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| number = ML101690171
| number = ML101690171
| issue date = 06/11/2010
| issue date = 06/11/2010
| title = Enclosure 6, Prairie Island Nuclear Generating Plant, Units 1 and 2, Supporting Engineering Evaluations, EC 16275, Effects of Pipe Whip Interactions for Various Pipe Combinations for Internal Flooding Sdp.
| title = Enclosure 6, Prairie Island Nuclear Generating Plant, Units 1 and 2, Supporting Engineering Evaluations, EC 16275, Effects of Pipe Whip Interactions for Various Pipe Combinations for Internal Flooding Sdp
| author name =  
| author name =  
| author affiliation = Northern States Power Co, Xcel Energy
| author affiliation = Northern States Power Co, Xcel Energy
Line 22: Line 22:


XcelEnergy° EC-0441 EC Closeout Package Report (Rev. 3)
XcelEnergy° EC-0441 EC Closeout Package Report (Rev. 3)
Report Date: 06/1112010 EC Number: 0000016275                                             Revision:                   000 Engineering Change EC Number         0000016275    000                          Facility                PI Status/Date       CLOSED       06/10/2010                   Type/Sub-type :         EVAL /
Report Date: 06/1112010 EC Number: 0000016275 Revision: 000 Engineering Change EC Number Status/Date 0000016275 CLOSED 000 06/10/2010 Facility PI Type/Sub-type :
EVAL /
EC
EC


==Title:==
==Title:==
EFFECTS OF PIPE WHIP INTERACTIONS FOR VARIOUS PIPE COMBINATIONS FOR INTERNAL FLOODING SDP Mod Nbr:                     KW1:           KW2:           KW3:             KW4:             KW5:
EFFECTS OF PIPE WHIP INTERACTIONS FOR VARIOUS PIPE COMBINATIONS FOR INTERNAL FLOODING SDP Mod Nbr:
Master EC                           Work Group                                   Temporary Outage                              Alert Group         : E-REG PROG             Aprd Req. Dt.         07/01/2010 WO Required                          Image Addr                                  Exp Insvc Date Adv Wk Appvd                        Alt Ref.                                    Expires On Auto-Advance                        Priority                                    Auto-Asbuild Caveat Outst                        Resp Engr          : PTTD06 Units and Systems Facility           Unit           System             System Description PI                 0               OTH                 OTHER Attributes Attribute Name     Value         Updated By     Last Updated       Notes SCRN NO            NA            PTTD06          06/10/2010         This evaluation does not support design basis.
KW1:
SIMULATOR SYSTEM HEALTH EVAL NO PORC DTE PRIORITY RANKING Pedigree Information                                                                                               Page 1 of 4
KW2:
KW3:
KW4:
KW5:
Master EC Outage WO Required Adv Wk Appvd Auto-Advance Caveat Outst Work Group Alert Group Image Addr Alt Ref.
Priority Resp Engr
: E-REG PROG
: PTTD06 Temporary Aprd Req. Dt.
Exp Insvc Date Expires On Auto-Asbuild 07/01/2010 Units and Systems Facility Unit System  
 
===System Description===
PI 0
OTH OTHER Attributes Attribute Name SCRN NO SIMULATOR SYSTEM HEALTH EVAL NO PORC DTE PRIORITY RANKING Value NA Updated By PTTD06 Last Updated 06/10/2010 Notes This evaluation does not support design basis.
Pedigree Information Page 1 of 4


Xcel Energy' EC-0441 EC Closeout Package Report (Rev. 3)
Xcel Energy' EC-0441 EC Closeout Package Report (Rev. 3)
Report Date: 06/11/2010 Topic Notes Notes DESCRIPTION                    See Attached in sharepoint.
Report Date: 06/11/2010 Topic Notes DESCRIPTION JUSTIFICATION REVIEWER COMMENTS Notes See Attached in sharepoint.
JUSTIFICATION                  See Attached in sharepoint.
See Attached in sharepoint.
REVIEWER COMMENTS              Owners comments:
Owners comments:
14" Table Interaction 186 should be interaction 188. Tthe remainder of data stay the same for the line item.
14" Table Interaction 186 should be interaction 188. Tthe remainder of data stay the same for the line item.
16" Table One interaction needs to be added (it will be bounded by interaction 15)
16" Table One interaction needs to be added (it will be bounded by interaction 15)
No 115 Unit 2 Elev 695 Row B Column 14 HE Line 20-2CD-7 [40] NPS 20 ID 19.25 Wall Thickness 0.375 Area (InA2)291     Crack Size 1.80 Target ID 16-2CL-9 [32] Sch 30 Thickness 0.375 Distance 6"
No 115 Unit 2
Elev 695 Row B Column 14 HE Line 20-2CD-7 [40]
NPS 20 ID 19.25 Wall Thickness 0.375 Area (InA2)291 Crack Size 1.80 Target ID 16-2CL-9 [32]
Sch 30 Thickness 0.375 Distance 6"
Operating Pressure of 20-2CD-7 = 420 psig 24" Table Interaction 20a needs to be added. The data is identical to Interaction 20.
Operating Pressure of 20-2CD-7 = 420 psig 24" Table Interaction 20a needs to be added. The data is identical to Interaction 20.
The above comments were incorporated.
The above comments were incorporated.
Interaction 151 was requested to be assessed. However, the results were not coming out favorably.
Interaction 151 was requested to be assessed. However, the results were not coming out favorably.
AES was requested not to pursue this piping interaction further as it was acknowledged that the interaction was not possible based upon field walkdowns.
AES was requested not to pursue this piping interaction further as it was acknowledged that the interaction was not possible based upon field walkdowns.
Cross References XRef Number           Sub         Status           Date           Reference DescriDtion AR     01178236                 APPROVED         04/15/2009     No HELB flooding calculation for Turbine Building Affected Documents Milestone Milestone               Date              ID                Name                          Req By APPROVED BY             06/10/2010         BRSM05             Brossart, Mark A             APPROVED Pedigree Information                                                                                                          Page 2 of 4
Cross References XRef Number Sub Status Date Reference DescriDtion AR 01178236 APPROVED 04/15/2009 No HELB flooding calculation for Turbine Building Affected Documents Milestone Milestone APPROVED BY Pedigree Information Date 06/10/2010 ID BRSM05 Name Brossart, Mark A Req By APPROVED Page 2 of 4


XcelEnergy" EC-0441 EC Closeout Package Report (Rev. 3)
XcelEnergy" EC-0441 EC Closeout Package Report (Rev. 3)
Report Date: 06111/2010 Milestone Milestone                 Date               ID                 Name               Req By Notes: Suitability review performed by a qualified individual and attached in Sharpoint. Comments listed in Topic Notes were incorporated. EC is approved.
Report Date: 06111/2010 Milestone Milestone CLOSE PRE JOB BRI PREPARED (E Date ID Name Notes: Suitability review performed by a qualified individual and attached in Sharpoint. Comments listed in Topic Notes were incorporated. EC is approved.
CLOSE                    06/10/2010         LDWHIP01           Whipple, Linda D   CLOSED Notes:
06/10/2010 LDWHIP01 Whipple, Linda D Notes:
PRE JOB BRI EF           06/10/2010         PTTD06             Potter, David J Notes:
EF 06/10/2010 PTTD06 Potter, David J Notes:
PREPARED (EEVL)           06/10/2010         PTTD06             Potter, David J   H/APPR Notes:
EVL) 06/10/2010 PTTD06 Potter, David J Req By CLOSED H/APPR Notes:
Document Referencei Facilty     Doc-Type           Sub-Type         Doc #                       Sheet Rev   Minor Rev Date PI          EC                                  0000016275                        000             06/10/2010 Pedigree Information                                                                                   Page 3 of 4
Document Referencei Facilty Doc-Type PI EC Sub-Type Doc #
0000016275 Sheet Rev Minor Rev Date 000 06/10/2010 Pedigree Information Page 3 of 4


XcelEnergy-EC-0441 EC Closeout Package Report (Rev. 3)
XcelEnergy-EC-0441 EC Closeout Package Report (Rev. 3)
Report Date: 06/11/2010 Pedigree Information                                             Page 4 of 4
Report Date: 06/11/2010 Pedigree Information Page 4 of 4


QF-0547 (FP-E-MOD-1 1) Rev. 2                                                                       Paae 1 of I QF-0547 (FP-E-MOD-11) Rev. 2                                                                       Paae I of I
QF-0547 (FP-E-MOD-1 1) Rev. 2 Paae 1 of I QF-0547 (FP-E-MOD-11) Rev. 2 Paae I of I
  &XcelEnergy-                                 External Design Document Suitability Review Checklist External Design Document Being Reviewed:Engineering Evaluation Title- Technical Backup for Turbine Building HELB Screening Evaluation Number: PI-996-83-S01                                                         Rev: 1             Date:   6/10/10 This design document was received from:
&XcelEnergy-External Design Document Suitability Review Checklist External Design Document Being Reviewed:Engineering Evaluation Title-Technical Backup for Turbine Building HELB Screening Evaluation Number:
Organization Name: AES                                       POor DIA  
PI-996-83-S01 Rev:
1 Date:
6/10/10 This design document was received from:
Organization Name: AES POor DIA  


==Reference:==
==Reference:==
EC16275 The purpose of the suitability review Is to ensure that a calculation, analysis or other design document provided by an External Design Organization complies with the conditions of the purchase order and/or Design Interface Agreement (DIA) and is appropriate for Its Intended use. The suitability review does not serve as an Independent verification. Independent verification of the design document supplied by the External Design Organization should be evident Inthe document, ifrequired.
EC16275 The purpose of the suitability review Is to ensure that a calculation, analysis or other design document provided by an External Design Organization complies with the conditions of the purchase order and/or Design Interface Agreement (DIA) and is appropriate for Its Intended use. The suitability review does not serve as an Independent verification. Independent verification of the design document supplied by the External Design Organization should be evident In the document, if required.
The reviewer should use the criteria below as a guide to assess the overall quality, completeness and usefulness of the design document. The reviewer is not required to check calculations Indetail.
The reviewer should use the criteria below as a guide to assess the overall quality, completeness and usefulness of the design document. The reviewer is not required to check calculations In detail.
REVIEW Reviewed      NIA
REVIEW
: 1.     Design inputs correspond to those that were transmitted to the External Design                               El Organization.
: 1.
: 2. Assumptions are described and reasonable.                                                                     Ii
Design inputs correspond to those that were transmitted to the External Design Organization.
: 3. Applicable codes, standards and regulations are identified and met.                                           El
: 2.
: 4. Applicable construction and operating experience is considered.                                               El
Assumptions are described and reasonable.
: 5. Applicable structure(s), system(s), and component(s) are listed.                                             El
: 3.
: 6.     Formulae and equations are documented. Unusual symbols are defined.                                         El
Applicable codes, standards and regulations are identified and met.
: 7. Acceptance criteria are identified, adequate and satisfied.                                                   Ez
: 4.
: 8.     Results are reasonable compared to inputs.
Applicable construction and operating experience is considered.
: 9. Source documents are referenced.                                                                             El
: 5.
: 10. The document is appropriate for its intended use.                                                             El
Applicable structure(s), system(s), and component(s) are listed.
: 11. The document complies with the terms of the Purchase Order and/or DIA.                                       El
: 6.
: 12. Inputs, assumptions, outputs, etc. which could affect plant operation are                       El enforced by adequate procedural controls. List any affected procedures.
Formulae and equations are documented. Unusual symbols are defined.
: 13. Plant impact has been identified and either implemented or controlled. (e.g., For piping analyses, the piping and support database is updated or a tracking item has been initiated.)
: 7.
: 14. Design and Operational Margin have been considered and documented.                               El         Z Completed by:       David Potter
Acceptance criteria are identified, adequate and satisfied.
* ji  ..
: 8.
Date:     6/10/2010 Form retained In accordance with record retention schedule identified In FP-G-RM-01.
Results are reasonable compared to inputs.
: 9.
Source documents are referenced.
: 10.
The document is appropriate for its intended use.
: 11.
The document complies with the terms of the Purchase Order and/or DIA.
: 12.
Inputs, assumptions, outputs, etc. which could affect plant operation are enforced by adequate procedural controls. List any affected procedures.
: 13.
Plant impact has been identified and either implemented or controlled. (e.g., For piping analyses, the piping and support database is updated or a tracking item has been initiated.)
: 14.
Design and Operational Margin have been considered and documented.
Reviewed El NIA El Ii El El El ElEz El El El El Z
Completed by:
David Potter Date: 6/10/2010 ji Form retained In accordance with record retention schedule identified In FP-G-RM-01.


Automated
Automated
  /'               Engineering           Calculation Package                       Page   1       of 39 z ~           Services Corp.
/'
Calculation Number:         PI-996-83-SO 1 Calculation
Engineering Calculation Package Page 1
of 39 z ~
Services Corp.
Calculation Number:
PI-996-83-SO 1 Calculation


==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation Client:                 XCEL Energy                                     Station: PINGP Project Number:         PI-996-83                                       Unit(s):
Technical Backup for Turbine Building HELB Screening Evaluation Client:
XCEL Energy Station: PINGP Project Number:
PI-996-83 Unit(s):
Project
Project


==Title:==
==Title:==
PRA HELB Screening Safety Related     Yes   -    No [
PRA HELB Screening Safety Related Yes No [
Revision     Affected Pages   Revision Description                   Approval Signature /   Signature / Initials of Date                   Preparers & Reviewers Prepared by:
Revision Affected Pages Revision Description Approval Signature /
Initial Issue                               A.V. Setlur 0              All David DeGrush Reviewed by:
Signature / Initials of Date Preparers & Reviewers Prepared by:
0 All Initial Issue A.V. Setlur David DeGrush Reviewed by:
Olof Andersson Prepared by:
Olof Andersson Prepared by:
1             All       Piping interaction tables and associated references revised.
1 All Piping interaction tables and associated references revised.
A.V. Setlur       David DeGrush 6/10/2010 Reviewed by:
A.V. Setlur David DeGrush 6/10/2010 Reviewed by:
Olof Andersson Form 3.1-10                                                                                                     Rev. I
Olof Andersson Form 3.1-10 Rev. I
 
Automated Engineering, Calculation Package Page 2
of 39 Services Corp.
REVIEWER'S CHECKLIST FOR DESIGN CALCULATIONS SHEET 1 of 2 STATION:
PINGP NUCLEAR SAFETY RELATED: YES [] NO Z PROJECT NO:
PI-996-83 CLIENT:
NMC, LLC CALCULATION TITLE: Technical Backup for Turbine Building HELB Screening Evaluation CALC. NO:
PI-996-83-SO 1 CALC. REV. NO:
I INDICATE THE DESIGN INPUT DOCUMENTS USED:
TYPE OF DOCUMENT DOCUMENT ID, REV AND/OR DATE YES N/A COMMENT
: 1. General Design Basis Ref. 1 - 11 X
: 2.


Automated Engineering,        Calculation Package              Page    2    of 39 Services Corp.
===System Description===
REVIEWER'S CHECKLIST FOR DESIGN CALCULATIONS                                    SHEET 1 of 2 STATION:            PINGP                  NUCLEAR SAFETY RELATED: YES [] NO    Z PROJECT NO:          PI-996- 83      CLIENT:    NMC, LLC CALCULATION TITLE: Technical Backup for Turbine Building HELB Screening Evaluation CALC. NO:            PI-996-83-SO 1            CALC. REV. NO: I INDICATE THE DESIGN INPUT DOCUMENTS USED:
X
TYPE OF DOCUMENT            DOCUMENT ID, REV AND/OR DATE    YES  N/A          COMMENT
: 3. Design information package x
: 1. General Design Basis          Ref. 1 - 11                      X
from related equipment vendor
: 2. System Description                                                   X
: 4. Electrical Discipline Input X
: 3. Design information package                                           x from related equipment vendor
: 5.
: 4. Electrical Discipline Input                                           X
Mechanical Discipline X
: 5. Mechanical Discipline                                               X Input
Input
: 6. Control Systems Discipline                                           x Input
: 6.
: 7. Structural Discipline Input                                         x
Control Systems Discipline x
: 8. Specifications                                                     X
Input
: 9. Vendor Drawings                                                     X
: 7. Structural Discipline Input x
: 10. Design Standards             Ref. 9                           X
: 8.
: 11. Client Standards                                                     x
Specifications X
: 12. Checked Calculations         Ref. 1, 7                         X
: 9.
: 13. Other (specify)                                                     X PREPARER'S SIGNATURE:                                             D. DeGrush DATE: 6/10/20 10 REVIEWER'S SIGNATURE:                       (LL                 0. Andersson DATE: 6/10/20 10 APPROVER'S SIGNATURE:                                             A.V. Setlur   DATE : 6/10/2010 Form 3.1-4                                                                                       Rev. 3
Vendor Drawings X
: 10.
Design Standards Ref. 9 X
: 11. Client Standards x
: 12. Checked Calculations Ref. 1, 7 X
: 13. Other (specify)
X PREPARER'S SIGNATURE:
D. DeGrush DATE: 6/10/20 10 REVIEWER'S SIGNATURE:
(LL
: 0. Andersson DATE: 6/10/20 10 APPROVER'S SIGNATURE:
A.V. Setlur DATE : 6/10/2010 Form 3.1-4 Rev. 3


Automated Engineering             Calculation Package   Page 3     of 39 SkmServices Corp.
Automated Engineering Calculation Package Page 3
REVIEWER'S CHECKLIST FOR DESIGN CALCULATIONS                               SHEET 2 of 2 PROJECT NO:                       PI-996-83 CALC. NO:                        PI1-996-X3-S1;0 REVIEWER TO COMPLETE THE FOLLOWING ITEMS:                                     COMMENT
of 39 SkmServices Corp.
REVIEWER'S CHECKLIST FOR DESIGN CALCULATIONS SHEET 2 of 2 PROJECT NO:
CALC. NO:
PI-996-83 PI1-996-X3-S1;0 REVIEWER TO COMPLETE THE FOLLOWING ITEMS:
COMMENT
: 1. Has the purpose of the calculation been clearly stated?
: 1. Has the purpose of the calculation been clearly stated?
2.. Have the applicable codes, standards and regulatory requirements been:
2..
Have the applicable codes, standards and regulatory requirements been:
A. Properly Identified?
A. Properly Identified?
B. Properly Applied?
B. Properly Applied?
: 3. Were the inputs correctly selected and used?
: 3. Were the inputs correctly selected and used?
: 4. A. Was Design Input Log used?
: 4.
A. Was Design Input Log used?
B. If 4A is No, provide Manager's signature in Comment column to signify approval of Design Input Documents used in the calculation.
B. If 4A is No, provide Manager's signature in Comment column to signify approval of Design Input Documents used in the calculation.
: 5. Are necessary assumptions adequately stated?
: 5. Are necessary assumptions adequately stated?
Line 128: Line 199:
A. Neat?
A. Neat?
B. Legible?
B. Legible?
I.
C. Easy to follow?
C. Easy to follow?
D. Presented in logical order?
D. Presented in logical order?
Line 140: Line 210:
E. Were they correctly used:
E. Were they correctly used:
F. Was data input correct?
F. Was data input correct?
G. Is the computer program and revision identified?                       LS-DYNA Form 3.1-4                                                                             Rev. 3
G. Is the computer program and revision identified?
I.
LS-DYNA Form 3.1-4 Rev. 3


T Automated                                                                                                                    e: 4 of 39 Engineering Zn        Services Corp                                                                                                        Calc. No.: PI-996-83-S01 Client: Xcel Energy Nuclear                                                                                                           Revision: 1 Station: Prairie Island Nuclear Generating Station                                                                                   Prepared By: D. DeGrush Calc.
Automated Engineering Zn Services Corp T
e: 4 of 39 Calc. No.: PI-996-83-S01 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.


==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation                                                         Reviewed By: 0. Andersson Safety Related                 Yes       D                                                                                           Date: 6/10/2010 TABLE OF CONTENTS Sectionn                                                                                                                                                          Page
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 Section 1.
: 1.      P u rp o se .......................................................................................................................................         5
2.
: 2.      M ethod o logy ..............................................................................................................................               5
3.
: 3.      Acceptance Criteria .............................................................................................................                           6
4.
: 4.      A ssum ption s .............................................................................................................................                 7
5.
: 5.      D esign Inp uts ............................................................................................................................                 8
6.
: 6.      A n aly sis ...................................................................................................................................             13
7.
: 7.      Su m m ary ..................................................................           ............................................................... 38
8.
: 8.      Conclusions ..........................................................................................                                                     38
9.
: 9.      References ................................................................................................                                               39 Form 3.1-3                                                                                                                                                                     Rev. 2
TABLE OF CONTENTS n
Page P u rp o se.......................................................................................................................................
5 M eth od o logy..............................................................................................................................
5 Acceptance Criteria.............................................................................................................
6 A ssum ption s.............................................................................................................................
7 D esign Inp uts............................................................................................................................
8 A n aly sis...................................................................................................................................
13 S u m m ary..................................................................
3 8 Conclusions.......................................................................................... 38 References................................................................................................ 39 Form 3.1-3 Rev. 2


Page: 5 of 39 Engineering
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~~                  Automated Services Corp                                                          Calc. No.: PI-996-83-SO 1 I .U Client: Xcel Energy Nuclear                                                               Revision: I Station: Prairie Island Nuclear Generating Station                                         Prepared By: D. DeGrush Calc.
Automated Engineering I.U Services Corp Page: 5 of 39 Calc. No.: PI-996-83-SO 1 Revision: I Client: Xcel Energy Nuclear Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.


==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation               Reviewed By: 0. Andersson Safety Related                 Yes   D                                                     Date: 6/10/2010 1.0     Purpose/Objective The purpose of this calculation is to perform analysis of pipe-on-pipe impact interactions using finite element simulation. The objective is to quantify the effect of impact of the projectile pipe on a target pipe. The anaylsis will evaluate the impact of specific postulated interactions at the Prairie Island Nuclear Generating Plant (PINGP).
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 1.0 Purpose/Objective The purpose of this calculation is to perform analysis of pipe-on-pipe impact interactions using finite element simulation. The objective is to quantify the effect of impact of the projectile pipe on a target pipe. The anaylsis will evaluate the impact of specific postulated interactions at the Prairie Island Nuclear Generating Plant (PINGP).
2.0     Methodology Analytical models of two pipe interactions (collisions) are prepared using the Finite Element Simulation code LS-DYNA. The models were comprised of a projectile or moving pipe and a stationary Target Pipe. The physical scenario being analyzed is a postulated catastropic failure occurring in a pressurized piping system producing a projectile pipe which ultimately impacts a stationary or target pipe. The damaged caused by the projectile pipe to the target pipe is evaluated using the finite element code.
2.0 Methodology Analytical models of two pipe interactions (collisions) are prepared using the Finite Element Simulation code LS-DYNA. The models were comprised of a projectile or moving pipe and a stationary Target Pipe. The physical scenario being analyzed is a postulated catastropic failure occurring in a pressurized piping system producing a projectile pipe which ultimately impacts a stationary or target pipe. The damaged caused by the projectile pipe to the target pipe is evaluated using the finite element code.
The analyses are performed on actual pipe to pipe interactions pairs identified via plant walkdown at PINGP.
The analyses are performed on actual pipe to pipe interactions pairs identified via plant walkdown at PINGP.
Engineering evaluations using key parameters identified the specific bounding interaction pairs for each target pipe size. These bounding interactions were modeled to determine the extent of the damage caused by a postulated collision. If the resulting damage for these limiting cases is shown to be acceptable then any damage resulting from the other interactions can be assumed to fall within acceptable limits.
Engineering evaluations using key parameters identified the specific bounding interaction pairs for each target pipe size. These bounding interactions were modeled to determine the extent of the damage caused by a postulated collision. If the resulting damage for these limiting cases is shown to be acceptable then any damage resulting from the other interactions can be assumed to fall within acceptable limits.
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LS-DYNA is used to analyze the pipe to pipe interactions. LS-DYNA is a general purpose explicit/implicit finite element code used to analyze the nonlinear dynamic response of three-dimensional and two-dimensional inelastic structures. Its fully automated contact analysis capability and error checking features have enable users in various industries worldwide to successfully solve many complex crash, forming and other problems. Previously LS-DYNA has been used successfully to analytically model actual experimental pipe to pipe interactions (Ref. 6) which makes it an ideal tool for this analysis. LS-DYNA is not on the AES Approved Software List but it has been used extensively in the industry for non-linear analyses.
LS-DYNA is used to analyze the pipe to pipe interactions. LS-DYNA is a general purpose explicit/implicit finite element code used to analyze the nonlinear dynamic response of three-dimensional and two-dimensional inelastic structures. Its fully automated contact analysis capability and error checking features have enable users in various industries worldwide to successfully solve many complex crash, forming and other problems. Previously LS-DYNA has been used successfully to analytically model actual experimental pipe to pipe interactions (Ref. 6) which makes it an ideal tool for this analysis. LS-DYNA is not on the AES Approved Software List but it has been used extensively in the industry for non-linear analyses.
As such its use is acceptable for this non-safety related application.
As such its use is acceptable for this non-safety related application.
Rev. 2 Form 3.1-3 3.1-3                                                                                                           Rev. 2
Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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A Automated Engineering Services Corp
Client: Xcel Energy Nuclear                                                               Revision: 1 Station: Prairie Island Nuclear Generating Station                                       Prepared By: D. DeGrush Calc.
!e: 6 of 39 Calc. No.: PI-996-83-S01 i
Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.


==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related               Yes   D                                                     Date: 6/10/2010 3.0   Acceptance Criteria This analysis will be utilized to provide technical backup to support an evaluation which attempts to screen postulated HELB piping interactions within the Turbine Building. The interactions will be screened as those which could significantly contribute to flooding and those that will not. Previous Probabalistic Risk Assessment (PRA) has concluded that leakage flows within the turbine building less than 5000 gpm do not pose a significant threat to plant design basis operation (Ref. 1).
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 3.0 Acceptance Criteria This analysis will be utilized to provide technical backup to support an evaluation which attempts to screen postulated HELB piping interactions within the Turbine Building. The interactions will be screened as those which could significantly contribute to flooding and those that will not. Previous Probabalistic Risk Assessment (PRA) has concluded that leakage flows within the turbine building less than 5000 gpm do not pose a significant threat to plant design basis operation (Ref. 1).
Analysis has shown that 5000 gpm would exceed the expected flowrate through a 4" diameter pipe at system operating pressures of approximately 100 psig which is roughly that of a service water or fire protection system (Ref. 2). The cross sectional flow area of a 4" pipe is approximately 12.7 in2 . Therefore a non-threatening pipe interaction will be that considered to cause no more than a 12.7 in2 opening in the target pipe.
Analysis has shown that 5000 gpm would exceed the expected flowrate through a 4" diameter pipe at system operating pressures of approximately 100 psig which is roughly that of a service water or fire protection system (Ref. 2). The cross sectional flow area of a 4" pipe is approximately 12.7 in2. Therefore a non-threatening pipe interaction will be that considered to cause no more than a 12.7 in2 opening in the target pipe.
Form 3.1-3                                                                                                           Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation               Reviewed By: 0. Andersson Safety Related               Yes                                                         Date: 6/10/2010 4.0     Assumptions
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 4.0 Assumptions
: 1. Only orthogonal perpendicular pipe interactions are considered due to their bounding nature based upon previous testing and analysis. (Ref. 5). Any departure from perpendicularity between the plane of motion of the projectile pipe and the axis of the target pipe would have resulted in a lesser component of the maximum impact force between the pipes.
: 1. Only orthogonal perpendicular pipe interactions are considered due to their bounding nature based upon previous testing and analysis. (Ref. 5). Any departure from perpendicularity between the plane of motion of the projectile pipe and the axis of the target pipe would have resulted in a lesser component of the maximum impact force between the pipes.
: 2. A conservative length of 15 ft is arbitrarily chosen for the projectile pipe to maximize impact forces. The longer the projectile pipe the larger the moment formed about the rotation hinge and thus the greater the impact force. Based upon typical piping geometries, support spacing and general clearances within the plant it is not reasonable to assume projectile pipe lengths longer than 15 ft could occur and move freely without interference from other structures.
: 2. A conservative length of 15 ft is arbitrarily chosen for the projectile pipe to maximize impact forces. The longer the projectile pipe the larger the moment formed about the rotation hinge and thus the greater the impact force. Based upon typical piping geometries, support spacing and general clearances within the plant it is not reasonable to assume projectile pipe lengths longer than 15 ft could occur and move freely without interference from other structures.
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: 11. The intemal pressure in both pipes is conservatively assumed to be atmospheric.
: 11. The intemal pressure in both pipes is conservatively assumed to be atmospheric.
: 12. Failure will occur at 25% Strain. (Ref. 8)
: 12. Failure will occur at 25% Strain. (Ref. 8)
Form 3.1-3                                                                                                               Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation         Reviewed By: 0. Andersson Safety Related               Yes -               HI                                 Date: 6/10/2010 5.0   Design Inputs 5.1   Material Properties The following true stress-strain curve is used for both pipes (Ref 3).
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes -
l-'Enig"       Eng.     True [--iie Strain I Stress strain 0.0 10 4.29E+*04j...........
HI Date: 6/10/2010 5.0 Design Inputs 5.1 Material Properties The following true stress-strain curve is used for both pipes (Ref 3).
                                                                                ...............          00010 Stress
l-'Enig" Eng.
                                                                                                                        ....... *
True [--iie Strain I Stress strain Stress 0.0 10 4.29E+*04j...........
                                                                                                                  .. 42965r 0.0020 1 4.39E+04     0.00201       44023 0.0025*   4.42E+04   0.0025       1443261 0.0050   ]4.45E+04     0.0050       '44766-1 007544E+4       0 0075         45247 0.0100   14.56E+04   0.0100         46008 0-12Y5   4.60E+04   0.0124--! 46585 0.0150     4.64E+04   0.0149         47053 0.0175     4.66E+04   0.0173         47374 0-d-.0-2004-75E+04     0T18j48427 0.0225     4.91 E+04 - 0.0223          50232 5ý.0_7E+04b 0.0247 5.29E+04   0.0296          516822 5.4 9E+04 0.0400 5.67E+04       0.0392 0-b.0450  5ý.82E+04                 608 19 0.0500                0. 0488        -0gg 62746 IV 0.0750 6.42E+04        0.0723         68969 0.1000 16.67E+04!     0.0953         73395 1 0.1250 6.85ýE_+04t 0.1500     6,92E+04   0.1398 78  j77027 79578 0.2000     6.97E+04   0.1823         83587 0.28406.97E+04 i0.2500               89438 lbf Density for Carbon Steel per Reference [23] : pCS:= 0.283     -
00010 42965r 0.0020 1 4.39E+04 0.00201 44023 0.0025*
3
4.42E+04 0.0025 1443261 0.0050 ]4.45E+04 0.0050  
                                                                      .n inl Form 3.1-3                                                                                                                       Rev. 2
'44766-1 0075 44E+4 0 0075 45247 0.0100 1 4.56E+04 0.0100 46008 0-12Y5 4.60E+04 0.0124--! 46585 0.0150 4.64E+04 0.0149 47053 0.0175 4.66E+04 0.0173 47374 0-d-.0-200 4-75E+04 0T18j48427 0.0225 0.0400 0-b.0450 0.0500 0.0750 4.91 E+04 -
5ý.0_7E+04b 5.29E+04 5.4 9E +04 5.67E+04 5ý.82E+04 6.42E+04 0.0223 0.0247 0.0296 0.0392
: 0. 0488 0.0723 50232 516822 608 19
-0gg IV 62746 68969 0.1000 16.67E+04!
0.0953 73395 1 0.1250 6.85ýE_+04t 78 j77027 0.1500 6,92E+04 0.1398 79578 0.2000 6.97E+04 0.1823 83587 0.28406.97E+04 i0.2500 89438 lbf Density for Carbon Steel per Reference [23] : pCS:= 0.283  
.n3 inl Form 3.1-3 Rev. 2


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9 6of 39 ZJ/IJZU Services Corp Caic. No.: PI-996-83-S01 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.


==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related               Yes D                                                     Date: 6/10/2010 5.2     Pipe Properties Target Pipe sizes considered in this evaluation are as follows (Ref. 7) 14 in Sch.XS, 14 in OD, 0.5 in wall thickness, 16 in Sch 30, 16 in. OD, 0.375 in wall thickness, 24 in Sch 20, 24 in. OD, 0.375 in wall thickness, Projectile Pipe sizes considered (Ref. 7) 8 in Sch 80, 8.625 in OD, 0.5 in wall thickness, 12in Std Sch., 12.75 in OD, 0.375 in wall thickness, 16 in Sch 30 (data given above for Target Pipe) 20 in Sch 20, 20 in OD, 0.375 in wall thickness, Target Pipe spans: 1/2 suggested max. span in ASME B31.1, Table 121.1.4 (Ref. 9) 14" pipe = 12.5 ft 16" pipe = 13.5 ft 24" pipe = 16 ft Six bounding pipe interaction cases are identified in Section 6.1 8.625          Case 1 - Interaction 186/190
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 5.2 Pipe Properties Target Pipe sizes considered in this evaluation are as follows (Ref. 7) 14 in Sch.XS, 14 in OD, 0.5 in wall thickness, 16 in Sch 30, 16 in. OD, 0.375 in wall thickness, 24 in Sch 20, 24 in. OD, 0.375 in wall thickness, Projectile Pipe sizes considered (Ref. 7) 8 in Sch 80, 8.625 in OD, 0.5 in wall thickness, 12in Std Sch., 12.75 in OD, 0.375 in wall thickness, 16 in Sch 30 (data given above for Target Pipe) 20 in Sch 20, 20 in OD, 0.375 in wall thickness, Target Pipe spans: 1/2 suggested max. span in ASME B31.1, Table 121.1.4 (Ref. 9) 14" pipe = 12.5 ft 16" pipe = 13.5 ft 24" pipe = 16 ft Six bounding pipe interaction cases are identified in Section 6.1
: 5. Projectile Pipe Parameters for Interaction Pairs (Ref. 7) 12.75         Case 2 - Interaction 191 16          Case 3 - Interaction 15 Outer Diameter                                              Dp.°            in 20          Case 4 - Interaction 19/109 16          Case 5 - Interaction 20/123 20 Case 6 - Interaction 48 "0.500" 0.375 0.375 Wall Thickness                                                t :=          in 0.375 0.375 10.375)
: 5. Projectile Pipe Parameters for Interaction Pairs (Ref. 7)
Rev. 2 Form 3.1-3                                                                                                               Rev. 2
Outer Diameter Dp.° Wall Thickness t :=
8.625 12.75 16 20 16 20 in Case 1 - Interaction 186/190 Case 2 - Interaction 191 Case 3 - Interaction 15 Case 4 - Interaction 19/109 Case 5 - Interaction 20/123 Case 6 - Interaction 48 "0.500" 0.375 0.375 0.375 0.375 10.375) in Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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Automated Engineering I.
Services Corp e: 10 of 39 Caic. No.: PI-996-83-S01 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.


==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation         Reviewed By: 0. Andersson Safety Related               Yes   -                                                Date: 6/10/2010 7.625 12.000 15.250 Inner Diameter             Dp~i:= Dp.o - 2tp       Dp i =
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 Inner Diameter Dp~i:= Dp.o - 2tp Operating Pressure in Projectile Pipe (Ref. 7)
n 19.250 15.250 19.250 "685" 420 420 Operating Pressure in Projectile Pipe (Ref. 7)      Pp :=
Mass of Pipe (Ref. 11)
420psi 420 420 "43.4' 49.6 62.6   lb Mass of Pipe (Ref. 11)                              mp.p :
Mass of Water Inside Pipe (Ref. 11)
78.6 ft 62.6
Dp i =
                                                                        ý78.6) 19.8 49.0 79.1     b Mass of Water Inside Pipe (Ref. 11)                m p.w :
Pp :=
125.7   iI 79.1 1125.7) 63.2 98.6 141.7   lb Total Mass of Pipe        mP  =M  .  + M P-        mp=
mp.p :
204.3   ft 141.7 1204.3)
7.625 12.000 15.250 19.250 15.250 19.250 "685" 420 420 420psi 420 420 "43.4' 49.6 62.6 lb 78.6 ft 62.6
Rev. 2 Form 3.1-3 Form 3.1-3                                                                                                   Rev. 2
ý78.6) 19.8 49.0 79.1 125.7 i
79.1 1125.7) 63.2 98.6 141.7 lb 204.3 ft 141.7 1204.3) n m p.w :
b I
Total Mass of Pipe mp=
m P =M.
+ M P-Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation   Reviewed By: 0. Andersson Safety Related               Yes D]                                           Date: 6/10/2010 45.7 113.1 Inner Cross-Sectional                       D*2 p.i 4T'D 182.7      .2 Area of Pipe                          A '"- 4                       ApI=               "11n 291.0 182.7 291.0)
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D]
Length of Projectile Pipe (Assumption #2)                           L := 15ft lp Theoretical Position of Impact on Projectile                       Ip := loft Pipe from hinge assuming Ideal hinge (Assumption #3)
Date: 6/10/2010 Inner Cross-Sectional Area of Pipe D*2 4T'D p.i A '"- 4 45.7 113.1 182.7 ApI=
Target Pipe Parameters for specific interaction pairs (Ref. 7) r14")
291.0 182.7 291.0)
14 16 Outer Diameter                                                      Dt.o            in 16 24
L lp
                                                                                      ,24)
:= 15ft
                                                                                  "0.500" 0.500 0.375 Wall Thickness                                                      tt :=            in 0.375 0.375 0.375) 13.00 13.00 15.25 Inner Diameter                   Dt~i: Dt.0   - 2tt               Dt.i =             -in 15.25 23.25 23.25)
.2 "11n Length of Projectile Pipe (Assumption #2)
Form 3.1-3                                                                                               Rev. 2
Theoretical Position of Impact on Projectile Pipe from hinge assuming Ideal hinge (Assumption #3)
Target Pipe Parameters for specific interaction pairs (Ref. 7)
Outer Diameter Ip := loft Dt.o r14")
14 16 16 24
,24)
"0.500" 0.500 0.375 0.375 0.375 0.375) in in Wall Thickness tt :=
Inner Diameter Dt~i:
Dt.0 - 2tt Dt.i =
13.00 13.00 15.25 15.25 23.25 23.25)
-in Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related             Yes D               N]                           Date: 6/10/2010 72.1 72.1 62.6 Iib Mass of Pipe (Ref. 11)                                             mt.p :=
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D N]
62.6   f 94.6 194.6 57.5 57.5 79.1   lb Mass of Water Inside Pipe (Ref. 11)                                mt.w :=
Date: 6/10/2010 Mass of Pipe (Ref. 11)
79.1   ft 184.0
Mass of Water Inside Pipe (Ref. 11) mt.p :=
                                                                                        ,184.0) 129.6 129.6 141.7    lb Total Mass of Pipe             mt := mt.w + mt p                   m t=
72.1 72.1 62.6 Ii 62.6 f
141.7   ft 278.6 278.6) 132.7' 132.7 Inner Cross-Sectional                  t r.Dtji                              182.7       2 Area of Pipe                        t' '- 4                        At.,=
94.6 194.6 57.5 57.5 79.1 79.1 184.0
182.7 424.6 424.6/
,184.0) b mt.w :=
Rev. 2 3.1-3 Form 3.1-3                                                                                             Rev. 2
lb ft Total Mass of Pipe Inner Cross-Sectional Area of Pipe mt := mt.w + mt p t r.Dtji t' '- 4 m t=
At.,=
129.6 129.6 141.7 lb 141.7 ft 278.6 278.6) 132.7' 132.7 182.7 182.7 424.6 424.6/
2 Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related                 Yes D                                                     'Date: 6/10/2010 6.0   ANALYSIS 6.1   Modeling Discussion The model considers only orthogonal / perpendicular pipe interactions based upon previous studies (Ref. 5).
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D  
'Date: 6/10/2010 6.0 ANALYSIS 6.1 Modeling Discussion The model considers only orthogonal / perpendicular pipe interactions based upon previous studies (Ref. 5).
Both pipes were modeled as cylinders containing water. The water itself was not specifically modeled but the water in the pipes were included in the model as a non-participating structural mass. Which is to say the water mass is evenly distributed about the structure but does not alter the material or dimensional properties of the pipes. The pipes were modeled with ASTM A106 Grade B Carbon Steel material properties.
Both pipes were modeled as cylinders containing water. The water itself was not specifically modeled but the water in the pipes were included in the model as a non-participating structural mass. Which is to say the water mass is evenly distributed about the structure but does not alter the material or dimensional properties of the pipes. The pipes were modeled with ASTM A106 Grade B Carbon Steel material properties.
The target pipe was modeled as a span of pipe supported at each end. At both ends the pipe was constrained axially (X direction) via a rigid spring. The pipe was rigidly supported from translational motion in the directions perpendicular to the pipe axis (Y-Z). Rotationally, the target pipe was allowed some movement about all axes via rotational springs. The length of the target pipe is based upon recommended B31.1 maximum support spacing as detailed in Assumption #7..
The target pipe was modeled as a span of pipe supported at each end. At both ends the pipe was constrained axially (X direction) via a rigid spring. The pipe was rigidly supported from translational motion in the directions perpendicular to the pipe axis (Y-Z). Rotationally, the target pipe was allowed some movement about all axes via rotational springs. The length of the target pipe is based upon recommended B31.1 maximum support spacing as detailed in Assumption #7..
The catastrophic failure of the moving pipe produces a jet force at the failed end which produces a moment arm and causes the pipe to rotate about a plastic hinge. This moment arm is conservatively assumed to be 15 ft in length and based upon previous testing (Ref. 2) is assumed to contact the target pipe 10 ft from the plastic hinge. The pipe rotates in a plane perpendicular to the axis of the target pipe and impacts the target pipe in a perfect "cross" blow at some point in its travel. The jet or blowdown force acting on the broken end of the moving pipe is determined via the equation Fbd = 1.2 x Pop x Acs where Pop is the line operating pressure and ACS = Pipe Cross Sectional Area. (Ref 10)
The catastrophic failure of the moving pipe produces a jet force at the failed end which produces a moment arm and causes the pipe to rotate about a plastic hinge. This moment arm is conservatively assumed to be 15 ft in length and based upon previous testing (Ref. 2) is assumed to contact the target pipe 10 ft from the plastic hinge. The pipe rotates in a plane perpendicular to the axis of the target pipe and impacts the target pipe in a perfect "cross" blow at some point in its travel. The jet or blowdown force acting on the broken end of the moving pipe is determined via the equation Fbd = 1.2 x Pop x Acs where Pop is the line operating pressure and ACS = Pipe Cross Sectional Area. (Ref 10)
The actual Blowdown Force acting on ProjectilePipe for the bounding interaction cases are as follows:
The actual Blowdown Force acting on ProjectilePipe for the bounding interaction cases are as follows:
                                                                                                      /I 3.8 x 104 5.7 x 104 I                    9.2 x 104 Blowdown force                             F P := (1.2PP-Ap.1)               Fp=               -lbf 1.5 x 105 9.2 x 104 5
/I 3.8 x 104 5.7 x 104 9.2 x 104 1.5 x 105 Blowdown force I
1.5 x 10 Form 3.1-3                                                                                                               Rev. 2
F P := (1.2PP-Ap.1)
Fp=
-lbf 9.2 x 104 1.5 x 10 5 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related               Yes   El               ]                                 Date: 6/10/2010 Two modeling scenarios were considered for the projectile pipe. In the first scenario at time = 0 the moving pipe was modelled just contacting the target pipe with a calculated angular velocity. The initial velocity was calculated assuming the projectile pipe rotates about a purely plastic hinge which offers no rotational resistance. The hinged end is constrained from any translational movement or rotation about any other axis.
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes El  
]
Date: 6/10/2010 Two modeling scenarios were considered for the projectile pipe. In the first scenario at time = 0 the moving pipe was modelled just contacting the target pipe with a calculated angular velocity. The initial velocity was calculated assuming the projectile pipe rotates about a purely plastic hinge which offers no rotational resistance. The hinged end is constrained from any translational movement or rotation about any other axis.
This scenario was much to conservative and too limiting when considering larger diameter moving pipes.
This scenario was much to conservative and too limiting when considering larger diameter moving pipes.
Reference 5 addresses this modelling scenario as completely theoretical and not being a credible "real-life" piping system behavior.
Reference 5 addresses this modelling scenario as completely theoretical and not being a credible "real-life" piping system behavior.
Line 268: Line 382:
The software then determines the deformation and the residual damage to both pipes at the conclusion of the event.
The software then determines the deformation and the residual damage to both pipes at the conclusion of the event.
Velocity at impact was determined using actual separation distances determined for specific interaction pairs considered from Reference 7. The interaction pairs could be categoried in two general groups, those where the moving pipe is thinner than the target pipe and those where the two pipe thickness are equal and the target pipe thickness to diameter ratio is less than 0.065. Additionally the interaction pairs contain only 3 distinct target pipe sizes, 24 inch, schedule 20; 16 inch, schedule 30 and 14 inch, schedule xs pipe.
Velocity at impact was determined using actual separation distances determined for specific interaction pairs considered from Reference 7. The interaction pairs could be categoried in two general groups, those where the moving pipe is thinner than the target pipe and those where the two pipe thickness are equal and the target pipe thickness to diameter ratio is less than 0.065. Additionally the interaction pairs contain only 3 distinct target pipe sizes, 24 inch, schedule 20; 16 inch, schedule 30 and 14 inch, schedule xs pipe.
Form 3.1-3                                                                                                               Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation               Reviewed By: 0. Andersson Safety Related                 Yes   Dl             [N]                                     Date: 6/10/2010 6.2   Determination of Bounding Cases Reference 7 identifies all of the applicable pipe interactions for the Turbine Building area where the projectile pipe thickness is either equal to or less than the target pipe thickness. From these interaction cases several critical cases were selected for detailed analysis. The interaction cases are summarize in tables in this section for all the interaction pairs for the respective target pipe sizes. The bounding interactions are highlighted in yellow. The bounding interactions were mostly identified using engineering judgement / logic by comparing critical parameters such as separation distance, operating pressure, size of target vs moving pipe and relative thickness of each pipe.
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Dl
[N]
Date: 6/10/2010 6.2 Determination of Bounding Cases Reference 7 identifies all of the applicable pipe interactions for the Turbine Building area where the projectile pipe thickness is either equal to or less than the target pipe thickness. From these interaction cases several critical cases were selected for detailed analysis. The interaction cases are summarize in tables in this section for all the interaction pairs for the respective target pipe sizes. The bounding interactions are highlighted in yellow. The bounding interactions were mostly identified using engineering judgement / logic by comparing critical parameters such as separation distance, operating pressure, size of target vs moving pipe and relative thickness of each pipe.
In cases where these parameters did not clearly differentiate the interaction a calculation of the theoretical impact momentum was performed to allow relative comparison of impact severity between specific pipe interactions. The higher the momentum of the projectile pipe, the higher the potential for damage to the target pipe. The method for calculating the theoretical impact momentum of the projectile pipe is shown below (the calculation is theoretical because the moving pipe is assumed to rotate about a pinned connection located at the end of the pipe with no resistance to rotation):
In cases where these parameters did not clearly differentiate the interaction a calculation of the theoretical impact momentum was performed to allow relative comparison of impact severity between specific pipe interactions. The higher the momentum of the projectile pipe, the higher the potential for damage to the target pipe. The method for calculating the theoretical impact momentum of the projectile pipe is shown below (the calculation is theoretical because the moving pipe is assumed to rotate about a pinned connection located at the end of the pipe with no resistance to rotation):
Moment at plastic hinge assuming moving pipe has pinned connection         Mp := (FpLp)
i M
(no resistance to rotation)
I P
Moment of Inertia of the                       mnP*L P*L 2 rotating pipe                              p.-       3 i        M                                                                              Mt'O = 1' li2 2' I        P From conservation of Energy L                                                                                                      2 p
L p
Solving for angular velocity at                  2-M P*0 27 impact
.I Moment at plastic hinge assuming moving pipe has pinned connection (no resistance to rotation)
                                                                                                                  , Ip
Moment of Inertia of the rotating pipe From conservation of Energy Solving for angular velocity at impact Where angle of rotation at impact is (see Figure XX for X and Y)
              .I Where angle of rotation at impact is      0 asin( X2 (see Figure XX for X and Y)
Mp := (FpLp) mn P*L P*L 2 p.-
Velocity at Impact                         Vp   0.667.L P W Momentum per unit                          PI = mPVp weight at impact Form 3.1-3                                                                                                                 Rev. 2
3 li2 Mt'O = 1' 2'
2 2-M P*0
, Ip 0 asin( X2 27 Velocity at Impact Momentum per unit weight at impact Vp 0.667.L P W PI = m PVp Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related                 Yes   D         lii                                   Date: 6/10/2010 14 inch Target Pipe High Energy                     1 Impact pipe     Separation Impact   Momentum Wall                     Wall     operating   Distance Velocity, per unit wt, Inte raction   Pipe ID Sched   IID FThckness Target ID Sched   Thickness             Ipressure (Inches) i ft/sec   lbf'sec/tt 8-2HD-8   80     7.625   0.5   14-ZX-161           0.5       685         48       161 190         [41]                           [53]
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D lii Date: 6/10/2010 14 inch Target Pipe Inte High Energy 1 Impact pipe Separation Impact Momentum Wall Wall operating Distance
8-2HD-6   80     762     05   14-ZX-161 188         [411           .65     .      [531   XS [57]   0.5       685         48       161       321 12-2CD-   t           0.37   14-ZX-161
: Velocity, per unit wt, raction Pipe ID Sched IID FThckness Target ID Sched Thickness Ipressure (Inches) i ft/sec lbf'sec/tt 8-2HD-8 80 7.625 0.5 14-ZX-161 0.5 685 48 161 190
              -4       4n rAn   std     12   0.35     r-,   XS [57]   0.5       420         48       163         501 Rev. 2 Form 3.1-3 3.1-3                                                                                                               Rev. 2
[41]
[53]
8-2HD-6 80 762 05 14-ZX-161 188
[411  
.65
[531 XS [57]
0.5 685 48 161 321 12-2CD-t 0.37 14-ZX-161
-4 4n rAn std 12 0.35 r-,
XS [57]
0.5 420 48 163 501 Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation                                       Reviewed By: 0. Andersson Safety Related                     Yes     DFXI                                                                   Date: 6/10/2010 16 inch Target Pipe High Energy Separation 1 Impact      Impact 1 Wall                                  Wall    pipe operating Distance Velocity, Momentum, Interaction I Pipe ID     Sched         ID     !Thicknessi Target ID I Sched        Thickness      pressure      (Inches) If/sec    lbftsec/ft 20-CD-7        20       19.25       0.375       16-CL-67 2       "                      [30]       30         0.375         420             16         133     846 15          [44]
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes DFXI Date: 6/10/2010 16 inch Target Pipe Interaction I Pipe ID 20-CD-7 15
16-CD-9      30    . 15.25       0.375       16-CL-67
[44]
16-CD-9 19
[44]
16-2CD-9 1 Wall Sched ID  
!Thicknessi Target ID 20 19.25 0.375 16-CL-67 2
[30]
16-CL-67 30 15.25 0.375
[30]
[30]
35 16-2CL-9 30 15.25 0.375 1r-,y I
High Energy Separation 1 Impact Wall pipe operating Distance
: Velocity, Sched Thickness pressure (Inches)
If/sec 30 0.375 420 16 133 30 0.375 420 36 158 30 0.375 420.
36 158 Impact
: Momentum, lbftsec/ft 846 697 697 24 inch Target Pipe Interaction 123 20 20a AR Pipe ID 1 Sc 20-2CD-7 2
[40]
20-CD-7 2
[44]
20-CD-7 2
[44]
16-CD-10 hed 0
0 0
0 ID 19.25 19.25 19.25 15.25 Wall Thickness Target ID 0375 24-2CL-56
[32]
24-CL-1 10 0.375
[30]
[30]
                                                          * .       .        [30]      30        0.375          420            36        158      697 19          [44]
24-CL-110 0.375
16-2CD-9      30          35 15.25      0.375       16-2CL-9 1r-,y      30        0.375         420.           36        158      697 24 inch Target Pipe 1 High Energy     Separation    Impact      Impact Wall                                Wall      pipe operating     Distance   Velocity, Momentum, Interaction    Pipe ID 1 Sc hed        ID    Thickness Target ID        Sched    Thickness        pressure        (Inches)     ft/sec   lbf*sec /ft 1 20-2CD-7      2 0      19.25      0375 24-2CL-56            20        0.375            420              24          155        990 123        [40]                                        [32]
[0[30]
20-CD-7      2                            24-CL-1 10 0      19.25      0.375        [30]        20        0.375            420              24          155        990 20        [44]
24-CL-1 10 0.375 r~ni Sched 20 20 20 20 Wall Thickness 0.375 0.375 0.375 0.375 1 High Energy pipe operating pressure 420 420 420 420 Separation Distance (Inches) 24 24 24 60 Impact
20-CD-7      2                    0.375    24-CL-110
: Velocity, ft/sec 155 155 155 201 Impact
[0 0      19.25                  [30]        20        0.375            420              24          155        990 20a          [44]
: Momentum, lbf*sec /ft 1 990 990 990 889 3
16-CD-10                                    24-CL-1 10 AR                    30        15.25      0.375        r~ni        20        0.375            420              60          201        889 Rev. 2 3.1-3 Form 3.1-3                                                                                                                                             Rev. 2
Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related                 Yes D                                                   Date: 6/10/2010 6.3   Determination of Initial Pipe Positions for Specific Controlling Interactions The pipe separation distance (S) was provided in Reference (7). Assumption #2 specifies that the projectile pipe is 15 ft long. Assumption #3 states that the location of theoretical contact was taken at a distance of about 2/3 this length, or 10 ft. Based on these parameters, the elevation of the target pipe or distance Y was determined.
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 6.3 Determination of Initial Pipe Positions for Specific Controlling Interactions The pipe separation distance (S) was provided in Reference (7). Assumption #2 specifies that the projectile pipe is 15 ft long. Assumption #3 states that the location of theoretical contact was taken at a distance of about 2/3 this length, or 10 ft. Based on these parameters, the elevation of the target pipe or distance Y was determined.
Smaller distances of Y were considered which would increase the angle of rotation at contact, but reduce the moment arm between the hinge and the target pipe. By comparing the impact velocity, it was determined that the worst case was when Y was maximized. This will be further demonstrated at the end of this section when the impact velocities are recalculated using Y = 0 (and thus e = 90 degrees).
Smaller distances of Y were considered which would increase the angle of rotation at contact, but reduce the moment arm between the hinge and the target pipe. By comparing the impact velocity, it was determined that the worst case was when Y was maximized. This will be further demonstrated at the end of this section when the impact velocities are recalculated using Y = 0 (and thus e = 90 degrees).
4.0 4.0 3.0 S:=          ft 1.333 Target                                Projectile                              5.0 Pipe                                  Pipe 2.0 /
Target Pipe S:=
X:= S + 0.5.(Dp.0 + Dt.0 )
4.0 4.0 3.0 1.333 5.0 2.0 ft Projectile Pipe
S "4.9' 5.1 y                                                                X= 4.3 ft 2.8 V
/
6.7 3.8, 8.7ý 8.6 Vertical position of Target Pipe                                               9.0 Y:=[ (0ft) 2
X:= S + 0.5.(Dp.0 + Dt.0)
                                                                    -X 2                         ft to allow a theoretical impact                                                  9.6 location of 10 ft on the Projectile Pipe                                                                7.5
S y
                                                                                            ,9.2 Form 3.1-3                                                                                                           Rev. 2
V "4.9' 5.1 4.3 X=
2.8 6.7 3.8, ft ft Vertical position of Target Pipe to allow a theoretical impact location of 10 ft on the Projectile Pipe Y:=[ (0ft) 2-X 2 8.7ý 8.6 9.0 9.6 7.5
,9.2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related               Yes                                             Date: 6/10/2010 29.6 30.8 Angle of rotation at impact             0 := asinf   X2   y             25.7
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 Angle of rotation at impact Angular Velocity at Impact Impact Velocity Momentum at Impact per unit pipe weight 0 := asinf X2 y
                                                                                          *deg 16.5 41.8
2(10.ft. w)
                                                                                  ,22.5j 16.2*
MI:= ((mp.Vp) 29.6 30.8 25.7 16.5 41.8
16.3 Angular Velocity at Impact                                                15.8     rad 13.3     sec 20.2 15.6, (162 163 Impact Velocity                                2(10.ft. w)                  158    ft Vp =
,22.5j 16.2*
133   S 202
16.3 15.8 13.3 20.2 15.6,
                                                                                    *,156, 319 500 696 Momentum at Impact                          MI:= ((mp.Vp)          MI =            -ft-lbf-s per unit pipe weight                                                        845       2 ft 888
* deg rad sec ft S
                                                                                    \988 Rev. 2 3.1-3 Form 3.1-3                                                                                             Rev. 2
-ft-lbf-s ft 2
Vp =
(162 163 158 133 202
*,156, 319 500 696 845 888
\\988 MI =
Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related               Yes D                                                   Date: 6/10/2010 Check case for Y=O, and ( = 90 degrees Angle of rotation at impact               02 := 90deg                       02 = 90.deg 28.3                 16.2 27.9                 16.3 Angular Velocity at Impact                        2.Mp.02 29.6   rad          15.8  rad w2 =
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 Check case for Y=O, and ( = 90 degrees Angle of rotation at impact 02 := 90deg Angular Velocity at Impact Impact Velocity 2.Mp.02
                                                              'p                          31.1   sec          13.3  see 29.6                 20.2
'p Vp2:= (X.w2) 02 = 90.deg 28.3 27.9 29.6 w2 =
                                                                                          \31.1                 15.6 140                 162 143                 163 Impact Velocity 128   ft            158  ft Vp2:= (X.w2)                    Vp2 =                Vp=
31.1 29.6
88   s              133  s 197                 202
\\31.1 140 143 128 Vp2 =
                                                                                            ý119)                 156)
88 197
ý119) rad sec ft s
16.2 16.3 15.8 13.3 20.2 15.6 rad see ft s
V p=
162 163 158 133 202 156)
As demonstrated, although the angular velocity is greater when the Y distance is taken as zero (i.e., hinge forms right at the same height as the target pipe), due to the smaller moment arm, the impact velocity is less for this case. Therefore maximizing the Y distance produces a higher impact velocity, and therefore a higher potential for damage to the target pipe. Also note that this analysis does not consider the effect of reduced blowdown flow due to the reduced cross-sectional area at the hinge or buckling location in the projectile pipe, and the corresponding force reduction associated with large values of 0 (see Section 6.5 for additional discussion).
As demonstrated, although the angular velocity is greater when the Y distance is taken as zero (i.e., hinge forms right at the same height as the target pipe), due to the smaller moment arm, the impact velocity is less for this case. Therefore maximizing the Y distance produces a higher impact velocity, and therefore a higher potential for damage to the target pipe. Also note that this analysis does not consider the effect of reduced blowdown flow due to the reduced cross-sectional area at the hinge or buckling location in the projectile pipe, and the corresponding force reduction associated with large values of 0 (see Section 6.5 for additional discussion).
Form 3.1-3                                                                                                             Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation               Reviewed By: 0. Andersson Safety Related               Yes                                                         Date: 6/10/2010 6.4     Boundary Conditions The boundary conditions for both the target pipe and the projectile pipe need to be established to provide a realistic approximation of the actual configuration. Certain assumptions have been made for the length of the target pipe, and the relative location of the contact point along the length of the projectile pipe as discussed in Section 6.3. The boundary conditions for both the projectile pipe and the target pipe will be discussed in this section.
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 6.4 Boundary Conditions The boundary conditions for both the target pipe and the projectile pipe need to be established to provide a realistic approximation of the actual configuration. Certain assumptions have been made for the length of the target pipe, and the relative location of the contact point along the length of the projectile pipe as discussed in Section 6.3. The boundary conditions for both the projectile pipe and the target pipe will be discussed in this section.
The boundary conditions for the projectile pipe are fairly simple. At the break location, the projectile pipe is conservatively considered free to displace based on the assumption of a full cross section guillotine break. A force is applied at the end of the projectile pipe perpendicular to the pipe axis. In order to preserve the integrity of the model behavior, a reinforcing ring is added to the model on the end of the projectile pipe where the load is applied to facilitate even load distribution to the model elements around the end of the pipe ensuring there is no localized deformation there. As it pertains to the real life situation, it is assumed there is a 90 degree elbow at the top of the break which is causing the whipping force. Note that the elbow was not modelled in LS-DYNA to simplify the modeling effort. The use of the rigid ring on the free end of the pipe is conservative in comparison to actually modelling the elbow in LS-DYNA.
The boundary conditions for the projectile pipe are fairly simple. At the break location, the projectile pipe is conservatively considered free to displace based on the assumption of a full cross section guillotine break. A force is applied at the end of the projectile pipe perpendicular to the pipe axis. In order to preserve the integrity of the model behavior, a reinforcing ring is added to the model on the end of the projectile pipe where the load is applied to facilitate even load distribution to the model elements around the end of the pipe ensuring there is no localized deformation there. As it pertains to the real life situation, it is assumed there is a 90 degree elbow at the top of the break which is causing the whipping force. Note that the elbow was not modelled in LS-DYNA to simplify the modeling effort. The use of the rigid ring on the free end of the pipe is conservative in comparison to actually modelling the elbow in LS-DYNA.
At the opposite end the projectile is fixed as an anchor. This end condition is conservative from the perspective that it will not allow deflection or displacement of the projectile pipe at this location up to and through pipe impact thus maximizing imparted energy to the target pipe. As can be seen from the results in Section 6.6, a plastic hing forms in the moving pipe at some distance above the fixed end of the moving pipe (approximately 1 to 2 diameters above the fixed point location. The consequential damage that occurs in the projectile pipe below the hinge point is not relevant to this investigation.
At the opposite end the projectile is fixed as an anchor. This end condition is conservative from the perspective that it will not allow deflection or displacement of the projectile pipe at this location up to and through pipe impact thus maximizing imparted energy to the target pipe. As can be seen from the results in Section 6.6, a plastic hing forms in the moving pipe at some distance above the fixed end of the moving pipe (approximately 1 to 2 diameters above the fixed point location. The consequential damage that occurs in the projectile pipe below the hinge point is not relevant to this investigation.
The boundary conditions placed upon the target pipe are more sophisticated and indicative of the remainder of the piping system which brackets the target pipe on each end. A single span of the target pipe was considered. In order to account for the continuation of the pipe, spring restraints were used on both ends of the target pipe. Parametric runs were made (see Section 6.7) that confirmed that the smaller the stiffness values of these springs, the higher the potential for damage to the target pipe. Conservatively low spring stiffnesses were used based on relatively long unsupported spans of the target pipe. Since the target pipes are non-safety, non-seismic, it is conservatively assumed that the pipe is mostly supported by spring or rod hangers with very few lateral supports. A conservative support scheme was used to calculate representative stiffnesses as shown on the next page.
The boundary conditions placed upon the target pipe are more sophisticated and indicative of the remainder of the piping system which brackets the target pipe on each end. A single span of the target pipe was considered. In order to account for the continuation of the pipe, spring restraints were used on both ends of the target pipe. Parametric runs were made (see Section 6.7) that confirmed that the smaller the stiffness values of these springs, the higher the potential for damage to the target pipe. Conservatively low spring stiffnesses were used based on relatively long unsupported spans of the target pipe. Since the target pipes are non-safety, non-seismic, it is conservatively assumed that the pipe is mostly supported by spring or rod hangers with very few lateral supports. A conservative support scheme was used to calculate representative stiffnesses as shown on the next page.
Evaluation has shown that damage results are sensitive to the span of the target pipe between supports. The degree of sensitivity depends upon a number of key factors including relative pipe thickness to each other, magnitude of the blowdown force, initial separation distance, etc. Parametric runs performed in Section 6.7 indicate that for the case where only the angular velocity is considered, a shorter pipe span produces the most conservative results. However, for cases where the jet force continues to be applied after the initial contact with the pipe, the longer the span the worse the damage to the target pipe. For this evaluation a reasonable support span of 1/2 the maximum recommended per ASME B31.1 was utilized.
Evaluation has shown that damage results are sensitive to the span of the target pipe between supports. The degree of sensitivity depends upon a number of key factors including relative pipe thickness to each other, magnitude of the blowdown force, initial separation distance, etc. Parametric runs performed in Section 6.7 indicate that for the case where only the angular velocity is considered, a shorter pipe span produces the most conservative results. However, for cases where the jet force continues to be applied after the initial contact with the pipe, the longer the span the worse the damage to the target pipe. For this evaluation a reasonable support span of 1/2 the maximum recommended per ASME B31.1 was utilized.
Rev. 2 Form 3.1-3                                                                                                               Rev. 2
Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related               Yes                                                       Date: 6/10/2010
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010
                    ././4Z//-
././4Z//-
40 ft 40 ft             I     Lt                   40 ft             -I T T1 40 ft 40 ft spans are considered in two directions on either side of the supports in the target pipe impact zone. At the ends the pipe is considered fixed assuming it terminates into some piece of equipment or anchor at a wall penetration. These spans are considered conservatively large. Using these spanse stiffness values are considered for the target pipe so it can be modelled as shown below:
40 ft 40 ft I
Form 3.1-3                                                                                                           Rev. 2
Lt 40 ft
-I T T1 40 ft 40 ft spans are considered in two directions on either side of the supports in the target pipe impact zone. At the ends the pipe is considered fixed assuming it terminates into some piece of equipment or anchor at a wall penetration. These spans are considered conservatively large. Using these spanse stiffness values are considered for the target pipe so it can be modelled as shown below:
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation               Reviewed By: 0. Andersson Safety Related               Yes D               N]                                       Date: 6/10/2010 KI                                                 KI K2 The axial stiffness is based on a simple cantilever bending of a 40 ft cantileved pipe as shown in the figure below
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D N]
                          -/14///
Date: 6/10/2010 KI K2 KI The axial stiffness is based on a simple cantilever bending of a 40 ft cantileved pipe as shown in the figure below
L:= 40.ft             E:= 27.9.10 6psi (Ref 9) 40 ft                                                                L483.8    4 14" XS I:=  562.1 -in    16" Sch. 30 1942)      20" Sch. 20 KE 3                                                366
-/14///
* Ibf 3.E.I K I := -             KI =   425 - -n-L1470)
40 ft K3E L:= 40.ft L483.8 I:= 562.1 -in4 1942)
E:= 27.9.10 6psi (Ref 9) 14" XS 16" Sch. 30 20" Sch. 20 366
* 3.E.I Ibf K I := -
K I =
425  
-n-L1470)
Use 500 lb/in for 14" and 16" pipe Use 1000 lb/in for 24" pipe For the rotational springs, the spring stiffness for a unit rotation is 4EI/L for a fixed end, and 3EI/L for a pinned end (Ref. 4). Since the end of the pipe segment has some flexibility due to the next 40 ft leg, use a stiffness of 3.5EI/L to represent a mid point between fixed and pinned.
Use 500 lb/in for 14" and 16" pipe Use 1000 lb/in for 24" pipe For the rotational springs, the spring stiffness for a unit rotation is 4EI/L for a fixed end, and 3EI/L for a pinned end (Ref. 4). Since the end of the pipe segment has some flexibility due to the next 40 ft leg, use a stiffness of 3.5EI/L to represent a mid point between fixed and pinned.
Form 3.1-3                                                                                                                 Rev. 2
Form 3.1-3 Rev. 2


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7,
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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation     Reviewed By: 0. Andersson Safety Related             Yes D             N                                 Date: 6/10/2010 11//1, 3.5.E.I K2.     L         K2 =
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D N
40 ft K- 3.5EI Use 1 x 108 in-lbf/rad for 14" and 16" pipe
Date: 6/10/2010 11//1, 3.5.E.I K2.
                                        "-"        L            Use 2 x 108 in-Ibf/rad for 24" pipe ZN Rev. 2 Form 3.1-3 Form 3.1-3                                                                                                 Rev. 2
L K2 =
40 ft K-3.5EI L
Use 1 x 108 in-lbf/rad for 14" and 16" pipe Use 2 x 108 in-Ibf/rad for 24" pipe ZN Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related               Yes                                                         Date: 6/10/2010 6.5 Jet Force Time History As the projectile pipe rotates about a plastic hinge, the cross-sectional area of the pipe is reduced. This occurs at two locations; at the hinge where the pipe buckles and at the impact location as the projectile pipe tends to wrap around the target pipe. As the pipe cross-sectional area is reduced there is a corresponding reduction in the blowdown flow from the pipe. This reduces the whipping force on the pipe as the pipe continues to deform.
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 6.5 Jet Force Time History As the projectile pipe rotates about a plastic hinge, the cross-sectional area of the pipe is reduced. This occurs at two locations; at the hinge where the pipe buckles and at the impact location as the projectile pipe tends to wrap around the target pipe. As the pipe cross-sectional area is reduced there is a corresponding reduction in the blowdown flow from the pipe. This reduces the whipping force on the pipe as the pipe continues to deform.
Following impact, as the collision continues, and both pipes deform, the flow is eventually reduced to zero at the point where the projectile pipe basically seals itself off and the blowdown force is gone.
Following impact, as the collision continues, and both pipes deform, the flow is eventually reduced to zero at the point where the projectile pipe basically seals itself off and the blowdown force is gone.
To account for this force reduction, the LS-DYNA runs were used to estimate the reduced cross sectional areas at both the plastic hinge, and at the impact location. Data was taken from preliminary runs to determine the reduced area at the deformed cross sections at specific times during the event. Using this data, more realistic force functions were utilized in the Case runs by applying a force time history based on a linear reduction in the area.
To account for this force reduction, the LS-DYNA runs were used to estimate the reduced cross sectional areas at both the plastic hinge, and at the impact location. Data was taken from preliminary runs to determine the reduced area at the deformed cross sections at specific times during the event. Using this data, more realistic force functions were utilized in the Case runs by applying a force time history based on a linear reduction in the area.
Conservatively, for most cases only the reduction of area at the collision point was considered. In one case, the reduction in the area at the moving pipe hinge location was also considered (for Case 5 where the separation distance was larger resulting in a large rotation in the moving pipe prior to impact. The shape of the force time history curve is shown below:
Conservatively, for most cases only the reduction of area at the collision point was considered. In one case, the reduction in the area at the moving pipe hinge location was also considered (for Case 5 where the separation distance was larger resulting in a large rotation in the moving pipe prior to impact. The shape of the force time history curve is shown below:
Typical Force Time History (Cases 2-4 and 6) t I time of impact t2 = time projectile pipe blowdown flow = 0 Force 0
Typical Force Time History (Cases 2-4 and 6) t I time of impact t2 = time projectile pipe blowdown flow = 0 Force 0
tI                             It2 Time Rev. 2 Form 3.1-3                                                                                                             Rev. 2
tI It2 Time Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related               Yes D               HI                                   Date: 6/10/2010 For Case 5, since the angle of rotation of the moving pipe was large, a two step force time history was used to account for the flow reduction at the plastic hinge.
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D HI Date: 6/10/2010 For Case 5, since the angle of rotation of the moving pipe was large, a two step force time history was used to account for the flow reduction at the plastic hinge.
Force Time History for Case 5 Fp t   = time moving pipe hinge begins to significantly kink
Force Time History for Case 5 Fp t  
                                                  - - - -t                     2   time of impact SI           t 3 = time projectile pipe Iblowdown                                     flow = 0 Force                                   I                                   oo           w 0
= time moving pipe hinge begins to significantly kink
tt II         t2                 t3 Time Form 3.1-3                                                                                                           Rev. 2
- - - -t 2 time of impact SI t 3 = time projectile pipe Iblowdown flow = 0 Force I
oo w
0 tt II t2 t 3 Time Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation                                           Reviewed By: 0. Andersson Safety Related                       Yes                                                                               Date: 6/10/2010 6.6   Analysis Results Six specific interaction cases were run as described in the sections above. A table summarizing the input parameters for these six load cases is provided below:
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 6.6 Analysis Results Six specific interaction cases were run as described in the sections above. A table summarizing the input parameters for these six load cases is provided below:
I     Targt Ppe oimnbry     MyigPp Bwr~t
I Targt Ppe oimnbry MyigPp Bwr~t I
___
___Conditions ConQditins Target Target Proectile ProjectiI Target d.taoL seaai' L
_____  I  ___  _            ___Conditions                                                 ConQditins Target Target Proectile ProjectiI Target                 seaai'        d.taoL L       Srn,     Spig~ Supi~ed         Fe n         eLlotre Pipe M1t, Pipe, 01) ePipe, t, SpftI                          o elevatiort                           End         re n       eu~otn 0Q n i Case                  n       in                 ft     dstne           ft         lin         ae)steps,                               rme-c Case1       14     G5     a625     Q5     125         4           49       a7         5M         100E      xed   F=37,5001bs         No Case2       14     05     1275     0375     125         4           51       86         5M         IOEB     Fxed     F=57,(X0bsI   t1 =64Kt 2=81 CGe3         16     Q375       16     0375     135         3         4,333       9         5M         1.OES   Axed     F=92,1W1bs     t1=5Zt 2=72 Case4       16     Q375     2)     0375     135       1333           28       96         500       I0EN     Fxed     F=147,0C01bs ti=3Zt 2=E2 tl=5, t2=ff, t3 Case5       24     0375       16     03"75     16         5           66       7.5       100         ZOE8     Fixed   F=92IBllbs Case6       24     0375     2M     0375     16         2           38       92           Ma I 2-0E8         Axed   I F=147,00Dtlbs t=40,t 2 =70
: Srn, Spig~ Supi~ed Fe n
          '1.5N.Iinearforce redLuidon 55to E9rnecLbased upon Y/oreduc-tion in Proiectle Pipe Secdcn in buddirg zone at antact Results for these six analysis cases are provided in the sections below:
eLlotre Pipe M1t, Pipe, 01) e Pipe, t, Spft I
Rev. 2 Form 3.1-3                                                                                                                                                         Rev. 2
o elevatiort End re n eu~otn Case 0Q n i
n in ft dstne ft lin ae)steps, rme-c Case1 14 G5 a625 Q5 125 4
49 a7 5M 100 E
xed F =37,5001bs No Case2 14 05 1275 0375 125 4
51 86 5M IOEB Fxed F=57,(X0bsI t1=64Kt 2=81 CGe3 16 Q375 16 0375 135 3
4,333 9
5M 1.OES Axed F=92,1W1bs t1=5Zt 2=72 Case4 16 Q375
: 2) 0375 135 1333 28 96 500 I0EN Fxed F=147,0C01bs ti=3Zt 2=E2 tl=5, t2=ff, t3 Case5 24 0375 16 03"75 16 5
66 7.5 100 ZOE8 Fixed F=92IBllbs Case6 24 0375 2M 0375 16 2
38 92 Ma I 2-0E8 Axed I F=147,00Dtlbs t=40,t 2=70
'1. 5N. Iinearforce redLuidon 55to E9rnecLbased upon Y/oreduc-tion in Proiectle Pipe Secdcn in buddirg zone at antact Results for these six analysis cases are provided in the sections below:
Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related               Yes DI'l]                                                   Date: 6/10/2010 6.6.1 Case 1 (Interaction 188/190) - 14" XS Target Pipe, 8" XS Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.065 msec (Initiation of contact)                     t = 0.077 msec (Projectile Pipe Blowdown = 0) t= 0.087 msec (Continued deformation)                       t = 0.100 msec (Conclusion of event)
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes DI'l]
Date: 6/10/2010 6.6.1 Case 1 (Interaction 188/190) - 14" XS Target Pipe, 8" XS Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.065 msec (Initiation of contact) t = 0.077 msec (Projectile Pipe Blowdown = 0) t= 0.087 msec (Continued deformation) t = 0.100 msec (Conclusion of event)
The results of the analysis show that no elements exceeded the strain limit of 25%. Therefore it is concluded that the interaction of the moving pipe with the target pipe will not create sufficient damage to the target pipe to add to the Turbine Building flooding concern.
The results of the analysis show that no elements exceeded the strain limit of 25%. Therefore it is concluded that the interaction of the moving pipe with the target pipe will not create sufficient damage to the target pipe to add to the Turbine Building flooding concern.
Form 3.1-3                                                                                                               Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation               Reviewed By: 0. Andersson Safety Related               Yes 11             N                                       Date: 6/10/2010 6.6.2 Case 2 (Interaction 190) - 14" XS Target Pipe, 12" Std Proiectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.064 msec (Initiation of contact)                   t = 0.081 msec (Projectile Pipe Blowdown Flow = 0) t= 0.096 msec (Continued deformation)                       t = 0.124 msec (Conclusion of event)
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes 11 N
Date: 6/10/2010 6.6.2 Case 2 (Interaction 190) - 14" XS Target Pipe, 12" Std Proiectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.064 msec (Initiation of contact) t = 0.081 msec (Projectile Pipe Blowdown Flow = 0) t= 0.096 msec (Continued deformation) t = 0.124 msec (Conclusion of event)
The results of the analysis show that no elements exceeded the strain limit of 25%. Therefore it is concluded that the interaction of the moving pipe with the target pipe will not create sufficient damage to the target pipe to add to the Turbine Building flooding concern.
The results of the analysis show that no elements exceeded the strain limit of 25%. Therefore it is concluded that the interaction of the moving pipe with the target pipe will not create sufficient damage to the target pipe to add to the Turbine Building flooding concern.
Form 3.1-3                                                                                                               Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related               Yes     jJ                                                  Date: 6/10/2010 6.6.3 Case 3 (Interaction 15) - 16" Sch. 30 Target Pipe, 16" Sch. 30 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.052 msec (Initiation of contact)                     t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation)                       t = 0.125 msec (Conclusion of event)
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes j J Date: 6/10/2010 6.6.3 Case 3 (Interaction 15) - 16" Sch. 30 Target Pipe, 16" Sch. 30 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.052 msec (Initiation of contact) t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation) t = 0.125 msec (Conclusion of event)
The results of the analysis show that 5 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 7.0 in2 . Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.
The results of the analysis show that 5 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 7.0 in2. Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.
Form 3.1-3                                                                                                         Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related                 Yes     li                                                Date: 6/10/2010 6.6.4 Case 4 (Interaction 19/109) - 16" Sch. 30 Tar-et Pipe. 20" Sch. 20 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.032 msec (Initiation of contact)                   t = 0.062 msec (Projectile Pipe Blowdown Flow = 0) t= 0.082 msec (Continued deformation)                       t = 0.125 msec (Conclusion of event)
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes l i Date: 6/10/2010 6.6.4 Case 4 (Interaction 19/109) - 16" Sch. 30 Tar-et Pipe. 20" Sch. 20 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.032 msec (Initiation of contact) t = 0.062 msec (Projectile Pipe Blowdown Flow = 0) t= 0.082 msec (Continued deformation) t = 0.125 msec (Conclusion of event)
The results of the analysis show that 3 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 4.2 in2 . Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.
The results of the analysis show that 3 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 4.2 in2. Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.
Form 3.1-3                                                                                                         Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation               Reviewed By: 0. Andersson Safety Related                 Yes                                                         Date: 6/10/2010 6.6.5 Case 5 (Interaction 20/20a/123) - 24" Sch. 20 Target Pipe, 16" Sch. 30 Progectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.055 msec (Cross-sectional area reduced                       t = 0.069 msec (Initiation of contact) 25% at hinge) t = 0.087 msec (Projectile Pipe                           t = 0.119 msec (Conclusion of event)
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 6.6.5 Case 5 (Interaction 20/20a/123) - 24" Sch. 20 Target Pipe, 16" Sch. 30 Progectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.055 msec (Cross-sectional area reduced t = 0.069 msec (Initiation of contact) 25% at hinge) t = 0.087 msec (Projectile Pipe t = 0.119 msec (Conclusion of event)
Blowdown flow = 0)
Blowdown flow = 0)
The results of the analysis show that 4 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 8.4 in2 . Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.
The results of the analysis show that 4 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 8.4 in2. Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.
Form 3.1-3                                                                                                               Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related                 Yes D                 ['1                                 Date: 6/10/2010 6.6.6 Case 6 (Interaction 48) - 24" Sch. 20 Target Pipe, 20" Sch. 20 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.040 msec (Initiation of contact)                   t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.085 msec (Continued deformation)                       t = 0.109 msec (Conclusion of event)
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D
The results of the analysis show that 2 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 4.2 in2 . Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.
['1 Date: 6/10/2010 6.6.6 Case 6 (Interaction 48) - 24" Sch. 20 Target Pipe, 20" Sch. 20 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.040 msec (Initiation of contact) t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.085 msec (Continued deformation) t = 0.109 msec (Conclusion of event)
Form 3.1-3                                                                                                         Rev. 2
The results of the analysis show that 2 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 4.2 in2. Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related               Yes   D               N-                                   Date: 6/10/2010 6.7   Parametric Evaluations A few select additional cases were run to determine the impact of altering some of the key input parameters to determine the sensitivity of the results to the variation of these parameters. The results of these parametric runs are included on the following pages:
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D N-Date: 6/10/2010 6.7 Parametric Evaluations A few select additional cases were run to determine the impact of altering some of the key input parameters to determine the sensitivity of the results to the variation of these parameters. The results of these parametric runs are included on the following pages:
Form 3.1-3                                                                                                           Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation             Reviewed By: 0. Andersson Safety Related               Yes   D               E                                   Date: 6/10/2010 Case 7 - Reduce spring stiffness boundary conditions on the targey pipe by a factor of 5 (run on base Case 3 (Interaction 15) - 16" Sch. 30 Tarqet Pipe, 16" Sch. 30 Proiectile Pipe )
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D E
Date: 6/10/2010 Case 7 - Reduce spring stiffness boundary conditions on the targey pipe by a factor of 5 (run on base Case 3 (Interaction 15) - 16" Sch. 30 Tarqet Pipe, 16" Sch. 30 Proiectile Pipe )
The results of this run confirmed that reducing the stiffness of the springs resulted in additional damage to the target pipe. Comparison of the screen shots below to those of the Base Case it is apparent that the lighter spring forces result in much more target pipe deformation. Since the stiffness used already represent lower bound values, the results from Cases 1 - 6 are still bounding. There is no need to make additional runs with stiffer springs as this will result in less damage to the target pipe.
The results of this run confirmed that reducing the stiffness of the springs resulted in additional damage to the target pipe. Comparison of the screen shots below to those of the Base Case it is apparent that the lighter spring forces result in much more target pipe deformation. Since the stiffness used already represent lower bound values, the results from Cases 1 - 6 are still bounding. There is no need to make additional runs with stiffer springs as this will result in less damage to the target pipe.
t = 0.052 msec (Initiation of contact)                 t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation)                   t = 0.125 msec (Conclusion of event)
t = 0.052 msec (Initiation of contact) t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation) t = 0.125 msec (Conclusion of event)
Rev. 2 Form 3.1-3 Form                                                                                                                    Rev. 2
Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation         Reviewed By: 0. Andersson Safety Related             Yes                 [K]                                 Date: 6/10/2010 Case 8 - Increase support span on target pipe by a factor of 2 (run on base Case 3 (Interaction 15) - 16" Sch. 30 Target Pipe, 16" Sch. 30 Projectile Pipe )
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes
t = 0.052 msec (Initiation of contact)               t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation)                 t = 0.125 msec (Conclusion of event)
[K]
Rev. 2 Form 3.1-3                                                                                                         Rev. 2
Date: 6/10/2010 Case 8 - Increase support span on target pipe by a factor of 2 (run on base Case 3 (Interaction 15) - 16" Sch. 30 Target Pipe, 16" Sch. 30 Projectile Pipe )
t = 0.052 msec (Initiation of contact) t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation) t = 0.125 msec (Conclusion of event)
Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related             Yes 1               N]                                     Date: 6/10/2010 Case 9 - Increase support span of target pipe by a factor of 2 (run on base Case 2 (Interaction 190) - 14" XS Target Pipe, 12" Std Projectile Pipe) t = 0.065 msec (Initiation of contact)                   t = 0.081 msec (Projectile pipe Blowdown flow = 0) t= 0.096 msec (Continued deformation)                       t = 0.134 msec (Conclusion of event)
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes 1 N]
Date: 6/10/2010 Case 9 - Increase support span of target pipe by a factor of 2 (run on base Case 2 (Interaction 190) - 14" XS Target Pipe, 12" Std Projectile Pipe) t = 0.065 msec (Initiation of contact) t = 0.081 msec (Projectile pipe Blowdown flow = 0) t= 0.096 msec (Continued deformation) t = 0.134 msec (Conclusion of event)
The results of the analyses for Cases 8 and 9 show that the damage to the Target Pipe did increase over that observed for the respective base cases but to relatively different extents. For Case 9, similar to Base Case 2, no elements exceeded the strain limit of 25% and the increase in damage was minimal. Case 8 showed appreciably more damage than it's Base Case 3 counterpart in that 13 elements were deleted compared to 5 in the base case. The conclusion is that the impact of increasing the target pipe length is significantly dependent upon other key parameters such as relative pipe thickness, initial separation distances, blowdown force, etc.
The results of the analyses for Cases 8 and 9 show that the damage to the Target Pipe did increase over that observed for the respective base cases but to relatively different extents. For Case 9, similar to Base Case 2, no elements exceeded the strain limit of 25% and the increase in damage was minimal. Case 8 showed appreciably more damage than it's Base Case 3 counterpart in that 13 elements were deleted compared to 5 in the base case. The conclusion is that the impact of increasing the target pipe length is significantly dependent upon other key parameters such as relative pipe thickness, initial separation distances, blowdown force, etc.
Form 3.1-3                                                                                                           Rev. 2
Form 3.1-3 Rev. 2


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Calic. No.: PI-996-83-SO1 Client: Xcel Energy Nuclear                                                                   Revision: 1 Station: Prairie Island Nuclear Generating Station                                             Prepared By: D. DeGrush Calc.
Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.


==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation                   Reviewed By: 0. Andersson Safety Related               Yes   E             [                                           Date: 6/10/2010 7.0   Summary Actual Turbine Building pipe to pipe interactions were evaluated resulting in a set of bounding interactions. Detailed Finite Element models were prepared for each of these bounding cases. The parameters for each of the bounding cases evaluated are provided in the table below.
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes E
Numberof            Failed Pipe Projecti I         Separation  Blowdown Surface Target Target Projectile              Target                                  Failed e Pipe, t,           Distance,   Force on Element,   Ae Pipe, Wall t, Pipe, OD,              Span, ft                              Elements in              Area in                  ft    Projectile Pipe                        Opening, in'2 Case     00, in    in        in                                                        Model Case 1       14     0.5     8.625       0.5     12.5         4     F= 37,500 1bs       None       1.22         0 Case 2       14     0.5     12.75       0.375   12.5         4     F = 57,000 1bs     None       1.22         0 Case 3       16   0.375     16       0.375   13.5         3     F = 92,100lbs         5         1.4       7.00 Case 4       16   0.375     20       0.375   13.5       1.333   F = 147,000 1bs       3         1.4       4.20 Case 5       24   0.375     16       0.375     16         5     F=92,100lbs           4         2.09       8.36 Case 6       24   0.375     20       0.375     16         2     F = 147,000 1bs       2         2.09       4.18 Parametric investigations were performed for a few key modeling parameters. The results show that a Target Pipe boundary condition with lower (lighter) spring constants tend to result in more damage to the Target Pipe.
[
Date: 6/10/2010 7.0 Summary Actual Turbine Building pipe to pipe interactions were evaluated resulting in a set of bounding interactions. Detailed Finite Element models were prepared for each of these bounding cases. The parameters for each of the bounding cases evaluated are provided in the table below.
Target
: Pipe, 00, in Target Wall t, in Projectile Pipe, OD, in Projecti I e Pipe, t, in Target Span, ft Separation
: Distance, ft Blowdown Force on Projectile Pipe Numberof Failed Elements in Model
: Element, Ae Failed Pipe Surface Area Opening, in'2 Case Case 1 14 0.5 8.625 0.5 12.5 4
F= 37,500 1bs None 1.22 0
Case 2 14 0.5 12.75 0.375 12.5 4
F = 57,000 1bs None 1.22 0
Case 3 16 0.375 16 0.375 13.5 3
F = 92,100lbs 5
1.4 7.00 Case 4 16 0.375 20 0.375 13.5 1.333 F = 147,000 1bs 3
1.4 4.20 Case 5 24 0.375 16 0.375 16 5
F =92,100lbs 4
2.09 8.36 Case 6 24 0.375 20 0.375 16 2
F = 147,000 1bs 2
2.09 4.18 Parametric investigations were performed for a few key modeling parameters. The results show that a Target Pipe boundary condition with lower (lighter) spring constants tend to result in more damage to the Target Pipe.
Physically the lower spring constants would represent a piping system with less support / less restraint.
Physically the lower spring constants would represent a piping system with less support / less restraint.
Another parameter investigated was the length of the Target Pipe span (distance of Target Pipe Support separation). The results show that for impacts with no sustained force on the Projectile Pipe that shorter Target Pipe spans are more conservative, i.e. more resultant damage to the Target Pipe. Conversely, for impacts which include a blowdown force on the Projectile Pipe the longer Target Pipe spans result in more Target Pipe damage.
Another parameter investigated was the length of the Target Pipe span (distance of Target Pipe Support separation). The results show that for impacts with no sustained force on the Projectile Pipe that shorter Target Pipe spans are more conservative, i.e. more resultant damage to the Target Pipe. Conversely, for impacts which include a blowdown force on the Projectile Pipe the longer Target Pipe spans result in more Target Pipe damage.
The sensitivity to each parameter variation is individual to each specific interation pair as it depends on a number of key interaction parameters such as relative thickness of the two pipes, blowdown force, initial separation of the two pipes, etc.
The sensitivity to each parameter variation is individual to each specific interation pair as it depends on a number of key interaction parameters such as relative thickness of the two pipes, blowdown force, initial separation of the two pipes, etc.
8.0   Conclusions The results of the analyses, included in the table above, show clearly that none of the cases would produce an excessive flooding event within the Turbine Building.
8.0 Conclusions The results of the analyses, included in the table above, show clearly that none of the cases would produce an excessive flooding event within the Turbine Building.
Form 3.1-3                                                                                                                     Rev. 2
Form 3.1-3 Rev. 2


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==Title:==
==Title:==
Technical Backup for Turbine Building HELB Screening Evaluation           Reviewed By: 0. Andersson Safety Related               Yes                                                     Date: 6/10/2010 9.0     References The following references were reviewed and used in the generation of this calculation.
Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 9.0 References The following references were reviewed and used in the generation of this calculation.
[1]   EC 15656, Rev. 0 dated 3/5/2010 - "EVALUATION OF FLOODING TIMES AND FLOW RATES ASSOCIATED WITH UNIT 1 AND UNIT.2 TB FOR SIGNIFICANCE DETERMINATION"
[1]
[2]   EC 16090, Rev.0, dated "In Process" - "TURBINE BUILDING FLOODING SDP: CL TURBINE BUILDING PIPE BREAK ANALYSIS
EC 15656, Rev. 0 dated 3/5/2010 - "EVALUATION OF FLOODING TIMES AND FLOW RATES ASSOCIATED WITH UNIT 1 AND UNIT.2 TB FOR SIGNIFICANCE DETERMINATION"
[3]   US NRC Piping Fracture Mechanics Database (PIFRAC), Version 3.1, from US NRC Pipe Fracture Encyclopedia, 1997."
[2]
[4]   Structural Engineering Handbook, Edwin H Gaylord, Jr. / Charles N. Gaylord, McGraw-Hill Book Co., 1968
EC 16090, Rev.0, dated "In Process" - "TURBINE BUILDING FLOODING SDP: CL TURBINE BUILDING PIPE BREAK ANALYSIS
[5]   NUREG / CR-3231 PNL-5779 Pipe-to-Pipe Impact Program, May 1987
[3]
[6]   Experimental Study and Numerical Simulation of Pipe-to-Pipe Impact, International Journal of Impact Engineering, May 2009
US NRC Piping Fracture Mechanics Database (PIFRAC), Version 3.1, from US NRC Pipe Fracture Encyclopedia, 1997."
[7]   Xcel Energy, NSPM Calculation No: ENG-ME-732 "Determination of HELB / Flooding Interactions in the Turbine Building", Rev. 0, 1/18/2010
[4]
[8]   Machine Design Theory and Practice, Deutschman, Michels, Wilson,Macmillan Publishing Co. 1975
Structural Engineering Handbook, Edwin H Gaylord, Jr. / Charles N. Gaylord, McGraw-Hill Book Co., 1968
[9]   ASME B31.1 - 1989 Edition, Power Piping
[5]
NUREG / CR-3231 PNL-5779 Pipe-to-Pipe Impact Program, May 1987
[6]
Experimental Study and Numerical Simulation of Pipe-to-Pipe Impact, International Journal of Impact Engineering, May 2009
[7]
Xcel Energy, NSPM Calculation No: ENG-ME-732 "Determination of HELB / Flooding Interactions in the Turbine Building", Rev. 0, 1/18/2010
[8]
Machine Design Theory and Practice, Deutschman, Michels, Wilson,Macmillan Publishing Co. 1975
[9]
ASME B31.1 - 1989 Edition, Power Piping
[10] Prairie Island Unit 1 Pipe Rupture Analysis Feedwater Piping System, NSC-PIP-M-SLR-9, Rev. 1, August 11, 1972
[10] Prairie Island Unit 1 Pipe Rupture Analysis Feedwater Piping System, NSC-PIP-M-SLR-9, Rev. 1, August 11, 1972
[11] Crane Technical Paper No. 410, "Flow of Fluids Through Valves, Fittings, and Pipe", 1988 Crane Co.
[11] Crane Technical Paper No. 410, "Flow of Fluids Through Valves, Fittings, and Pipe", 1988 Crane Co.
Rev. 2 3.1-3 Form 3.1-3                                                                                                         Rev. 2}}
Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2}}

Latest revision as of 04:27, 14 January 2025

Enclosure 6, Prairie Island Nuclear Generating Plant, Units 1 and 2, Supporting Engineering Evaluations, EC 16275, Effects of Pipe Whip Interactions for Various Pipe Combinations for Internal Flooding Sdp
ML101690171
Person / Time
Site: Prairie Island  Xcel Energy icon.png
Issue date: 06/11/2010
From:
Northern States Power Co, Xcel Energy
To:
Office of Nuclear Reactor Regulation
References
EA-10-070, IR-10-010, L-PI-10-060 EC 16275
Download: ML101690171 (45)


Text

ENCLOSURE6 PRAIRIE ISLAND NUCLEAR GENERATING PLANT SUPPORTING ENGINEERING EVALAUTIONS EC 16275 44 Pages Follow

XcelEnergy° EC-0441 EC Closeout Package Report (Rev. 3)

Report Date: 06/1112010 EC Number: 0000016275 Revision: 000 Engineering Change EC Number Status/Date 0000016275 CLOSED 000 06/10/2010 Facility PI Type/Sub-type :

EVAL /

EC

Title:

EFFECTS OF PIPE WHIP INTERACTIONS FOR VARIOUS PIPE COMBINATIONS FOR INTERNAL FLOODING SDP Mod Nbr:

KW1:

KW2:

KW3:

KW4:

KW5:

Master EC Outage WO Required Adv Wk Appvd Auto-Advance Caveat Outst Work Group Alert Group Image Addr Alt Ref.

Priority Resp Engr

E-REG PROG
PTTD06 Temporary Aprd Req. Dt.

Exp Insvc Date Expires On Auto-Asbuild 07/01/2010 Units and Systems Facility Unit System

System Description

PI 0

OTH OTHER Attributes Attribute Name SCRN NO SIMULATOR SYSTEM HEALTH EVAL NO PORC DTE PRIORITY RANKING Value NA Updated By PTTD06 Last Updated 06/10/2010 Notes This evaluation does not support design basis.

Pedigree Information Page 1 of 4

Xcel Energy' EC-0441 EC Closeout Package Report (Rev. 3)

Report Date: 06/11/2010 Topic Notes DESCRIPTION JUSTIFICATION REVIEWER COMMENTS Notes See Attached in sharepoint.

See Attached in sharepoint.

Owners comments:

14" Table Interaction 186 should be interaction 188. Tthe remainder of data stay the same for the line item.

16" Table One interaction needs to be added (it will be bounded by interaction 15)

No 115 Unit 2

Elev 695 Row B Column 14 HE Line 20-2CD-7 [40]

NPS 20 ID 19.25 Wall Thickness 0.375 Area (InA2)291 Crack Size 1.80 Target ID 16-2CL-9 [32]

Sch 30 Thickness 0.375 Distance 6"

Operating Pressure of 20-2CD-7 = 420 psig 24" Table Interaction 20a needs to be added. The data is identical to Interaction 20.

The above comments were incorporated.

Interaction 151 was requested to be assessed. However, the results were not coming out favorably.

AES was requested not to pursue this piping interaction further as it was acknowledged that the interaction was not possible based upon field walkdowns.

Cross References XRef Number Sub Status Date Reference DescriDtion AR 01178236 APPROVED 04/15/2009 No HELB flooding calculation for Turbine Building Affected Documents Milestone Milestone APPROVED BY Pedigree Information Date 06/10/2010 ID BRSM05 Name Brossart, Mark A Req By APPROVED Page 2 of 4

XcelEnergy" EC-0441 EC Closeout Package Report (Rev. 3)

Report Date: 06111/2010 Milestone Milestone CLOSE PRE JOB BRI PREPARED (E Date ID Name Notes: Suitability review performed by a qualified individual and attached in Sharpoint. Comments listed in Topic Notes were incorporated. EC is approved.

06/10/2010 LDWHIP01 Whipple, Linda D Notes:

EF 06/10/2010 PTTD06 Potter, David J Notes:

EVL) 06/10/2010 PTTD06 Potter, David J Req By CLOSED H/APPR Notes:

Document Referencei Facilty Doc-Type PI EC Sub-Type Doc #

0000016275 Sheet Rev Minor Rev Date 000 06/10/2010 Pedigree Information Page 3 of 4

XcelEnergy-EC-0441 EC Closeout Package Report (Rev. 3)

Report Date: 06/11/2010 Pedigree Information Page 4 of 4

QF-0547 (FP-E-MOD-1 1) Rev. 2 Paae 1 of I QF-0547 (FP-E-MOD-11) Rev. 2 Paae I of I

&XcelEnergy-External Design Document Suitability Review Checklist External Design Document Being Reviewed:Engineering Evaluation Title-Technical Backup for Turbine Building HELB Screening Evaluation Number:

PI-996-83-S01 Rev:

1 Date:

6/10/10 This design document was received from:

Organization Name: AES POor DIA

Reference:

EC16275 The purpose of the suitability review Is to ensure that a calculation, analysis or other design document provided by an External Design Organization complies with the conditions of the purchase order and/or Design Interface Agreement (DIA) and is appropriate for Its Intended use. The suitability review does not serve as an Independent verification. Independent verification of the design document supplied by the External Design Organization should be evident In the document, if required.

The reviewer should use the criteria below as a guide to assess the overall quality, completeness and usefulness of the design document. The reviewer is not required to check calculations In detail.

REVIEW

1.

Design inputs correspond to those that were transmitted to the External Design Organization.

2.

Assumptions are described and reasonable.

3.

Applicable codes, standards and regulations are identified and met.

4.

Applicable construction and operating experience is considered.

5.

Applicable structure(s), system(s), and component(s) are listed.

6.

Formulae and equations are documented. Unusual symbols are defined.

7.

Acceptance criteria are identified, adequate and satisfied.

8.

Results are reasonable compared to inputs.

9.

Source documents are referenced.

10.

The document is appropriate for its intended use.

11.

The document complies with the terms of the Purchase Order and/or DIA.

12.

Inputs, assumptions, outputs, etc. which could affect plant operation are enforced by adequate procedural controls. List any affected procedures.

13.

Plant impact has been identified and either implemented or controlled. (e.g., For piping analyses, the piping and support database is updated or a tracking item has been initiated.)

14.

Design and Operational Margin have been considered and documented.

Reviewed El NIA El Ii El El El ElEz El El El El Z

Completed by:

David Potter Date: 6/10/2010 ji Form retained In accordance with record retention schedule identified In FP-G-RM-01.

Automated

/'

Engineering Calculation Package Page 1

of 39 z ~

Services Corp.

Calculation Number:

PI-996-83-SO 1 Calculation

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Client:

XCEL Energy Station: PINGP Project Number:

PI-996-83 Unit(s):

Project

Title:

PRA HELB Screening Safety Related Yes No [

Revision Affected Pages Revision Description Approval Signature /

Signature / Initials of Date Preparers & Reviewers Prepared by:

0 All Initial Issue A.V. Setlur David DeGrush Reviewed by:

Olof Andersson Prepared by:

1 All Piping interaction tables and associated references revised.

A.V. Setlur David DeGrush 6/10/2010 Reviewed by:

Olof Andersson Form 3.1-10 Rev. I

Automated Engineering, Calculation Package Page 2

of 39 Services Corp.

REVIEWER'S CHECKLIST FOR DESIGN CALCULATIONS SHEET 1 of 2 STATION:

PINGP NUCLEAR SAFETY RELATED: YES [] NO Z PROJECT NO:

PI-996-83 CLIENT:

NMC, LLC CALCULATION TITLE: Technical Backup for Turbine Building HELB Screening Evaluation CALC. NO:

PI-996-83-SO 1 CALC. REV. NO:

I INDICATE THE DESIGN INPUT DOCUMENTS USED:

TYPE OF DOCUMENT DOCUMENT ID, REV AND/OR DATE YES N/A COMMENT

1. General Design Basis Ref. 1 - 11 X
2.

System Description

X

3. Design information package x

from related equipment vendor

4. Electrical Discipline Input X
5.

Mechanical Discipline X

Input

6.

Control Systems Discipline x

Input

7. Structural Discipline Input x
8.

Specifications X

9.

Vendor Drawings X

10.

Design Standards Ref. 9 X

11. Client Standards x
12. Checked Calculations Ref. 1, 7 X
13. Other (specify)

X PREPARER'S SIGNATURE:

D. DeGrush DATE: 6/10/20 10 REVIEWER'S SIGNATURE:

(LL

0. Andersson DATE: 6/10/20 10 APPROVER'S SIGNATURE:

A.V. Setlur DATE : 6/10/2010 Form 3.1-4 Rev. 3

Automated Engineering Calculation Package Page 3

of 39 SkmServices Corp.

REVIEWER'S CHECKLIST FOR DESIGN CALCULATIONS SHEET 2 of 2 PROJECT NO:

CALC. NO:

PI-996-83 PI1-996-X3-S1;0 REVIEWER TO COMPLETE THE FOLLOWING ITEMS:

COMMENT

1. Has the purpose of the calculation been clearly stated?

2..

Have the applicable codes, standards and regulatory requirements been:

A. Properly Identified?

B. Properly Applied?

3. Were the inputs correctly selected and used?
4.

A. Was Design Input Log used?

B. If 4A is No, provide Manager's signature in Comment column to signify approval of Design Input Documents used in the calculation.

5. Are necessary assumptions adequately stated?
6. Are the assumptions reasonable?
7. Was the calculation methodology appropriate?
8. Are symbols and abbreviations adequately identified?
9. Are the calculations:

A. Neat?

B. Legible?

C. Easy to follow?

D. Presented in logical order?

E. Preparedin proper format?

10. Is the output reasonable compared to the inputs?
11. If a computer program was used:

A. Is the program listed on the ASL and has the SRN been reviewed for any program use limitations?

B. Have existing user notices and/or error reports for the production version been reviewed as appropriate?

C. Were codes properly verified?

D. Were they appropriate for the application?

E. Were they correctly used:

F. Was data input correct?

G. Is the computer program and revision identified?

I.

LS-DYNA Form 3.1-4 Rev. 3

Automated Engineering Zn Services Corp T

e: 4 of 39 Calc. No.: PI-996-83-S01 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 Section 1.

2.

3.

4.

5.

6.

7.

8.

9.

TABLE OF CONTENTS n

Page P u rp o se.......................................................................................................................................

5 M eth od o logy..............................................................................................................................

5 Acceptance Criteria.............................................................................................................

6 A ssum ption s.............................................................................................................................

7 D esign Inp uts............................................................................................................................

8 A n aly sis...................................................................................................................................

13 S u m m ary..................................................................

3 8 Conclusions.......................................................................................... 38 References................................................................................................ 39 Form 3.1-3 Rev. 2

~~

Automated Engineering I.U Services Corp Page: 5 of 39 Calc. No.: PI-996-83-SO 1 Revision: I Client: Xcel Energy Nuclear Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 1.0 Purpose/Objective The purpose of this calculation is to perform analysis of pipe-on-pipe impact interactions using finite element simulation. The objective is to quantify the effect of impact of the projectile pipe on a target pipe. The anaylsis will evaluate the impact of specific postulated interactions at the Prairie Island Nuclear Generating Plant (PINGP).

2.0 Methodology Analytical models of two pipe interactions (collisions) are prepared using the Finite Element Simulation code LS-DYNA. The models were comprised of a projectile or moving pipe and a stationary Target Pipe. The physical scenario being analyzed is a postulated catastropic failure occurring in a pressurized piping system producing a projectile pipe which ultimately impacts a stationary or target pipe. The damaged caused by the projectile pipe to the target pipe is evaluated using the finite element code.

The analyses are performed on actual pipe to pipe interactions pairs identified via plant walkdown at PINGP.

Engineering evaluations using key parameters identified the specific bounding interaction pairs for each target pipe size. These bounding interactions were modeled to determine the extent of the damage caused by a postulated collision. If the resulting damage for these limiting cases is shown to be acceptable then any damage resulting from the other interactions can be assumed to fall within acceptable limits.

This calculation is classified as Non-Safety Related since it does not result in a design document. The inputs were based upon reasonable and, where possible, conservative values which produced generally conservative results.

Software MathCad software is used to generate this calculation. All MathCad calculations are independently verified for accuracy and correctness as if they were manually generated.

LS-DYNA is used to analyze the pipe to pipe interactions. LS-DYNA is a general purpose explicit/implicit finite element code used to analyze the nonlinear dynamic response of three-dimensional and two-dimensional inelastic structures. Its fully automated contact analysis capability and error checking features have enable users in various industries worldwide to successfully solve many complex crash, forming and other problems. Previously LS-DYNA has been used successfully to analytically model actual experimental pipe to pipe interactions (Ref. 6) which makes it an ideal tool for this analysis. LS-DYNA is not on the AES Approved Software List but it has been used extensively in the industry for non-linear analyses.

As such its use is acceptable for this non-safety related application.

Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

A Automated Engineering Services Corp

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Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 3.0 Acceptance Criteria This analysis will be utilized to provide technical backup to support an evaluation which attempts to screen postulated HELB piping interactions within the Turbine Building. The interactions will be screened as those which could significantly contribute to flooding and those that will not. Previous Probabalistic Risk Assessment (PRA) has concluded that leakage flows within the turbine building less than 5000 gpm do not pose a significant threat to plant design basis operation (Ref. 1).

Analysis has shown that 5000 gpm would exceed the expected flowrate through a 4" diameter pipe at system operating pressures of approximately 100 psig which is roughly that of a service water or fire protection system (Ref. 2). The cross sectional flow area of a 4" pipe is approximately 12.7 in2. Therefore a non-threatening pipe interaction will be that considered to cause no more than a 12.7 in2 opening in the target pipe.

Form 3.1-3 Rev. 2

Automated Page: 7 of 39 Engineering CALCULATION SHEET J/J Services Corp Caic. No.: PI-996-83-SO1 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Caic.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 4.0 Assumptions

1. Only orthogonal perpendicular pipe interactions are considered due to their bounding nature based upon previous testing and analysis. (Ref. 5). Any departure from perpendicularity between the plane of motion of the projectile pipe and the axis of the target pipe would have resulted in a lesser component of the maximum impact force between the pipes.
2. A conservative length of 15 ft is arbitrarily chosen for the projectile pipe to maximize impact forces. The longer the projectile pipe the larger the moment formed about the rotation hinge and thus the greater the impact force. Based upon typical piping geometries, support spacing and general clearances within the plant it is not reasonable to assume projectile pipe lengths longer than 15 ft could occur and move freely without interference from other structures.
3. The theoretical impact point on the projectile pipe is chosen as 10 ft from the fixed base to maximize imparted energy to the target pipe. Previous testing has shown that maximum damage will occur when the impact occurs from 50 to 75% length of the projectile pipe from the hinge Ref.(6). In the event that the plastic hinge forms away from the base the impact zone should fall within this range on the Projectile Pipe.
4. The impact point on the Target pipe is conservatively chosen at the midpoint of the span which maximizes the imparted forces to the pipe. (Ref. 5)
5. The intact end of the projectile pipe is conservatively modeled as rigidly supported (fixed) to maximize impact forces to the Target Pipe. A lesser boundary condition would allow the intact end to deflect or move away from the projected impact and thus reducing the severity of the impact.
6. The blowdown force is assumed to always act perpendicular to the axis of the Projectile pipe. This will maximize the rotational moment of the Projectile pipe, increasing the angular velocity and maximizing the impact force.
7. The length of the Target pipe is reasonably chosen as 1/2 the recommended maximum spacing between piping supports as specified in ASME B31.1 piping code, Table 121.1.4.(Ref. 9) Piping support spacing can vary somewhat throughout the plant and between plants but this is a reasonable input based upon actual field installations.
8. Both pipes are modeled as filled with water. The greater mass will increase the impact energy and maximize the impact result.
9. Material properties for Al 06 Grade B Carbon Steel are assumed for both pipes.
10. The identical True Stress-Strain curve at elevated temperature is used for both pipes which is conservative due to the fact that the Target pipe is actually at lower temperature which would increase the material strength of this pipe.
11. The intemal pressure in both pipes is conservatively assumed to be atmospheric.
12. Failure will occur at 25% Strain. (Ref. 8)

Form 3.1-3 Rev. 2

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Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes -

HI Date: 6/10/2010 5.0 Design Inputs 5.1 Material Properties The following true stress-strain curve is used for both pipes (Ref 3).

l-'Enig" Eng.

True [--iie Strain I Stress strain Stress 0.0 10 4.29E+*04j...........

00010 42965r 0.0020 1 4.39E+04 0.00201 44023 0.0025*

4.42E+04 0.0025 1443261 0.0050 ]4.45E+04 0.0050

'44766-1 0075 44E+4 0 0075 45247 0.0100 1 4.56E+04 0.0100 46008 0-12Y5 4.60E+04 0.0124--! 46585 0.0150 4.64E+04 0.0149 47053 0.0175 4.66E+04 0.0173 47374 0-d-.0-200 4-75E+04 0T18j48427 0.0225 0.0400 0-b.0450 0.0500 0.0750 4.91 E+04 -

5ý.0_7E+04b 5.29E+04 5.4 9E +04 5.67E+04 5ý.82E+04 6.42E+04 0.0223 0.0247 0.0296 0.0392

0. 0488 0.0723 50232 516822 608 19

-0gg IV 62746 68969 0.1000 16.67E+04!

0.0953 73395 1 0.1250 6.85ýE_+04t 78 j77027 0.1500 6,92E+04 0.1398 79578 0.2000 6.97E+04 0.1823 83587 0.28406.97E+04 i0.2500 89438 lbf Density for Carbon Steel per Reference [23] : pCS:= 0.283

.n3 inl Form 3.1-3 Rev. 2

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9 6of 39 ZJ/IJZU Services Corp Caic. No.: PI-996-83-S01 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 5.2 Pipe Properties Target Pipe sizes considered in this evaluation are as follows (Ref. 7) 14 in Sch.XS, 14 in OD, 0.5 in wall thickness, 16 in Sch 30, 16 in. OD, 0.375 in wall thickness, 24 in Sch 20, 24 in. OD, 0.375 in wall thickness, Projectile Pipe sizes considered (Ref. 7) 8 in Sch 80, 8.625 in OD, 0.5 in wall thickness, 12in Std Sch., 12.75 in OD, 0.375 in wall thickness, 16 in Sch 30 (data given above for Target Pipe) 20 in Sch 20, 20 in OD, 0.375 in wall thickness, Target Pipe spans: 1/2 suggested max. span in ASME B31.1, Table 121.1.4 (Ref. 9) 14" pipe = 12.5 ft 16" pipe = 13.5 ft 24" pipe = 16 ft Six bounding pipe interaction cases are identified in Section 6.1

5. Projectile Pipe Parameters for Interaction Pairs (Ref. 7)

Outer Diameter Dp.° Wall Thickness t :=

8.625 12.75 16 20 16 20 in Case 1 - Interaction 186/190 Case 2 - Interaction 191 Case 3 - Interaction 15 Case 4 - Interaction 19/109 Case 5 - Interaction 20/123 Case 6 - Interaction 48 "0.500" 0.375 0.375 0.375 0.375 10.375) in Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 Inner Diameter Dp~i:= Dp.o - 2tp Operating Pressure in Projectile Pipe (Ref. 7)

Mass of Pipe (Ref. 11)

Mass of Water Inside Pipe (Ref. 11)

Dp i =

Pp :=

mp.p :

7.625 12.000 15.250 19.250 15.250 19.250 "685" 420 420 420psi 420 420 "43.4' 49.6 62.6 lb 78.6 ft 62.6

ý78.6) 19.8 49.0 79.1 125.7 i

79.1 1125.7) 63.2 98.6 141.7 lb 204.3 ft 141.7 1204.3) n m p.w :

b I

Total Mass of Pipe mp=

m P =M.

+ M P-Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

Automated Page: 11 of 39 Engineering CALCULATION SHEET L

Services Corp Calc. No.: PI-996-83-SO1 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Caic.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D]

Date: 6/10/2010 Inner Cross-Sectional Area of Pipe D*2 4T'D p.i A '"- 4 45.7 113.1 182.7 ApI=

291.0 182.7 291.0)

L lp

= 15ft

.2 "11n Length of Projectile Pipe (Assumption #2)

Theoretical Position of Impact on Projectile Pipe from hinge assuming Ideal hinge (Assumption #3)

Target Pipe Parameters for specific interaction pairs (Ref. 7)

Outer Diameter Ip := loft Dt.o r14")

14 16 16 24

,24)

"0.500" 0.500 0.375 0.375 0.375 0.375) in in Wall Thickness tt :=

Inner Diameter Dt~i:

Dt.0 - 2tt Dt.i =

13.00 13.00 15.25 15.25 23.25 23.25)

-in Form 3.1-3 Rev. 2

Automated Page: 12 of 39 Engineering CALCULATION SHEET Pa12 of 39 l/

Z Services Corp Caic. No.: P1-996-83-S01 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D N]

Date: 6/10/2010 Mass of Pipe (Ref. 11)

Mass of Water Inside Pipe (Ref. 11) mt.p :=

72.1 72.1 62.6 Ii 62.6 f

94.6 194.6 57.5 57.5 79.1 79.1 184.0

,184.0) b mt.w :=

lb ft Total Mass of Pipe Inner Cross-Sectional Area of Pipe mt := mt.w + mt p t r.Dtji t' '- 4 m t=

At.,=

129.6 129.6 141.7 lb 141.7 ft 278.6 278.6) 132.7' 132.7 182.7 182.7 424.6 424.6/

2 Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

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Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D

'Date: 6/10/2010 6.0 ANALYSIS 6.1 Modeling Discussion The model considers only orthogonal / perpendicular pipe interactions based upon previous studies (Ref. 5).

Both pipes were modeled as cylinders containing water. The water itself was not specifically modeled but the water in the pipes were included in the model as a non-participating structural mass. Which is to say the water mass is evenly distributed about the structure but does not alter the material or dimensional properties of the pipes. The pipes were modeled with ASTM A106 Grade B Carbon Steel material properties.

The target pipe was modeled as a span of pipe supported at each end. At both ends the pipe was constrained axially (X direction) via a rigid spring. The pipe was rigidly supported from translational motion in the directions perpendicular to the pipe axis (Y-Z). Rotationally, the target pipe was allowed some movement about all axes via rotational springs. The length of the target pipe is based upon recommended B31.1 maximum support spacing as detailed in Assumption #7..

The catastrophic failure of the moving pipe produces a jet force at the failed end which produces a moment arm and causes the pipe to rotate about a plastic hinge. This moment arm is conservatively assumed to be 15 ft in length and based upon previous testing (Ref. 2) is assumed to contact the target pipe 10 ft from the plastic hinge. The pipe rotates in a plane perpendicular to the axis of the target pipe and impacts the target pipe in a perfect "cross" blow at some point in its travel. The jet or blowdown force acting on the broken end of the moving pipe is determined via the equation Fbd = 1.2 x Pop x Acs where Pop is the line operating pressure and ACS = Pipe Cross Sectional Area. (Ref 10)

The actual Blowdown Force acting on ProjectilePipe for the bounding interaction cases are as follows:

/I 3.8 x 104 5.7 x 104 9.2 x 104 1.5 x 105 Blowdown force I

F P := (1.2PP-Ap.1)

Fp=

-lbf 9.2 x 104 1.5 x 10 5 Form 3.1-3 Rev. 2

Automated Page: 14 of 39 Engineering CALCULATION SHEET Page: 1of 39 Services Corp Calc. No.: P1-996-83-SO1 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes El

]

Date: 6/10/2010 Two modeling scenarios were considered for the projectile pipe. In the first scenario at time = 0 the moving pipe was modelled just contacting the target pipe with a calculated angular velocity. The initial velocity was calculated assuming the projectile pipe rotates about a purely plastic hinge which offers no rotational resistance. The hinged end is constrained from any translational movement or rotation about any other axis.

This scenario was much to conservative and too limiting when considering larger diameter moving pipes.

Reference 5 addresses this modelling scenario as completely theoretical and not being a credible "real-life" piping system behavior.

A more realistic modelling approach was possible due to the capabilities of the LS-DYNA software. This software allowed the entire actual event to be modelled rather just a portion which used theoretical, ideal initial conditions as inputs. Specifically the model was made using actual bounding orientations of Target pipe vs Projectile pipe interactions as obtained from Reference 7. At t =0 an instantaneous force was applied to the stationary projectile pipe simulating the blowdown force due to a pipe break. The other end of the projectile pipe was constrained as would be the case in an actual piping system. The model calculated the formation of the actual plastic hinge in the projectile or moving pipe rather than assuming an ideal actual hinge at an assumed location. As this hinge formed the projectile pipe rotates via the blowdown force and contacts the Target pipe.

The software then determines the deformation and the residual damage to both pipes at the conclusion of the event.

Velocity at impact was determined using actual separation distances determined for specific interaction pairs considered from Reference 7. The interaction pairs could be categoried in two general groups, those where the moving pipe is thinner than the target pipe and those where the two pipe thickness are equal and the target pipe thickness to diameter ratio is less than 0.065. Additionally the interaction pairs contain only 3 distinct target pipe sizes, 24 inch, schedule 20; 16 inch, schedule 30 and 14 inch, schedule xs pipe.

Form 3.1-3 Rev. 2

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Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Dl

[N]

Date: 6/10/2010 6.2 Determination of Bounding Cases Reference 7 identifies all of the applicable pipe interactions for the Turbine Building area where the projectile pipe thickness is either equal to or less than the target pipe thickness. From these interaction cases several critical cases were selected for detailed analysis. The interaction cases are summarize in tables in this section for all the interaction pairs for the respective target pipe sizes. The bounding interactions are highlighted in yellow. The bounding interactions were mostly identified using engineering judgement / logic by comparing critical parameters such as separation distance, operating pressure, size of target vs moving pipe and relative thickness of each pipe.

In cases where these parameters did not clearly differentiate the interaction a calculation of the theoretical impact momentum was performed to allow relative comparison of impact severity between specific pipe interactions. The higher the momentum of the projectile pipe, the higher the potential for damage to the target pipe. The method for calculating the theoretical impact momentum of the projectile pipe is shown below (the calculation is theoretical because the moving pipe is assumed to rotate about a pinned connection located at the end of the pipe with no resistance to rotation):

i M

I P

L p

.I Moment at plastic hinge assuming moving pipe has pinned connection (no resistance to rotation)

Moment of Inertia of the rotating pipe From conservation of Energy Solving for angular velocity at impact Where angle of rotation at impact is (see Figure XX for X and Y)

Mp := (FpLp) mn P*L P*L 2 p.-

3 li2 Mt'O = 1' 2'

2 2-M P*0

, Ip 0 asin( X2 27 Velocity at Impact Momentum per unit weight at impact Vp 0.667.L P W PI = m PVp Form 3.1-3 Rev. 2

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Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D lii Date: 6/10/2010 14 inch Target Pipe Inte High Energy 1 Impact pipe Separation Impact Momentum Wall Wall operating Distance

Velocity, per unit wt, raction Pipe ID Sched IID FThckness Target ID Sched Thickness Ipressure (Inches) i ft/sec lbf'sec/tt 8-2HD-8 80 7.625 0.5 14-ZX-161 0.5 685 48 161 190

[41]

[53]

8-2HD-6 80 762 05 14-ZX-161 188

[411

.65

[531 XS [57]

0.5 685 48 161 321 12-2CD-t 0.37 14-ZX-161

-4 4n rAn std 12 0.35 r-,

XS [57]

0.5 420 48 163 501 Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

Automated Page: 17 of 39 Engineering CALCULATION SHEET i//Il Services Corp Calc. No.: PI-996-83-S01 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes DFXI Date: 6/10/2010 16 inch Target Pipe Interaction I Pipe ID 20-CD-7 15

[44]

16-CD-9 19

[44]

16-2CD-9 1 Wall Sched ID

!Thicknessi Target ID 20 19.25 0.375 16-CL-67 2

[30]

16-CL-67 30 15.25 0.375

[30]

[30]

35 16-2CL-9 30 15.25 0.375 1r-,y I

High Energy Separation 1 Impact Wall pipe operating Distance

Velocity, Sched Thickness pressure (Inches)

If/sec 30 0.375 420 16 133 30 0.375 420 36 158 30 0.375 420.

36 158 Impact

Momentum, lbftsec/ft 846 697 697 24 inch Target Pipe Interaction 123 20 20a AR Pipe ID 1 Sc 20-2CD-7 2

[40]

20-CD-7 2

[44]

20-CD-7 2

[44]

16-CD-10 hed 0

0 0

0 ID 19.25 19.25 19.25 15.25 Wall Thickness Target ID 0375 24-2CL-56

[32]

24-CL-1 10 0.375

[30]

24-CL-110 0.375

[0[30]

24-CL-1 10 0.375 r~ni Sched 20 20 20 20 Wall Thickness 0.375 0.375 0.375 0.375 1 High Energy pipe operating pressure 420 420 420 420 Separation Distance (Inches) 24 24 24 60 Impact

Velocity, ft/sec 155 155 155 201 Impact
Momentum, lbf*sec /ft 1 990 990 990 889 3

Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

//a Automated Engineering Services Corp

,e: 18 of 39 Calc. No.: PI-996-83-SO 1 Client: Xcel Energy Nuclear Revision: I Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 6.3 Determination of Initial Pipe Positions for Specific Controlling Interactions The pipe separation distance (S) was provided in Reference (7). Assumption #2 specifies that the projectile pipe is 15 ft long. Assumption #3 states that the location of theoretical contact was taken at a distance of about 2/3 this length, or 10 ft. Based on these parameters, the elevation of the target pipe or distance Y was determined.

Smaller distances of Y were considered which would increase the angle of rotation at contact, but reduce the moment arm between the hinge and the target pipe. By comparing the impact velocity, it was determined that the worst case was when Y was maximized. This will be further demonstrated at the end of this section when the impact velocities are recalculated using Y = 0 (and thus e = 90 degrees).

Target Pipe S:=

4.0 4.0 3.0 1.333 5.0 2.0 ft Projectile Pipe

/

X:= S + 0.5.(Dp.0 + Dt.0)

S y

V "4.9' 5.1 4.3 X=

2.8 6.7 3.8, ft ft Vertical position of Target Pipe to allow a theoretical impact location of 10 ft on the Projectile Pipe Y:=[ (0ft) 2-X 2 8.7ý 8.6 9.0 9.6 7.5

,9.2 Form 3.1-3 Rev. 2

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Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 Angle of rotation at impact Angular Velocity at Impact Impact Velocity Momentum at Impact per unit pipe weight 0 := asinf X2 y

2(10.ft. w)

MI:= ((mp.Vp) 29.6 30.8 25.7 16.5 41.8

,22.5j 16.2*

16.3 15.8 13.3 20.2 15.6,

  • deg rad sec ft S

-ft-lbf-s ft 2

Vp =

(162 163 158 133 202

  • ,156, 319 500 696 845 888

\\988 MI =

Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

Automated Page: 20 of 39 Engineering CALCULATION SHEET j/jJk Services Corp Calc. No.: P1-996-83-SO1 Client: Xcel Energy Nuclear Revision: 1 Station: Prairie Island Nuclear Generating Station Prepared By: D. DeGrush Calc.

Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D Date: 6/10/2010 Check case for Y=O, and ( = 90 degrees Angle of rotation at impact 02 := 90deg Angular Velocity at Impact Impact Velocity 2.Mp.02

'p Vp2:= (X.w2) 02 = 90.deg 28.3 27.9 29.6 w2 =

31.1 29.6

\\31.1 140 143 128 Vp2 =

88 197

ý119) rad sec ft s

16.2 16.3 15.8 13.3 20.2 15.6 rad see ft s

V p=

162 163 158 133 202 156)

As demonstrated, although the angular velocity is greater when the Y distance is taken as zero (i.e., hinge forms right at the same height as the target pipe), due to the smaller moment arm, the impact velocity is less for this case. Therefore maximizing the Y distance produces a higher impact velocity, and therefore a higher potential for damage to the target pipe. Also note that this analysis does not consider the effect of reduced blowdown flow due to the reduced cross-sectional area at the hinge or buckling location in the projectile pipe, and the corresponding force reduction associated with large values of 0 (see Section 6.5 for additional discussion).

Form 3.1-3 Rev. 2

Automated Page: 21 of 39 Engineering CALCULATION SHEET j

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Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 6.4 Boundary Conditions The boundary conditions for both the target pipe and the projectile pipe need to be established to provide a realistic approximation of the actual configuration. Certain assumptions have been made for the length of the target pipe, and the relative location of the contact point along the length of the projectile pipe as discussed in Section 6.3. The boundary conditions for both the projectile pipe and the target pipe will be discussed in this section.

The boundary conditions for the projectile pipe are fairly simple. At the break location, the projectile pipe is conservatively considered free to displace based on the assumption of a full cross section guillotine break. A force is applied at the end of the projectile pipe perpendicular to the pipe axis. In order to preserve the integrity of the model behavior, a reinforcing ring is added to the model on the end of the projectile pipe where the load is applied to facilitate even load distribution to the model elements around the end of the pipe ensuring there is no localized deformation there. As it pertains to the real life situation, it is assumed there is a 90 degree elbow at the top of the break which is causing the whipping force. Note that the elbow was not modelled in LS-DYNA to simplify the modeling effort. The use of the rigid ring on the free end of the pipe is conservative in comparison to actually modelling the elbow in LS-DYNA.

At the opposite end the projectile is fixed as an anchor. This end condition is conservative from the perspective that it will not allow deflection or displacement of the projectile pipe at this location up to and through pipe impact thus maximizing imparted energy to the target pipe. As can be seen from the results in Section 6.6, a plastic hing forms in the moving pipe at some distance above the fixed end of the moving pipe (approximately 1 to 2 diameters above the fixed point location. The consequential damage that occurs in the projectile pipe below the hinge point is not relevant to this investigation.

The boundary conditions placed upon the target pipe are more sophisticated and indicative of the remainder of the piping system which brackets the target pipe on each end. A single span of the target pipe was considered. In order to account for the continuation of the pipe, spring restraints were used on both ends of the target pipe. Parametric runs were made (see Section 6.7) that confirmed that the smaller the stiffness values of these springs, the higher the potential for damage to the target pipe. Conservatively low spring stiffnesses were used based on relatively long unsupported spans of the target pipe. Since the target pipes are non-safety, non-seismic, it is conservatively assumed that the pipe is mostly supported by spring or rod hangers with very few lateral supports. A conservative support scheme was used to calculate representative stiffnesses as shown on the next page.

Evaluation has shown that damage results are sensitive to the span of the target pipe between supports. The degree of sensitivity depends upon a number of key factors including relative pipe thickness to each other, magnitude of the blowdown force, initial separation distance, etc. Parametric runs performed in Section 6.7 indicate that for the case where only the angular velocity is considered, a shorter pipe span produces the most conservative results. However, for cases where the jet force continues to be applied after the initial contact with the pipe, the longer the span the worse the damage to the target pipe. For this evaluation a reasonable support span of 1/2 the maximum recommended per ASME B31.1 was utilized.

Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

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././4Z//-

40 ft 40 ft I

Lt 40 ft

-I T T1 40 ft 40 ft spans are considered in two directions on either side of the supports in the target pipe impact zone. At the ends the pipe is considered fixed assuming it terminates into some piece of equipment or anchor at a wall penetration. These spans are considered conservatively large. Using these spanse stiffness values are considered for the target pipe so it can be modelled as shown below:

Form 3.1-3 Rev. 2

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Date: 6/10/2010 KI K2 KI The axial stiffness is based on a simple cantilever bending of a 40 ft cantileved pipe as shown in the figure below

-/14///

40 ft K3E L:= 40.ft L483.8 I:= 562.1 -in4 1942)

E:= 27.9.10 6psi (Ref 9) 14" XS 16" Sch. 30 20" Sch. 20 366

  • 3.E.I Ibf K I := -

K I =

425

-n-L1470)

Use 500 lb/in for 14" and 16" pipe Use 1000 lb/in for 24" pipe For the rotational springs, the spring stiffness for a unit rotation is 4EI/L for a fixed end, and 3EI/L for a pinned end (Ref. 4). Since the end of the pipe segment has some flexibility due to the next 40 ft leg, use a stiffness of 3.5EI/L to represent a mid point between fixed and pinned.

Form 3.1-3 Rev. 2

7,

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Date: 6/10/2010 11//1, 3.5.E.I K2.

L K2 =

40 ft K-3.5EI L

Use 1 x 108 in-lbf/rad for 14" and 16" pipe Use 2 x 108 in-Ibf/rad for 24" pipe ZN Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

A'.

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 6.5 Jet Force Time History As the projectile pipe rotates about a plastic hinge, the cross-sectional area of the pipe is reduced. This occurs at two locations; at the hinge where the pipe buckles and at the impact location as the projectile pipe tends to wrap around the target pipe. As the pipe cross-sectional area is reduced there is a corresponding reduction in the blowdown flow from the pipe. This reduces the whipping force on the pipe as the pipe continues to deform.

Following impact, as the collision continues, and both pipes deform, the flow is eventually reduced to zero at the point where the projectile pipe basically seals itself off and the blowdown force is gone.

To account for this force reduction, the LS-DYNA runs were used to estimate the reduced cross sectional areas at both the plastic hinge, and at the impact location. Data was taken from preliminary runs to determine the reduced area at the deformed cross sections at specific times during the event. Using this data, more realistic force functions were utilized in the Case runs by applying a force time history based on a linear reduction in the area.

Conservatively, for most cases only the reduction of area at the collision point was considered. In one case, the reduction in the area at the moving pipe hinge location was also considered (for Case 5 where the separation distance was larger resulting in a large rotation in the moving pipe prior to impact. The shape of the force time history curve is shown below:

Typical Force Time History (Cases 2-4 and 6) t I time of impact t2 = time projectile pipe blowdown flow = 0 Force 0

tI It2 Time Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D HI Date: 6/10/2010 For Case 5, since the angle of rotation of the moving pipe was large, a two step force time history was used to account for the flow reduction at the plastic hinge.

Force Time History for Case 5 Fp t

= time moving pipe hinge begins to significantly kink

- - - -t 2 time of impact SI t 3 = time projectile pipe Iblowdown flow = 0 Force I

oo w

0 tt II t2 t 3 Time Form 3.1-3 Rev. 2

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Title:

Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 6.6 Analysis Results Six specific interaction cases were run as described in the sections above. A table summarizing the input parameters for these six load cases is provided below:

I Targt Ppe oimnbry MyigPp Bwr~t I

___Conditions ConQditins Target Target Proectile ProjectiI Target d.taoL seaai' L

Srn, Spig~ Supi~ed Fe n

eLlotre Pipe M1t, Pipe, 01) e Pipe, t, Spft I

o elevatiort End re n eu~otn Case 0Q n i

n in ft dstne ft lin ae)steps, rme-c Case1 14 G5 a625 Q5 125 4

49 a7 5M 100 E

xed F =37,5001bs No Case2 14 05 1275 0375 125 4

51 86 5M IOEB Fxed F=57,(X0bsI t1=64Kt 2=81 CGe3 16 Q375 16 0375 135 3

4,333 9

5M 1.OES Axed F=92,1W1bs t1=5Zt 2=72 Case4 16 Q375

2) 0375 135 1333 28 96 500 I0EN Fxed F=147,0C01bs ti=3Zt 2=E2 tl=5, t2=ff, t3 Case5 24 0375 16 03"75 16 5

66 7.5 100 ZOE8 Fixed F=92IBllbs Case6 24 0375 2M 0375 16 2

38 92 Ma I 2-0E8 Axed I F=147,00Dtlbs t=40,t 2=70

'1. 5N. Iinearforce redLuidon 55to E9rnecLbased upon Y/oreduc-tion in Proiectle Pipe Secdcn in buddirg zone at antact Results for these six analysis cases are provided in the sections below:

Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes DI'l]

Date: 6/10/2010 6.6.1 Case 1 (Interaction 188/190) - 14" XS Target Pipe, 8" XS Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.065 msec (Initiation of contact) t = 0.077 msec (Projectile Pipe Blowdown = 0) t= 0.087 msec (Continued deformation) t = 0.100 msec (Conclusion of event)

The results of the analysis show that no elements exceeded the strain limit of 25%. Therefore it is concluded that the interaction of the moving pipe with the target pipe will not create sufficient damage to the target pipe to add to the Turbine Building flooding concern.

Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes 11 N

Date: 6/10/2010 6.6.2 Case 2 (Interaction 190) - 14" XS Target Pipe, 12" Std Proiectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.064 msec (Initiation of contact) t = 0.081 msec (Projectile Pipe Blowdown Flow = 0) t= 0.096 msec (Continued deformation) t = 0.124 msec (Conclusion of event)

The results of the analysis show that no elements exceeded the strain limit of 25%. Therefore it is concluded that the interaction of the moving pipe with the target pipe will not create sufficient damage to the target pipe to add to the Turbine Building flooding concern.

Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes j J Date: 6/10/2010 6.6.3 Case 3 (Interaction 15) - 16" Sch. 30 Target Pipe, 16" Sch. 30 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.052 msec (Initiation of contact) t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation) t = 0.125 msec (Conclusion of event)

The results of the analysis show that 5 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 7.0 in2. Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.

Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes l i Date: 6/10/2010 6.6.4 Case 4 (Interaction 19/109) - 16" Sch. 30 Tar-et Pipe. 20" Sch. 20 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.032 msec (Initiation of contact) t = 0.062 msec (Projectile Pipe Blowdown Flow = 0) t= 0.082 msec (Continued deformation) t = 0.125 msec (Conclusion of event)

The results of the analysis show that 3 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 4.2 in2. Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.

Form 3.1-3 Rev. 2

/

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 6.6.5 Case 5 (Interaction 20/20a/123) - 24" Sch. 20 Target Pipe, 16" Sch. 30 Progectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.055 msec (Cross-sectional area reduced t = 0.069 msec (Initiation of contact) 25% at hinge) t = 0.087 msec (Projectile Pipe t = 0.119 msec (Conclusion of event)

Blowdown flow = 0)

The results of the analysis show that 4 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 8.4 in2. Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.

Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D

['1 Date: 6/10/2010 6.6.6 Case 6 (Interaction 48) - 24" Sch. 20 Target Pipe, 20" Sch. 20 Projectile Pipe The figure below shows the deformation for both pipes at specific time points throughout the collision event t = 0.040 msec (Initiation of contact) t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.085 msec (Continued deformation) t = 0.109 msec (Conclusion of event)

The results of the analysis show that 2 elements exceeded the strain limit of 25% creating a calculated surface area opening in the Target Pipe of 4.2 in2. Because this pipe area opening is less than the acceptance criteria of 12.7 in2 this piping interaction is not expected to cause adverse Turbine Building flooding.

Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes D N-Date: 6/10/2010 6.7 Parametric Evaluations A few select additional cases were run to determine the impact of altering some of the key input parameters to determine the sensitivity of the results to the variation of these parameters. The results of these parametric runs are included on the following pages:

Form 3.1-3 Rev. 2

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Date: 6/10/2010 Case 7 - Reduce spring stiffness boundary conditions on the targey pipe by a factor of 5 (run on base Case 3 (Interaction 15) - 16" Sch. 30 Tarqet Pipe, 16" Sch. 30 Proiectile Pipe )

The results of this run confirmed that reducing the stiffness of the springs resulted in additional damage to the target pipe. Comparison of the screen shots below to those of the Base Case it is apparent that the lighter spring forces result in much more target pipe deformation. Since the stiffness used already represent lower bound values, the results from Cases 1 - 6 are still bounding. There is no need to make additional runs with stiffer springs as this will result in less damage to the target pipe.

t = 0.052 msec (Initiation of contact) t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation) t = 0.125 msec (Conclusion of event)

Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes

[K]

Date: 6/10/2010 Case 8 - Increase support span on target pipe by a factor of 2 (run on base Case 3 (Interaction 15) - 16" Sch. 30 Target Pipe, 16" Sch. 30 Projectile Pipe )

t = 0.052 msec (Initiation of contact) t = 0.072 msec (Projectile Pipe Blowdown Flow = 0) t= 0.088 msec (Continued deformation) t = 0.125 msec (Conclusion of event)

Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2

/,

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes 1 N]

Date: 6/10/2010 Case 9 - Increase support span of target pipe by a factor of 2 (run on base Case 2 (Interaction 190) - 14" XS Target Pipe, 12" Std Projectile Pipe) t = 0.065 msec (Initiation of contact) t = 0.081 msec (Projectile pipe Blowdown flow = 0) t= 0.096 msec (Continued deformation) t = 0.134 msec (Conclusion of event)

The results of the analyses for Cases 8 and 9 show that the damage to the Target Pipe did increase over that observed for the respective base cases but to relatively different extents. For Case 9, similar to Base Case 2, no elements exceeded the strain limit of 25% and the increase in damage was minimal. Case 8 showed appreciably more damage than it's Base Case 3 counterpart in that 13 elements were deleted compared to 5 in the base case. The conclusion is that the impact of increasing the target pipe length is significantly dependent upon other key parameters such as relative pipe thickness, initial separation distances, blowdown force, etc.

Form 3.1-3 Rev. 2

/,

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[

Date: 6/10/2010 7.0 Summary Actual Turbine Building pipe to pipe interactions were evaluated resulting in a set of bounding interactions. Detailed Finite Element models were prepared for each of these bounding cases. The parameters for each of the bounding cases evaluated are provided in the table below.

Target

Pipe, 00, in Target Wall t, in Projectile Pipe, OD, in Projecti I e Pipe, t, in Target Span, ft Separation
Distance, ft Blowdown Force on Projectile Pipe Numberof Failed Elements in Model
Element, Ae Failed Pipe Surface Area Opening, in'2 Case Case 1 14 0.5 8.625 0.5 12.5 4

F= 37,500 1bs None 1.22 0

Case 2 14 0.5 12.75 0.375 12.5 4

F = 57,000 1bs None 1.22 0

Case 3 16 0.375 16 0.375 13.5 3

F = 92,100lbs 5

1.4 7.00 Case 4 16 0.375 20 0.375 13.5 1.333 F = 147,000 1bs 3

1.4 4.20 Case 5 24 0.375 16 0.375 16 5

F =92,100lbs 4

2.09 8.36 Case 6 24 0.375 20 0.375 16 2

F = 147,000 1bs 2

2.09 4.18 Parametric investigations were performed for a few key modeling parameters. The results show that a Target Pipe boundary condition with lower (lighter) spring constants tend to result in more damage to the Target Pipe.

Physically the lower spring constants would represent a piping system with less support / less restraint.

Another parameter investigated was the length of the Target Pipe span (distance of Target Pipe Support separation). The results show that for impacts with no sustained force on the Projectile Pipe that shorter Target Pipe spans are more conservative, i.e. more resultant damage to the Target Pipe. Conversely, for impacts which include a blowdown force on the Projectile Pipe the longer Target Pipe spans result in more Target Pipe damage.

The sensitivity to each parameter variation is individual to each specific interation pair as it depends on a number of key interaction parameters such as relative thickness of the two pipes, blowdown force, initial separation of the two pipes, etc.

8.0 Conclusions The results of the analyses, included in the table above, show clearly that none of the cases would produce an excessive flooding event within the Turbine Building.

Form 3.1-3 Rev. 2

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Technical Backup for Turbine Building HELB Screening Evaluation Reviewed By: 0. Andersson Safety Related Yes Date: 6/10/2010 9.0 References The following references were reviewed and used in the generation of this calculation.

[1]

EC 15656, Rev. 0 dated 3/5/2010 - "EVALUATION OF FLOODING TIMES AND FLOW RATES ASSOCIATED WITH UNIT 1 AND UNIT.2 TB FOR SIGNIFICANCE DETERMINATION"

[2]

EC 16090, Rev.0, dated "In Process" - "TURBINE BUILDING FLOODING SDP: CL TURBINE BUILDING PIPE BREAK ANALYSIS

[3]

US NRC Piping Fracture Mechanics Database (PIFRAC), Version 3.1, from US NRC Pipe Fracture Encyclopedia, 1997."

[4]

Structural Engineering Handbook, Edwin H Gaylord, Jr. / Charles N. Gaylord, McGraw-Hill Book Co., 1968

[5]

NUREG / CR-3231 PNL-5779 Pipe-to-Pipe Impact Program, May 1987

[6]

Experimental Study and Numerical Simulation of Pipe-to-Pipe Impact, International Journal of Impact Engineering, May 2009

[7]

Xcel Energy, NSPM Calculation No: ENG-ME-732 "Determination of HELB / Flooding Interactions in the Turbine Building", Rev. 0, 1/18/2010

[8]

Machine Design Theory and Practice, Deutschman, Michels, Wilson,Macmillan Publishing Co. 1975

[9]

ASME B31.1 - 1989 Edition, Power Piping

[10] Prairie Island Unit 1 Pipe Rupture Analysis Feedwater Piping System, NSC-PIP-M-SLR-9, Rev. 1, August 11, 1972

[11] Crane Technical Paper No. 410, "Flow of Fluids Through Valves, Fittings, and Pipe", 1988 Crane Co.

Form 3.1-3 Rev. 2 Form 3.1-3 Rev. 2