ML20082G690

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Solenoid Valve
ML20082G690
Person / Time
Site: LaSalle Constellation icon.png
Issue date: 07/06/1982
From:
SARGENT & LUNDY, INC.
To:
Shared Package
ML20082G653 List:
References
CQD-002844, CQD-002844-R0, CQD-2844, CQD-2844-R, NUDOCS 8311300300
Download: ML20082G690 (13)


Text

. s. .

. ' . - 'i

. PROJECT NAME: o[cfLL6u t.8.j PROJECTNO.:[S/7-00 /

FILE NO.: CQD- 002 f/j./7

[ SPEC. NO.: ~J- 2 5 n a Reviewed By: 4 ' 6 ' bM5 Date:

Review (signature)

BOP @NSSS Approved By: df( J w n r: A Ant! Date:

j 4

/ ,.

'/ (signature) -

COMPONENT NAME: C I' > *

  • M l'd" P4kO 7C'i E 1 A A "*T" EHE VENDOR / MANUFACTURER: A - 3 d., #

0 COMPONENT NO./MODEL NO.: 7 h F- 2.

VENDOR'S REPORT NO. AND DATE: LA<f- IN- e I /' 'b/# ' / . N-20-72 I,) , b $ ,u + Y d W220,

/

// ~ S - 7 ? 1- 0 . b . Y , i A > .. V $ -? " 7 7 J 02 A. _ CONCLUSION OF REVIEW

@Arcepted Rej ected Comments:

B. CLASSIFICATION AND FUNCTION l 1. Classification A-(N)% @ Nuclear Safety-Related, Active .

{ Nuclear Safety-Related, Passive

, Non-Nuclear Safety-Related E

d 2. The-component function is 7~i g h u, 7, e,/.:,/ y,/ve, hd' '/-

l l .5 I

?>

o 3.

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

~{, h During and after postulated dynamic and accident events 2 Only af ter postulated dynamic and accident events

. *C 2g cv __ MEc4ANICAL OEPARTMENT RTa> NARD i

!c ""

  • CHECKLIST FOR DYNAMIC QUALIFICATION 0F l (9 t

,,e MECHANICAL AND ELECTRICAL EQ!IIPMENT i

FOR OFFICE USE ONLY - NOT TO BE t

SENT OU'T SIDE OF SARGENT f, LUNDY SAilGEJT&l.U.'mY l

-ancmannel Page 1 of 9 '

0311300300 831120 ~

PDR ADOCK 05000373 P

PDR i

,o .

,,- *t- -

. - - PROJECT NO.: l,S 'l C - 0 0 -

FILE NO.: CQD- o o 2 [ If tj  ;

g Location and Mounting 'R u

1. Location Building: .09releIL Elevation: P %, MC Mim n~ E. D. I.' ! :' %
2. Field Mounting Condition l @ Panel / Pipe /HVAC Duct: f y,3 % Q ,, , pf]g.

O wail /rioor O other:

3. Mounting Attachment h ',ge y m W mn-

@ Bolting Number: , Size:

Material:

Welding Welding Type: .

Leg: , Length: , Pitch:

Oother:

J D. METHOD OF QUALIFICATION Static Analysis

[ Test Dynamic Analysis i

& Other: L.l(e Y;,1. , - ). .. ,, L .afii,o!, ) 1m p- 2 5 d 4 ,, n d ?.

i

  • y l

E. VIBRATION INPUT

1. Dynamic Loads Considered Seismic Hydrodynamic m

N

.bSeismicandHydrodynamic g O other: '

7 2. Required Frequency Range: / !? /,

O O

r 3. Required Input f O Response Spectra ,

. $ a) Required response spectra (attach graphs, identify):

i FOR OFFICE USE ONLY - NOT TO DE g SENT OUTSIDE OF SARGENT f, LUNDY

,amunet) Page 2 of 9 '

I

.. PROJECT NO.: G Pl .Y - CO FILE NO.: CQD- 002giif f b) Method of combinirig required response spectra: -

C Absolute Sum C SRSS O not applicable c) Damping Upset / Service Level B

.EmergencyServiceLevelC}

Faulted Service Level D; d) Basis for Damping:

@ Seismic Coefficients (Required acceleration in each direction)

Upset / Service Level B H ,H 2 V 9

Emergenc Service Level C Hy p,g H Faulted Service Level D ' 2 2*9 'V 2*s

4. Is support amplification considered?

g pmf .r . < u v.t . # 4' I. .. o..i.._.3 o nC) . s~ Mh

@ Yes No Not Applicable 9, u (d L%. .f' - 2 ifa 3, , p ,, . , ,,.,g ( g, p g , 6 ,_A Comments:

'! E' [' I ' }l d'-*l%O A ca. Jf '

i b 5. Is fatigui. considered?

Yes NNo Not applicable l Comments: " I*" ' ' d ^ " ' ' - ' ' ' **- N I ' ~

l '

m, ~

e...+.

fr.. . A -

l i

F. _ QUALIFICATION BY TESTING

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

@ Yes .

O No - justify similarity:

m 2. Mounting

<m [ p & ) G) [.. 'q ' ? I'. e a) Mounting Method: ~Ill M Of " (*

l d' (-- -,.,A, .be /-l' C, h Bolting Number: C16 C > e:A<'y E d O f l I' ' h '.. Size; %f',,'.,yu '

gy ,

iv

" Material:

Welding Welding Type:

oo Am Leg: , Length: , Pitch; FOR OFFICE USE ONLY - NOT TO BE g SENT OUTSIDE OF SARGENT r, LUNDY gg g

,uma.e.asas41 Page 3 og 9 i i

t ,

w. -- _ -

V

[ ,

PRO, JECT NO.: C T d*#

  • FILE NO.: CQD eg 2/ptf Q O other: .-

)

b) Does the Vendor's report indicate that the laboratory mounting n ulates the actual service mounting?

Yes

/

O wo - explain differences:

3. _ Input Motion Single-Axis

@ Multi-Axis S'M Other:

Comments:

4. Test Method O Sine dwell (single frequency):

a) Frequency range:

b) Dwells at: (Hz) c) Number of tests in each orientation:

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

el Input acceleration in each direction:

Upset / Service Level B Hy ,H2 V Emergency crvice Level C Faulted Service Level D H ,H2 Y 1

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

A

= -

b O Sine beat (single frequency):

< a) Frequency range:

,. b) Number of tests in each orientation:

S Upset / Service ,Emergenc Service Level C Level B Faulted Service Level D FOR OFFICE USE ONLY - NOT TO BE SARGENTLLUI)DY SENT OUTSID,E OF SARGENT & LUNDY 2nuo. nema._ Page 4 of 9

PROJECT NO.: ' bl I ~ O d -

FILE NO.: C D- af f f Il l/

('

c) Number of beats: , Number of cycles per beat:

d) Beats at: (Hz) e) Input acceleration in each direction:

Upset / Service Level B Hy ,Hy ,V Emergenc Service Level C H H Faulted Service Level D 1 '2 V f) How is cross coupling and modal participation accounted for?

@ Random motion (multi frequency):-

a) Frequency range: l % 40 4 b) Number of tests in each orientation:

Upset / Service Level B 6 mergency/SeMceLevelC f

, Faulted / Service Level D c) Duration: 2 o /a M -c.1 e k

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

{O O Yes - Provide RRS and TRS as attachment

' @ No -

Explain:

gdg ,, f:/, g a- 3 ,/,ett MA #

y& lnuEu ., ,, , I n .in ilt l-h. . U t"Ac aw . ./h ?? n,n . c. C

}r<!- 9 r , s ~. A I.. . f.) . e ,, e , ? J!. . A .

  • M n . , , , l. . , n
5. Dynamic Characteristics , c. , .

l 0 Natural frequencies: Hy H

,2 .V 6 Natural frequencies not determined.

6. Additional Loads -s

< ;; Are normal operating loads considered?

A*

Not applicable ff T$ @ Yes

< 0 No - explain:

E ::

ea O

FOR OFFICE USE ONLY - NOT TO BE SARGEUTTa LUNDY SENT OUTSIDE OF SARGENT & LUNDY , , , , , , , . , page 5 og 9 I

L

, a e .

PRO, JECT NO.: f., SM - 00

  • FILE NO.: CQD- /C) i ffl)
7. Monitoring ~

' a) Is the component functionally monitored?

@Yes No Not applicable b) Is component's operability ver'ified?

, Yes O No Not applicable

8. Does the test meet the recuirements of IEEE 344 19 7 I?

{Yes No-explain:

G.

QUALIFICATION BY ANALYSIS f

1. Type of Analysis l 0 Static Analysis Simplified Dynamic Analysis l Modal Analys-is h Time History Analysis Other:
2. Analytical Model Finite Element -

Other:

l

3. Method of Analysis -

Computer-Aided Calculat. ion 1

a) Programs used:

1C

} b) Have the programs been validated?

513" Yes No Hand Calculation ba O D FOR OFFICE USE ONLY - NOT TO DE ' gg gg SENT OUTSIDE OF SARGENT & LUNDY ,cwm a no Page 6 Of- 9 I

h

..,..~.

PROJECT NO.: (, Di f - eo .

FILE NO.: CyD- CD 2 l'4 9 g 4. Operating Loads re the operating loads considered in the analysis?

Not applicable Yes .

No - explain:

5 Static / Simplified Dynamic Analysis a) Acceleration coefficients:

Upset / Service Level B Hy ,H '

2 ,V Emergency / Service Level C H 'H 2 Faulted / Service Level D 1 ,V b) Are dynamic loads applied in the horizontal and vertical directions simultaneously?

Yes -

No-explain:

O 6- xea 1 ^= 1vei- .

l l a) Identify Response Spectra used:

i b) Damping factor used:

c) Number of significant modes considered:

d) Natural period / frequency of each:

e) Method of combining modal responses:

Absolute Sum

S O Square root of sum of the squares (SRSS) l 5 In compliance with NRC Regulatory Guide 1.92, 7 Rev. , Date dO Other

B; h

"O FOR OFFICE USE ONLY - NOT TO BE SARGEijTGLUi!DY SENT OUTSIDE OF SARGENT f, LUNDY  ;,y , p g 9 7

,. PROJECT NO. : f.fHf-M -

FILE NO.: CQD- 00 2 g 4 4 e 3

7. Time History Analysis ~

i i

i l

I 8. Results i

l a) Stress evaluation at critical locations:

I l

LOAD DYNAMIC TOTAL ALLOWABLE LOCATION COMBINATION STRESS STRESS STRESS i

O i

i I

l O

=

4

't 0

.j l l Y

FOR OFFICE USE ONLY - NOT TO BE l' ggg g ggggy SENT OUTSIDE OF SARGENT & LUNDY me,umsane. Page 8 of 9 i

i L

{h . -, . < . ~ *

. PROJECT NO.: f. C')1 - e d FILE NO.: CQD- 0 02 S4}

b) Deflection evaluation at critical locations (Active Components only): .

l

. LOCATION LO W LE DEFLECTION DEFLECTION l

H. COMMENTS l

t 49 \

am '

16 gm W8 l v g.

s2 ,

iD FOR OFFICE USE ONLY - NOT TO BE ggy gg

, SENT OUTSIDE OF SARGENT & LUNDY swomma ns Page 9 of 9 i

l t h _, .m,g. - . - - . - . . - - - - - - - - . . . - - - . . - - - - - - - -

e

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