ML20249B175
| ML20249B175 | |
| Person / Time | |
|---|---|
| Site: | Clinton  |
| Issue date: | 01/23/1997 |
| From: | ILLINOIS POWER CO. |
| To: | |
| Shared Package | |
| ML20249B170 | List: |
| References | |
| IP-M-0435, IP-M-0435-R00, IP-M-435, IP-M-435-R, NUDOCS 9806220136 | |
| Download: ML20249B175 (250) | |
Text
,
Attachment 3 to U-603026 I' '
SHEETIOF 14 CALCULATION COVER SHEET DEIrr/DIV CALCULATION NO.
TITLE / DESCRIPTION:
NSED/M IP-M-0435 .
EOP-6. POTENTIAL FOR WATER HAMMER TOPIC BLDG /ELEV/ AREA QUALITY SYSTEM CODE
' RELATED (or NA) (or NA)
(Q or N)
O VP M91 , ,fNA
-4.
. 6 N.
..J. APPROVALS -NAME/ SIGNATURE /DATE VOLUME <
READY MR INCORPORATION: , , ,
CORP PREPARING REVISION PREP REDBY _
FRIC HALVERSON DUS REV; + g 7 g] 7 -~
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- MICROHCHE ATTACHED:'
oAn , samAwas CONFIRMATION REQUIRED ,
.s w YES Y ,NO YES NO PAGE NO(s) _
CHECKED BY ,Not Applicable : *
' 'wr VOLINCORP. ASSGNMNT.
b . $NMAw=E MOD. ECN CR MWR (Q COMMENTS:
7fMy' G.L. 96-06
, REVIEWED BY Ec[.b A-
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CORP PREPARING TIIIS REV. NO N/A 4
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04n sum 4was CONFIRMATION REQUIRED YES NO f YES NO PAGE N0(s)
CIIECKED BY ramt VOL. INCORP. ASSGNMNT.
COMMENTS: MWR REVIEWED BY ramt i I !
9006220136 900615 l l PDR ADOCK 05000461 L__________________P____ _ _ .
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CALCULATION NO. REYlSION VOLME - SHEET e CALCUtADON DEPTSVfSECTION
/
- , 3, IP-M-0435 0
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f";4 9py&qq . gf, 3- -
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64, ' .:9. .-W S .i, _L >L _- x,.r; ..,h.,sy.m.e-n 9l-f METHODOLOGY, .u'n .4 .L2o '[A 1g - .i 'M.A ..-r; 74gM,p.N( M.
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.dltobe'use.d evaluate)' water h.'_4_-
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a:lifi approach. a _J. ... ,,* tionah.ty of
- ,'.f nM3- vz y ;A.:.sunp w '.
- C% )Eco61d the systeni need not be assured since thM a're n'on-s, afeh systemsci A gross failure ofcontainme be a'codcern.iSince snplified melhods vAlllie adplied, s'omejudgment will be Used toi
/dN u i ailcatastro.p_h c f,a ure... S.ee analysis for additional in
.s ,, 9 ;- . '
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. +S " REFERENCES ^
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t7 p 4 1.s- f 3-q:. . v; .. u.
o 9-0.02.R/W! . _ -
4 MI kg)v ,1.M05,11.0,S ,p .;I. ,ti -
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+a.+ ,e,...] t . .
_ r m,- m.: , o gw M66-1109 003.R/S - . w4 uu .11 ,p4 M c .
te v) W $*3 y } [ t
- .3 s; ',,4 y% @y 4-t e~ vp v.m. ..
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~V5 J4 M06-1109-005 R/U j . _l ,
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. ~ - ..p 6.r & ~ - .rl o -"
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syMQy . tu v.i &.~.v.t J , .,
, -- .. - - .,- = + , ,
- ' 4 m- ~ +. y +,
a4 dWQf W 7-:
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American'
.: n irFilterDrawingi.
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w e $ ,$ M:p,77m) rid 701110832-C4 a. . s-M}
l Z ff) ' } b).R1070)1110543-C - 1 l
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v #n. .+c ..r. ~,a )iR1070;1380336-B
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77). ' M05-1117-019 R/N ' 1 l
8); .M05-1117-026 R/E 1 ,
1 l . 9) M06-1117-060 R/P 1
l
- 10) M06-1117-061 R/T l
l 4
1 i
N1117(9S0) i i l
NF.1613 (tSOl REVISION VOLUME SHEET' DEPilDMSECTION CALCULATION NO.
CALCULATION O. 4; IP-M-0435 .
4
- 11) M06-1117-062 R/G - s
- 12) : M06-111'l.063 .R,/..G.n y t ;+n . wn
+ -
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,- ,..2; m e.o .
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1_ j ', %.a, f,lV.P02 R/2
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- p. :c)i1VP03;R/3 '- t '
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- 3
- 15) : Hydrauli :ofpipelines, J, Paul Tullis, C1989, John [Wiley & Sons.;
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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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REVISION VOLUME-
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- 2) U lPef RAferencel17,!AAmant 2,:pg.!6lthe pressure surge equation for vapor bubble 9 3 6[ . ]c6tlapsliAH = C/2g AV.EWave speed'(C) canbe determined using EQN 8.11
'g.' ; i p.p y:p p,w;; .~.nQ h,.-m., cts)afe froE T, unis='CQ=K/p-]"ag!,tKd/Ee]",.from. pg J
s 200 an,dwn 201m /iv 4+%q;:qq@
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m%y fy 6 of M is X10'n .w psipp v 1.94' Slug L /fy; E = 30 X_10. t ps.v and from y %y; papr tu &g pn y g gm-g/forsteelpipeKe3;2:gdp m . A ..; .+ nm a ,..
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Per.Ref.e,diametel'r
- ofhg.4e re.nc.ebir At nesthrou h i.-.oL6,h a -- 57 t s~t'The system branches m.to small h.w-~
throu,si13 and Ma e; ~
14~'t.h Aai j ifihns asthsyijyiroscliD%g ~
c6olers.iAt conbranchesammen .
the pressure wave would be reduced
% /j by$ltAsthey.q* "0thtwafe'splitlMAt' size increases,it#T
. i 13.[2 gr-' woul i.5* [Udi5mefers%i)ared,$qw.edrddMij5;$C.2.
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l M at one pomt doe.s not s6bject, pg',; I Torcomplexpipenetworks,atransientgenerated _W P f Mth$ $ eidire p 1
l Q (;
$x vg$@@" ,,,,, ; pp j
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- 1, Ba, sed t. on the discu, ssio. n above, water hammer is not a concern relative to containment.11 ~7
- ' Integrity for the;WO tysthmiue'ttthelongdissace between Drywell and the ' .pf 1 -
- containme'nt isolation' valves (CIVs),!small diameter piping in the Drywell and multipl8Ei ~ <(b
- 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. ' l 1
I 4
N1111(MK5 l
i NF.1613 (1/90)
CALCL'LATION NO. REVISION If0LUME SHEET CALCULATION DEPil0nftSECTl0N
.6
' IP.M-0435 0 ,
~
- 4) 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
..], ' loo'p systeins inside containmcht (Ref.1,2,7,' & 8) a significant polume%i%;ifiyduld
([. ' 4
' be developed since there's nowhere for the expanding va
~'
- valve IVP024B is set'at 140 psid, which gives it a saturation temperature s6id330 F, ' i i '
J. G j Ref.19). Not withstanding the above, the configurations such that Af4ipdiWould be '
2 - present in the header supply and return headers as shown beloW (from ..Ref;14d). L ,( ,
, . . . , _ . . . _ * .,.+,..,__4,t.. -
- [1t _ WOI_
p _
SQQW
~s --
Iwposoaa jvp " [4vposooi.R .
@ ovrowc.> -ovam.; e where vapor .
will collect
- l & r @ O r 4.comm. o d, s .- _m (eveo2LH 4 . - - .--- < " "y*.g.,hg*
O l : ~ '
nuw. 4
@w Y
- 4 .,
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L. :c ,.
p S tx eam n.i . i. , , . ,
,4 j ,'.> ,e n.naw py@pn ,
j Q. Q 7 "( ~' <
, [; 4
' = a .,
+4 iy f ^ ' 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 f[W Ml, j intdce in the 4" lines.kince the vapor is readily colla;kible it offers nearly no resistance. a.f 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 .
l
~
- discussion in 3). ' On the return side of the heat exchangers the collapse and impact would 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.
N1117 @90) .
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< NF.1613(U90) t CALCULATION NO. , REVISION '- . VOLUWE . SHEET m
.e l'l' ,
c CALCULATION
~s
. DEPTOWSECTION I
- M p @njg -
,eq y ,s . IP-M-0435 0 <
17 3 -
%.; . J.p
'c'g ,& ,A N'M , ,, j o IE i. , _
- 6)f lFrom thel figure shown on RLs 14a'and 14c it is apparent that the paths through~thef O
~
- N N 8%upply leader and the various 4" line are different lengths so that an advancing water;@
header at .different times. ;The brarich flow'with -thetka
'gM,g, 44 F wk4 MM front r.w eaches n~the 8" wreturn w .- shortesA %3s- A le m the return he~de~r:first,.?T at 1 mM .a - '.
.Wwq ilis~tance to travel would co. llapse th~e vap~or &a'S,u
- ~ . ~ . . . . .
v- a n J X to co w
.c
- M n .~ ~ -
n c. y p@w T W#
1 6Ww yd 4%y.flo.p~s app ~E=-
5.5 fthec veloday in the pipe under a full flow condition.?It.is e W "4@
Nyg W J d_be.i_mu* c. h_ lo. w_er th,in_t_his ~du p ib ksdon'di,sc,usson above.W 3,a _!
$j r . -w 4,W_ lowWiocityf5]
-i : y$ pggj. th_e vil'_esty._w_sd_,5 ft/see wilbe,used in thisE.. a, rin ,
~.4. .,w-. n 4 my a - . - u _ w , .,y.4 .
y Moccur[sh destion~ of he' system 8 fo
-e r %o. p, a4%.q g. o s .,
qv ., qm . ,
j t , c,
' 1%, m.[7)hFoEco Rb mu'st d@ocud%a thisto h' p~ pen the containmentisolation Q'valv
~YY L
g 7 ^1the epressure puls'e'would travel through the gate valves o j '
tv ; l pip *mg'systembaly using simple Waas e s ' N, -
e a ?
ywu Q ~oy tf e~q av by % ,f;pTr y n. - . ,.
,. , . f ; y *.s w L Ze Q n)+O ..j A. l.evelD all.owable,Wf _36000, 8 .
-n -, , ov . r Hfollowpg6quation: rL'- . ..
g 7F psi.%g
- 1. '
(2,.7- ;{L
.1 a y:g p~@tym:p~a~w mr awtge . a p< v qlm?y
,m - +
v ~. p s y; Qxp ,
v;;:g f y'q.:a{jf.jg{ (
cl+4 -
PDog M,,7 - ;
aWW O & ;.$ M + 9,b ;
v @n[N nmps wN .c JM M 4t- - Zuae o A - 44+%
.a a u.
I,v" m$'.h N h.4 N y
P V V;.
s, .'Y!
h ;w*
.q
,, M % mbws;% w mg.w>e +
. . cf r
.. r, .. ,.
to the allowable .
,@Me~L N m .ote tint A shape factor of. .1.7 fian Marks l pg.n 5-21 .
could be ap+ li 1,
- 7. 1 ; W. nnation ofth.. e ..,- OK..- -.ded we. don,t
~
/g nce plastic pipmgis provi ,
'wikeq %;l{!
%ypq sU Y above d Will n$t sii td ussd w wis the de.fo.- analysis, - . which is; conservative. xC V J 9n%+
r ' -
iX -
m in L2}ma m gi %y&3 %m ys y up >
- y. u -mnw y a g n e
9 c.
fg .I9)Qw%;
w -m vwpm.}pmw"s illfoeti .n ,- on;c. .s ,, .ThNiiajl s ~gv siss.nvy: areas n +-clos i sthe area ofmterest.gYt .-
1p, 4.c e ' '@v.
%p;N 'L ' ,' w[ &v3[wL Lv '
, 4:g ' '
n ,~f
} ,:& Mj&&W9f, ~~
s al*inment walls are very strong. [Thhy will wnot be' rigo sa .Q:n[
a "10)$y Anchors Am atDrywelland conta .
i ; jdd
'J. ,..;_ .ilooked at here'. They are u ge to not e t e weak link. The configuration b h is such thath
?.' ! pip lc ' stress.w. .~ .y ~ill ebe. li:niting. -
l u
11i
,y a _, .
I 6
4 1
. N1117 990)
l i
NF 161-3 (1/90J CALCULATION NO. REVISION VOLUME SHEET ,.
CALCULADON DEPTfDIVCECTION IP-M-0435 0 . 8-
- g.
ANALYSJfi .
The configuration of thepiping in question inside Drywellis shown below.),a -
v -
[ .y.t_;p,y ;;j .
~
!pT
^
s g j j:ridp
+ -
,,;W. g n... a, g ,..
= , -
- u < ,. . . . ,
d ,'* -Qj? % 6
[. .g /{. ]. [
. 8 i,,. W ):' ,
n "gg;gy
.. s
..i- .
? .,*.. - Vk..w .$'Y
.,u
/
ltypt,,' ..
. GQ( o n - ,
, t:No a T* 8' (7) k 4.024' '% _
a 99f -
L t 11E*
1.7M" 8 ! ! ! -l '
.( . ;q
, 4VP03DB40h 6 s g
El. 770.00' t
. EL 7
/
0 p
rOR CONT.SEE 9 / , 71 -
1VPO4 SHT.4 ,
N:k, [ (MsM '
f f 0.74 5'~
)f
~
. 4.76 5'-
.o : lV
'LTS( ,. - *. . Y r ,
MO.583'- W:, . . '
.e.6%'d 7' 43G.>a 1.rwm _
1 t'k .. ( ; ,
,,. ~ hlVPQ3002IV' t ;
.= ,
+o
/f .
p '. . h ~, e f , ,
u , , -
'*tt ;
g ,
- r ,
&'[t'f;l' ' '
q ,
- .v
- t .
~
QvPtBBAk) y . ,f'%, J .
% N s s '.
/ .- .,
~;i ^ '
n y $, h e .
E ; *
(4VP03DO 8 Y( Y ,,
34.,723*. .-
, FORCgT.SEE e PLAN B SHI2 -
4 Reference 14? Plan A l
Ntt1 4 W) .
r
]
,, . o .. l NF.1613 0190) -
REVISION VOLUME SHEET.
DEPrfJNI5ECTION CALCULATION NO.
CALCULATION
\
~
. IP-M-0435 0 . 9 .
2 a .
\
.r.
1
- mar e
. e m4m m a;ca y
, s
+
c,m. . ., + ,
.we go , .3 -
ss.aswr. -
, y,: . g,.n ', ,
._ewsmo %n
.o sL. s U . ,
- s. m . . w.c w :S s a <-
- (
- x 1,. _ 2. o
__ .4."u$
7 g.y i y?dge 4 < px Mj. w 3l _f ;,,.gn _. i .
- e. m 3,e
- .,v n @ sy
.s., x, . g;+ - .
a -
- ewu.a u .
- :,4 ..
w m_. p; w,.i o o .
,#.m , #. y, gp. . , ,.s i. e g
p
~
"; q q c
~ ?v.q; T g ;, O.
, ,g' ,
~
^
.; Mbda=Md m. h.2 i y
. .L d,[w-.e; M
, posAm a Me AE.8, 99 ,
WPoem
~=W
- ... ,~. _p.
1 7 .- ...
~b.,'.
, .sccinon 'e-2' m . . . .
f ' '
.,L" '
.y. ;
, Reference 14c.
.c ; - .e .
e ... :.
z a-3 , +;; . .. .
u iThe inipact would be~ expected to occur'near node 85. Coriservativel[u, sing p5.5 ft/se
,a .] :,
g j'i(assumption [6)andu, : ~,sing AP7. 29 AV(Input,2)'
. c.: $C c c, y.a .am' ,: .y m -
n: ;;
. w :. ..
y%m.
"L_APM.29..t.5,57160s psi ,
. ... . w .. e. m, ._.
, y )'3: ;4 ?. .. .
1 1 .,
p q.y qQ - . ., Q >p j , , , sb,ov ,t is;ap. jparent that as the press,ure wave travels upstream
,, s , x Based on,7the sectioriview 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 w - . c .
'.%s.M~/.
.. 00 1 L
- i restrained.?Hence the. worst case scenario wasjudged to be an impact at node 45 resulting - "
.o 1 u +
7 q
.. .. ;,.ifoEe perpendicular to the pipe as follows below.-
- .3 y ;, . .
, [ !. Using pressure ilmes fl6w area of 8" pipe (50 sq. in Ref.19) the force at no e.d 45 would
- be F =='160
- 50 == 8000 lb. NOTE that pressure times area is conservative since it.
- m. -. . . .
assumes a full...reflect.. ion.
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)
REVISION VOLUME SHEET ,
DEPTOVCECTK)N CALCULATION NO.
CALCULATION
~
IP-M-0435 0 . >10 From the figures above L can be calculated as follows:
' A 1
- s. ,
..a ,.c-
. , ~
g y 's_
[ ,x . _q ,
w .., r M w .e yi c.
s .se , , . .
f f r, " 4 *. f' ~, .g 4y;v .k ; y, g,: [ r,," ~ s ;f ,
e y
. ..f, A e 2.146 + 1,761 + , 1.9 + .472 + A29 + .603 +.1A9,2 + 4.021.+ 7.863 - 14.723(& 7 4,4 ' 4. 4. :.
a; .
.a. - . <;.
..-= . .4.974' r ~
~
S.
B= 1.752 + 1'.436 = 3.188'
' .,?
r: 3
..m, s . . ., .
.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 .cW ,; . .
, . r b 2; " >
, P io'= 160
- s
>a '
I
'-JD.10d.
.a. ,4.
r7,98132- , y m ;. .' ! ,
r . . =* 160
- s ~'
4 -; j . (10.02s c. ,'.T . 4
, . n,
,x.,c;.
g, gw -
.+3.. '
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)
CALCULADON NO. REVISOf YOLUME ' $HEET h 3f, : CALCut.ATION ' DEPWlVSECDON s s 0- 11 3 q, h :W
&. , IP-M-0435
-p 4e m,v- m- se a, .
,a . . . . .
- Then due to 4" branches IVP71 AB and IVP03BB th si pressure would be reduced as v wu 7W~ f- . . -
- .~. , e' - ,
AjQ; :%, if. M U Ag;~3.{O
.m. --p..O Wp, s , -. , .
. 3 -
sc ...
$;h~ ..
.p.d r.f4.Q J v4L L.M,.M N.-
Y J * %
p~
hNff mr U k % h"')%f
- J 2./.'d.- b'" b d l-.~ . s ;.
jC"E y
. sM A Mg @e e awt h@T ,A:.N[f. Br. nc a;& 'h m,
,i= 12.73 sq{. , +.4(R'd" /eU9)m- y
-7a/C M b d p %Mepnm a w " n Brana
'2 S C h rea - . :.
y ~ ~J-sq. h. .:(Rd.y gg, .
~+, +ggn,-; Ares;1,0$a w .chg7,8.9 9)<;f i 7w,r+engpy
- , %ae v %n $+~ %.-Jr
~
u~ A, .,'. . 4e a.
?
- 4. y~ ~,, r r
, n, -
M w,
Jl xG.
M, ~ ,W:pp; w,e I %p;. . s 4? Ia'
' 4- 4: j P
i, ** e ~ 'wt9-6 J j %':Q y &r b' mwmm m 1 : .6C M- ?" .
A 2~' ! ' wT
~ v r'7
' ' E ~ %m(For&@&*hes)w@ Mt " W' ! 4 5 :
n'+@m w
- g. m a;jgn #
NJ WW Par.% 7 w 1 8.9 y' 101 .
f 3,7ep. , ym to branc r 7, - s umpa e, 91.@m mF
.y@
",- _M,.~W._r F U .8 ', 4 2 73 y Wunu 4 e.e. n. .m 'n.,.n . r *4 4 4
~ ,
n ',
.. ,n1.
~.
s
,, y o6
$3 i, ' : ), . . $ ' , '; Vn]a. + - e . - .,.ur n e,.
e' y
,,L,,; k ]i l' .sn > c
- e [ j QJm, ^2 N . r 5 e s ,
a*. . ,. .. ,3w
.92 , < ms"m" s s .a
- . nt
. - . '& ,x.p.~q.
g, . . - .. .-
- 9. r p
q 3 w+,e z~p' 4 . #
n.-
J. '
Ed. + m_wy . .O l w '; . L w+ ww. : .. c. -. ..
MlJ ,
dzsmg w s...; the equation u nom input 8,l10" pipe data from Ref' 19 and using a maximum 4 .
i j r- operating pressure Dom Ref"14c, pg. 5, the above moment' and 151.0 (since we have
'o .f -
4;3 n: e. ,
... W .$. , y4straight 4 4 mp'fat y + highest m.. t,1 # ,' stress po'mt)..
~ ,~n
= 1.
W, ,.
Mb r -
- M t%, x- f ' ' vi :. r* .
' ':~ %f.
1 ,
%;,%RW
@, k . rMty pr(1,35 t75)l0.75 -
47300*12- -- M* m .l +~'"--~r - T T. f '
>,L
+
J M' L.>
M9 v. gtM M _, p g[., hh.h h f 7 N,.i4 ~
y.,3.,6$ k._>.f of
+ i 299- ,
- . ._.f. n .
- m. . ~ .
- Q. c Q U YY. gll.. d l' %. , w;, 3G.,&M 3. :My-)+;1, i :~.+
c g, , , .
.,v . n.. . < -
~' p' o
.#smpul( ,p' m c54 . . , .c.. + +
2...-
't~ : :
-~
, m ' . .m. 1y ",
o m, #.WR*
- N A;aQ ':Ht:6 9 M, b 3 .,. o .5 K.. 4 %g{ ..S_li 2.
4d 'r. . r,..
.o. ~
-4 .-
w$,- p" 1.
. . ~
j l, L. j ,, # , c
- y" J4
%gj p3 p h'[ .- ; . .! g
,I. [ p. , . 6. ',L;. a ,3 c +4, qn-#,,.~.,
)+.?,w. ~ '.f,y} O/]a( w ,> T ~'
,, ,., e ,.t. . - . m m, s * '4 .. v a * .,.. :7;. ~,a n .,vm, t,
/m 3 fa. , :r s- p ;. . a Y., .-- 7F c--.~1. + r
,,,.l
,g:
- a ;s. 3 y .
P 1~ v..T ,,/ *.1,6 %.9 JGe J This% kyrwell . 4_. ou.rl.ev.,el.D allowable. - ip ,y- ' 4, ,e. #. N. w.
3, q'), b. , _, ., -o.s t . , . .
m.
7 m ... _ . . *i '
i; i1 .] }f > b' j ,[. ,
E -
, h}
.. mu.A A,_m p,..p.g.n:6, gay i ,,
- /g u n, a.
_Xu %rget .g. h ; ., / w.;. 4, p .,_ m
,J hf. ?0 hk khi h.h,,.{1 kM] ,h h"{! $ '
,>.: _' 5"l l _l .
w h5%.
< , . - . y + hg &g{.m= mt . n -,i t i4. - + . : 4v ;.-g a i
- w . - ;2
(,.a :%*:: h . <~ 4 wV.c w 'v% Y . s.cv 1
a v s+ -
lv Ni ge > -
p j: g!
f yW 4 i ,
.{. tSe Q j,; % .=.. ,yy g!2 3 .Q; n b. . - t ,. .
c M , g ". p c.e.
o
,z;._..q);
- .e,+ wyh4 e.
sw k.r. ..y .. ,- c n 1
, s L, s .w a, 3 y-u- ,
.p w, ? f gu; m
3
- 4. 4.
gisa e.
.p
- 4 a (s
- m ,
[ y
,> .,m c_
s 4 t ,
. .u f : . }; . . . ;3
_ , . - n, __: -
e'"
Y +
a,+ S svQ Q.'. [ct , wd::~a{ . [; . j; t
..,e
..a, 1 ,
m'.a . . , n _ -
2: . . #a , tu i .
4 i , i . ,, -
.t:
'.-,3,$,..i _ .4 .. t a. ,m
. s v _. - _. c _-
, er . .
t
-+
l l
l u lW ef i lu I
I M111,7e"m"~
m NF 161-3 p001 CALCULATION NO.
- REVISION YOLUME SHEET.
CALCULATK)N DEPTOWSECTION . . '
IP-M.0435 < - 0' . 12 %
v ,
m- , -.
. The configuration inside containment, outside Drywell is as shown below: .,
f p-
[ #,y j
.iv,.y' r, s ' i u. , y. . , , i .
,~
t a., .- :r. 7. r, v..- _...y s c.,g,u,
~ _, p. $ . +
' - .m' .' .
.C 'j' +
,T'1i d O 6, p e y [;
y
) .k 1 3 4
. r
, J,k'g*7 [ hTh [t dh 1
'g .. j~'
7%$g.~.
y
'ElvP02 BB 40}-- ij I h *4 ; i
' [ l; ; ,. &,./ , nfg-MQ4.l;l Ql+3;k.Q
+
& tuypo.o*[ Q%,
' % Q , < ,, . me,
...m y n
,- > - , . t ,. , a ,,a +a- .di ..-
v.. e . ..r v ,
'Ekj)* h
( *ht
- I, Y$ .
4( f;
') 3 Lsyposa ., .'q p ,h.$..g ' '-QQg, y% Ikh. n;p.: ' '.S .
(&'.Q.y.
).y h WT- u-, l l ,. t
,3.. . : ,. . -
5 f ._
~c +
s -
n x.
m -, .
g s .., # .u - -
j
' im '
- ,3a
'/'
- / -iwporooslA]; W j; ~ , , , .h flh '.
mgg
'. G.4 % :k8 $).3.
.u ' -
, g, W. , ,
7
" r.
.i. wt y ..- ss i a . - (..sy,.. . W..
,, . i. j - e ,
..-c_,,,
s 1e / >
- , ~
Y 's ' ,
, q. , l' ih t
m f ,
s .
~
s _ , . , -su o-sp . .,
< u, ew - n.sse i A
{'
1 " ' - 2
, .oa. .
.9 TO SUI,T - ,l
+ .
c' t 3 *
' i [ . . ft 2
' l
, e
- (
r
(~
1 -'
c -
3
.z/ a c
e '-.
ii t !,y 3 $ e .(' y ,
y ,j '-' g (.4', .' '= j
, (
p +
') .g , t 4 i 5 . . , .c
~ ,~r
. sw . 'q. og , . : , g,W' t _' , , gog .
I m, . . , , , ', ,
4,. , . > 'l ' ,
(, 4 Y f,LAtl *
- i A. , ,%
<0+vjM .e.
.r ,
- k. (',
- . . ?~ j, r f;.'^? l
- [ ', .)j w :y$4 ),.
y-'
);i y
- , Q, [b,
.x ,(
h r e, . :
,s.
+
3 . " , p c'+k-p
- [5 'l M 7: .
t #
N, ^"
1.-
s j
- 7 ."U,
.e . ,, , . ,
1..s3< >e wu. .J- ',' ,9- ' 97 ,
G.;;.. ,
Reference 14b, JE F,, {, w~ v i.'s'u, /a
- i, ? 'w. D f yg,,',
+N,*2 # , * ^ I U l!i
^
U.-9t Wi .
b, e a m% 6 i- .y
< j J .w.-s .;w L.b s . *. ,g%g
.- 3.
4 r .
'd '
.++.- : *^3
~ ' * . (;:?37y asj/M' 4
r ,s
't L- ,F - .'t,'
'[;E
- j'+ !<? . ,D; . $,)h ' . f. y, -
., q'-t,,$ ,4,7
- +
3., s . . ,e 5 M>i s
i
- g y ,. y
- j
(-.. ,, <,
f
y-
, 9 . ..*
l i ,
,'C s + ' .
,; (. e l
l t
. 'm i l y
. , _ . I s ?;n )
_,. * >% 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)
.i. YOLUME SHEET ~
CALCULATION NO. REY!$10N CALOJLATION ! , ^ DEPilDMSECTION
~.- 1'~. " - m i IP-M-0435 0- .131 .
&,qg- g, .
. e x A ,
. . ..- ,,...:: n..s . '
a,
.? ' ?
- e a.
y J -
c .- .. 1 e t ,
i The afrect of the 75 psid pressure surge 'on the above piping can be assessed using ths 7:2
);(
- @c[:,; 3 a ffollowing simple' beam modeltTlie worst case force being at N. ode 20. ;~ 3. .
m _, .. m , ,
xA. 3 v. .,e.. :.m $;?)4 p A'jy, . s ,. ,. y nep w%n.g?
t ., y*
el p.g.y;;'p l. *. q,a- .m . .
[5,6<;.pmw} i;;+!t . a.g; ., S,
-,d .
'f
.p g. e ..
g' ~.y. T, &p* .a;5gps.m p.eyAyy 3,, m; .k 'o44- - . g m'rs. q. , M, ,(;x,,
+ t : c
..- e j;p nr j,
(?, . pspe.u.
'V y l.1
. . a g
.D s y n y p q(
r f.y.- #- : M6g;\. ohW , _
e m .;,,, J. ; _ ..
w wj?q1.;m ad- m , A;m.** ; o, 9 t g
- y, o. .: ' pfy%g? .%
...a '<, *
%y; 9/ $Wy p o g.Q .9
,$[ L 7yy4 p* *3 3 l .- -+
- n. wry.:*nf wrme
.y.y : 4&f&
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NF.1613 (1/90)
REYislON VOLUME SHEET DEPTIDIVISECTON CALCULATON NO.
CALCULATION IP-M-0435 0 14 Calculating i (stress intensification factor) for 10" standard (1.5 dia) elbow using equation from Reference 22 2
e i = .9/(tn R/r )2a l
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- 2.48 *33300 *12 29.9 4(3 65)
= 26.4 KSI This is well below level D allowables.
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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~
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_ 155 2958 iVP03AF 4 D 100 A- to6 B 150 13 5 46 165 345B 4VP03AE 4 D 400 y A tog B 150 135 45 355 727 1VP03BA 4 D 400 A 106 B 450 135 4!
605 660 1VP03GA 4 D 400 ' A to6 B 150 13 5 4d 707 76 5 4VP03AD 2 D 100 A-tos B '450 135 45 708 805 4VP03AC 2 D 400 4-10 6 B 150 13 5 47 712 845 4VP03AB 2 D 100 A -to6 B 150 43 5 4d 720 '895 4VP03A A 2 D 100 g 4 106 B 150 13 5 4(
VALV@
R NODE POINTS VAL. STROKING VAL./ FIT. WT. LBS. OPERATOR WT. L([
TYPE PRESSURE TIME (SEC.)
E FROM RATING PRELIM. PRELIM.
V. TO OPEN CLOSE ACyAL ACTM
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- AD- 45 .. GLOBE 450 ,
5 76
- 65~ ~10 - - j[p % 300 (134.7( / u c w o e.s wr. oc fae f S'1 200 205 GLOBE 450 - 120 \ , _
-- 245 :250.1 GLOBE 450 j20 N R' i 285 290. GLOBE 450 120 /U 325 330-GLOBE 150 120 /
AlO 415 -GLOBE 450 120 /
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\ _ 650 655 GATE 150 83
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! RELEASE RECORD J
I REV. DATE PREPARED CHECKED ENG'R APP'L R EV. DESCRIPT(
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OD SCHED WALL INSUL. WElGHTS - LBS/ LINEAL FT.
P
- 1. PIPE [2. ft \. INSUL. T 1+2+3 4. WATE R HYDRO 1+4 10.750 40 0.365 $$ 40Isoo] 34.@ (274j 6 9.9747 3(200] 74fyoo]
10.750 40 0.365 0.50 40. 500 34. 200 8.625 40 0.322 0.50 28 QOjO 21.$oo
- 1. 9( 73) G00 \ ] / ~/
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4.500 40 0.237 0.50 i 10.790 5.510 0 90LF \ 17. M \" /
4.500 4.500 40 0.237 0.50 0.237 0.50 10.790 5.51l] I V(' ,h y,./
40 10.79 0 5.5d0 .
U U _ N 33 Y r-4.500 40 0.237 0.50 10.790 . 5.5% :- /\
4.500 40 0.237 0.50 10.790 _5. 510__
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/ \
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4483 6) 74 7' Apyhum 3 2.375. 80 0.218~ . 0.3a 5.020 1.279 448 6 74 7
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2.375 _80.. _ 0.218 .0.38. 5.020 1.279 0.h4 8 6 747 / \
2.375. _ 80 z0.218. 0.3 8 ~ 5.020 4.279 0.heB; 6.(I47/
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@PeCIAL FITTINGS DATA FLEXIBILITY INFO.
VENDOR DRAWING NO.
T REMARKS O.D. E THICK y,
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10.750 ANCHOR / DARLING Co., W 7920250 A 4VP014 A
% 8.625 CRANE K-6660 C 4VP013 C O 8.625
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. BLE 1
_76 5 775B :1VP 3 D 100 F Wos B 150 135
- 805 8108 IVP 3 D 100 Am B 150 135
. _845 850B IVP 3 D 100 M06 B 150 135
_. 29 A20 iVP7l AA 4 D I00 A-io(, 6 ( Vo 13 G
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VAlt R NODE POINTS VAL. STROKING VAL./ FIT. WT. LBS. OPERATOR WT.
E TYPE PRESSURE TIME (SEC.)
FROM TO RATING PRELIM. ACTUAL PRELIM.
V. OPEN CLOSE AC1 735 740 GLOBE 600 [23*T 785 790 GLOBE 600 l 23"y 825 830 GLOBE 600 '
23*f 865 870 GLOBE 600 (23*/
205 210 FLANGE 450
- 30 2#
220B 225 FLANGE 450 10 250 255A FLANGE 150
- 30 2'
2955 300 FLANGE 150 10 I. _
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745 750 FLANGE 600
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b
- WALL INSUL. WEIGHTS - LBS/ LINEAL FT.
THICK g THICK P P
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) 3.500 40 0.216 0.38 7.580 3.200 [0.6091 11.569T\ /
3.500 40 0.2f6 0.38 7.580 i
3.500 40 3.200 ' O.609 11.2 89 I
\ /
i 0.216 0.38 7.580 3.200 l 0.609 y 11.3 89 \ /
3.500 40 0.38 7.580 '
11.3 69
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? 1.050 80 0.216 0.38 1.470 3.200 QQ09 ; \/
0.15 4 0.188 0.2Q8) I.9 $6 } ,'N
> 1.050 I. 2.050 80 0.154 0.38 1.470 0.18 8 , N , V / \
80 0.38 1.470 /
0.154 0.188 ' z' [ \
I 1.050 80 0.154 038 i.470 0.186 Y ! N
> 1.050 80 0.154 0.38 1.470 0.188 J J __ L 5 4.90 Ao 0.2h7 0.sio ' I0 79 5.51 [0.904 l 7. t o # . ,_ . nm
, ~ _ . - _ s gaaiav nPERTL RE CARD 9 8 0 6 22 013 6 CD mo Avaeyn
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R VENDOR DRAWING NO. E REMARKS L O.D. THICK y.
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V. OPEN CLOSE ACT 770B 775~ FLANGE 190 40 795 800' FLANGE Goo
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l 5 % WEIGHTS IAICLUDE 2 M&
RELEASE RECORD I REV. DATE PREPARED CHECKED ENG'R APP'L R EV. DESCRIP1
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SCHED.
THICK THICK 3P. 1. PIPE 2.f[hfD 3. INSUL. TO 142+3 4. WAT E R HYDRO 1+4
=
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2.375 "
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260 45 F -0.008 -0 013 -0.007 ._ / 1VP02SC COOLING COIL A.
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/ 4VP02SC COOLING COIL A.
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775 45 F -0.004 -0005 0.009 __
/ iVPO2SA COOLING COIL Ag 815 45 F.o.004 - 0.011 Ofr9 / 1VP02S A COOLING COIL A.,
- _ 855 45 F 0.009' -0.011 0.003 / 1VPO2SA COOLING COIL As
@ 905 45 F 0.009..-1 0050.005 / 4VPO2SA COOLING COIL A.,
I RELEASE RECORD k REV. DATE PREPAR'ED CHECKED ENG'R. APP'L. REV. DESCQ g 01: 12-24.80 J.WWF./tGau . _
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ANSTEC APERTURE CARD Also Aveliable on Aperture Card
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NODE REMARKS POINT TEMP.
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. jR107D-1110543 C 225 330'F 0.093 0.071 OD76 /
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". R107D -1110543 C 350 330* F 0.054 0.071 2 0.108 /
R107D-1110543 C 77S' 330*F 0.042 0.055 -0.100 /
". R107D-1110543 C 815 330*F 0.042 0.119 -0.100 v F
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l
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O.D. EHED. WALL INSUL. WElGHTS - LBS/ LINEAL FT.
- p, THICK TH P
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