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)


Text

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4 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:

O~ W I WE3 Date:

Review (signature) 3 O BOP

@NSSS Approved By:

,, p,.x,ry pyf u Date: 9/1d/83

//

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

1 c

preuivrw oa c+owy sou o awaf vitc w ismon 4Da/-t os3 or.9r*,T v, i;pa,9 s

s 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 Eoa 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

[

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 Size:

Bolting Number:

Material:

I

\\

Weldirig Welding Type:

Leg:

, Length:

, Pitch:

Bother:

scet=n >H ry'P =. e e-hPsefs vi Pseovirr:n ro c w&veivr z

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

% Test Dynamic Analysis O Other:

E.

VIBRATION INPUT 1.

Dynamic Loads Considered

+

b Seismic O ityarodynamic I

m 7

h Seismic and liydrodynamic 4 "T O Other:

W s

cy O 2.

Required Frequency Range:

/ p dopp (T E jy t 3.

Required Input

, 5. O

@ Response Spectra seet b2 Required response spectra (attach graphs, identify): ca M u d cl a

j w a; y:- #)A /\\'efa) dv.93+98-3 Da-lcel '//=/77 7-*ye4-7--> S2 cda:,uf.sk oE UA EttDf/LG // o ?oto?.vs17a.D $~/2 7/?/.

y

! :I SARGENTSt.t!UDY MAS-CQD-2.4 q

f FOR OFFICE USE ONLY - NOT TO DE 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 S=W edcww" A

SRSS Gr E 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 a n D nta g 0 y(Required acceleration in each direction) 903 Upset / Serv.ce Level B 111 j,733ff, H2 /-? W V m M 7 H

Emergenc Service Level C H g,73,g7 2 B 7fi27,V d-53cf y

Faulted Service Level D 4.

Is support amplification considered?

% Yes No Not Applicable 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>

4, j Leg:

, Length:

Pitch 0

l FOR OFFICE USE ONLY - NOT TO DE SARGEUT&LUDDY nAS-C & 2.4 SENT OUTSIDE (F SARGENT f,

LUNDY 3

9 swe.weena.

Page o t' Fr

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 & n/r a mea a M lc N O

)J' n n a,,,;,,,.n +

Poffe XV//-35 c/ 3?T f*W"/".W C

) Other:

m g,,acs a 77 w c,up o a essw ~ a x

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:

(Hz) b) Dwells at:

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 Faulted Service Level D 11

,H2 Y

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

9 l

  • d

}

aL

's O"

{k'N "k'byWt Sh 5(Sc$

0 a

8-33//2

$s: t a) Frequency range:

o b) Number of tests in each orientation:

g.

/47dSC oe Upset / Service

, Emergency Service Level C f,e;-,mwr W5 Level B Faulted Service Level D

,,,u.~

,.,a j

l FOR OFFICE USE ONLY - NOT TO DE

!!AS-CQD-2. 4 SAT GEiiTall)TJD'/ ]

4 of 9 SENT OUTSIDE OF SARGENT L LUNDY Page 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 +-v v +-o (f~Avvh /0 -> 331/g How is cross coupling and modal participation acco)unted for?

f) t Random motion (multi frequency):

a) Frequency range:

/-M o #P-

.3FI N N O B#S " #

'l b) Nu.aber of tests in eac$ //2.7t S EnVSLcf4 Rhb I

/

orientation:

f jjj, mergency Senice Mel d

,,,3,jj&

Upset / Service Level B f

j

' A < SSs tr'2'/z f

, Faulted Service Level D c) Duration:

d ).

Does Test Response Spectra (TRS) envelop the c..

Required Response Spectra (RRS)?

%Yes-ProvideRRSandTRSasaNtachment 'st//*

a tvl cosimM6, ?/4.q s. cmcGf> S.

Rits e:2 (L{p ffc crJen a sz '/. 7R G - 7W S crnvrio,/,.1 KR

_L]No - Explain:

l l

S.

Dynamic Chrracteristics

[ Nature 1 frequencies:

y.3F//f--

H !$?

/!

H 2

V O Naturti frequencies not determined.

^m 6.

Additional Loads

.'y l

-e 'ji Are normal operating loads considered?

r. y hv 0 Not alplicabic Yes m

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 5

l 1aucemmeses.

Page 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 l

O Static Analysis 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 O No g,

EN Han'd Calculation Ie es

.2S hV U.E ONLY - NOT TO BE S

SARGEUTSLUDDY MAS-CQI)-2. 4 FOR OFFICE 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 H

,H y

2

,V Emerginc ervice Level C H

'H Fault d Service Level D 1

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:

e) Metiod of combining modal responses:

mm a

[] Absolute Sum C

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

/

(

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

Time History Analysis fG:

8.

Results a) Stress evaluation at critical locations:

//

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

4 i

^m

)0 O

v Ec tc cz:

FOR OFFICE USE ONLY - NOT TO DE

'f M

S-4 SENT OUTSIDE OF SARGENT & LUNDY p38e 8

Of 9

.i: '

,~

i

--. -a

s.

FILE NO.: CQD-C/Gg7 REV. : CD PROJECT NO.:

37 g b) Deflection evaluation at critical locations (Active Components only): ////f s

CALCULATED ALLOWABLE LOCATION DEFLECTION DEFLECTION Yw H.

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

N,~<'re % fi% m, anl 4 a c&nk.ur~./

A, s,,< A 4 ~ r 4,,p Y, -,,e /l / n d.d r S,

/,>,.,, ~ /

Y d s v $,, / d s k v

%./A a b hr

/rp r N s, *s~hk

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y cnfu,x< D,,.// yM <e>A4 yci -s c s,,e )

al e >,,w...+

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2 m

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a.*f fe B ::

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FOR OFFICE US: ONLY - NOT TO BE i

SARGErJT&LUPJDY mas-CQD-2.4 SENT.OUTSIDE )F SARGENT f,

LUNDY

,e woamass==

Page 9

of 9

(

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V 1.00 10 i 100 @

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SPECIMEN LOCATION NO.

b ie AXIS '

2 TEST RUN NO.

37 7

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SPE01 MEN LOCAT!ON NO.

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TEST RUN NO.

39

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