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)
v • d • e


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o[cfLL6u t.8.j PROJECTNO.:[S/7-00 FILE NO.: CQD- 002 f/j./7 PROJECT NAME:

/

[

SPEC. NO.:

~J-2 5 n a 4

' 6 '

bM5 Reviewed By:

Date:

Review (signature)

BOP

@NSSS Approved By:

df( J w n r: A Ant!

Date:

/

'/

(signature) -

j 4

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 ?

0. b. Y, i A >.. V $

-? " 7 7 1-

/

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

__ MEc4ANICAL OEPARTMENT RTa> NARD i

cv

!c CHECKLIST FOR DYNAMIC QUALIFICATION 0F i

l (9 MECHANICAL AND ELECTRICAL EQ!IIPMENT

,,e t

FOR OFFICE USE ONLY - NOT TO BE SAilGEJT&l.U.'mY l OU' SIDE OF SARGENT f,

LUNDY t

SENT T

-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 [ I tj f

g Location and Mounting

'R u

1.

Location Building:

.09releIL Elevation:

P %,

MC Mim E.

D. I.' ! :' %

n~

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 ?. y i

l E.

VIBRATION INPUT 1.

Dynamic Loads Considered Seismic Hydrodynamic

.bSeismicandHydrodynamic m

N g

O other:

7 2.

Required Frequency Range:

/ !? /,

O O

r 3.

Required Input O Response Spectra f

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 H

p,g H

y 2

2*9

'V 2*s Faulted Service Level D f

4 I... o..i.._.3 g pm.r. < u v.t. #

4.

Is support amplification considered?

o nC)

L%..f' - 2 ifa Mh s~

@ Yes No Not Applicable 9, u (d 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 '

~

fr... A l

m,

~

e...+.

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:

2.

Mounting m

" (* [ p & ) G) [..

'q ' ?

I'. e

<m

(--

- A b /-l',

l d'

a) Mounting Method: ~Ill M Of h

C16 C > e:A<'y E d O f l I' ' h '.. Size; %f',,'.,yu

,.,,. e C

gy Bolting Number:

iv Material:

Welding Welding Type:

oo Am Leg:

, Length:

Pitch; FOR OFFICE USE ONLY - NOT TO BE g

gg g

SENT OUTSIDE OF SARGENT r, LUNDY 3

i

,uma.e.asas41 Page og 9 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 ulates the actual service mounting?

n 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 H

,H2 V

y 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 I l/

l

(

c) Number of beats:

, Number of cycles per beat:

d) Beats at:

(Hz) e) Input acceleration in each direction:

Upset / Service Level B H

,H

,V y

y Emergenc Service Level C H

H 1

'2 Faulted Service Level D 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

{O t

Required Response Spectra (RRS)?

O Yes - Provide RRS and TRS as attachment

' @ No

,/,ett MA #

Explain:

gdg f:/, g a-3 y& lnuEu

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

}r<!- 9 r, s ~.

A I... f.). e,, e, ? J!..

A.

  • M n.,,, l.., n 5.

Dynamic Characteristics

, c.

l 0 Natural frequencies:

H H

y

,2

.V 6 Natural frequencies not determined.

6.

Additional Loads

-s Are normal operating loads considered?

A*

ff Not applicable T$

@ Yes 0 No - explain:

E ::

ea O

FOR OFFICE USE ONLY - NOT TO BE SARGEUTTa LUNDY SENT OUTSIDE OF SARGENT & LUNDY 5

page og 9 I

L

a e.

PRO, JECT NO.:

f., SM - 00 FILE NO.: CQD- /C) ffl) i 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?

51 "3 Yes No Hand Calculation b

a 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 H

,H '

y 2

,V Emergency / Service Level C H

'H Faulted / Service Level D 1

2

,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

7 g 9

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't0

.j l

l Y

FOR OFFICE USE ONLY - NOT TO BE ggg g ggggy l'

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 LO W LE

. LOCATION DEFLECTION DEFLECTION l

H.

COMMENTS l

t 49

\\

am 16 gm W.!.

l 8 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.

P;ga No. 79 e

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