Text

Rev 0 to Calculation IP-M-0435, EOP-6,Potential for Water Hammer
	ML20249B175
Person / Time
Site:	Clinton
Issue date:	01/23/1997
From:	; ILLINOIS POWER CO.
To:	;
Shared Package
ML20249B170	List: ML20249B175; U-603026, Submits Response to RAI Re Illinois Power Response to GL 96-06, Assurance of Equipment Operability & Containment Integrity During Design-Basis Accident Conditions;
References
	IP-M-0435, IP-M-0435-R00, IP-M-435, IP-M-435-R, NUDOCS 9806220136
	Download: ML20249B175 (250)
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Attachment 3 to U-603026 I'

CALCULATION COVER SHEET SHEETIOF 14 DEIrr/DIV CALCULATION NO.

' TITLE / DESCRIPTION:

NSED/M IP-M-0435 EOP-6. POTENTIAL FOR WATER HAMMER QUALITY SYSTEM CODE TOPIC BLDG /ELEV/ AREA RELATED (or NA)

(or NA)

(Q or N)

O VP M91

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_a,ssess,the,lik,eliho.,o. d of a catastro.p_h c f,a ure... S.ee analysis for additional i i

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. +S " REFERENCES ^

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Hydrauli :ofpipelines, J, Paul Tullis, C1989, John [Wiley & Sons.;

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ij w INPUTS ASSUMPTIONS 1)

Per EOP 6 interlocks for VP and WO may be defeated if Drywell temperatures go above i

135 F. This requires operator actions. As such, it is inconceivable that this would occur at the precise point of the LOCA. This analysis will look at a water hanuner as a stand alone event.

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2) U lPef RAferencel17,! Amant 2,:pg.!6lthe pressure surge equation for vapor bubble 9 3 6[

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1, Ba, sed on the discu, ssio. n above, water hammer is not a concern relative to containment.11 4,

t.

~7 containme'nt isolation' valves (CIVs),!small diameter piping in the Drywell and multipl8Ei ~ <(b

' Integrity for the;WO tysthmiue'ttthelongdissace between Drywell and the '.pf 1 branches.;VPlon the other hand has a cooler (IVP02SC) that is fed by an eight inch line i

close to the inboard containment isolation valve. This location will be analyzed as the :

worst case. '

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CALCULATION DEPil0nftSECTl0N CALCL'LATION NO.

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Supply side of IVP02SC: Under the scenario ofinterest high temperature in the Drywell.

4

. could result in the formation of vapor (i.e. steam) at high points near coolers (Refd l8)g g,

Thir could only occur if the system were depressurized: Since VP and WO a~re close'd '

I

' be developed since there's nowhere for the expanding v

' loo'p systeins inside containmcht (Ref.1,2,7,' & 8) a significant polume%i%;ifiyduld

..],

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4

valve IVP024B is set'at 140 psid, which gives it a saturation temperature s6id330 F, ' i i

~'

j Ref.19). Not withstanding the above, the configurations such that Af4ipdiWould be '

J. G

- present in the header supply and return headers as shown beloW (from Ref;14d). L,(

2

.,.+,..,__4,t..

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^ ' I (The vapor collapse :.nd impact would occur, on the supply side, in the.4" supply headers :

JF.i

since as water comes in the 8" header it starts to fill the 4" lines, which already liave somed W7~

' water level (they're lower), hence the vapor bubble collapse will occur at the water

[W j intdce in the 4" lines.kince the vapor is readily colla;kible it offers nearly no resistance. a.f f Ml, iUritil all the vapor is collaRnb significant impact occurs. It's logical based on'they#

4J3"

'd pipe c. configurations that any major impact of concern to piping integrity would,thYoccur :

. at the end of the line near node 235. Since smaller impacts would occur in the smaller j

di unet;er lines and, the resulting pressure surge would split at branches, the resulting

, pressure surge on the supply side of the heat exchanger would not be ofconcern (see.

discussion in 3). ' On the return side of the heat exchangers the collapse and impact would l

~

occur somewhere in the 8" pipe. Only the return side will be looked at in detail.

5)

Return sid'e of 1VP025C: The worst case pipe routing i e associated with subsystems.

' IVP03 and IVP04 (Ref.14c and 14d). This analysis will look at these two subsystems as they are similar to the other retums but worst case (Reference also other analyticals in 14.). Piping in these subsystems are shown on P&ID, Ref. 2.

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6)f lFrom thel figure shown on RLs 14a'and 14c it is apparent that the paths through~thef

'c'g

N N 8%upply leader and the various 4" line are different lengths so that an advancing water;@ O

~

'gM,g, eaches le m the return he~de~r:first,.?T

- tka MM front r.w n~the 8" return header at.different times. ;The brarich flow'with the shortesA A

%3s-F wk4

.Wwq ilis~tance to travel would co. llapse th~e vap~or S,u 44 a

n

- ~

. ~.

.a

'. at 1 w w mM

.c M.~

J &a' n c. y p@w 6Ww %y.flo.p~s

~E=-

v-X to co n

1

~

5.5 fthec veloday in the pipe under a full flow condition.?It.is W T W#

w e

' "4@

yd 4 app d_be.i_mu* h_ lo. w_er th,in_t_his ~dup ib ksdon'di,sc,usson above.W _! $j W

J pggj. th_e vil'_esty._w_sd_,5 ft/see wilbe,used in this a, rin E..

Nyg 4,W_ lowWiocityf5]

c.

3,a Moccur[sh destion~ of he' system fo r. -w

-i : y$

~.4..,w-. n 4 my a -. - u _ w,. y..

., r %o. p, a %.q g.

t,

c,

, 4 o

-e s

qm 4

y

.,qv j

8

' 1%, m.[7)hFoEco Rb mu'st d@ocud% thisto h' p~ pen the containmentisolation valv Q'

~YY a

7 ^1the pressure puls'e'would travel through the gate valves L

e o

j g

s N,

tv ; l pip *mg'systembaly using simple Waas e

?

a e

y Q ~ y tf e~q by %,f;pTr y n wu o av n)+O..j A. l.evelD all.owable,Wf 36000, psi. (2,.7-.1

,. f ; y *.s w L 8

-n -,, ov. r

_ g 7F

%g

{L

1. '

Q Hfollowpg6quation:

L'-

p< v Ze p~@tym:p~a~w awtge.

a qlm?y v;;:g y'q.:a{jf (

r a y:g mr

,m

- +

Qxp

.jg{

v ~. p s y; f

cl+4 PDog M,,7 -

v @n nmps w.c M 4t- -

Zuae o A 44+%

aWW O & ;.$ M + 9,b [N N P N JM V;.

u.

.a a

.'Y!

h ;w*

y m$'.h h.4 I,v" V

N mbws;% w mg.w>e

.. cf r s,

r,

.q

+

,, M

,@Me~L.ote tint A shape factor of 1.7 fian Marks l pg. 5-21 could be ap+ li to the allowable.

N 1, 1 ; W.

n.

%ypq above sii w w de.fo.- -.

fth....,-.. OK..- -.ded we. don,t m

nce plastic nnation o e pipmgis provi

~

7.

/g sU Y d Will n$t td ussd is the analysis, which is conservative. J 9n%+ i X

' eq %;l{!

m L }ma gi in 2

%y&3 %

xC V r

wik

.I9)Qw%; wpm.}pmw"s on;c.,,.ThNiiajl siss.nvy: areas clos m

m y.

-mnw y g n u

a ys y up illfoeti 9

fg

'L

',' w[ &v3[wL, 4:g n

+-

~gv

-m v

.n

.s s

e

' '@v.

w

%p;N sthe area ofmterest.gYt i

1p, 4.c c.

e

.Q:n[

Lv n,~f Mj&&W9f, s al*inment walls are very strong. [Thhy will not be' rigo

}

,:& "10)$y A m sa w

~~

a Anchors atDrywelland conta

,..;_.ilooked at here'. They are u ge to not e t e weak link. The configuration is such thath i

jdd b h

'J.

11i l

?.'

! pip lc ' stress.w. ~ill be li:niting. -

u

,y a

.~.y e.

I 6

4 1

. N1117 990)

l i

NF 161-3 (1/90J CALCULADON DEPTfDIVCECTION CALCULATION NO.

REVISION VOLUME SHEET,.

IP-M-0435 0

8-g.

ANALYSJfi The configuration of thepiping in question inside Drywellis shown below.),

v

[ _;p,y a

.y.t

j.

^

~

+

s

!pT dp

,,' g j j

';W. :ri g

... a, g,.

u

=, -

n

[..g

/{. ].

[

d

-Qj?

6 i,,. W ):'

n "gg;gy 8

Vk..w.$'Y

.. s

..i-

?.,*.. -

. GQ( o ltypt,,'

/

.,u n

t:No a T* 8' (7) k L t 11E*

1.7M" 8 ! ! ! -l 4.024' '

.(

. ;q a 99f 4VP03DB40h 6

s El. 770.00' g

. EL 7 rOR CONT.SEE 0

/

t

/

71 -

p 9

1VPO4 SHT.4 N:k,

[

(MsM f

0.74 5'~

, )f f

~

. 4.76 5'-

.o :

lV

'LTS(

Y MO.583'- W:,..

r 7'

.e.6%'d 43G.>a 1.rwm

~ hlVPQ3002IV' t'k

.. ( ;

1

/f

+o t

u,,

.=

p '.. h ~, e f

'*tt q

g

.v 'f;l' ' '

r,

&'[t t

~

QvPtBBAk) y

.,f'%,

J s

/

~;i ^

s '.

N n y $, h E

e (4VP03DO 8 Y( Y 34.,723*.

FORCgT.SEE PLAN B SHI2 e

4 Reference 14? Plan A l

Ntt1 4 W)

r

]

. o..

NF.1613 0190) -

CALCULATION DEPrfJNI5ECTION CALCULATION NO.

REVISION VOLUME SHEET.

\\

~

. IP-M-0435 0

9 2

\\

a

.r.

1

mar e

. e m m m a;ca y 4

s c,m..., +

+

ss.aswr.

.we go

,.3

._ewsmo g,.n

, y,:

%n U

s a

(: x

.o w.c w :S sL.

1,. _. o s

2 s.

m..

7 g.y y?dge 4

< p Mj. 3l _f ;,,.gn _.

i __."u$

i w

.4 e.

m 3,e

.,v n @ sy w u.: :,4 x

.s.,

x,. g;+ -.

a m_. p; w,.i u.a o

w

e o

,#.m,

gp..

y, T

,,.s i. e O.

~

~ ?v. ;

q

,g' p

g g

"; q q c

h.2 Mbda=Md y

^

i m.

~

d,[w-.e; M M

.L e

~=

, posAm a AE.8, 99,

WPoem W

, ~.

_p.

1 7.-

.sccinon 'e-2'

~b.,'.

m f

Reference 14c.

.y.

.,L"

.e

.c ; -

u

, +;;

e... :.

p z a-3

.]

iThe inipact would be~ expected to occur'near node 85. Coriservativel[u, sing 5.5 ft/se

,a j'i(assumption [6)andu, sing AP7. 29 AV(Input,2)'

. c $C g

c c, y.a.am',:

.y

~,

y%m m

n:

. w :...

"L_APM.29..t.5,57160 psi,

s w..

e.

m, p q.y qQ -.., Q >p j,,, sb,ov,t is;ap. jparent that as the press,ure wave travels upstream 1

the sectioriview

, y )'3:

4 ?.

1 s, x Based on,7 ei jx;4

' it'would be dissipited by the many branches..The header piping between node 85 and 230

,is well restrained by four 4" pipes connected to equipment anchors. The wave impam at -

d" vd.

",f.i,.t n.od..e 85;80 a.n.d,60 wo. uld. be.c,on. sequent.ly card.ed by the subject h.eade.r whic.h is w

'.%s.M~/.

?

w

. c 00 1 L

i restrained.?Hence the. worst case scenario wasjudged to be an impact at node 45 resulting -

7

.... ;,.ifoEe perpendicular to the pipe as follows below.-

.o 1 q

.3 y

u +

, [ !. Using pressure ilmes fl6w area of 8" pipe (50 sq. in Ref.19) the force at no e.d 45 would m.

be F=='160

50== 8000 lb. NOTE that pressure times area is conservative since it.

assumes a full... flect.. ion.

re Conservatively, model the pipe as a cantilever Ognoring supports) as follows:

4 p

L 4 8000 lb. at node 45 4

N111-7 (9!90)

sa

=

NF 161-3 (1f/J)

CALCULATION DEPTOVCECTK)N CALCULATION NO.

REVISION VOLUME SHEET,

~

IP-M-0435 0

>10 From the figures above L can be calculated as follows:

1 A

s.

..a

~

,.c-g y

's_

[,x.

_q w.., r M w.e yi c.

.se f f r, " 4 *.

f'

~,

.g 4y;v

.k ; y, g,: [ r,," ~

f,

s

., A e 2.146 + 1,761 +.9 +.472 + A29 +.603 +.1A9,2 + 4.021.+ 7.863 - 14.723(& 7 4,4

' 4. 4. :.

s y

.f

, 1 e

a;

.a. -. <;.

.. - =.4.974' r ~

B=

1.752 + 1'.436 = 3.188' S.

~

r: 3

.,?

s

..m,

.Le.;[(4.974)2,[3,3gg)2j% =.5.91'

..5,.....

and

. M = 8000

5.91= 47300 fL. Ib..

p

. It should be noted tidt the peak pressure at the highest stress point (node 7, Pg. 8) due to '

this sce.,nario would be red,uced due to branches, etc. as follows:

\\ c.

~ DLie to tlic largerires in the 10".' pipe' '

3 y

.:.{,, ;r y; J r ' 't W,;.

.c r

b 2; s

, P o'= 160 *

'-JD.10d.

I

> a i

! r7,98132-

,4.

.a.

y m ;.

r.. = 160

s

-; j.

~'

(10.02s c.,'.T 4

,c;.

.+3..

4

,. n,

,x.

gw g,

2p

m.c.101 psid 1-t e

8.

4 e

4 N1111(J/90)

S l T, ' g,4r'- -

4 o

?

NF 1614 $90) 3f,

CALCut.ATION

' DEPWlVSECDON CALCULADON NO.

REVISOf YOLUME

' $HEET h s q, h 3

W IP-M-0435 0-11 s

-p 4e m,v-se a,.

,a i

ld be reduced as m-

Then due to 4" branches IVP71 AB and IVP03BB th s pressure wou v wu 7W~ f-..

-:.~.

, e' AjQ; :%, if.

M U Ag;~3.{O O Wp,

3 -

s,

.m.

2./.'d.-

b'"

b d l-.~

. s ;.

--p..

4.Q 4L L.M,.M N.- $;h~..

sc Nff

.Y

J J

j.p.d r.f J v U k % h"')%f

%Mepnm a w

,A:.N[f. Br. a;& 'h,i= 12.73 sq{., +.4(R'd" /eU9)m-p~

-7a/C M b d

y h

h@T h

" n

@e e awt M Mg C"E A

C rea nc m,

y mr

'2 S

. s

Ares;1,0$a w.chg7,8.9 sq. h..: (Rd.y 9)<;f 7w,r+engpy

4. y~ ~,,

j r

gg,.

a p

Bran J

, %ae y

M, ~,W:pp;

%n $+~

~+, +ggn, i

, n, w, x.

a.

A e s'# '

?

~ ~ -

u~

A,.,'. e

~

' ' E ~ %m(For&@&*hes)w@

r n'+@m

. 4 Jl G

M 4: ?5 D d

W' ! 4 5 6 J r CM A

%p;.

v 4 -

i, w,e I P

- e

~ 'wt9-

%':Q

. s 4? Ia' Jr m :.6C M-j y &r b' 1 Mt "

. ?". A 2~' ! ' w T

w 91.@mmF

~ v r'7 w 1 8.9 y' mwmm

..,n

,, y

- s ump e,.y@

g. m f

to branc r

a;jgn 101.

NJ WW Par.%

3,7ep. ym 7, W e.e. ",- _M,.~W._r F U.8 ', 4 2 73 y 7

1.

4 4

~,

a 4

5

$3 i, ' : ),.. $ ', '; Vn]a. + - e. -

n

~.

e'

'n.,.n. r

4

.,.ur s

o 6 unu n.

.m

,,L,,; k ]i l'

. -. '&,x.p.~q.

e [ j QJm, ^2 N.

n y

e,.

.sn

.92

,3 s"m" s s

.a r

> c a*.

e s

nt p

w w+,e z~p'

9. r 3J. g,.. -..

4 q

m n.-

m_..O l w ';

L wy c.

Ed.

+

dz w s...; u nom input 8,l10" pipe data from Ref' 19 and using a maximum ww.

w+

smg the equation i

4.

MlJ j

r-operating pressure Dom Ref"14c, pg. 5, the above moment' and 151.0 (since we have fat

'o

.f straight p' y + highest stress po'mt)..

. W y4 4 4 m 4;3 m.. t,1 #,'

1.

n:

e.,

=

x-f ' ' vi :.

Mb r*

r

~,~n W,

M t%,

~ %f.

%;,%RW

' ': @,. r 47300*12-M* m.l - T T. f 1

Mty pr(1,35 t75)l0.75 k

L L.>

J M'

+~'"--~r

+

h f 7 N,.i4,3.,6$ k._>.f f

+ i 299-M9 v. gtM M _, p g[., hh.h

._.f. n

Q.

y.

Q U YY. gll..

m.. ~.

o M )+;1, i :

.c..

+ +

~

d

. m l( ' m c54.

%., w;,

3G.,&M l'

3. :

c

~ p' o

.,v. n..

g, y-2... -

m '. 1 ",

~

c

-~

't~

~.+

s pu,p, ':

.5 K....S_li r.. r,..

4 4d '

H o m, #.WR*

- N A;aQ t:6 9 M, b 2.

.m.

3.,. o

.o.

%g{

y

-4 j l, L. j,, #,

w - p" 1.

%g p h'[,I. [ p.

~

,. 6. ',L;.,,,., e

)+.?. ~ '.f,y} O/]a(

y "

,> T ~'

c p3 J4

j

,3 g

t, c +4,

-#,,.~.,

a

'4

~,a

., m,

/m 3 qn.. v a,. 7;

,w w

,.t.

. m m, s

n v

This%

c--.~1. + r 4_.ou.rl.ev.,el.D allowable.

s. 3 y

7F fa., :r s-p ;.. a Y.,

JGe P 1~ v..T,,/ *.1,6 %.9

,y- ' 4,

,e. #. N. w.

kyrwell.

,,,. l

,g:

a 3, q'), b.,

J

_,., -o.s ip t

> b' E

7 m... _..

i '

i i; i1

.] }f j

,[.

m.

, h}

., / w.;. 4, p.,_

.. mu.A A,_m p,..p.g.n:6, u n, M],h h"{!

/g gay 5"l l _l

,J hf. ?0 hk

_Xu %rget

.g. h ;

a.

m k

+ hg &g{.m=. n -,i t i4. -

khi h.h,,.{1 g

h5%.

w

.a :%*:: <~ w w 'v% Y. s.cv

+

4v ;.- a i lv ge > -

1 2

mt

.{.

j: g!

(,

h. 4 V.c tSe w

a v s+

<,. -. y Ni

. +w h4 2 3.Q; n b.. - t p

4 i

j,;.=..,yy g!

f yW

.p w, ? f gu;

4. 4.. p

,z;._..q); y Q

u-e.

k.r...y.

s L,

c s.w a, 3 y-M, g ". p a e.

3 gis m

c.e.

1

.,- c n e, sw o

f :. };... 3 a

(s 4

[

y

.,m m,

s 4

n, e'"

c_

t

..u a,+ S svQ Q.'. [ct, wd::~a{. [;. j;

..,e

+

Y t

1

..a,

.., n _

2:

m'.a

a,

tu i i, i.,, -

4

'.-,3,$,..i _.4.. t a.

.t:

,m

, er

- _. c _->.

. s v _.

t

- +

l l

l lu lW ef i u

I I

M111,7 "m"~

e

m NF 161-3 p001 CALCULATK)N DEPTOWSECTION CALCULATION NO.

REVISION YOLUME SHEET.

< - 0' 12 %

IP-M.0435 m-v

. The configuration inside containment, outside Drywell is as shown below:

f p-

[

,y j

~ _, p. $.

i.

.i, r, s '

i u., y..,,

r. 7. r, v..-

, _...y s c.,g,u,

,~

t

' -.m'.'.

1 a.,

+

'j' +

,T'1i O 6, p e y [;

v

, J,k'g*7 [

d

.y'

'g.. j~'

).k 1

.C h *4 4

hTh [t dh 3

y r

& tuypo.o*[ l; ;,. &,./, nfg-MQ4.l;l Ql+3;k.Q 7%$g.~.

' [

'ElvP02 BB 40}--

ij I y

i

+

Q%,

' % Q, <,,

.di..-

. me,

...m y n

,. t,., a

,,a

+a-

'.S (&'. h Q.y.

,h.$..g ' '-QQg, Ikh.

v.. e.

..r

ht v

f; Y$

4(

(

') 3 I,

'Ekj)* h

).y y% n;p.:

.'q p

Lsyposa WT, l l,. t,3...

f._

s n x.

.u g s..,

m

- u-

-,3 5

j

' im '

'/'

/ -iwporooslA]; W j; ~,,,

.h flh '.

~c

+

a

' % k $).3.

.u '

7 g,

mgg W.

r.

. G.4

8

.i.

wt i

i.

(..

W..

y s

a j

e s

sy,

..-c_,,,

1e /

s

~

q.

l'.'

's ',

Y ih t

f s

. m

-su o-sp.

s

- n.sse

~

u, ew

{'

i A

1 " ' -

2

. 9 TO SUI,T -

,l

.oa.

+

3 c'

t

[

.. ft l

- (

(~

' i e

r c

3

.z/

c 1 -'

2 a

e ii

!,y t

e

.('

y 3

j

')

y,j '-' g (.' '=

,~r

. sw.

'q. og,.

.g g,W' t _',, gog

+

t 4

i

(

..,.c

.4',

p I

5

~

(,

4 4,.,.

f,LAtl m,

'l '

<0+ M.e.

Y i A.,,%

k.

(',

.r vj j,

r f;.'^?

l

?~

[ ',.)j w 4 ),.

y$

^"

.x,(

3. ", p c'+k-p y-'

N,

) y

+

;i

Q [b, h r e,. :

[5 'l M 7:

s 1.-

j

,s.

t s3

>e

,9 97

."U, 1.. < wu..J-

7

.e.

i, ? 'w. D f yg,,',

Reference 14b, JE F,, {,

w~ v i.'s'u, /a G.;;..

^ I U l!i U. Wi.

< j J.w.-s L.b s.

+N,*2

^

b, e a m%

.,g%g.

-9t 4

6 i-

.y r

3

^3

'd

. + +. -

.;w 4

L-

,F

.'t,' ~ ' *. (;:? y asj/M'

$,)h '. f.

r

,s

j' <?.,D; t

't

., q',,$,4,7 37 y, -

'[;E M>i

+

+ 3., s..

5 s

i

,e

,. y *

- (-..

- g y

j 9...*

,'C f

y-l l

,; (. e s

+

i l

t i

'm l

y I

?;n

)

s I

- s 4

1 l

l 1

1 N1117 (HO)

I i

1 i

l

[

7 i s

.o

! 'o

. +

NF 161;3(1/90)

CALOJLATION !,

^ DEPilDMSECTION CALCULATION NO.

REY!$10N YOLUME SHEET ~

.i.

1'~.

" - m

~.-

i IP-M-0435 0-

.131.

&,qg-g, e

A a,

x y

J

....-,,...:: n..s.

c 1

e t

?

e a.

.?

);(

i The afrect of the 75 psid pressure surge 'on the above piping can be assessed using ths 7:2 a ffollowing simple' beam modeltTlie worst case force being at N. ode 20.

~ 3..

@c[:,;

3 m

3 v..,e.. :.m $;?)4 p A'jy,. s,.

m m s. q. %n.g?,(;x,,

xA.

el p.g.y;;'p g' T, &p* 5 p 3,, ;

,. y nep y*

.a; gps.m.k 'o - -. [5,6<;.pmw} i;;+!t. a.g; S, q,a-l.

g

.m t

w

-,d

.eyAyy

+

.p g.

m 44 nr j,

., t

- 'f e

e j;p e.u.

'r c

'V

(?,. psp f.y.-

~.y.

.. a g l.1 M,.D s y n y p q(M6g;\\.

y,

t

.. wj?q1.;m m,

A; ** ; o, 9 ohW, _

r ad-

-

y, o..:

e m.;,,, J. ; _

' pfy%g?

w

,$[ L 7yy4

...a m.

p o g.9 s'%

n. wry.:*nf wrme p* *3 3 l.- -+

g

%y; 9/

$Wy

.Q

, &); Wh; bk h $ h ] A h2g'4U15 % iK M h??;. '

A-.y.y :

4&f& f l

&R

& kdL, J GQ 1

y, %w@N.%n.uw!)a pm Wpwyngkw ;ppkg.-w. : 4 u' age 11 as follows!

v

.1 > p+@:.u:s.i ax.4 pn u

y 7:gny j;4b~cinbe%m Ry4 ra

,f 1igt calculated froin~the, figure on p 1 T O Thele:

. ;W.

n e g w p %y g:en.mp-tp 1.- > - -yyr-.

.;~ m g

+

p y'; z a

y;+MNa d(4.202t5.071)2d10.876+ 9.008)'J"l

L 9 W; p n af.s n

< L,

. r,

-..._h.a a w% e,r; rwa,

.y-,,,;.-

.4

_.g w

.~,.s.y,.mww..wm y

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CALCULATION DEPTIDIVISECTON CALCULATON NO.

REYislON VOLUME SHEET IP-M-0435 0

14 Calculating i (stress intensification factor) for 10" standard (1.5 dia) elbow using equation from Reference 22 i =.9/(tn R/r )2a 2

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CONCLUSION Based on the simplified analysis of worst case piping both inside Drywell and containment, recognizing the robustness of typical piping systems, the conservativeness of this calculation and the relatively low pressures introduced by the transients the effect of the transient is judged to be insufficient to cause a catastrophic failure of containment.

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DATE PREPARED CHECKED ENG'R APP'L R EV. DESCRIP1
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1. PIPE 1+2+3

4. WATER HYDRO 1+4

3. INSUL.
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1. PIPE 2 fL

3. INSUL.
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~~4. WATE R HYDRO 1+4 D~~
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PIPE DATA l-WALL INSUL. WElGHTS - LBS/ LINEAL FT. ~ O.D. SCHED* WP. THICK THICK P
2. ftU D

1. PlPE

3. INSUL.
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