ML20082G675

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Linearly Variable Differential Transformer
ML20082G675
Person / Time
Site: LaSalle  Constellation icon.png
Issue date: 09/28/1983
From:
SARGENT & LUNDY, INC.
To:
Shared Package
ML20082G653 List:
References
CQD-010048, CQD-010048-R0, CQD-10048, CQD-10048-R, NUDOCS 8311300294
Download: ML20082G675 (11)
v • d • e


Text

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  • FILE NO.: CQD- O /CCM PROJECT NAME:l./JS/14/ -2 PROJECT NO. : //-267-00 REVISION NO.: c0 SPEC. NO.: W o./9//C6 Reviewed.By:

Review O~ W (signature)

Date: I WE3 3 O BOP @NSSS Approved By:

//

,, p,.x ,ry pyf u (signature)

Date: 9/1d/83 v

1 c COMPONENT NAME: _O. y,97 f"L /NGARLY VAki/ .BLE Z)irFEs rJY/A4 -rppNsrcMrice}

preuivrw oa c+owy sou o awaf vitc w ismon 4Da/-t os3 or .9r*,T s v, i;pas ,9 VENDOR / MANUFACTURER: cwoSBy COMPONENT NO./MODEL NO.: sc-E cWoS3 y Vncyg f-Ggge co :pw6r#ys-c-664.ff S89 xt: v-b.

VENDOR'S REPORT NO. AND DATE: VU/F FN m v 7-

  • 4 C4."-G~-2 IMED ////Yff2 A. CONCLUSION OF REVIEW QAccepted ORejected Comments: Acccerc_v Wirst rist- S uffoer/MGr e n.c s $ w n n o n wr/6 wira n/r cR;= f>e /e r B. CLASSIFICATICN AND FUNCTION
1. Classification

('.

% Nuclear Safety-Related, Active

{ Nucicar Safety-Related, Passive O Non-Nucicar Safety-Relatea E

o a 2. The component function in 52 ppss<,jpg igpir se A7?ow . Devic i ~. n tr/&Js 7ap 7 af 7T>b/ ner) O /= \/ A L VE S 75m 5

?>

o 3. Operability Requirements (Active Components Only) h This component is required to operitte:

3  % During and after postulated dynamic and accident events N H dd Only after postulated dynamic and accident' events 0.

a3 2e g ,. MFCHANICAL DEPARTMENT STANOAPD EE CHECKLIST FOR DYNAMIC QUALIFICATION OF l MECHANICAL AND ELECTRICAL EQUIPMENT l FOR OFFICE USE ONLY - NOT TO BE C j ,

y I!AS-CQD-2. 4

  • SENT OUTSIDE OF SARGENT 6 LUNDY zeuamaana , Page 1 of 9 [

8311300294 831128 PDR ADOCK 05000373 t P PDR

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r .

PROJECT No.: 42.267- @ FILE NO.: CQD- O /0048' REV.:

C. Location and Mounting

1. Location Building: 'P/?/,~7/W y (c N7/1/WMZ-fv7~

Elevation: /=r7am. 7?G '-o 7 a' 7Pm / oc

2. Field Mounting Condition O Panel / Pipe /HVAC Doct:

O Wall /rioor

@other: Meunbd crrL C.7f y $f tp p?c g g q & rg y p g j ,f ofy g y;

,2. M /- Fo/3 M r,9 s, w

3. Mounting Attachment Bolting Number: , Size:

Material: I

\

Weldirig Welding Type:  ;

Leg: , Length: , Pitch:

Bother: scet=n >H ry'P = . e e-hPsefs vi Pseovirr:n ro c zw&veivr wonno,v. csce s.a.uk, cak >&,,a,d.&u.ac .m e "

T & : O ^ t

. '*P O / O "2 C D. METHOD OF QUALIFICATION i

Static Analysis Dynamic Analysis

% Test

O Other

E. VIBRATION INPUT

1. Dynamic Loads Considered +

! b Seismic O ityarodynamic I

! m

! 7 h Seismic and liydrodynamic 4 "T W s O Other:

cy O 2. Required Frequency Range
/ p dopp (T E jy t

, 5. O

3. Required Input

@ Response Spectra seet b2 Required response spectra (attach graphs, identify): ca M u d cl a oE j w a; y:- #)A /\'efa) dv.93+98-3 Da-lcel '//=/77 7-*ye4-7--> S2 cda:,uf .sk UA EttDf/LG // o ?oto? .vs17a.D $~/2 7/?/. .

y f :I FOR OFFICE USE ONLY - NOT TO DE SARGENTSt.t!UDY MAS-CQD-2.4 q SENT OUTSIDE OF SARGENT f, LUNDY - in edo* mss s*u . Page 2 of 9 f

l .. ..

. PROJECT NO.: 4-287- N FILE NO.: CQD- o/oo//-g- REV. : CD b) Method of combinirig required response spectra:

0 Absolute Sum

& SRSS Gr E S=W A edcww" O Not applicable _

c) Damping Upset / Service Level B MX Emergency Service Level C ;g y, Faulted Service Level D d) Basis for Damping: #E67. Gow s /.g/ oc roes /R /'/73 5

@ Seismic Co fficientsf=.rp m 903 a n D nta g 0 y(Required acceleration in each direction)

Upset / Serv.ce Level B 111 j,733ff , H2 /-? W V m M 7 Emergenc Service Level C Hy g,73,g7 H 2 B 7fi27,V d- 53cf Faulted Service Level D

4. Is support amplification considered?

No Not Applicable

% Yes Ccmments:

3; 5. Is fa':igue considered?

@ Yes No Not applicable -

Consnent a i '~"4" " U"' "* " ^ d'A*I* c'M# N * **

cmcuc J & % "/h:orec7t. # tbre d e e c y h A W -e m s a A 0 NC - See cn ch- x e~t w . n n-r .r;. ,w . '

F. QUALIFICATION BY TESTING

1. Does the Vmdor's report indicate that the component is identical to that to_be_ installed?

% Yes No - justify similarity:

C e

4 2. Mounting

~t a y4 a) Mount ng Method:

a s

@v .lolting Number: ., Size:

Y io t

Material

% Welding Welding Type: 777cr v/z-L.1uw6f. Ncffs,f[f57 ,

E>

0 4, j Leg: , Length: , Pitch l

FOR OFFICE USE ONLY - NOT TO DE nAS-C & 2.4 SARGEUT&LUDDY SENT OUTSIDE (F SARGENT f, LUNDY swe.weena. Page 3 o t' 9 F

r

b PROJECT NO.: 4267- C@ FILE NO.: CQD- O /CC4-S~ REV.: ce g 4 Jrad a wse<= -r w u m c<d y &nn/r n a,,,;,,,.n +

a mea a M lc N O

) Other: wPoffe c,upXV//-35 o a c/ 3?T f*W"/".W essw ~ a Cx m g,,acs a 77 )J' fcW$Wut- . CWSe e b o ! W f ,%!/A- 0" /22C )y/-/7 el b) Does the Ve or's report indicate that the laboratory mountingA; g,/

simulates the actual service mounting? 17#./

$ Yes Sc2 t'46tE x-I of rys rasr gesBr*

O No - explain differences:

3. Input Motion Single-Axis Multi-Axis O Other:

Comments:

4. Test Method Sine dwell (single frequency): /t/[/)

a) Frequency range:

b) Dwells at: (Hz) ,

c) Number of tests in each orientation:

Upset / Service Emergency Service Level C Level B Faulted Service Level D d) Duration:

e) Input acceleration in each direction:

Upset / Service Level B 11 ,H2 Y 1

Emergency Service Level C Service Level D ,H2 Y Faulted 11 1

f) How is cross coupling and modal participatior accounted for ?

9 l

  • d }

aL

's 0

{k'N "k'byWt Sh "

5(Sc$ a O" a) Frequency range: 8- 33//2

$s:o t

g. b) Number of tests in each orientation:

oe

/47dSC W5 Upset / Service - , Emergency Service Level C f,e;-,mwr .

Faulted Service Level D ,,,u.~ ,.,a j Level B  % l FOR OFFICE USE ONLY - NOT TO DE SAT GEiiTall)TJD'/  !!AS-CQD-2. 4 SENT OUTSIDE OF SARGENT L LUNDY , , ,,,,,, ] Page 4 of 9 1

I PROJECT NO.: M67-SS FILE NO.: CQD- O/C048 REV. : CD c) Number of beats:

, Number of cycles per beat: / S' d) Bea ts at : 2,s.S, 3. .'?,4..o, 5~ G. 3, er, ,o is.g, /c,:o,.gr. , 3 7,33,23, s.z (?:';

e) Input acceleration in each direction: /~D B ' - /o * S * # F""c ^ "- O Titet t/ yir-Si Op 77/d FiTM T Upset / Service Level B Hy -

jH2 ~

'Y ~

%!" "*7":"!:: i:":' "1 +-o . "2 (f~Avvh /0 -> 331/g

+-v v +-o f) How is cross coupling and modal participation acco)unted for?

t Random motion (multi frequency):

a) Frequency range: /-M o #P- .3FI N N O B#S " # 'l I /

b) Nu.aber of tests in eac$ //2 .7t S EnVSLcf4 Rhb orientation:

Upset / Service Level B ' mergency Senice Mel d f ,,,3,jj& f jjj, j

, Faulted Service Level D c) Duration: ' A < SSs tr'2'/z f d ). Does Test Response Spectra (TRS) envelop the c.. Required Response Spectra (RRS)?

a

%Yes-ProvideRRSandTRSasaNtachment tvl 'st//*crJen Rits e:2 (L{p ffc a

_ sz cosimM6,

'/. 7R G - 7W?/4S .q s. cmcGf>

crnvrio,/,.1 KRS.

L]No - Explain:

l l

S. Dynamic Chrracteristics

[ Nature 1 frequencies: H y .3F//f-- H2 !$? " /!

V O Naturti frequencies not determined.

^

m

.'y 6. Additional Loads l -e 'ji Are normal operating loads considered?

r. y hv 0 Not alplicabic m Yes No O No - .xplain:

0 >*

O$

4 1

FOR OFFICE USE ONLY - NOT' TO BE gygggg MAS-CQD-2. '4 SENT OUTSIDE OF SARGENT L LUNDY l 1aucemmeses . Page 5 og 9 1

i i \

l i . .

PROJECT NO.: ef.2g7- e:rp FILE NO.: CQD- O / cog 3' REV.: ay i~

7. Monitoring a) Is the component functionally monitored?

Yes O No O Not applicable b) Is component's operability verified?

Yes No O Not applicable

8. Does the test meet the requirements of IEEE 344 19 [b] ?

@Yes No-explain:

G. QUALIFICATION BY ANALYSIS / M

1. Type of Analysis O Static Analysis l 0 Simplified Dynamic Analysis Modal Analysis

")

Q Time History Analysis O Other:

2. Analytical Model Finite Element O Other:
3. Method of Analysis O Computer-Aided Calculation O a) Programs used:

co k

  • 7' m[ b) Have the programs been validated?  ;

dv Yes g, O No EN Han'd Calculation Ie es

.2S h

V FOR OFFICE U.E S ONLY - NOT TO BE SARGEUTSLUDDY MAS-CQI)-2. 4 SENT OUTSIDE OF SARGENT & LUNDY ,mwawasae. Page 6 of 9 l

4 PROJECT NO.: g6 7- Op FILE NO.: CQD- C/OOg REV. : CS

+

_. 4. Operating Loads Are the o;erating loads considered in the analysis?

O Not applicable Yes No - explain:

5 Static /Sivplified Dynamic Analysis g a) Acceleration coefficients:

Upset' Service Level B Hy ,H

,V 2

Emerginc ervice Level C Fault d Service Level D H

1

'H 2 ,V b) Are dinamic loads applied in the horizontal and vertical direc: ions simultaneously?

O Yes C No-explain:

t'

6. Modal Aralysis p' [

l l a) Ider tify Lesponse Spectra used:

l 1

b) Dam)ing factor used:

c) Num~.er of significant modes considered:

d) Natural period / frequency of each:

m e) Metiod of combining modal responses:

m C

a - [] Absolute Sum 3y [] Square root of sum of the squares (SRSS) n-fd C In compliance with NRC Regulatory Guide 1.92, g, Rev. , Date 4g []Other:

Es ea e

FOR OFFICE US. ONLY - NOT TO DE gggggg SENT OUTSIDE ilF SARGENT f, LUNDY ,ewoemassa. Page 7 of 9 p

/

(

PROJsCT NO.: g26 7- 99 FILE NO.: CQD- C/OS/fff REV.: cm ,

7. Time History Analysis fG:
8. Results  ; ;

a) Stress evaluation at critical locations: //

LOAD DYN/LMIC TOTAL ALLOWABLE COMBINATION STRESS STREST STRESS LOCATION I

4 i

^

m

)0 ,

Ov Ec t

c cz:

'f FOR OFFICE USE ONLY - NOT TO DE M S- 4 SENT OUTSIDE OF SARGENT & LUNDY , , - , , , ,, p38e 8 Of 9

.i

' ,~

i

--._-a

.. s.

PROJECT NO.: 37 g FILE NO.: CQD- C/Gg7 REV. : CD b) Deflection evaluation at critical locations (Active Components only): ////f s

CALCULATED ALLOWABLE LOCATION DEFLECTION DEFLECTION Y

w # -

H. COMMENTS Ree >UI- 7 cr/ $ fodnedd./ S/ c5 /4/ N sbW~ jcx.wc& j?c,<-

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SARGErJT&LUPJDY SENT.OUTSIDE )F SARGENT f, LUNDY ,e woamass== . Page 9 of 9

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V 1.00 10 i 100 @ 10000 DAMPlNG M

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SPECIMEN LOCATION NO. b ie AXIS ' 2 TEST RUN NO. 37 7 t i

T PIga No. XII-46 Report 1a. 45645-2 FULL SCALE SHOCK SPECTRUM (g Peakt .

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, AXIS v 3 TEST RUN NO. 39 '" I l{

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