r/

I HrATur nATr

/ ;'

/

AccEPTAstE o

1250 ll' UP TO 400 t/Hr.

/

/

OPERATION a

j i i f

/

i *

,w i i :,

i i e

t i

/!

/

r i i

1000 'l l l ll ll l

/

=

., e i,

i i !

> + t

/

V g

e a it ii s

/

/

750

, e' ' '

i, i

\\/

n e i e r O

i t e s

. i,

500 l

lll l

e e i

,ii i

1_

e e i t i e N

i 6 e i,e

. i X

i 250 CRITICALITT LikIT RASED OM I ' '

IM5ERVICE HYDROET& TIC TEST i

TEMPERATURE late FI FOR THE i

! a i!

i e it i e e **

SERVICE PERIOD UP 70 1.

0 EFPY l

i 0

0 5'O Id0 150 200 2$0 380 3$0 480 4$0 500 Indicated Temperature (Deg.F)

Figure 2.1 Braidwood Unit 1 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/hr) Applicable for the First 16 EFPY (Without Margins for Instrumentation Errors)

'4

BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT -

MATERIAL PROPERTY BASIS LIMITING MATERIAL WELD METAL I,IMITING ART VALUES AT 16 EFPY:

. t/4.t. 76.6*F

3/4-t, 65.4*F

.2500 l

}

sessessessase 8

4!

l J

2250.

j' l ;'

1 m

- ing._

J 1

2000

/

l f

00 m.

l

)

i i

/

l750

_'_uN A c c r P T A s t r-i cu-OPrRATioN J

I

/

1500

/

l sn

. cc

/

o 1250.

AccrPTAstr b

i fl !

oPrRATION

  1. ',h 1

i r

1000 i

g.

2r i

s,,,

W e

f a

~~

o AP a

6

- C00LDOWN jyj

===8

- RATES 7

l,'

l

=

750 -- r/ur.

g.

it i

6 o

cx,-

'e

-500

'S

',f l l,

ll

,,l

~~

=

q i

6 250 4,,

0 0

50 Id0 150 2 d O' 250 300 350 400 450 500 I n d i c a t e-d Temperature (Deg..F)

Figure 2.2 Braidwood Unit 1 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to 100 *F/hr) Applicable for the First 16 EFP.Y (Without Margins for Instrumentation Errors)

~5 i>

n m.un www-w.:..

PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.1 BRAIDWOOD Unit 1 Heatup* and Cooldown* Data Points at 16 EFPY" (Without margins for instrumentation errors)

HEATUP CURVES COOLDOWN CURVES l 100 F Heatup Leak Test curve Criticahty Limit UmH Steady State 26 DEO F So DEO F 100 DEO F P

T P

T I

P T 4 P T I P

T I P

T 4 P T

80 0 00 210 l 0 00 188l2000 60 1 0 00 60 1 0 00 60 1 0 00 60 f 0 00 60 565 09 210 1 611 83 210l2495 80 ! 620 27 60 l 577 45 80 534 28 60 1 446 98 65 565 09 210 l 597.56 I

65 1 621.00 65 1 590 68 65 548 52 85 i 463 79 70 565 09 210 ! 585 60 i

70 f 621.00 70 1 605 03 70 1 563 98 70 ' 481.93 565 09 210 i 576 77 I

75 l 62100 75 l 620 51 75 1 560 67 75 1 501 49 75 i

80 585 09 210 1 570 35 I

80 ! 621 00 80 i 621 00 80 l 598 51 80 I 522 88 85 84509 210 6 586 61 1

85 l 621.00 85 l 62100 85 I 617 90 85 6 545 50 90 565 09 210 j 565 09 l

90 1 621 00 90 1 621 00 90 1 621.00 90 1 570.23 596 83 95 585 09 210 1 565.87 l

95 1 621.00 95 621.00 95 1 621 00 95 i

100 565 87 210 f 568 89 i

100 l 62100 100 621 00 100 l 621.00 1{l 621 00 105 568 89 210 i 573 56 l

105 621.00 105 1 621 00 105 1 621 00 e

621.00 110 573 58 210 i 580 30 i

110 1 621.00 110 1 621 00 110 1 621.00 110 t 62140 115 580 30 210 1 585 84 110 I 795 92 110 1 786 92 110 l 739.27 110 l 890 04 120 1 588 84 210 I 599.36 115 ! 821 55 115 7e4 59 115 1 769 53 115 l 726.2 125 599 36 210 1 811.78 120 I 849 00 120 824 45 120 } 801 97 120 1 785 12 130 611.78 210 i 626 07 l

125 1 818 42 125 856 54 125 1 836 87 125 I 807.07 135 626C7 210 i 64216 l

130 1 91025 130 890 97 130 1 874 41 130 1 852.23 140 642 16 210 I 860 36 1

135 l 944 34 135 l 928 00 135 i 915 0",

135 } 900 91 145 660 36 210 1 680 59 l

140 i 980 89 140 i 967.79 140 l 958 57

'40 1 953.33 150 680 59 210 1 702 80 1

145 1 1020.15 145 1 1010 84 145 11005 42 145 l 1009 81 155 i 702 80 210 ! 727.33 i

150 l 1062.35 150 i 1056 88 150 11055 76 l

727.33 210 1 754 07 i

155 t 1107.92 155 j 1106.38 l

l 160 i

165 754 07 210 t 783 17 160 11156 42

}

I 17:

78317 215 I 814 98 i

165 ! 1208 78 l

175 814 98 223 I 849 37 I

170 I 1265 05 I

I 175 i1325.37 i

i i

180 849 37 225 ! 886 54 185 886 f _

230 ! 926 73 1

180 1 1390 04 l

l l

190 926 73 235 i 970 11 185 l 1459 41 I

I i

195 970 11 240 1 1016 91 190 1 1533 55 i

1 I

200 1016 91 245 t 1067.33 195 i 1613 49 l

205 1067.33 250 i 1121 63 200 11699 01 l

l 210 1121 63 255 1 1180 01 205 ' 1790.55 l

t i

215 1180 01 260 l 1242 62 210 i 1888 81 I

I i

220 1242 62 285 i 1309 84 215 619C3 61 I

I 225 1309 84 270 ' 1382 03 220 : 2105 6e i

230 1382 03 275 1 1459 45 225 2225.77 i

235 1459 45 280 t 1542.27 230 ! 2353 75 6

i i

240 1542.27 285 : 1630 97 4

245 1630 97 290 i 1728 05 i

I i

250 1726 05 295 1 1827 80

+

l i

255

'827 80 300 ' 1936 51 I

i 260 193651 305 ; 2052 39 565 2052 39 310 ! 2176 33 i

i 270 2176 33 315 2308 42 i

i 275 2308 42 320 ' 2449 09 1

280 2449 09 i

  • Heatup and C,ooldown data include vessel flange requirernents of 110 F and 621 psig pr 10CFRSO, Appendix G

" For e8ch cooldown rate, the steady-state pressure values shall govern the ternperature where no allowab 8 pressure values are provided 6-

GRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT i i i I i l I Il lII i

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! I i i l! l i i i j i I l II I I i

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't i i i ! i i i i i l i i j i i i j -

1 I I i l i i i i i l l l l l l l II I l 1 i ! j i

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! i 1

t l

! ! ! i iil i i i! ! l l 1 I i i l 0

so 100 160 200 260 300 sao AUCTIONEERED LOW RCS TEMPERATURE (DEG, F)

Figure 2.3 Braidwood Unit 1 Maximum Allowable Nominal PORV Setpoints for the Low Temperature Overpressure Protection (LTOP) System Applicable for the First 16 EFPY 7

BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.2 Data Points for Braidwood Unit ! Maximum Allowable PORV Setpoints for the LTOP Sy5 tem Applicable for the First 16 EFPY PCV-455A PCV-456 (1TY 0413M)

(1TY-0413P) b AUCTIONEERED LOW RCS PRESSURE AUCTIONEERED LOW RCS PRESSURE RCS TEMP. (DEG. F)

(PSIG) 8tCS TEMP. (DEG. F)

(PSIG) 50 497 50 513 70 497 70 513 iOO 497 100 513 110 497 110 513

(

160 497 160 513 200 616 203 634 250 603 250 619 300 588 300 604 350 588 350 604 450 2350 450 2350 Note: To determine maximum allowable fift setpoints for RCS Pressure and RCS Temperatures greater than 350 F, linearly interpolate betwetn the 350 F and 450 F data points shown above.

r n

E

BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0

- Reactor Vessel Material Sun'e.illance Program

' The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determine changes in material properties. The removal schedule is provided in Table 3.1, The results of these anslyses shall be used to update Figures 2.1 and 2.2 and Table 2.1. The time of

- specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns most closely approaching the withdrawal schedule.

The pressure vessel material surveillance program (Reference 6)is in compliance with Appendix H to 10 CFR 50, " Reactor Vessel Radiation Surveillance Program." The material test requirements and the acceptance standards utilize the reference nil-ductility temperature, RTmr,

which is determined in accordance with ASME Section III Paragraph NB-2331. The empirical relationship between RTer nd the fracture toughness of the reactor vessel steel is developed in a

accordance with Appendix G," Protection Against Non-Ductile Failure," to Section XI of the AShE Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM E18F 82.

i

BRAIDWOOD-UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT Table 3.1 Braidwood Unit 1 Capsule Withdrawal Schedule Capsule Vessel Location Capsule Lead Removal Time'"

Estimated Capsule 2

(Decrees)

Factor (EFPY)

Fluence (n/cm )

U 58.5*

4.03 1.10 (Removed) 3.814 x 10'8 X

238.5' 4.03 4.234 (Removed) 1.144 x 10

W 121.5' 4.03 7.95 (EOL Wall) 2.239 x 10'*

11.93 (1.5 EOL Z

301.5*

4.03 Wall'4) 3.359 x 10" __

V 61.0' 3.73 Standby Y

241.0*

3.73 Standby (a) Effective Full Power Years (EFPY) from plant startup.

(b) Maximum end oflicense (32 EFPY) inner vessel wall fluence.

(c) Derived from Table C-3 of WCAP-14824, Rev. 2 (Reference 2, which is the Attachment to this report).

10

BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT 4.0 Supplemental Data Tables The following tables provide supplemental information on reactor vessel material properties and are provided to be consistent with Generic Letter 96-03. Some of the material property values shown were used as inputs to the P/T limits.

Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance capsule data.

Table 4.2 provides the reactor vessel material properties.

Table 4.3 provides a summary of the Braidwood Unit 1 adjusted referer.ce temperatures (ARTS) at the 1/4T and 3/4T locations for 16 EFPY.

Table 4.4 shows the calculation of ARTS at 16 EFPY for the limiting Braidwood Unit I reactor vessel material -Weld Metal WF562 (Based on Surveillance Capsule Data).

Table 4.5 provides the RTns alues for Braidwood Unit 1 for 32 EFPY.

v Table 4.6 provides the RTns alues for Braidwood Unit i for 48 EFPY.

v It

BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.1 Braidwood Unit 1 Calculation of Chemistry Factors Usine Surveillance Capsule Data Fluence Material Capsule (ri/cm,

FF")

Measured FF*ARTmr (FF)2 2

E> l. 0 ARTsm Mev), f Lower Shell Forging U

3.814 x10" 0.733 5

3.666 0.538 24-3 (Tangential)

X 1.144 x10" 1.038 30 31.127 1.077 Lower Shell Forging U

3.814 x10" 0.733 0

0 0.538 24-3 (Axial)

X 1.144x10" 1.038 25 25.939 1.077 Sum:

60.733 3.228 Chemistry Factor d' = 60.733 + 3.228 = 18.8'F Braidwood 1 Weld U

3.814x10" 0.733 10")

7.333 0.538 Metal WF562*'

X 1.144x10" 1.038 25")

25.95 1.077 Braidwood 2 Weld U

3.933x10" 0.741 0

0 0.550 Metal WF562")

X 1.126 x I0" 1.033 20"'

20.66 1.067 Sum:

53.943 3.232 Chemistrv Factor "' = 53.943+ 3.232 = I6.7'F (a) FF = Fluence Factor = f*2" "'*"'

(b) Braidwood Unit 1 ARTxor values were obtained from WCAP-14243 (Reference 7).

l (c) Braidwood Unit 2 capsule fluence, FF, and ARTxo1 values obtained from WCAP-14970 (Reference 12)-

(d) Chemistry Factor = I (FF*ARTxoT) / I ((FF) 2)

(e) ARTsot per Ratio Procedure of 10 CFR 50.61 (Reference 10)is not affected, since Ratio = 1.0. See Table B-4 of WCAP 14824, Rev. 2 (Reference 2).

12 l

f

BRAIDWOOD - UNIT 1 PRESSURE AND TEh!PERATURE LIMITS REPORT Table 4.2 Braidwood Unit 1 Reactor Vessel Material Pro perties Chemistry Initial Material Cu (%)")

Ni (%)")

Factor'"

RT mr ('F)'"

Description Closure Head

-20'"

Flange

- 10"'

Vessel Flange Lower Shell 0.04 0.74 26.0

-20 Forging 24-3 Intermediat-Shell 0.05 0.73 31.0

-30 Forging 24 2 Weld Metal (i.03 0.67 41.0 40 WF562 (a) Chemist y Factors are calculated from Cu and Ni values per Regulatory Guide 199, Position 1 (Reference 11).

(b) initial RTer alues are measured, WCAP-14243 (Reference 7) v (c) Closure head and vessel flange Initial RTer values are used for considering flange requirements for the heatup/cooldown curves, WCAP-14243.

13 1

BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3 Summary of Braidwood Unit 1 Adjusted Reference Temperatures (ARTS) at the 1/4T and 3/471.ocations for 16 EFPY")

16 EFPY Material Description 1/4T ART (*F) 3/4T ART (*F)

Lower Shell Forging

-26.2 12.1 24-3 Using credible surveillance capsule data 13.4*)

3.2*'

7 (RG Position 2))

Intermediate Shell 25.1 8.2 Forgi..g 24-2 (RG Position 1)

Circumferential Weld 112.9 90.5 (RG Position 1)

~

Using credible 76.6*'

65.4*'

surveillance capsule data (RG Position 2))

(a) Calculated using a chemistry factor based on Pegulatory Guide (RG) 1.99, Position 2 (Reference 11).

(b) These ART values were used to generate the Braidwood Unit I heatup and cooldown curves, WCAP-14243 (Reference 7).

(c) Based on evaluation of WCAP-14243; however, applicability date has been increased to 27.9 EFPY per evaluation in WCAP-14824, Rev. 2-Appendix D: Weld Mctal Integration for Braidwood Units 1 and 2 (Reference 2).

14 l

l

l BRAIDWOOD - UNIT 1 1

PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.4 Braidwood Unit 1 Calculation of Adjusted Reference Temperatures (ARTa) at 16 EFPi*' at the Limiting Reactor % ssel Mcterial Weld Metal WF562 (Based on Surveillance Capsule Data)

Parameter Values r

Operating Time 16 EFPi*'

Location"'

1/4T ART 3/4T ART fhemistry Factor, CF ('F) 20.6 20.6 Fluence (f), n/cm' 0.73x10" 2.43x10" (E>1.0 Mev))"'

Fluence Factor, FF 0.889 0.616 ARTmr= CFxFF ('F) 18.31 12.70 Initial RT mr, I (*F) 40 40 Margin, M ( F) 18.31 12.70 ART = 1+(CF*FF)+M, *F 76.6 65.4 per RG 1.99. Rwision 2 (a) Fluence, f, is based upon f.s(E>l.0 Mev) = 1.120x10" at 16 EFPY, WCAP-14241 (Reference 3).

(b) Based on evaluation of WCAP 14243; however, applicability date has been increased to 27.9 EFPY per evaluation in WCAP-14824, Rev. 2 Appendix B: Weld Metal Integration for Braidwood Units 1 and 2 (Reference 2).

(c) The Braidwood Unit I reactor vescel wall thickness is 3.5 inches at the beltline region.

t 15

BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT T

Table 4.5 RTers Values for Braidwood Unit 1 for 32 EFPY CF p.

ppm M

RTane ARTns RTns Material

(*F)

(*F)

(*F)

(*F)

(*F)

Lower Shell Forging 26.0 2.239 1.218 31.68

-20 31,68 43.4 MK 24 3 Using Sun'eillance 18.8 2.239 1.218 17.0

-20 22.90 19.8 Capsule Data"'

~

Intermediate Shell Forging 31.0 2.239 1.218 34.0

-30 37.77 41.8

~

24 2 Circumferential Weld 41.0 2.239 1.218 49.95 40 49.95 ! 139,9 Metal WF562 Using Sun eillance 16.7 2.239 1.218 20.34 40 20.34 80.7 Capsule Data")

(a) 2.239x10 n/cm'(E>l 0 Mev) for 32 EFPY from Braidwood 1 PTS report, WCAP-14242 (Reference 8).

(b) FF (Fluence Factor) = fo.2w io w,o r

(c) Calculoted with CF based c. surveillance capsule data per RG 1.99, Position 2 (Reference 11).

16

BRAIDWOOD - UNIT I PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.6 RTns Values for B aidwood Unit 1 for 48 EFPY CF M

RTmrrm)

ARTns RTns f.>

ppm Material

('F)

('F)

('F)

('F)

('F)

Lower Shell Forging 26.0 3.358 1.317 34.0

-20 34.25 48.3 MK 24 3 Using Surveillance 18.8 3.358 1.317 17.0

-20 24.76 21.8 Capsule Data"'

Intermediate Shell Forging 31.0 3.358 1.317 34.0

-30 40.83 44.8 24-2 C'rcumferential Weld 41.0 3.358 1.317 54.00 40 54.00 148.0 Metal WF562 Using Surveillance 16.7 3.358 1.317 21.99 40 21.99 84.0 Capsule Data")

(a) 3.358x10 n/cm (E>l.0 Mev) for 48 EFPY from Braidwood 1 PTS repon, WCAP-14242 2

(Reference 5).

(b) FF (Fluence Factor) = f"#'*80 (c) Calculated with CF based on surveillance capsule data per RG 1.99, Position 2 (Reference 11).

17

BRAIDWOOD - UNIT 1 PRESSURE AND TEMPERATURE LIMITS REPORT.

5.0 References 1.

Andrachek, J.D., et al., WCAP-14040-NP-A, " Methodology used to Develop Cold Overpressure Mitigating System Setpoints and RCS Heatup and Cooldown Limit Curves," Revision 2, January 1996.

2.

Grendys, P.A., WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"

Revision 2, November 1997 3.

Peter, P.A., et al., WCAP-14241, " Analysis of Capsule X from the Commonwealth Edison Company Braidwood Unit 1 Reactor Vessel Radiation Surveillance Program,"

March 1995.

4.

Terek, E., et al., WCAP-12685, " Analysis of Capsule U from the Commonwealth Edison Company Braidwood Unit 1 Reactor Vessel Radiation Surveillance Program," August 1990.

5.

Westinghouse Letter to Conunonwealth Edison Company, CCE-95 186, "Braidwood Unit 1 LTOPS Setpoints Based on 16 EFPY Pfr Limits," June 5,1995.

6.

Yanichko, S.E., et al., WCAP-9807, " Commonwealth Edison Company, Braidwood Station Unit i Reactor Vesse! Surveillance Program," February 1981.

7.

Peter, P.A, WCAP-14243, "B,raidwood Unit i Heatup and Cooldown Limit Curves for Normal Operation," March 1995.

8.

Peter, P. A., WCAP-14242, " Evaluation of Pressurized Thermal Shock for Braidwood Unit 1," March 1995.

9.

Lippencott, E.P., WCAP-14044, " Westinghouse Surveillance Capsule Neutron Fluence Reevaluation," April 1994, 10, 10 CFR 50.61, " Fracture Toughaess Requirements for Protection Against Pressurized Thermal Shock Events," (PTS Rule) January 18,1996.

I1. U.S. Nuclear Regulatory Commission, Regulatory Guide 1.99, " Radiation Embrittlement of Reactor Vessel Materials," Revisicn 2, May 1988.

12. Laubham, T. J., WCAP-14970,"Braidwood Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," October 1997 and Erratta Sheet (Westinghouse Letter CAE 210, CCE 97-289).

18

1; i

I' BRAIDWOOD - UNIT l' PRESSURE AND TEMPERATURE LIMITS REPORT References (Continued)

13. Comed Ca'culation BRW-96-9061/BYR 96-293, " Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 1 Original Steam Generators and Replacement Steam Generators)," Revision 0.
14. Comed Nuclear Fuel Services Department, NDIT No. 960194, " Maximum Allowable LTOPS PORV Setpoints for Braidwood Unit I with RSGs," Revision 2.
15. Westinghouse Letter to Commonwealth Edison Company, CAE 97-211, CCE 290,

" Comed Byron and Braidwood Units 1 and 2 ATmetal Evaluation for Commonwealth Edison," November 7,1997.

T 4

19 i

ATTACHMENT 1 WCAP-14824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD 20 -

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- BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT i

Table of Contents

- Section Page 1.0 - Introduction 1

.- 2.0 Operating Limits 1-2.1 RCS Pressure and Temper ture (PR) Limits 1

2.2 - Low Temperature Overpressure Protection (LTOP) System Setpoints 2

2.3 LTOP Enable Temperature 2

2.4 Reactor Vessel Boltup Temperature 3

2.5 Reactor Vessel Minimum Pressurization Temperature 3

3.0 Reactor. Vessel Material Surveillance Program 9

4.0 Supplemental Data Tables 11 5,0 References 18 Attachment WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron and Braidwood," Revision 2, November 1997.

i-

i 100.*F/hr) Applicable for the First 12 EFPY (Without Margins for Instmmentation Errors) 2.2 Braidwoc,d Unit 2 Reactor Coolant System Cooldowa Limitations (Cooldown Rates up 5 to 100 'F/hr) Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors) 2.3

_ Braidwood Unit 2 Maximum Allowabic Nominal PORY Setpoints for the Low 7

Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY n

'Es _

CRAIDWOOD. UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT List of Tabler Table -

Page 2.1 Braidwood Unit 2 Heatup and Cooldown Data Points at 12 EFPY

> 6

-(Without Margins for Instrumentation Errors) 2.2 Data Points for Braidwood Unit 2 Maximum Allowable PORY Setpoints 8

for the LTOP System Applicable for the First 12 EFPY 3.1 Braidwood Unit 2 Cap.me Withdrawal Schedule 10 4

-4.1-Braidwood Unit 2 Calculation of Chemistry Factors Using Surveillance 12 Ct.psule Data 4.2 -

Braidwood Unit 2 Reactor Vessel Material Properties 13 4.3 Summary ofBraidwood Unit 2 Adjusted Reference Temperatures (ARTS) at 14 the 1/4T and 3/4T Locations for 12 EFPY 4.4 Braidwood Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 15 12 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on Sun eillance Capsule Data) i 4.5 RTus Values for Braidwood Unit 2 for 32 EFPY 16 4.6 RTm Values t'or Braidwood Unit 2 for 48 EFPY 17 tii

  • i HRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 1.0 Introduction Reference to Technical Specifications (TS) numbers are given in both the Braidwood Station current Technical Specifications (CTS) and Improved Technical Specifications (ITS). The CTS number is presented first, followed by the ITS number in brackets [ ].

This PTLR for Unit I has been prepared in accordance with the requirements of.

TS 6.9.1.11/[ITS-5.6.6]. Revisions to the PTLR shall be provided to the NRC after issuance.

The Technical Specifications addressed in this report are listed below:

LCO 3.4.9.1 Pressure /femperature Limits; and LCO 3.4.9.3 Overpressure Protection Systems.

[ITS-LCO 3,4.3 RCS Pressure and Temperature (Pff) Limits; and LCO 3.4.12 Low Temperature Overpressure Protection (LTOP) System].

2.0 Operating Limits The FTLR limits were developed using a methodology specified in the Technical Specifications.

The methodolcgy listed in WCAP-14040-NP-A (Reference 1) was used with four exceptions:

a Use of ENDF/B-IV neutron transport cross-section library and ENDF/B-V dosimeter reaction cross-sections,

b. Optional use of AShE Code Section XI, Appendix G, Article G-2000,1996 Addenda,
c. Use of AShE Code Case N-514, and
d. Use of RELAP computer code for calculation of LTOP setpoints for Unit I replacement steam generators.

WCAP-14824, Revision 2, is included s an attachment for reference. WCAP-14824, Rev,2 contains the D/T curves for Byron Unit 4, along with th: weld metal data integration for Byron and Braidwood Units 1 and 2 and the Byron /Braidwood fluence methodologyjustifica: ion for ENDF/B-VI cross sections.

21 RCS Pressure and Temperature (P/T) Limits (LCO 3.4.9.1/ [ITS-LCO 3.4.3])

2.1.1 The RCS temperature rate-of-change limits defined in Reference 7 are:

a. A maximum heatup of 100"F in any 1-hour period,

- b A maximum cooldown of 100*F in any 1-hour period, and c A maximum temperature change ofless than or equal to 10 F in any 1-hour period during j.

inseivice hydrostatic and leak testing operations above the heatup and cooldown limit curves.

I-

BRAIDWOOD - UNIT 2 1

PRESSURE AND TEMPERATURE LIMITS REPORT Operating Limits (Continued) 2.1.2 The RCS P/T limits for heatup, insenice hydrostatic and leak testing, and criticality are specified by Figure 2.1 and Table 2.1. The RCS P/T limits for cooldown are shown in Figure 2.2 and Table 2.1. These limits are defmed in Reference 7. Consistent with the methodology described in Reference 1, the RCS P/T limits for heatup and cooldown shown in Figures 2.1 and 2.2 are provided without margins for instrument error. In determining compliance with Figures 2.1 and 2.2 and Table 2.1, instrument uncertainties need not be considered since appropriate station operating procedures ensure that the limits contained in the figures and table are not exceeded. The criticality limit curve specifies pressure-temperature limits for core operation to provide additional margin during actual power production as specified in 10 CFR 50, Appendix G.

The P/T limits for core operation (except for low power physics testing) are that the reactor vessel must be at a temperature equal to or higher than the minimum temperature required for the insenice hydrostatic test, and at least 40'F higher than the minimum permissible temperature in the corresponding P/T curve for heatup and cooldown.

2.2 Low Temperature Overpressure Protection (LTOP) System Setpoir.ts (LCO 3.4.9.3/

[ITS-LCO 3.4.12]).

The power operated relief valves (PORVs) shall each have maximum lift settings in accordance with Figure 2.3 and Table 2.2. These limits are based on References 5,13 and 14.

The LTOP setpoints are based on P/T limits which were established by 10 CFR 50, Appendix G without allowance for instrumentation error in accordance with the methodology described in Reference 1. The LTOP PORY maximum lift settings shown in Figure 2.3 and Table 2.3 account for appropriate instrument error.

2.3 LTOP Enable Temperature The as taalyzed LTOP enable temperature is 200 F (Reference 15)

The TS required enable temperature for the PORVs shall be 2 350*F RCS temperature.

(Braidwood Unit 2 procedures governing tne heatup and cooldown of the RCS require the arming of the LTOP System for RCS temperature of 350*F and below and disarming of LTOP for RCS temperature above 350*F).

Note that the last LTOP PORY segmer : in Table 2.2 extends to 450 F where the pressure setpoint is 2350 psig This is intended to prohibit PORV lift for an inadvertent LTOP system arming at power.

t 2

's BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Op: rating Limits (Continued) 2.4 Reactor Vessel Boltup Temperature (Non-Technical Specification)

The minimum boltup temperature for the Reactor Vessel Flange shall be 2 60'F, Boltup is a condition in which the Reactor Vessel head is installed with tension applied to any stud, and with the RCS vented to atmosphere (Reference 7).

2.5 Reactor Vessel Minimum Pressurization Temperature (Non-Technical Specification)

The minimum temperature at which the Resctor Vessel may be pressurized (i.e., in an unvented concDion) shall be 2 60*F, plus an allowance for the uncertainty of the temperature instrument, determined using a technique consistent with ISA-S67.04-1994.

3

BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Material Property Basis LIMITING MATERIAL: CIRCUMFREtGIAL WELD (using sun'. capsule data)

LIMITING ART VALUES AT 12 EFPY:

1/4T,66.9'F 3/4T, 58.I'F 2500 i.,......

t I

i g

  • Ii i

l' 2250 M

/,

'l

~

gn LEAK TEST LIMIT 7I

/>

V i

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r f

f

'I s

i I

2000

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v

,i.

g y

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_I U 1750 Y

uMACCEPTABLE OPERATION

/

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UP To 300 r/Er.

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1250 f,

if i.

1 l

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OPERATION

=

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1000 e

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6 500 i

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e TemE' crit:Cativt t wit e49to OR m

INSERVICE RYDROST4"lC TEST TEMPERaTURS dIst F i FOR TWE f

I SERVICE PER!dD UP PO 88.0 EFPY 0.

0 50 100 150 200 250 300 350 400 450 500 Moderator Temperature (Deg.F) l Figure 2.I Braidwood Unit 2 Reactor Coolant System Heatup Limitations (Heatup Rates up to 100 'F/hr)

Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix G Methodolgy) 4

BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Material Property Basis LIMIT!NG MATERIAL: CIRCUMFRENTIAL WELD (using sury capsule data)

LIMITING ART VALUES AT 12 EFPY:

1/4T. 66.9'F 3/4T, 58.I'F 2500

.,. 4 u...-

i i

i...

gi i i.

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i 88 250~,

N Boltup 4

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g P.

6 i...

0 0

5'O Id0 150 20 2$0 300 3$0 4 0 480 500 Moderator Temperature (Deg.F)

Figure 2.2 Braidwood Unit 2 Reactor Coolant System Cooldown Limitations (Cooldown Rates up to 100*F/hr)

. Applicable for the First 12 EFPY (Without Margins for Instrumentation Errors; Using 1996 Appendix G methodolgy) 5

~

~

~

orwvvvi.ivuivivu e

~~

~ '

~

PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.1 BRAIDWOOD Unit 2 Hestup* and Cooldown* Data Points at 12 EFPY"

(Using 1996 Appendix G Methodolgy Without margins for instrumentation errors)

HEATUP CURVES

' COOLDOWN CURVES 100 F Heat 4 Leek Test curve CatacelHy Lindt Undt Stee8y 8tste 28 D80 F 88 DSO F 100 080F T

P T

1 P T I P T i P T i P T i P T + P 80 C

192 1 0 17012000 80 1 0 to 1 0 80 i- 0 80 1 0 to 821 1 92 708 192i2485 80 l 821 to i 821 to I 801 80 ' 511 85 821 192 741 f

85. 821 85 t 821 85 ! 819 85 i 532 70 821-192 729 1

70 I 821 70 l 821 70 1 821 70 1 555

-75 821 192 I 720 I

75 821 75 i 821

- 75 1 821 75 1 579 821 192 I 715 l

80 821 80 l 821 80 821 80 { 805 80 85 821 192 4 713 1

85 821 85 i 821 85 821 85 l 821 90 i 821 192 1 114 20 821 to 821 to 821 90 1 821 95 f'71 192 1 719 95 l 821 95 821 95 I 821 95 i 821 100 821 192 i 728 6

100 l 821 100 421 100 I 821 100 i 821 105 821 192 1 735 1

105 1 821

-105 I 821 105!

821

-105 1 821

'110 821 192 748 i

'10 1 821 110 l 821 110 821 110 4 821 115 : 821 192 783 f

115 i 821 115 l 821 1151 821 115 821 120 ; $21 192 700 1

120 821 120 l 821 120-821 120 821 125 821 192 I 801 l

125 821 125 821 125 821 125 821 130 i - 821 192 1 824 1

130 821 130 821 130 821 130 1 821 135 821 195 ! 850 1

135 821 135 821 135 821 135 I 821 140 821 200 1 879 140 i 821 140 1 821 140 1 821 f

140 700

_.205 911 l

140 1 1138 140 ! 1131 140 l 1128 1

145 1 801 210 [ 948 1

145 l 1187 145 ! 1184 145 1188 i

824 215 l 984 i

150 ! 1240

(-

i 150 155 850 220 ' 1028 6

155 i 1297 l

180 879 225 i 1071 1

180 6 1357 L

I i

185 911 230 1 1120 l

185 1 1423 I

i l

170 948 235 t 1174 170 l 1493 I

I i

175 984 240 t 1231 1F5 l 1589 I

i l

180 1028 245 1 1294 i

180 f 1850 f

I i

185 1071 250 1381 i

185 i 1738 i

l i

190 1120 255 l 1433 190 1 1832 l

l t

195 1174 280 ; 1511 195 1 1933 I

I t

200 1231 285 ! 1595 200 ? 2041 i

I 1

205 1294 270 1886 205 i 2158 i

i 1

210 1381 27f 1783 210 1 2284 i

I 215 1433 280 1888 215 2419 i

220 1511 285 ' 2000 i

t i

i 225 1595 290 2121 t

I 230 1886 295 2251 i

i i

235 1783 300 ' 2391 i

i t

l l

240

-1888 6

1 i

245 2000 i

250 2121' 4

255 2251 1

4 l

280 2391 I

i i

)

i i

i

  • HeStup and C00100wn data inclu0e vessel flange requirements of 140 F Snd 621 psig per 10CFR50. Appendix G l

" For each c00ldOwn rate, the steady-state pressure values shall govern the temperature where no ellowable pressure values are provided.

l:

6 l

GRAIDWOOD - UNIT 2 4

L PRESSURE AND TEMPERATURE LIMITS REPORT

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M 100 1H 200 2H 300 3M AUCTIONEERED LOW RCS TEMPERATURE (DEG, F)

Figure 2.3 Braidwood Unit 2 Maximum Allowable Nominal PORV Setpoints for the Low Temperature Overpressure Protection (LTOP) System Applicable for the First 12 EFPY

'(

7

BRAIDWOOD - UNIT 2 s

PRESSURE AND TEMPERATURE LIMITS REPORT Table 2.2 Data Points for Braidwood Unit 2 Madmum Allowable PORV Setpoints for the LTOP System Applicable for the First 12 EFPY PCV-455A '

PCV-456 (2TY-0413M)

(2TY-0413P)-

AUCTIONEERED LOW RCS PRESSURE AUCTIONEERED LOW RCS PRESSURE RCS TEMP. (DEG. F)

(PalG)

RCS TEMP. (DEG. F)

(PSIG) 50 497 50 513 70 497 70 513 100-497 100 513 120 452 120 469 170 451 170 468 200 614 200 630 250 599 250 615 300 584 300 600 350 584 350 600 450 2350 450 2350 Note: To determine maximum allowable lift setpoints for RCS Pressure and RCS Temperatures greater than 350*F, linearly interpolate between the 350'F and 450 F data points shown above.

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BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 3.0 Reactor Vesse! Material Surveillance Program The reactor vessel material irradiation surveillance specimens shall be removed and analyzed to determine changes in material properties. Tne removal schedule is provided in Table 3.1. The results of these analyses shall be used to update Figures 2.1 and 2.2 and Table 2.1.' The time of specimen withdrawal may be modified to coincide with those refueling outages or reactor shutdowns rnost closely approaching the withdrawal schedule.

The pressure vessel material surveillance program (Reference 6) is in compliance with Appendix H to 10 CFR 50, " Reactor Vessel Radiation Surveillance Program." The material test requirements and the acceptance standards ntilize the reference nil-ductility temperature, RTr,w,

which is determined in accordance with ASME Section III Paragraph NB 2331. The empirical relationship between RTum and the fracture toughness of the reactor vessel steel is developed in accordance with Appendix G, " Protection Against Non Ductile Failure," to Section XI of the ASME Boiler and Pressure Vessel Code. The surveillance capsule removal schedule meets the requirements of ASTM E185 82.

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BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORf Table 3.1 Braidwood Unit 2 Capsule Withdrawal Schedule Capsule Vessel Location Capsule La.ad Removal Time"'

Estimated Capsule 2

(Degrees)

Factor (EFPY)

Fluence (n/cm )

U 58.5' 4.00 1.15 (Removed) 3.933 x 10" X

238.5*

4.02 4.215 (Removed) 1.126 x 10" W

121.5*

4.02 7.97 (EOL Wall) 2.199 x 10"N 11,95 (1.5 EOL Z

301.5' 4.02 Wall'")

3.299 x 10" V

61.0*

3.70 Standby Y

t 241.0*

3.70 Standby (a) Effective Full Power Years (EFPY) from plant startup.

(b) Maximum end oflicense (32 EFPY) inner vessel wall fluence.

(c) Derived from Table C-4 of WCAP-14824, Rev. 2 (Reference 2, which is the Attachment to this report).

10

BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 4.0

. Suppicmental Data Tables The following tables provide supplemental information on reactor vessel material propenies and are provided to be consistent with Geaeric Letter 96-03. Some of the material property values shown were used as inputs to the P/T limits.

Table 4.1 shows the calculation of the surveillance material chemistry factors using surveillance capsule data.

Table 4.2 provides the reactor vessel material properties.

Table 4.3 provides a summary of the Brsidwood Unit 2 adjusted reference temperatures (ARTS) at I

the 1/4T and 3/4T locations for 12 EFPY.

Table 4.4 shows the calculation of ARTS at 12 EFPY for the limiting Braidwood Unit 2 reactor vessel material -Weld Metal WF562 (Based on Surveillance Capsule Data).

Table 4.5 provides the RTns values for Braidwood Unit 2 for 32 EFPY.

i Table 4.6 provides the RTns alues for Braidwood Unit 2 for 48 EFPY, v

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BRAIDWOOD - UNIT 2 2-PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.1 Braidwood Unit 2 Calculation of Chemistry Factors Using Surveillance Capsule Data Fluence Material Capsule (n/cm',

FF"' -

- Measured FF*ARTm1

- (FF)2 E>l.0 ARTet Mev). f Lower Shell Forging U

3.933 x10

O.741 0

0.000 0.550 50D102/50C97 (Tangential)

X 1.126 x10

l.033 2

3.099 1.067 Lower Shell Forging U

3.933 x10

O.741 5

3.707 0.550 50D102/50C97 (Axial)

X 1.126x10

l.033 35 36.160 1.067 Sum:

42.996 3.234 d

Chemistry Factor ' = 42.996 + 3.234 = 13.3*F Braidwood 1 Weld U

3.814x10

O.733 10"'

7.333 0,538 Metal WF562*'

_X 1.144x10

l.038 25")

25.95 1.077 Braidwood 2 Weld U

3.933 x 10

O.741 0

0 0.550 Metal WF562"'

X l.126 x10

l.033 20'"

2066 1.067 Sum:

53.943 3.232 Chemistry Factor d' = 53.943+ 3.232= 16.7'F (a) FF = Fluence Factor = fo.2a innn (b) Braidwood Unit 1 ARTer alues were obtained from WCAP-14243. (Reference 12).

v (c) Braidwood Unit 2 capsule fluence, FF, and ARTm1 values were obtained from WCAP-14970 (Reference 7).

(d) Chemistry Factor = I (FF* ARTmT) / I ((FF) 2),

(e) ARTer per Ratio Procedure of 10 CFR 50.61 (Reference 10) is not affected, since Ratio = 1.0.

See Table E.-4 ofWCAP 14824, Rev. 2 (Reference 2)

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BRAIDWOOD - UNIT 2 PRESStJRE AND TEMPERATURE LIMITS REPORT Table 4.2 Braidwood Unit 2 Reactor Vessel Material Pro perties Chemistry Initial Material Cu (%)"'

Ni (%)"'

Factor"'

RT er ('F)*'

Description Closure Head Not 0.75 20"'

Flange Reported Vessel Flange 0.07 0.70 20"'

Lower Shell 0.06 0.77 37.0

-30 Forging Upper Shell 0.03 0.71 20.0

-30 Forging Weld Metal 0.03 0.67 41.0 40 WF562 (a) Chemistry Factors are calculated from Cu and Ni values per Regulatory Guide 1.99, Position 1 (Reference 11).

(b) Initial RTervalues are measured, WCAP-14970 (Ref:rence 7).

(c) Closure head and vessel Dange Initial RTervalues are used for considering Dange requirements for the heatup/cooldown curves, WCAP-14970.

13

BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.3 Summary of Braidwood Unit 2 Adjusted Reference Temperatures (ARTS) at the 1/4T and 3/4T Locations for 12 EFPY 12 EFPY Material Description 1/4T ART (*F) 3/4T ART ('F)

Lower Shell Forging 29.5 10.1 Using credible surveillance capsule datt.

(RG Position 2'")

-8.6

-15.6 Upper Shell Forging 2.2

-8.3 (RG Position l'")

Weld Metal 105 o 84.4 (RG Position l'")

Using credible 66.9*

58.l*

surveillance capsule data (RG Position 2'")

(a) Calculated using a chemistry factor based on Regulatory Guide (RG) 1.99, Position 1 and Position 2 (Reference 11).

(b) These ART values were used to generate the Braidwood Unit 2 heatup and cooldown curves, WCAP-14970 (Reference 7).

14

BRAIDWOOD - UNIT 2 t

PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.4 Braidwood Unit 2 Calculation of Adjusted Reference Temperatures (ARTS) at 12 EFPY at the Limiting Reactor Vessel Material Weld Metal WF562 (Based on Surveillance Capsule Data)

Parameter Values Operating Time 12 EFPY Location")

1/4T ART 3/4T ART f.

Chemistry Factor, CF ('F) 16.7 16.7 2

Fluence (f), n/cm 4.95x10" 1.78x10" (E>1.0 Mev)i')

Fluence Factor, FF 0.804

_ 0.542 ARTmn= CFxFF('F) 13.43 9.05 Initial RTm. I('F) 40 40 Margia, M(*F) 13.43 9.05 ART = 1+(CF'FF)+M, 'F 66.9 58.1 per RG 1.99. Revision 2 (a) Fluence, f, is based upon f r(E>l.0 Mev) = 1.100x10'* at 16 EFPY, WCAP 14228 (Reference 3).

(b) The Braidwood Unit 2 reactor vessel wall thickness is 8.5 inches at the beltline region.

15

BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4.5 RTru Values for 13raidwood Unit 2 for 32 EFPY CF p.>.

pgi

.M RTsum ARTeis-RTers Material-('F)

(*F)

('F)

('F)

('F)-

Upper Shell Forging 20.0 2.199 1.214 24.28

-30 24.28 18.6 MK 24 3 Lower Shell Forging 37.0 2 199 1.214 34,0

-30 44.92 48.9 Using Surveillance Capsule Data 13.3 2.199 1214 34.0")

30 16.15 20.2 Circumferential Weld 41.0 2.199 1.214 49.77 40 49.77 139.5 Metal WF562 Using Surveillance 16.7 2.199 1.214 20.27 40 20.27 80.5 Capsule Data")

(a) 2.199x10" n/cm' (E>l.0 Mev) for 32 EFPY from Braidwood 2 PTS report WCAP-14229 (Reference 8)

(b) FF (Fluence Factor) = fa2:en n (c) Calculated using CF based on surveillance capsule data per RG 1.99, Position 2 (Refaence 1l)

(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one s:gma criteria from the credibility evaluation. See WCAP-14824, Rev. 2 (Reference 2).

16

BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT Table 4 6 RTns Values for Braidwood Unit 2 for 48 EFPY CF p.>

pp M

RTsortv)

ARTns RTns Matenal

("F)

(*F)

(*F)

('F)

('F)

Upper Shell Forging 20.0 3.298 1.313 26.26

-30 26.26 22.5 Lower Shell Forging 37.0 3.298 1.313 34.0

-30 48.58 52.6 N

Using Surveillance 13.3 3.298 1.313 34.0 )

-30 17.46 21.5 Capsule Data (*)

Circumferential Weld 41.0 3.298 1.313 53.83 40 53.83-147.7 Metal WF562 Using Surveillance 16.7 3.298 1.313 21.93 40 21.93 83.9 Capsule Data'*)

(a) 3.298x10" rt cm (E>l.0 Mev) for 48 EFPY from Braidwood 2 PTS report WCAP-14229

/

2 (Reference 8).

(b) FF (Fluence Factor) = f*2'#'*"*'O (c) Calculated using a CF based on surveillance capsule data per RG 1.99, Position 2 (Reference 11).

(d) Double margin is used here due to the base metal surveillance capsule data exceeding the one sigma criteria from the credibility evaluation. See WCAP-14824 Rev. 2 (Reference 2).

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BRAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT 5.0 References 1.

Andracheck, J.D., et al., WCAP-14040-A. " Methodology used to Develop Cold Overpressure / Mitigating System Setpoints and RCS Heatup and Cooldown Limit Curves," Revision 2 January 1996.

2.

' Grendys, P.A., WCAP-14824, " Byron Unit 1 Heatup and Cooldown Limit Curves for Normal Operation and Surveillance Weld Metal Integration for Byron & Braidwood,"

Revision 2, November 1997.

i 3.

Peter, P.A., et al., WCAP-14228, " Analysis of Capsule X from the Commonwealth Edison Company Braidwood Unit 2 Reactor Vessel Radiation Surveillance Program,"

March 1995.

i 4.

Terek, E., et al., WCAP-12845, " Analysis of Capsule U from the Commonwealth Edison Company Braidwood Unit 2 Reactor Vessel Radiation Surveillance Program,"

March 1991.

5.

Westinghouse Letter to Commonwealth Edison Company, CCE-96-104, "Braidwood Unit 2 LTOPS Setpoints Based on 16 EFPY P/T Limits," January 24,1996.

6.

Singer, L.R., WCAP-11188, " Commonwealth Edison Company, Braidwood Station Unit 2 Reactor Vessel Surveillance Program," December 1986.

7.

Laubham, T. J., WCAP-14970, "Braidwood Unit 2 Heatup and Cooldown Limit Curves for Normal Operation," October 1997 and Erratta Sheet (Westinghouse Letter CAE-97 210, CCE-97 289).

8.

Peter, P. A., WCAP 14229, " Evaluation of Pressurized Thermal Shock for Braidwood Unit 2," March 1995.

9.

Lippencott, E.P. WCAP-14044, " Westinghouse Surveillance Capsule Neutron Fluence Reevaluation," April 1994.

10.

10 CFR 50.61, " Fracture Tou'ghness Requirements for Protection Against Pressurized Thermal Shock Events,"(PTS Rule) January 18,1996.

11.

U.S. Nuclear Regulatory Commission, Regulatory Guide 1.99, "Radation Embrittlement of Reactor Vessel Materials," Revision 2, May 1988.

12.

Peter, P.A., WCAP-14243, "Braidwood Unit i Heatup and Cooldown Limit Curves for Normal Operation," March 1995.

ERAIDWOOD - UNIT 2 PRESSURE AND TEMPERATURE LIMITS REPORT References (Continued) 13.

Comed Calculation BRW 96-9061/BYR 96-293," Channel Accuracy for Power Operated Relief Valve (PORV) Setpoints and Wide Range RCS Temperature Indication (Unit 2 Origimd Steam Generators)," Revision O.

14.

Westinghouse Letter to Commonwealth Edison Company, CCE-97-278, "CemEd Braidwood Unit 2 COMMS Setpoint for 12 EFPY," October 23,1997.

15.

Westinghouse Letter to Commonwealth Edison Company, CAE-97-211, CCE-97 290,

" Comed Byron and Braidwood Units 1 and 2 ATmetal Evaluation for Commonwealth Edison," November 7,1997, 1

19

e, ATTACHMENT I WCAP-14824, REVISION 2, BYRON UNIT 1 HEATUP AND COOLDOWN LIMIT CURVES FOR NORMAL OPERATION AND SURVEILLANCE WELD METAL INTEGRATION FOR BYRON AND BRAIDWOOD 20-

,