ML20082G715

Feed-Through Adapter Module Assemblies for Amphenol Sams Penetrations

ML20082G715
Person / Time
Site:	LaSalle
Issue date:	11/23/1983
From:	SARGENT & LUNDY, INC.
To:
Shared Package
ML20082G653	List: ML20082G650 ML20082G657 ML20082G667 ML20082G675 ML20082G690 ML20082G698 ML20082G715 ML20082G721
References
CQD-011131, CQD-011131-R0, CQD-11131, CQD-11131-R, NUDOCS 8311300308
Download: ML20082G715 (35)

Text

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SPOJECT NAME: 4./)CM / /E -4 PROJECT NO.:.p26 7-00 RVSOh'N0 g

iw.

1. 'N T 855.P-d /

Reviewed By:

Date:

/

SPEC. NO.:

,q, : l.h-(SiCuature Date: ll-2 3-U C

Review h

(

@ BOP NSSS Approved By:

(sicnature)

V/

Fa/D M Mr<tB OfM a*

M.mLE/1M i~1P w.S Ed //t/f//Y '-

COMPONENT NAME:

C f) M $

(,dE 7/* t' 7/ 6'tv Es

/*

VENDOR / MANUFACTURER:

ar//7X /W'fc / /> r7&/

2 7/2?e:S. <7 7 f.-

7 4' d " ?'75 COMPONENT NO./MODEL NO.:

/

VENDOR'S REPORT NO. AND DATE: MS" "E E'E S'#'l d' #l /^ 'E 7 ""# # # '

'^

' r #-

n/wvc

""t-U / 't! >

/ r p p 7/!Prund s7.MP7& A' /'?c.une t Mc '"!:'/in pr-r>& r,c/17s n /r : /*r: 1c n =v77 = n l-.7i-r 3 l

A.

CONCLUSICN OF REVIEW Accepted ORejected Cocunents :

l B.

CLASSIFICATION AND FUNCTION s

.a f

1.

Classification O Nuclear Safety-Related, Active

{

Nuclear Safety-Related, Past ive O Non-Nuclear Safety-Related E

2.

The component function is

/_m,f s /, din

/,- ;w,!,c c ' - b,. d": '

/

t/

N

?

[

3.

Operability Requirements (Active Components Only) h This component is required to operate:

ed V

During and after postulated dynamic and accident events 4d

&d Only after postulated dynamic and accident events crYA s

v> e N$

AtECH ANI C AL DEPARTMPNT S T,MJp A R D g g o e 5=

2 CHECKLIST FOR DYNAMIC QUALIFICATIO: OF MECHANICAL AND ELECTRICAL EOUIPMENT fur OFFICE USE ONLY - NOT TO BE f

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g,4 r[

lj]g f MAS-CQD-2.4 Page 1

of 9 SENT OUTSIDE OF SARGENT 6 LUNDY gag 8311300308 831128 PDR ADOCK 05000373 P

PDR J

FILE NO.: CQD-0///,3/

REV.: (o

?ROJEC'C NO. : p f /- 027

///3.

C.

Location and Mounting tra 1.

Location i

Building: PsriMARY rMrA rdethr)7~

Elevation:

7 "~ t '- o " TO 7 7 'T '- n '/

2.

Field Mounting Condition

/

O Pane 1/ Pipe /HVAC Duct:

[ Wall / Floor O other:

ri 3.

Mounting Attachment Size:

O solting number:

Material:

Welding Type: AS cnown on AMtWws skis.DwsW 'Joo!+'273 & o.

Welding Leg:

, Length:

, Pitch:

hOther:

vleSY ln b' or wtbed$ ok % "Wll a

D.

METil0D OF QUALIFICATION O static Analysis pTest ODynamicAnalysis O other:

E.

VIBRATION INPUT t

1.

Dynamic Loads considered h Seismic O ityarodynamic

?

Seismic and 11ydrodynamic 4 a a1 O Other:

o.d 2.

Required Frequency Range _:

/ --9 60 //-p E^

Yi c

yt 3.

Required Input _

.o Response Spectra identify):

h$

a) Required response spectra (attach graphs, Sec )~/ G1 /G ?/ M 3 c/ W /r.'I rkds:P !@s, Wo :A /]

~"

s FOR OFFICE USE ONLY - NOT TO BE SARGEijTal.U!JDY MAS-CQD-2.4 2

of 9 SENT OUTSIDE OF SARGENT f,

LUNDY

,sweenas as Page

/

PROJECT NO.: </-26 7 - CD FILE NO.: CQD-d///3/

REV.: (y).

b) Method of combinitig required response spectra:

Absolute Sum SRSS Not applicable

/%

c) Damping Upset / Service Level B Emergency Service Level C

.2 7.

Faulted Service Level D

~

s d) Basis for Damping:

REG,. 6,vs ps /. 6 /

c c 7e uen /773 O Seismic Coef ficients (Required acceleration in each direction) g Upset / Service Level B H

,H y

2 V

Emergency / Service level C H

H y

2

'V Faulted / Service Level D 4.

Is support amplification considered?

Yes ONo

%NotApplicable Comments:

{

5.

Is fatigue considered?

O Yes O No Not applicable

'*^^*"D

^ '"' # "'E''

Comments:

L /7.S A 4- / t:~

F.

QUALIFICATION BY TESTING 1.

Does the Vendor's report indicate that the component is identical to that to be installed?

Yes LJ No - justify similarity:

C a

4 2.

Mounting t,a 44 a) Mounting Method:

O Bolting Number:

Size:

Yd Material:

g O weldina welding Type:

0 >*

O$

Leg:

, Length:

, Pitch; ggg gg MAS-CQD-2.4 FOR OFFICE USE ONLY - NOT TO DE SENT OUTSIDE OF SARGENT & LUNDY swoweasae d -

Page 3

og 9

' ^ - ~ * * '

' - ~ ' -

...m,

~

FILE NO.: CQD-O ///3 /

REV.: co

,PROJF,CT NO.: 9-37-ed

& Othet: Me crArel AOh >?lo/ r m' c' ::/<.o\\/ tenf.ti:c e en

<t

% & a x m i.',i w t tcwa ' ~ c e, cs wo t n &

4 d.,s.ucu y otAchicci

$q x mHvt!Len-tev5 s e s abe cyc.y Paar ny..y n covAg gi mpy b) Does the Vendor's report ind{cate that the Iaboratory mounting n,u _,;

e simulates the actual service mounting?

/Ga m/,ek Yes O no - explain differences:

~

3.

Input Motion Single-Axis g% Multi-Axis Other:

O ""**" ! 6'"!"

""'h l^*

Comments:

4.

Test Method Sine dwell (single frequency):

A i

a) Frequency range:

(Hz) b) Dwella at:

i

~

c) Number of tests in each orientation:

Upset / Service Emergency Service Level C Level B Faulted Service Level D f

d) Duration:

e)

Input acceleration in each direction:

Upset / Service Level B Hi

.V

,H2 Emergency Service Level C Y

Faulted Service Level D H

,H2 y

How is cross coupling and modal participation accounted for ?

f) 9 m

I s',j Ak b~

O Sine deat (single frequcacy):

gg Qt a) Frequency range:

c o b) Number of tests in each orientation:

a, oE A se Upset / Service

, Emergency Service Level C Faulted Service Level D Level B SARGl:11TQLtJilDi' MAS-CQ D--2. 4 FOR OFFICE USE ONLY - NOT TO BE 4 or 9 SENT OUTSIDE OF SARGENT f,

LUNDY awomeaans.

Page n

r

,. m PROJECT NO.: 4 287--68 FILE NO.: CQD-O///3/

REV.: eo c) Number of beats:

, Number of cycles per beat:

(Hz) d) Beats at:

e) Input acceleration in each direction:

Upset / Service Level B H

,H

,V y

2 Emergency / Service Level C H

H y

'2 V

Faulted / Service Level D f) How is cross coupling and radal participation accounted for?

s

@ Random motion (multi frequency):

/ -? Mc //d a) Frequency range:

b) Number of tests in each orientation:

I m rgenc enice Level C

/

Upset / Service Level B

, Faulted Service Level D c) Duration:

t n se c.,.

d) Does Test Response Spectra (TRS) envelop the Required Response Spectra (RRS)?

,c I'

% Yes -- Provide RRS and TRS as attachment i

Nu /= cm ic.2, 'C.5 of rua rear-Tr:es553sef Ors:,c.(kp1(2,./M-603 L eo ^' T ce o 4CC }in:

- Expla No 5.

Dynamic Characteristics

/4 7,75 !

17 2, so. o, 3o.r,43 2 H v4.q, /M.o H *d'G'b##'#'. V " ' #'# # #'6

% Natural frequencies:

y

,2 O Natural frequencies not determined.

O m

6.

Additional Loads s

a, y Are normal operating loads considered?

"d hv Not applicable

%s O Tes 1e O No - explain:

E::

ea MAS -CQD-2. 4 FOR OFFICE USE ONLY - NOT TO DE g

gg 5/

SENT OUTSIDE OF SARGENT & LUNDY

- >sNo*Nasas-Page og 9

i e

e n

PROJECT NO.: 4-M 7-C.9 FILE NO.: CQD-O ///3 /

REV.: cd j

7.

Monitoring a) Is the component functionally monitored?

No O Not applicable

%Yes b) Is component's operability verified?

%Yes O No Not applicable 8.

Does the test meet the requirements of IEEE 344 19 [ f ?

O Yes O No-explain:

G.

QUALIFICATION BY ANALYSIS

/

1.

Type of Analysis Static Analysis O Simplified Dynamic Analysis Modal Analysis Time History Analysis Other:

2.

Analytical Model O Finite Element Other:

3.

Method of Analysis Computer-Aided Calculation Q

a) Programs used:

7.4

'* Y b) Have the programs been validated?

N A

Yes No g,

O nand Calculation 5t mm

~

FOR OFFICE USE ONLY - NOT TO DE gg SENT OUTSIDE OF SARGENT f,

LUNDY

,2 No.== = a Page 6

of 9

m,

I PROJECT NO.: 4267-vD FILE NO.: CQD-o /N3/

REV.:ec)

M' 4.

Operating Loads Are the operating loads considered in the analysis?

O Not applicable O res No - explain:

1 5

Static / Simplified Dynamic Analysis h

a) Acceleration coefficients:

Upset / Service Level B H

,H

,V y

2 Emergene ervice Level C H

'H

,V 2

Faulted Service Level D 1

b) Are dynamic loads applied in the horizontal and vertical directions simultaneously?

O ves O No-explain:

C t' " '

6.

Modal Analysis g

a)

Identify Response Spectra used:

b) Damping factor used:

c) Number of significant modes considered:

d) Natural period / frequency of each:

e) Method of combining modal responses:

O Absolute Sum Square root of sum of the squares (SRSS) s

.3 y In compliance with NRC Regulatory Guide 1.92, N H fd Rev.

, Date g

a#

0 Other:

N5 8::

en

~.

(

FOR OFFICE USE ONLY - NOT TO BE SARGEijTaLUrJDY MAS-CQD-2.4 SENT OUTSIDE OF SARGENT & LUNDY awomesas.

Page 7

of 9

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FILE NO.: CQD-o// /3/

REV.: cf7 PROJECT NO.: 4 2'S 7-C8

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7.

Time 111 story Analysis

,s 4

%I =

8.

Results_

M Stress evaluation at critical locations:

a)

LOAD DYNAMIC TOTAL ALT.0VABLE LOCATION COMBINATION STRESS STRESS STRESS

. p yt Ce d

~* 1 Ad A v 8

t to "N Y o

E s e s avaa SARGEriT&LUfjDY MAS-CQD-2. 4 FOR OFFICE USE ONLY - NOT TO DE SENT OUTSIDE OF SARGENT & LUNDY j'

2 a mmesant. -

Page a

of 9

.v

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PROJECT NO.:

sfygy g FILE NO.: CQD-ol)l3 /

REV.: e

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b) Deflection evaluation at critical locations (Active Components only): Mh CALCULATED ALLOWABLE I

LO M ON DEFLECTION DEFLECTION k

f e

-I

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0.1 0.1 1.0 10 100 FREQUENCY, Hz FIGURE 11.15 HORIZONTAr., RESPONSE SPECTRUM, OBE NO.2, Y-Z EXCITATION, RRS 2.0% Damping, TRS 2.5% Da= ping.

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FIGURE 11.16 VERTICAL RESPONSE SPECTRUM, OBE NO.2, Y-Z EXCITATION, RRS 2.0% Damping, TRS 2.5% Damping.

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-====- 100 0.1 1.0 10 0.1 FREQUENCY, HZ FIGURE 11.19 HORIZONTAL RESPONSE SPECTRUM,OBE NO.4, Y-Z EXCITATION, RRS 2.0% Damping, TRS 2.5% Damping. O

34 100 _ _ - _ _. -. _ _ __ _ _ _ - _ = = = = _ _ _ =.. _. = _. - - -_ -. - - _, _.. _ _ _ _ _ _.. ~. _.. _ _.. - _ _ _ - _ .. _ _ = _, _. _ - - - - = - -. __-.=.==_m_ _--=_=_-_=---.-ny__--__=-=====------3_--_.___=____.3 m 10 = o. TRS Q c-- wvM RRS

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==uc:=:.== q_._:_._.=-- = - -- ---- :_ = =z_= -2n = : - = =m==- w z O Q. W a: 1.0 - g:gg= 2 :q;_=;. =Ds.=r=- 3 q;;g=3--=.--- - =+=g==.i=_w=1=== _ p-- u----==-=2_._-;======.===:==..===-----. _ _ _ _ _ _ - - - - - - - - - _ - - - = = = - = n.7-- 0.1 0.1 1.0 10 100 FREQUENCY, Hz-FIGURE 11.20 VERTICAL RESPONSE SPECTRUM, OBE NO.4, Y-Z EXCITATION, RRS 2.0% Damping, TRS 2.5% Da:nping.

35 g 100 t ~;-.._

---

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-.------------w-- y ~ - --- -:=--.:- - - --= y .m. Li b 10 2 F. ' TRS x . u - =_ - g m Jw WM RRS g g_ _ _ = .= - - - =- .==---:---.----. g = _r=.r a 9 t;u Cf. 1.0 _ _ - _ -..__ = _ =. - l h__._. w w w w b b 0.1 0.1 1.0 10 100 FREQUENCY,HZ t l i L b FIGURE 11. 21 HORIZONTAL RESPONSE SPECTRUM, OBE NO.5, Y-Z EXCITATION, RRS 2.0% Damping, TRS 2.5% Damping. i t 4 w

36 100_ - - = = _ _ = - ~-

- -..- - - - -. -

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==-==.::=_=.==-_=_=_=_-==:==:=._._-.. _. _a -== n.- RRS ~ - - -. = =. =. = = _ = - _ = = - =.. = = - - _ - -_=_=__=i = u z = = = - = _ _ = - - = - - - _ = = - ... -. =. r e ^ 1.0 - ~ = = n ~~ L- -Crn.~ _~ ~ Z T====== -~~ T_E-"t_ -- =_ Er: _ss=a==5==g_=Ea.1:gi-r-w_. ~~_ :==i5===-5~ =:2^ ~'~ ~3G~._ =_-X ~~ ~3 eg=g.:z==c. -c =.anw==2=inm====~~ M=-~~- =.. ~ - _ _ =. = = - =- _ _ ~ - = = -. =. _g 1 100 10 0.1 1.0 0.1 b FREQUENCY, Hz OBE NO. 5, Y-Z EXCITATION, VERTICAL RESPONSE SPECTRUM, FIGURE 11.22 RRS 2.0% Damping, TRS 2.5% Damping. e _J

f. 37 [ i. t i I 100~ 4 t, l ";= :=g=====

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y

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3.,

FIGURE 11. 23 HORIZONTAL RESPONSE SPECTRUM, SSE NO.1, Y-Z EXCITATION, 5_ RRS 2.0% Damping, TRS 2.5% Damping. 1 -3 =

49 38 f 100- __=___=_=__=.:==_2___-:_ =__ g --_ _. _ _ _ _ _ __ _- = = = _ - - -

==_ = ~ m ..I' / 10 s TRS 5 s-4 L 3 u _ ___. w v RRS M g_ _= _.___ - - =_-- ------ 3 ;_y - = o 5u cz: 1.0 ' 7=--------_g--_---;--------=,--- } ~~ ~ \\ . _. _ _ = _ _ _ = = - _ _ = - _ _ _ - _ -_- =__ - - - - - = _ = = - - - - _ w 0,1 0.1 1.0 10 100 FREGUENCY, Hz FIGURE 11.24 VERTICAL RESPONSE SPECTRUM, SSE NO.1, Y-Z EXCITATION, RRS 2.0% Damping, TRS 2.5% Damping. .}}