ML19332B088: Difference between revisions
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| Line 22: | Line 22: | ||
gs,ppp .:-) - | gs,ppp .:-) - | ||
nP.rH Co /e /^ />:n1 '/5,- Nu //fCZ Sy: Pin s . C , /. . t | nP.rH Co /e /^ />:n1 '/5,- Nu //fCZ Sy: Pin s . C , /. . t | ||
{. | {. | ||
/9. /drA!~.m ~ h//n,71 l | /9. /drA!~.m ~ h//n,71 l 7b de A'/tri'N At: /' /> N r'= r c~r> c/a ptsc& c f e;,orin vSs-ri f M 24 //so c~Z fc- ee iW 7 r>> n.7 a -Y. 7i cv %i ,6 /"JM 7:}/En], / | ||
7b de A'/tri'N At: /' /> N r'= r c~r> c/a ptsc& c f e;,orin vSs-ri f M 24 //so c~Z fc- ee iW 7 r>> n.7 a -Y. 7i cv %i ,6 /"JM 7:}/En], / | |||
p,, v se6 e/ 6e | p,, v se6 e/ 6e | ||
/-//xZ c!.vi n An1 ^ | /-//xZ c!.vi n An1 ^ | ||
.~ | .~ | ||
/3. /?os 7c/f' Fk w 7 pang //P^NA N M M A' Affric GfoYf rP c/= PF H: 0 N Af C | |||
/3. /?os 7c/f' | |||
Fk w 7 pang //P^NA N M M A' Affric GfoYf rP c/= PF H: 0 N Af C | |||
( 79 Sobo /pc SS. K 2 /. o | ( 79 Sobo /pc SS. K 2 /. o | ||
/3 SOOO /CO SS.86' 2 /. O C SM) /VC .?: 59 z i. c O CCCC /(fC 32 3S 2 /. o | /3 SOOO /CO SS.86' 2 /. O C SM) /VC .?: 59 z i. c O CCCC /(fC 32 3S 2 /. o E SGrC /c ' l'' SS.fff' z i. O fhrj,pr}-h &/2??e&.x A- 5x15 r; ,'ir .-n Ce n.-d 5 '* i -> /b.,,o 49:cll< < > c 74- /&? rth- Ms.r:c-L - A//&pe yf/ rC.ns c \ | ||
E SGrC /c ' l'' SS.fff' z i. O fhrj,pr}-h &/2??e&.x A- 5x15 r; ,'ir .-n Ce n.-d 5 '* i -> /b.,,o 49:cll< < > c | |||
74- /&? rth- Ms.r:c-L - A//&pe yf/ rC.ns c \ | |||
/2 .5's/inj /A'~ | /2 .5's/inj /A'~ | ||
r n -) [rs & 3*' e (* cf', . | r n -) [rs & 3*' e (* cf', . | ||
| Line 48: | Line 35: | ||
-rE,-- Ah ie i, n u ; c - Z ccc, /1e e.i e | -rE,-- Ah ie i, n u ; c - Z ccc, /1e e.i e | ||
; C - 9& -6, -i ,4~in 5~., .. u e : .a . / -&- A , s'.:.>,,: /.? : /: .t | ; C - 9& -6, -i ,4~in 5~., .. u e : .a . / -&- A , s'.:.>,,: /.? : /: .t | ||
: -/- /N',v : ./ . ,/?r .: c~. - A ' . - ,G.-=.. : i c . . . ,< . | : -/- /N',v : ./ . ,/?r .: c~. - A ' . - ,G.-=.. : i c . . . ,< . | ||
l | l | ||
/%el re f .de . /> e.w i ! " | /%el re f .de . /> e.w i ! " | ||
| Line 57: | Line 41: | ||
~~ AD03301W | ~~ AD03301W | ||
/wac/w. # r. E.o P.ir: | /wac/w. # r. E.o P.ir: | ||
. .0< | . .0< | ||
2 e f* V $-il- EO f 9/:,qo -2. | |||
2 e f* V $-il- EO | |||
f 9/:,qo -2. | |||
. /l/03 7 C et & c h b .'1 5 : ~fr $*c /fe(. 5y. fn > | . /l/03 7 C et & c h b .'1 5 : ~fr $*c /fe(. 5y. fn > | ||
. .c. CrJhi | . .c. CrJhi | ||
( | ( | ||
2c;e' 4-6 ef '*7?' & (G<f-) | |||
/.) .Sc cAsri zGm Sc,zei e:s/cn ,4 cL , /$ n p c/ crane c v / ?r.n rk < ph.c.:e L - A iv p :n W. 1 | /.) .Sc cAsri zGm Sc,zei e:s/cn ,4 cL , /$ n p c/ crane c v / ?r.n rk < ph.c.:e L - A iv p :n W. 1 32,,yu-:. /n- p. t- et7 / ': r ./,, e.::: i c . | ||
32,,yu-:. /n- p. t- et7 / ': r ./,, e.::: i c . | |||
E- .52c-/>M ifem Cn r ct' >:c. i?. | E- .52c-/>M ifem Cn r ct' >:c. i?. | ||
s7''il.c, .. | s7''il.c, .. | ||
/<.',w/2 & + h -r <- | /<.',w/2 & + h -r <- | ||
ff- AC 6,in Ginr6, >:es?" | ff- AC 6,in Ginr6, >:es?" | ||
S'}sc,..c.~ ,- | S'}sc,..c.~ ,- | ||
Tem /:, | Tem /:, | ||
. 1 Q. /Je.4i/ c~-. 4 e A n n;.: | |||
. 1 | |||
Q. /Je.4i/ c~-. 4 e A n n;.: | |||
c w e.,w n ; | c w e.,w n ; | ||
m ac. w Tc ,m k. | m ac. w Tc ,m k. | ||
* + | * + | ||
| Line 101: | Line 70: | ||
l | l | ||
='e -) o. S 4 C.O O , | ='e -) o. S 4 C.O O , | ||
F4I Lto Fe7 ao | F4I Lto Fe7 ao | ||
/- | /- | ||
| Line 107: | Line 75: | ||
s ('' 44s /.9er* | s ('' 44s /.9er* | ||
\ | \ | ||
4 | 4 | ||
/1e/r: | /1e/r: | ||
| Line 114: | Line 81: | ||
2.. The //,'2CI p.'<,yo an.=mAh .Sc cn.or ' y,,p ic ;&m spricin, /4 c& e-et : : 7~ / .- 75W.-/ a,;9, ,. . e ,. | 2.. The //,'2CI p.'<,yo an.=mAh .Sc cn.or ' y,,p ic ;&m spricin, /4 c& e-et : : 7~ / .- 75W.-/ a,;9, ,. . e ,. | ||
crt ni, *, . O' & c,c ri ~!c h . | crt ni, *, . O' & c,c ri ~!c h . | ||
.y | .y l#1lt's F ~4 / + FC's 2 ru c- /:' iim ", r .' 's/; Prc t/ | ||
l#1lt's F ~4 / + FC's 2 ru c- /:' iim ", r .' 's/; Prc t/ | |||
' ^ | ' ^ | ||
: 3. - - | : 3. - - | ||
| Line 123: | Line 87: | ||
, - e /- c i c o | , - e /- c i c o | ||
- .n trac Ainut h> Efa J'vi.; | - .n trac Ainut h> Efa J'vi.; | ||
/Sy $ .' f W $-Z/~EC | /Sy $ .' f W $-Z/~EC | ||
* /:MPP- 2 * | * /:MPP- 2 * | ||
'~ | '~ | ||
. tvATM C % /4 /'i ' -r /I : //K Z Fy./ca, | . tvATM C % /4 /'i ' -r /I : //K Z Fy./ca, | ||
..- G-A | ..- G-A | ||
| Line 140: | Line 98: | ||
yc. fi c : fcv2.,sev.'~ ,=- y .<c 2 cyc iw / | yc. fi c : fcv2.,sev.'~ ,=- y .<c 2 cyc iw / | ||
2 c.: -e m ., . co.e. in.:7. ><. i.< i,a) | 2 c.: -e m ., . co.e. in.:7. ><. i.< i,a) | ||
S, ya miw mt .: . c <ec = f c <, + r1 w r: :p 41n c A | S, ya miw mt .: . c <ec = f c <, + r1 w r: :p 41n c A pi n ,p i. 42c c' .-~ 7, (,9)cen c cr e r i eo c.c. i: w | ||
/9c C i.e os i., | /9c C i.e os i., | ||
( [ 7' . ,. j t<h /r' c ! # ': ~ \ fs:' '?? '' '' | ( [ 7' . ,. j t<h /r' c ! # ': ~ \ fs:' '?? '' '' | ||
soc.L ,i,,n'.: F c <,* i >- F c o 2 sar % ,:,-/.'?c,/I- | soc.L ,i,,n'.: F c <,* i >- F c o 2 sar % ,:,-/.'?c,/I-cpcn ..,,o( F c 'Y u ll' i' -*n 1 n ri c/:/> w <! . i . /* ! | ||
cpcn ..,,o( F c 'Y u ll' i' -*n 1 n ri c/:/> w <! . i . /* ! | |||
vaire Fc | vaire Fc | ||
* I r f -:. 2. <,, c. r; if, ey. c n. 7nzo, fr e et wi /s * | * I r f -:. 2. <,, c. r; if, ey. c n. 7nzo, fr e et wi /s | ||
* fy <, . , - + c ir 2.c . | |||
fy <, . , - + c ir 2.c . | |||
[ r /f r I'' l'i e | [ r /f r I'' l'i e | ||
./ h~h'f_ j r~ _ AWt'2* _, L/, _rlf j. _/9 ~ E ' | ./ h~h'f_ j r~ _ AWt'2* _, L/, _rlf j. _/9 ~ E ' | ||
f sm/s= P c''-?" ) + C2,- 2 d - C vp r-D)9 avtc c: | f sm/s= P c''-?" ) + C2,- 2 d - C vp r-D)9 avtc c: | ||
| Line 160: | Line 111: | ||
7z?ff2?"f6 2 2. =- .,7/ r W c #. << 4 n* eZ .@ : 6C/ 2 .4 . -h, /f'.. ,p, Cr'/ .), ,, ,- .x.#s-/ | 7z?ff2?"f6 2 2. =- .,7/ r W c #. << 4 n* eZ .@ : 6C/ 2 .4 . -h, /f'.. ,p, Cr'/ .), ,, ,- .x.#s-/ | ||
2r= L o n.- u,<Pr .A. c ~L .i+ | 2r= L o n.- u,<Pr .A. c ~L .i+ | ||
c'5 7 ce n 2 c. - | c'5 7 ce n 2 c. - | ||
. ,,,,,,., , r:: / . , | . ,,,,,,., , r:: / . , | ||
c e c: .:. . . o | c e c: .:. . . o | ||
,,se .- < * /d ) , p , | ,,se .- < * /d ) , p , | ||
Vp = hnp e .o ec.:n c <~f af: L i; i w( a% | Vp = hnp e .o ec.:n c <~f af: L i; i w( a% | ||
o,,- yy i- , .*,' c y (,,a sse.' .) , ,o , c: s- 7.~ 7.r ( :c.~'t'. | o,,- yy i- , .*,' c y (,,a sse.' .) , ,o , c: s- 7.~ 7.r ( :c.~'t'. | ||
e vy..- %f | e vy..- %f | ||
/){ = Fric 6ni .de:s sn :uchtr, ', fly 1E ( p.rs e/ ) . | /){ = Fric 6ni .de:s sn :uchtr, ', fly 1E ( p.rs e/ ) . | ||
pe<- X R=Sc! . | |||
I | I i g D**D ]D f 0[ $ | ||
i g | |||
oo oJuu2UAIfd., | oo oJuu2UAIfd., | ||
1 | 1 | ||
~~'~ fir'schptsgr "o E=.; . 4-?;;.: | ~~'~ fir'schptsgr "o E=.; . 4-?;;.: | ||
/{ 9 '''/ | /{ 9 '''/ | ||
g - 2 7-gc, revpr+-2 | |||
g - 2 7-gc, | |||
revpr+-2 | |||
. tyf).'~M G /cc Ar 4.'n ' fr h- /7VYZ S_-4,v] | . tyf).'~M G /cc Ar 4.'n ' fr h- /7VYZ S_-4,v] | ||
i | i | ||
: s. s n& | : s. s n& | ||
h /#pf' l/Q / /'." N A fftW $f) | h /#pf' l/Q / /'." N A fftW $f) | ||
$$ 'd $ ) | $$ 'd $ ) | ||
J = c:1.77(,t/Cr'f:) | J = c:1.77(,t/Cr'f:) | ||
f' = /4' '7p:ih | f' = /4' '7p:ih e 2= su. coe 2i= S 8 1. 2. 2 H lep = .. '1 Spi (.- t /.' c 'f ) | ||
e 2= su. coe 2i= S 8 1. 2. 2 H lep = .. '1 Spi (.- t /.' c 'f ) | |||
/> + = 7.yCp:2 seu = iv. ,C,".V,) + (so.2g- su s.c3 - c. rs n 2 n )ks sw:/ m = /2 Y. /O H + W, 2 S , V .) - / 9. </ c , , y riti: is.x = SS. & G f-f | /> + = 7.yCp:2 seu = iv. ,C,".V,) + (so.2g- su s.c3 - c. rs n 2 n )ks sw:/ m = /2 Y. /O H + W, 2 S , V .) - / 9. </ c , , y riti: is.x = SS. & G f-f | ||
( | ( | ||
| Line 219: | Line 147: | ||
* i- c./G } l$c | * i- c./G } l$c | ||
/tP ~//// = I3 I 'f. S S t- /*A SV) s'2 7 e y | /tP ~//// = I3 I 'f. S S t- /*A SV) s'2 7 e y | ||
/M //d = 32. 3 s ff | /M //d = 32. 3 s ff l | ||
l | |||
l l | l l | ||
Q DD D = O m | Q DD D = O m | ||
& ~ | & ~ | ||
3+ (")y l xt p :~x AWA A aw & ~ | 3+ (")y l xt p :~x AWA A aw & ~ | ||
My ' ~ v # | My ' ~ v # | ||
9 P. 76 | 9 P. 76 d Cuwk p | ||
d Cuwk p | |||
* 3' D**O cc e J.. 2 1 | * 3' D**O cc e J.. 2 1 | ||
yso,no m.$w~s A s | yso,no m.$w~s A s | ||
& . p'd,6Aar i - - _ | & . p'd,6Aar i - - _ | ||
( _ _ __ - _ . | ( _ _ __ - _ . | ||
M wapp i f | M wapp i f | ||
- s s m a w a. | - s s m a w a. | ||
( ~ p l n & x: | ( ~ p l n & x: | ||
A/AC W //D./G .. ~ . . . | A/AC W //D./G .. ~ . . . | ||
4+3#-. m., og 6e w-e --' * " * * | 4+3#-. m., og 6e w-e --' * " * * | ||
-. - m aarmes- | -. - m aarmes- | ||
* Y am a , | * Y am a , | ||
/ | / | ||
oo o o. .' | oo o o. .' | ||
k . . . _ _ _ . . _ _ _ - I l | k . . . _ _ _ . . _ _ _ - I l | ||
' ~ ~ ' ~ ~ ~ ~^^^^ ~ ~ ~ ~ ~ ~ ~ ~ | ' ~ ~ ' ~ ~ ~ ~^^^^ ~ ~ ~ ~ ~ ~ ~ ~ | ||
I. | I. | ||
- DOCUV- M i PAGE _ | |||
- DOCUV- M i | |||
PAGE _ | |||
I U-- ' | I U-- ' | ||
ANO. smemsa . | ANO. smemsa . | ||
l NO. OF PAGES 2 ru.AS REASON-O PAGE ILLEGIBLE: | l NO. OF PAGES 2 ru.AS REASON-O PAGE ILLEGIBLE: | ||
| Line 278: | Line 183: | ||
OTHER MED ON APERTURE CARD NO. | OTHER MED ON APERTURE CARD NO. | ||
OO mod [/3 h0%qos73-f/ | OO mod [/3 h0%qos73-f/ | ||
. AT[l.OF._L._ TIII. DET ROIT I I$1 SON CO. ENGINEEltING DLl'Airl'.11.NTS SUS. N O. | . AT[l.OF._L._ TIII. DET ROIT I I$1 SON CO. ENGINEEltING DLl'Airl'.11.NTS SUS. N O. | ||
'9 | '9 | ||
*- ,,l7n DESCRlrTION m,1 ,, | *- ,,l7n DESCRlrTION m,1 ,, | ||
"V,7 1 -- A A 'Is "x s'/z" P4i'L ips weome A*acWoRe, wG-12 s 4 Z M.i 4 . EMB. ' Tiz." | "V,7 1 -- A A 'Is "x s'/z" P4i'L ips weome A*acWoRe, wG-12 s 4 Z M.i 4 . EMB. ' Tiz." | ||
" fi'. 5/p, x o wie w/(4)Sho*'d McLES4mh A% | " fi'. 5/p, x o wie w/(4)Sho*'d McLES4mh A% | ||
| Line 297: | Line 197: | ||
F 4 P W 6t.0cm s V4 *Y2 x1 \ _ # R/ ^ 4% | F 4 P W 6t.0cm s V4 *Y2 x1 \ _ # R/ ^ 4% | ||
= Ve#- eM k ry,= | = Ve#- eM k ry,= | ||
.) | .) | ||
2 (r.o.) ,, | 2 (r.o.) ,, | ||
i 3-- .yr Tr;r _- , | i 3-- .yr Tr;r _- , | ||
. hg g | . hg g | ||
ly c M-"- | ly c M-"- | ||
l4G | l4G z. | ||
z. | |||
.E. 2 EI . 547'-l'/2.h , -- --' - - - - - --- - | .E. 2 EI . 547'-l'/2.h , -- --' - - - - - --- - | ||
' .[' . ' s f | ' .[' . ' s f | ||
u n nt~u.m -b _ . _ _ _ .. _ _ - _ _ _ _ _ _ | u n nt~u.m -b _ . _ _ _ .. _ _ - _ _ _ _ _ _ | ||
:i* p a k * - . ,. . . . . . , | :i* p a k * - . ,. . . . . . , | ||
w,n _ c.iocAw | w,n _ c.iocAw | ||
.:. a | .:. a | ||
:$ o E | :$ o E | ||
A | A | ||
, t. | , t. | ||
4 I eg gppy,* ( * ** | 4 I eg gppy,* ( * ** | ||
JU[ | JU[ | ||
g[ _.3dg. p > .qq | g[ _.3dg. p > .qq | ||
,vu ,i~ 'o'" | ,vu ,i~ 'o'" | ||
- ye mw= --- | - ye mw= --- | ||
. W.P44, , ,mZG8(.ilt k | . W.P44, , ,mZG8(.ilt k | ||
y' ' . .* .,t u 9 Wi'* . I z ; R_ _m._ _ - | y' ' . .* .,t u 9 Wi'* . I z ; R_ _m._ _ - | ||
h - | h - | ||
l-> | l-> | ||
0 | 0 O | ||
o )- | |||
$ $ 2 M cT e'51._ _. _._-' _,. | $ $ 2 M cT e'51._ _. _._-' _,. | ||
q6 S .3 3 . - WM("r , | q6 S .3 3 . - WM("r , | ||
t)ACL 4 ELDS PERvaps Too2 ' | t)ACL 4 ELDS PERvaps Too2 ' | ||
w _.T U41.EES McTEQ tt 3 | w _.T U41.EES McTEQ tt 3 e ' Ftve2Ty 2 eM* ~ 4)Q cLEA:t/ act Redo. S' 3 d. . "-t-2 o (C4-5)J2 %T8 TEfi. LEE 4' Lowest i.ucas, g(.tiLF)--G-M d li I-us . r catwns i+s=. . -Auo :.Tews @ N YnD1 : | ||
e ' Ftve2Ty 2 eM* ~ 4)Q cLEA:t/ act Redo. S' 3 d. . "-t-2 o (C4-5)J2 %T8 TEfi. LEE 4' Lowest i.ucas, g(.tiLF)--G-M d li I- | |||
us . r catwns i+s=. . -Auo :.Tews @ N YnD1 : | |||
__ 9! fli 2 | __ 9! fli 2 | ||
# re | # re o : ~,. | ||
o : ~,. | |||
J .i en@ | J .i en@ | ||
' Ad | ' Ad | ||
| Line 367: | Line 234: | ||
uT . | uT . | ||
SIGN ATUR E DT ISSUED: MARK NO.W.P44-2MS-C3On c c / '''* | SIGN ATUR E DT ISSUED: MARK NO.W.P44-2MS-C3On c c / '''* | ||
U ' *" | U ' *" | ||
"*' "ocgfo[l o[R oc - | "*' "ocgfo[l o[R oc - | ||
| Line 377: | Line 243: | ||
l B/nt Deco File No. | l B/nt Deco File No. | ||
T6S APPROVAL S;S3!ES T!!AT Trans=1stal Date vendor TEI "APPEUV23 AS UOIIU' Engineering Approved l 1e Noted cc 2*L'{TS cY F.011CT EllC2. Approved As noted Quality Assurance Dir. | T6S APPROVAL S;S3!ES T!!AT Trans=1stal Date vendor TEI "APPEUV23 AS UOIIU' Engineering Approved l 1e Noted cc 2*L'{TS cY F.011CT EllC2. Approved As noted Quality Assurance Dir. | ||
P.AVI CEI IO.0EPOMTED . | P.AVI CEI IO.0EPOMTED . | ||
c ,a / a l f'lqO/ Systes Engineer E l | c ,a / a l f'lqO/ Systes Engineer E l m m1 3 | ||
m m1 3 | |||
'IC Proj. Director-Operation 9' | 'IC Proj. Director-Operation 9' | ||
D ' | D ' | ||
u l 6b b ' '" Project Ergineer Approved As Noted Be1. For Fab. Or Constr. | u l 6b b ' '" Project Ergineer Approved As Noted Be1. For Fab. Or Constr. | ||
n dA0dN?D _ | n dA0dN?D _ | ||
4 | 4 3 | ||
3 | |||
I I 'N | I I 'N | ||
. t | . t | ||
/, g , , - . 3, x t . 4 i o /''. | /, g , , - . 3, x t . 4 i o /''. | ||
.~-'\ N f df?_U'd 'b 'I4 | .~-'\ N f df?_U'd 'b 'I4 | ||
~ | ~ | ||
D 4 '/2 " r '; /4 " '!''L l >S ''''.*3'' | D 4 '/2 " r '; /4 " '!''L l >S ''''.*3'' | ||
91dd.A.'J3 j 'A;..C W?.6-iT u :2*/2 " _ _ | 91dd.A.'J3 j 'A;..C W?.6-iT u :2*/2 " _ _ | ||
b ,'' ** | b ,'' ** | ||
.- _ i r2 a s s v. . ? i e ra v. I '- t i " i . cs . | .- _ i r2 a s s v. . ? i e ra v. I '- t i " i . cs . | ||
$ O 2 L 2 K 5Y'/2 X ~IL 4 E- ___ ._0 7_'d . | $ O 2 L 2 K 5Y'/2 X ~IL 4 E- ___ ._0 7_'d . | ||
, p_. i L z e a w/4 x i Vz " L C, . -_ W.- . _ _ _ _ _ | , p_. i L z e a w/4 x i Vz " L C, . -_ W.- . _ _ _ _ _ | ||
: o. __ .__ | : o. __ .__ | ||
g | g | ||
~ | ~ | ||
E N' NW~ | E N' NW~ | ||
| Line 435: | Line 271: | ||
o 0 . . | o 0 . . | ||
,r gt- --- | ,r gt- --- | ||
a | a O II .'. ~-3 | ||
O II .'. ~-3 | |||
- fl.}_-p1 6 52 '-l'/z" _ r- g\ | - fl.}_-p1 6 52 '-l'/z" _ r- g\ | ||
'p{ l lj 'l l " | 'p{ l lj 'l l " | ||
W ',* *, i 7--- | W ',* *, i 7--- | ||
>- 4 EL. s sas s o ps re g . _ j . g* q __ _ _ | >- 4 EL. s sas s o ps re g . _ j . g* q __ _ _ | ||
_.__' .4 | _.__' .4 | ||
*. . :" ,, ., 3e | *. . :" ,, ., 3e | ||
.,2 | .,2 4 . , ., | ||
4 . , ., | |||
h - | h - | ||
._ ... _ _ _ _ _. _ _ _ _ _ _ _ . _ _ '.' fh,j L .GY a -4l' ,' , . l .'i | ._ ... _ _ _ _ _. _ _ _ _ _ _ _ . _ _ '.' fh,j L .GY a -4l' ,' , . l .'i 6 | ||
a 1 g | |||
U N C LR. | |||
.e s | |||
- m .: cas 1 | |||
.e | |||
s | |||
- m .: cas | |||
1 | |||
'' l. cuciquLcAo | '' l. cuciquLcAo | ||
* crm. wpr N8I -- 3 V -~ | * crm. wpr N8I -- 3 V -~ | ||
| Line 472: | Line 293: | ||
g WP5 3co2 eMLess RaiiEp | g WP5 3co2 eMLess RaiiEp | ||
- 9 W A 3 e ,n . - | - 9 W A 3 e ,n . - | ||
d i | d i k )- -< > | ||
k )- -< > | |||
6 r 3 ,j 3 | 6 r 3 ,j 3 | ||
.5 ( _. | .5 ( _. | ||
m i -., _ | m i -., _ | ||
@ O | @ O | ||
<g a | <g a 3 .. r ._ | ||
3 .. r ._ | |||
_g | _g | ||
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6F l - 'h *~ | 6F l - 'h *~ | ||
.' l N | .' l N | ||
T | T | ||
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u or | |||
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SIGN ATUR E | SIGN ATUR E | ||
{ 65U E D. MARK NOW $ 4 ' 211b - ~~ | { 65U E D. MARK NOW $ 4 ' 211b - ~~ | ||
3 | 3 DE SIGN J. vv(a 5 Q3 [ f *>b_,,_ f | ||
DE SIGN J. vv(a 5 Q3 [ f *>b_,,_ f | |||
/\ | /\ | ||
CHK' P NS/ d d. ( | CHK' P NS/ d d. ( | ||
g;.'A PORT &ON OF THl$ DAG l$ AfIf CTED Bv Fif LD REVISION ST ATUS---** / ,)- | g;.'A PORT &ON OF THl$ DAG l$ AfIf CTED Bv Fif LD REVISION ST ATUS---** / ,)- | ||
l2QP/p)1 '**Ie 0HIGIN AL DCH/DCN. [I DCR/DCN. | l2QP/p)1 '**Ie 0HIGIN AL DCH/DCN. [I DCR/DCN. | ||
) | ) | ||
D I C. SUPV. _ | D I C. SUPV. _ | ||
B.M NO: H_f.V- , | B.M NO: H_f.V- , | ||
~ | ~ | ||
[CL-C - l t.a. A.T--- -- HGR. tSO (w% m., | [CL-C - l t.a. A.T--- -- HGR. tSO (w% m., | ||
Fif LD F AB ST ATUS: 5(11 f N4 c il?/f H I V. A'- | Fif LD F AB ST ATUS: 5(11 f N4 c il?/f H I V. A'- | ||
,w | ,w Doe m atattoo No. - | ||
Doe m atattoo No. - | |||
1,contion Approval t | 1,contion Approval t | ||
P.O. Installation | P.O. Installation 3/N pgco ytle go. | ||
3/N pgco ytle go. | |||
Transsittal Date Tender Engineering Approved l As Note L Approved As Noted Quality Assurance Dir. ; | Transsittal Date Tender Engineering Approved l As Note L Approved As Noted Quality Assurance Dir. ; | ||
$ l | $ l | ||
@F 'T 9* 0 $ | |||
@F 'T | |||
9* 0 $ | |||
6b b * ' | 6b b * ' | ||
IC Proj. Director-Operatione | IC Proj. Director-Operatione u 1 1 Projoet haineer l pege4 /7 As Noted Rel. Por Pab. Or Constr. J | ||
u 1 1 Projoet haineer l | |||
pege4 /7 As Noted Rel. Por Pab. Or Constr. J | |||
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A% i 3 4 '/2 | |||
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| Line 570: | Line 346: | ||
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a | |||
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m et ss2 .w | m et ss2 .w | ||
' r g g g e pip p,' D l bd l | ' r g g g e pip p,' D l bd l | ||
' :P "a ' - | ' :P "a ' - | ||
N$'af , .* - | N$'af , .* - | ||
O i | O i | ||
0-- - | 0-- - | ||
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| Line 597: | Line 364: | ||
E - | E - | ||
*.**. ya a | *.**. ya a | ||
5 h - | 5 h - | ||
%*Ct.e: | %*Ct.e: | ||
-(2)Seoes | -(2)Seoes | ||
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> d, 4 .F(veR 1: (Av ./ | > d, 4 .F(veR 1: (Av ./ | ||
| Line 622: | Line 381: | ||
* m' | * m' | ||
.1 | .1 | ||
!u | !u ac/ 3p I'2 | ||
ac/ 3p I'2 | |||
* T. l | * T. l | ||
@ O b-~ | @ O b-~ | ||
* a o ; | * a o ; | ||
s e, | |||
s | ss sw r .. | ||
e, ss | |||
sw r .. | |||
a | a | ||
= | = | ||
| Line 645: | Line 397: | ||
,t: | ,t: | ||
,e | ,e | ||
- g,~ | - g,~ | ||
y - | y - | ||
| Line 651: | Line 402: | ||
~- | ~- | ||
9 4 E* OCCW + & &CW n s) P E 5'AMO RG TORM TO f7 s.4 CL M.JMPS (Scof L4 Ce AcTot. BLO6. LJM 6"I"E h4 l SIGNATURE 07 ISSUED: | 9 4 E* OCCW + & &CW n s) P E 5'AMO RG TORM TO f7 s.4 CL M.JMPS (Scof L4 Ce AcTot. BLO6. LJM 6"I"E h4 l SIGNATURE 07 ISSUED: | ||
OESIGN/DWG. G CS/ .ALO'5 | OESIGN/DWG. G CS/ .ALO'5 876 MARK NOwF44-21%-c7o*3 C H K. | ||
876 MARK NOwF44-21%-c7o*3 C H K. | |||
-4S/ M | -4S/ M | ||
# A PORTION OF THl3 DWG. IS AFFECTED BY ORIGINAL OCR/DCN: 1 FIELD 9EVISION STATUS: | # A PORTION OF THl3 DWG. IS AFFECTED BY ORIGINAL OCR/DCN: 1 FIELD 9EVISION STATUS: | ||
D.: c Sury. RuP/ w~m '"e/e l OCR/DCN: | D.: c Sury. RuP/ w~m '"e/e l OCR/DCN: | ||
* 8/M NO: REV. | * 8/M NO: REV. | ||
FIE LD F AO 3TATUS: : SEISL 1 l Ct. C lG A. I HGR. ISObJA&f.{4 2iT6ri NY. <k | FIE LD F AO 3TATUS: : SEISL 1 l Ct. C lG A. I HGR. ISObJA&f.{4 2iT6ri NY. <k Documentation No. PD 102 (879) | ||
Documentation No. PD 102 (879) | |||
- - Appreval Location F.O. Installation B/M DECO File No. | - - Appreval Location F.O. Installation B/M DECO File No. | ||
TBS APPliOVAL StGEIS T!!AT transmittal Date vendor Ili '' APP;;Cli20 f.S i;GT&' W ineering w rovea l As Noted CG.IciTS CY F;:5CT EJC2. Approved As Noted Quality Assurance Dir. | TBS APPliOVAL StGEIS T!!AT transmittal Date vendor Ili '' APP;;Cli20 f.S i;GT&' W ineering w rovea l As Noted CG.IciTS CY F;:5CT EJC2. Approved As Noted Quality Assurance Dir. | ||
e , / . l LM5 Systen Engineer 1 | |||
e , / . l LM5 Systen Engineer | Project Engineer Approved As Noted Rel. For Fab. Or Constr. | ||
. MdM | . MdM | ||
or l' illi. Ist ilWil l itiWN (0.1..t,1Ni | or l' illi. Ist ilWil l itiWN (0.1..t,1Ni | ||
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un e. n DL $CitiPilON y N.I a Iv t, A% | |||
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| Line 684: | Line 423: | ||
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F ' | F ' | ||
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a l | |||
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s . _ ;(2 ) SIDE 5 ''' | s . _ ;(2 ) SIDE 5 ''' | ||
| Line 723: | Line 444: | ||
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.V BIfan = | .V BIfan = | ||
$ 1 F (V F.R. | $ 1 F (V F.R. | ||
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G LE.s/A t so N.t "A-A" | |||
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A ggATIONag | A ggATIONag | ||
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N3 g | |||
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g @AJI a: | g @AJI a: | ||
2 @cCW + &acW SQ P Pt.Y AMO Re TOR.M Toq_64 Q 14. sups (So 01" M4 Q9 ACTOR SIGN ATUR E 07 ISSUED: MARK NO'.N'b4.; D*lb 4@__ | 2 @cCW + &acW SQ P Pt.Y AMO Re TOR.M Toq_64 Q 14. sups (So 01" M4 Q9 ACTOR SIGN ATUR E 07 ISSUED: MARK NO'.N'b4.; D*lb 4@__ | ||
DE SIGN /DWG. CmD$[ M # | DE SIGN /DWG. CmD$[ M # | ||
8M A PORTION OF THIS OWG 15 AFFECTED til FIELD REVislON STATUS: __ | 8M A PORTION OF THIS OWG 15 AFFECTED til FIELD REVislON STATUS: __ | ||
| Line 768: | Line 470: | ||
D.I.c. SuPv. quP/ SAS '% I . . | D.I.c. SuPv. quP/ SAS '% I . . | ||
SEIS. I l CL. C l 0. A. ".C HGR.ISOMA4fd4 2tT61 REV.k l FIE LD F AB ST ATUS: | SEIS. I l CL. C l 0. A. ".C HGR.ISOMA4fd4 2tT61 REV.k l FIE LD F AB ST ATUS: | ||
P& 102 (R791 | P& 102 (R791 Documentation No. | ||
. Location Approval l P.O. Installation B/11 Deco File No. | . Location Approval l P.O. Installation B/11 Deco File No. | ||
Ti'iS APPROVAL $;STJ!ES TIIAT trans:1ttal Date v.naar II'.E "iJ?ECO3 f S IIOII.D* Engineering Approved l As Noted CGC.f.2TS C't F.~0;;CT E?im. Approved as Noted Quality Assurance Dir. | Ti'iS APPROVAL $;STJ!ES TIIAT trans:1ttal Date v.naar II'.E "iJ?ECO3 f S IIOII.D* Engineering Approved l As Noted CGC.f.2TS C't F.~0;;CT E?im. Approved as Noted Quality Assurance Dir. | ||
D.'.'I CCl C',2EP03ATED . i e _s ' | D.'.'I CCl C',2EP03ATED . i e _s ' | ||
/ , 1 Mf l | / , 1 Mf l d'd/gdj Systen Engineer DPp ~ | ||
''D IC I | |||
d'd/gdj Systen Engineer | |||
DPp ~ | |||
''D | |||
IC I | |||
Proj. Director.0perations | Proj. Director.0perations | ||
* W3 " | * W3 " | ||
j ::3 QA l Project Engineer Approved As Noted Rel. For Fab. Or Constr. | j ::3 QA l Project Engineer Approved As Noted Rel. For Fab. Or Constr. | ||
./1/L *WS | ./1/L *WS | ||
Tile DETRO i)!'Sd5 O E G 1 ,'DEP5 .\lENTS Sus.5:0.. I G.' | Tile DETRO i)!'Sd5 O E G 1 ,'DEP5 .\lENTS Sus.5:0.. I G.' | ||
JCF % -- | JCF % -- | ||
| Line 798: | Line 488: | ||
ass | ass | ||
$ O 2 t 2 K 2 w /4 % 4" L.cs. Jan | $ O 2 t 2 K 2 w /4 % 4" L.cs. Jan | ||
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E F' 4 Pip e t UCs S Y4.v.'/2 % % '4 W g m.- m e, re ~ | |||
.em A. Li %t111 | .em A. Li %t111 | ||
/. . . - n m : | /. . . - n m : | ||
| Line 806: | Line 494: | ||
3 s | 3 s | ||
\TV I AUGO 81980 m l | \TV I AUGO 81980 m l | ||
g - w. a)~ '', 2y - c. --- - _ r. 2 ) | g - w. a)~ '', 2y - c. --- - _ r. 2 ) | ||
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5 o j 6 4g g4 # 4 l ged. j | 5 o j 6 4g g4 # 4 l ged. j r- n-.41 l | ||
r- n-.41 l | |||
, EC s s2 ' i h '* R''. | , EC s s2 ' i h '* R''. | ||
' tsmse eies:-?Fih | ' tsmse eies:-?Fih E | ||
o MCJA_ | |||
MCJA_ | |||
e. | e. | ||
...,.,4.- | ...,.,4.- | ||
.E-+- c W = | .E-+- c W = | ||
-5 .A o | -5 .A o | ||
| Line 829: | Line 507: | ||
" ? | " ? | ||
var ete.._ | var ete.._ | ||
(2;SiOEE | (2;SiOEE t _ CESi72M MO.' REF" sPPT" Mat | ||
t _ CESi72M MO.' REF" sPPT" Mat | |||
$[.d 23 q | $[.d 23 q | ||
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4 j | |||
NL | |||
j | |||
; | ; | ||
l e | |||
l | G .:n K { . . | ||
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^ | ^ | ||
| Line 871: | Line 528: | ||
b g __ - | b g __ - | ||
n. | n. | ||
p a | p a | ||
sECTioN"6 6* i | sECTioN"6 6* i | ||
< ,w e;-3ect I -- . ' "h,. . I | < ,w e;-3ect I -- . ' "h,. . I N | ||
b or | |||
< s NP. .- = | < s NP. .- = | ||
a s 7 Am . | a s 7 Am . | ||
| Line 886: | Line 540: | ||
D E SIGN /DWG. GDS / M~ 8e en A PORTtON OF WIS DWG 13 AFFECTED BN FIELD REVISION STATUS: | D E SIGN /DWG. GDS / M~ 8e en A PORTtON OF WIS DWG 13 AFFECTED BN FIELD REVISION STATUS: | ||
CH K. c4S) M - | CH K. c4S) M - | ||
ORIGINAL DCR/DCN: l DCR/DCN; D.I.C SUPV. @lP/ Mb 'T2 1 9/M NO: REV FIE LD F AB STATUS: SEIS. E lCL C la A. I HGR. ISO:/,.uJAAS44 2LTfd REV.k F0102 (879; | ORIGINAL DCR/DCN: l DCR/DCN; D.I.C SUPV. @lP/ Mb 'T2 1 9/M NO: REV FIE LD F AB STATUS: SEIS. E lCL C la A. I HGR. ISO:/,.uJAAS44 2LTfd REV.k F0102 (879; Docu=entation No. | ||
Docu=entation No. | |||
Location Approval P.O. Installation B/14 DECO File No. | Location Approval P.O. Installation B/14 DECO File No. | ||
TEiS APPROVAL S:0N!ES TMT Tranesitt:1 Date vendor TEE *AFPKCVID f.S i:3 TID | TEiS APPROVAL S:0N!ES TMT Tranesitt:1 Date vendor TEE *AFPKCVID f.S i:3 TID | ||
| Line 899: | Line 551: | ||
l | l | ||
.. - -. .. . l 3--..- | .. - -. .. . l 3--..- | ||
$wT- l er __] THE DETROIT EDISON CO. EtulNFERING DEPARTMENTS S U S. N O. 4"f 4 G7, 9 M7 , ,"q0 o DESCRIPTION ,,,,.t. u7 1 -- A I E '/2. x 4 1 f%'/2 , | $wT- l er __] THE DETROIT EDISON CO. EtulNFERING DEPARTMENTS S U S. N O. 4"f 4 G7, 9 M7 , ,"q0 o DESCRIPTION ,,,,.t. u7 1 -- A I E '/2. x 4 1 f%'/2 , | ||
ASC* ._- | ASC* ._- | ||
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Op 2 */2 *x 6'/2'' P41t.t t A'h W E06 E A. MCuot W S-12 54 | |||
W hi, E Mb, s 'a> */ 2" - | |||
e | e | ||
--- C 4 t. 3 x 3 E Vs K l'- i t" L 6. A% | --- C 4 t. 3 x 3 E Vs K l'- i t" L 6. A% | ||
| Line 917: | Line 562: | ||
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g ts | g ts | ||
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| Line 957: | Line 584: | ||
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g 3y - | g 3y - | ||
6 | 6 5 b | ||
5 b | |||
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| Line 968: | Line 591: | ||
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z | z j | ||
us | |||
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g 2 | g 2 | ||
u o | u o | ||
au | au P Q) 6 4 m E 7% | ||
P Q) 6 4 m E 7% | |||
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l O g o ( # - | l O g o ( # - | ||
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SIGN ATUR E DT QIM h '} | SIGN ATUR E DT QIM h '} | ||
| Line 1,009: | Line 614: | ||
-~~FIE LD F AB STATUS. SEIS- E _ | -~~FIE LD F AB STATUS. SEIS- E _ | ||
I P' f*- !aA T HCR ISD E2.si@t141 i 'E V. /a\ | I P' f*- !aA T HCR ISD E2.si@t141 i 'E V. /a\ | ||
m anentau on so. PD.102 (8-71 5 Loostion Approval P.O. Installation - , | m anentau on so. PD.102 (8-71 5 Loostion Approval P.O. Installation - , | ||
E/M DECO Pile No. | |||
Transmittal Date fondor Engineering Approved l As Noted Approved As Noted Quality Aseurance Dir. | Transmittal Date fondor Engineering Approved l As Noted Approved As Noted Quality Aseurance Dir. | ||
_. . I mq m Q | _. . I mq m Q M //[*/M$h Systen Engineer D > | ||
l cc 0 b ' # IC Proj. Director-Operatio.e G l t | |||
M //[*/M$h Systen Engineer D > | |||
l cc 0 b ' # IC Proj. Director-Operatio.e | |||
G l t | |||
Projoet Engineer - | Projoet Engineer - | ||
. Approvand As Noted' Be1. Por Pab. Or Constr. | . Approvand As Noted' Be1. Por Pab. Or Constr. | ||
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| Line 1,030: | Line 629: | ||
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| Line 1,139: | Line 697: | ||
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$lG% ATUN E OT ISSUED. MARK NOW 744 2 4 76 - Ca C '7 | $lG% ATUN E OT ISSUED. MARK NOW 744 2 4 76 - Ca C '7 | ||
| Line 1,158: | Line 708: | ||
' ,, f. | ' ,, f. | ||
, , , A PORTION OF THIS D.*.G 15 AF F FCTF O Bv FIELD REVistDN ST ATUS i t. \. | , , , A PORTION OF THIS D.*.G 15 AF F FCTF O Bv FIELD REVistDN ST ATUS i t. \. | ||
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'4 a T BE LD e #5 $T ATUS: SEls. I lCL C luA I. ''n 6 50 'r a * * 't.h*tU -I M V/^h PD 102 16 796 | '4 a T BE LD e #5 $T ATUS: SEls. I lCL C luA I. ''n 6 50 'r a * * 't.h*tU -I M V/^h PD 102 16 796 | ||
~ | ~ | ||
Dccuantatice No. | Dccuantatice No. | ||
apprevel t ..L -- o c a t_i o n - - ~ ' | |||
P.O. Insta13attoa - - - | P.O. Insta13attoa - - - | ||
3/nf D Co File Wo. | 3/nf D Co File Wo. | ||
| Line 1,170: | Line 718: | ||
__A_ ;p r e v e d l As Noted 44f 4 , , c Ecq,i, nee r1M A;; roved i As Ested C oltty Arrurance Dir.~ ' | __A_ ;p r e v e d l As Noted 44f 4 , , c Ecq,i, nee r1M A;; roved i As Ested C oltty Arrurance Dir.~ ' | ||
a l c | a l c | ||
Y h% Oystca D:ctecer E I | Y h% Oystca D:ctecer E I E Proj. Director.cperatione CA ! | ||
E Proj. Director.cperatione CA ! | |||
Project Er.sitneer _ | Project Er.sitneer _ | ||
e | e appry e4 /- As Itoted Rel. For Feb. Or Corstr. | ||
appry e4 /- As Itoted | |||
Rel. For Feb. Or Corstr. | |||
Irlq>'9.zy [ ? _. - | Irlq>'9.zy [ ? _. - | ||
4 ..[.;o, [ Tile DETROIT EDISON CO. EhGINEERING IJEPARTMENTS sua. N o. . . ; | 4 ..[.;o, [ Tile DETROIT EDISON CO. EhGINEERING IJEPARTMENTS sua. N o. . . ; | ||
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| Line 1,204: | Line 739: | ||
y SIGNATURE NOT REQUIRED $ D 3 | y SIGNATURE NOT REQUIRED $ D 3 | ||
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| Line 1,238: | Line 762: | ||
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| Line 1,252: | Line 771: | ||
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3 B LO'-a . O *"f" ETO RWE FVM | |||
s I b R$ccW (60 {JTulE.ScwJ 50PPL5')CG.REiTJE4 12 crA<. | |||
SIGN ATUR E Dr ISSUED: MAPK NO.%j.9.$4 21"l$. Cg6 DESIGN /DWG. Gt DS[Nd M cnK. cast # n ^77oa 0 ,t"oca'j7P o , ofa oc f'75" mm mm mm A D.LC. SUPV. M/AOb NA B/M No: REV. | SIGN ATUR E Dr ISSUED: MAPK NO.%j.9.$4 21"l$. Cg6 DESIGN /DWG. Gt DS[Nd M cnK. cast # n ^77oa 0 ,t"oca'j7P o , ofa oc f'75" mm mm mm A D.LC. SUPV. M/AOb NA B/M No: REV. | ||
F8 ELD F AB STATUS: $Eli T. lCL C lh I HGR.150M 944.'llTB-l REVM PD102 (8 79) | F8 ELD F AB STATUS: $Eli T. lCL C lh I HGR.150M 944.'llTB-l REVM PD102 (8 79) | ||
Docucentation 30. | Docucentation 30. | ||
Location Approval | Location Approval P.O. Installation B/M DECO File No. | ||
P.O. Installation B/M DECO File No. | |||
Tr'iS APPE0Vitt S;%!Fl!S T!!!LT Transmittal Date vendor 11:2 " APP;;CE3 AS !;3TED* Engineering Approved l As Noted CG:.2lEiTS CY F.WCT E:!C3. ,,,7,y,a 3, ,,,,3 gy,33,7 3,,,,,nc,33,, | Tr'iS APPE0Vitt S;%!Fl!S T!!!LT Transmittal Date vendor 11:2 " APP;;CE3 AS !;3TED* Engineering Approved l As Noted CG:.2lEiTS CY F.WCT E:!C3. ,,,7,y,a 3, ,,,,3 gy,33,7 3,,,,,nc,33,, | ||
ERU CCI C%P03ATED g _s I , | ERU CCI C%P03ATED g _s I , | ||
| Line 1,285: | Line 789: | ||
g@A p r, m g g M, , Systes Engineer | g@A p r, m g g M, , Systes Engineer | ||
@ O s , | @ O s , | ||
3 IC Proj. Director-operations CA l Project Engineer | 3 IC Proj. Director-operations CA l Project Engineer Approved l As Noted Ra1. For Fab. Or Constr. | ||
Approved l As Noted Ra1. For Fab. Or Constr. | |||
t 0.$. ktteNh.'#_ . . . . _ - | t 0.$. ktteNh.'#_ . . . . _ - | ||
7,t cF . I _ THE DETRO!T LDISON CO. ENGINEERING DEPARTMENTS SUB.N3.S.** 'U. | 7,t cF . I _ THE DETRO!T LDISON CO. ENGINEERING DEPARTMENTS SUB.N3.S.** 'U. | ||
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A 4 C43ag 8'/z' t 6. Pun t.ips WED6E AMC40R. WS4884 Mi4. EuB. s e3.j2a r | |||
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| Line 1,316: | Line 805: | ||
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| Line 1,334: | Line 819: | ||
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| Line 1,366: | Line 838: | ||
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| Line 1,381: | Line 847: | ||
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e t.' Au WELDS PER'~' _ | |||
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g-4 4 - w BotTow e @ mLu4rama shmo | |||
. sag _. | . sag _. | ||
p ul (4)"/t/dr- / - | p ul (4)"/t/dr- / - | ||
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7(me # | 7(me # | ||
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a | |||
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NA i 4 o N {Egggggggggg ygg p 6 Tic $.bb _ , | NA i 4 o N {Egggggggggg ygg p 6 Tic $.bb _ , | ||
SicN_ATURE DT 1 ISSUED. | SicN_ATURE DT 1 ISSUED. | ||
| Line 1,416: | Line 869: | ||
q .gA PORTION OF THIS DWG 15 AFFECTED BN FIELD REVISION STATUS: /C^ | q .gA PORTION OF THIS DWG 15 AFFECTED BN FIELD REVISION STATUS: /C^ | ||
ORIGINAL DCA/DCN: 1 DCR/DCN: | ORIGINAL DCA/DCN: 1 DCR/DCN: | ||
@9/M | @9/M D t.C. SUPV. ' *J*g l 8/M NO: ' R E V. | ||
D t.C. SUPV. ' *J*g l 8/M NO: ' R E V. | |||
FIELD F AB STATUS: SEIS, I, lCL C. l 0. A, 'f HGR. lSO4*4 9444676-1 REVM PD102 (&79) | FIELD F AB STATUS: SEIS, I, lCL C. l 0. A, 'f HGR. lSO4*4 9444676-1 REVM PD102 (&79) | ||
Documentation No. | Documentation No. | ||
Location Approval P.O. Icata11ation B/M EEco File No. | Location Approval P.O. Icata11ation B/M EEco File No. | ||
| Line 1,428: | Line 878: | ||
e E. s 1 i | e E. s 1 i | ||
l jf/m)48g Systes Engineer | l jf/m)48g Systes Engineer | ||
( Projoet Engineer l l ApproTed As Noted Rel. For Fab. Or Constr. I i | ( Projoet Engineer l l ApproTed As Noted Rel. For Fab. Or Constr. I i | ||
iwkJ:n | iwkJ:n | ||
-_ - -- . w __ _ _. | -_ - -- . w __ _ _. | ||
su e. ND. . -I. * . . | su e. ND. . -I. * . . | ||
| Line 1,453: | Line 899: | ||
/ 'G\ .;h | / 'G\ .;h | ||
'es. t. 2 x-2 w */ 4 x l ye i_e . /J 7 on 1 As e | 'es. t. 2 x-2 w */ 4 x l ye i_e . /J 7 on 1 As e | ||
m.g | m.g | ||
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| Line 1,465: | Line 910: | ||
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F*l w | |||
4 | 4 | ||
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| Line 1,476: | Line 917: | ||
" c INF0!EATE DE) e i | " c INF0!EATE DE) e i | ||
4 | 4 | ||
==- | ==- | ||
d.. 4. | d.. 4. | ||
| Line 1,485: | Line 924: | ||
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| Line 1,521: | Line 946: | ||
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| Line 1,539: | Line 959: | ||
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WhL | WhL s e a" v w % mOT r u n.r m. m ~.mSIGNATURE ISSUEO. MARK NOMdd.M"[8-Qto D E SIGNIDWG. ''3Df8f MS | ||
s e a" v w % mOT r u n.r m. m ~.mSIGNATURE ISSUEO. MARK NOMdd.M"[8-Qto D E SIGNIDWG. ''3Df8f MS | |||
.: *bM A PORTION OF THIS MG IS AMCTED BN FIE LO REVISt0N STATUS: | .: *bM A PORTION OF THIS MG IS AMCTED BN FIE LO REVISt0N STATUS: | ||
"< ew CHE. f3 MP / >M ORIGINAL DCR/DCN: 1 LCR/DCN: i s/u No: Rtv. | "< ew CHE. f3 MP / >M ORIGINAL DCR/DCN: 1 LCR/DCN: i s/u No: Rtv. | ||
| Line 1,547: | Line 965: | ||
$4t' .T. C laA T. HGR. lSO:6GA 944076 4 RtyM FIELD F AS ST ATUS: l CI. | $4t' .T. C laA T. HGR. lSO:6GA 944076 4 RtyM FIELD F AS ST ATUS: l CI. | ||
PD402 (8 79) | PD402 (8 79) | ||
Docu entation No. | Docu entation No. | ||
Location Approval | Location Approval | ||
~' | ~' | ||
P.O. Installation B/lf Deco File No. | P.O. Installation B/lf Deco File No. | ||
Ti'iS APPliOVAL SMf!ES Til.if Trans=1ttal cate vendor | Ti'iS APPliOVAL SMf!ES Til.if Trans=1ttal cate vendor II:E "AMsiCE3 AS l'0IED* Engineering Approved l As Noted Approved As Noted Quality Assurance Dir. | ||
II:E "AMsiCE3 AS l'0IED* Engineering Approved l As Noted Approved As Noted Quality Assurance Dir. | |||
., c y9 s I r l | ., c y9 s I r l | ||
, 1MO[ Systes Engineer Proj. Director-operations | , 1MO[ Systes Engineer Proj. Director-operations | ||
| Line 1,560: | Line 975: | ||
! ##Ah6@ , | ! ##Ah6@ , | ||
'hT. l_,_cr 0 Tile DETROt r EDISON CO. ENCL'NEERING'DEP,tRTMENTS - .300. . _ _c_3.. . . _- - f. | 'hT. l_,_cr 0 Tile DETROt r EDISON CO. ENCL'NEERING'DEP,tRTMENTS - .300. . _ _c_3.. . . _- - f. | ||
[ gay gg DESCRIPTION na ars, wt. | [ gay gg DESCRIPTION na ars, wt. | ||
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| Line 1,573: | Line 983: | ||
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| Line 1,599: | Line 1,000: | ||
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SIGNATURE DT ISSUED: MARK NO.%).244-206-Gn DE StGNIDWG. 306 l *,5 '*s ia A PORTt0N OF THIS DwG IS AFFECTED BN FIE LD REVISION STATUS: | SIGNATURE DT ISSUED: MARK NO.%).244-206-Gn DE StGNIDWG. 306 l *,5 '*s ia A PORTt0N OF THIS DwG IS AFFECTED BN FIE LD REVISION STATUS: | ||
CHK. WVll Mb - ' l' ORIG N AL DCR/DCN. DCR/DCN: | CHK. WVll Mb - ' l' ORIG N AL DCR/DCN. DCR/DCN: | ||
REV. | REV. | ||
E DFA STAT SEIS, E \CL C [ CL A. "C HGR. ISOpf44,2Jf6-1 REV.dh PD$102 (8 79) | E DFA STAT SEIS, E \CL C [ CL A. "C HGR. ISOpf44,2Jf6-1 REV.dh PD$102 (8 79) | ||
| Line 1,640: | Line 1,023: | ||
Documentation No. | Documentation No. | ||
Location Apprwal - '"** | Location Apprwal - '"** | ||
* F.O. Installattoo | * F.O. Installattoo yN Deco File No. | ||
Transmittal Date Tendor Engineering Approved l As Noted r"h o o g- - - | Transmittal Date Tendor Engineering Approved l As Noted r"h o o g- - - | ||
A@ Droved as Noted Quality Assurance Dir7 e _% . l | A@ Droved as Noted Quality Assurance Dir7 e _% . l CC @ w 2 _ _M //N /.D' States Engineer I l IC Froj. Director-Operations aA i | ||
CC @ w 2 _ _M //N /.D' States Engineer I l IC Froj. Director-Operations | |||
aA i | |||
& Projoet haineer . | & Projoet haineer . | ||
* Appre1pt As NotM 2el. For Fab. Or Constr. | * Appre1pt As NotM 2el. For Fab. Or Constr. | ||
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THE DETROIT EtslSON CO. ENGINEERING DEI'ARTMENTS SU'8. N O. 'a 7* ' | THE DETROIT EtslSON CO. ENGINEERING DEI'ARTMENTS SU'8. N O. 'a 7* ' | ||
| Line 1,676: | Line 1,041: | ||
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toes.ouir oma tecApcd fbj-3:GNATURE DT IS$UfD: | toes.ouir oma tecApcd fbj-3:GNATURE DT IS$UfD: | ||
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| Line 1,764: | Line 1,099: | ||
TP.iS APMOVAL SismmS THAT Transmittal Date vendor TI:E "APNC"'D AS fiGTED* | TP.iS APMOVAL SismmS THAT Transmittal Date vendor TI:E "APNC"'D AS fiGTED* | ||
Engineering Approved l As Noted | Engineering Approved l As Noted | ||
. Approved As Noted Quality Asst ance Dir. | . Approved As Noted Quality Asst ance Dir. | ||
n l l | n l l M /hN' System Engineer D** 9 ' " | ||
M /hN' System Engineer D** 9 ' " | |||
* I IC Proj. Director-Operations dW W - .P CA l | * I IC Proj. Director-Operations dW W - .P CA l | ||
Project Engineer | Project Engineer | ||
| Line 1,775: | Line 1,106: | ||
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| Line 1,847: | Line 1,157: | ||
FIELD REVi$lON $TATUS: | FIELD REVi$lON $TATUS: | ||
FIE LO FAS STATUS: 8/M NO: ' R E V. | FIE LO FAS STATUS: 8/M NO: ' R E V. | ||
j S E t t. | j S E t t. | ||
7 lCL < l(L A.1. HGR. ISO:fAJM % 4 2173.}REV. M Docucentation No. POWul (8-79) | 7 lCL < l(L A.1. HGR. ISO:fAJM % 4 2173.}REV. M Docucentation No. POWul (8-79) 1,ocation Approval P.O. Installation 3/lf DECO File No. | ||
Ti'iS APPiiOVAL 5:MJ1ES TilAT Trans=1tt:1 Date vendor it:E " APP;;CG f.S f;GTED* | Ti'iS APPiiOVAL 5:MJ1ES TilAT Trans=1tt:1 Date vendor it:E " APP;;CG f.S f;GTED* | ||
Engineering Approved l As Noted l | Engineering Approved l As Noted l Approved As Noted Quality Assurance Dir. I 7 | ||
Approved As Noted Quality Assurance Dir. I 7 | |||
e as _ l hMW Systes Engineer | e as _ l hMW Systes Engineer | ||
~ | ~ | ||
| Line 1,862: | Line 1,167: | ||
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Approved _ _ As Voted Rol. For Fab. Or Constr. l n a. a.w | Approved _ _ As Voted Rol. For Fab. Or Constr. l n a. a.w | ||
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At.LvsELos PER. | At.LvsELos PER. | ||
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' WP5-Wat.Nuss5dqat | ' WP5-Wat.Nuss5dqat J | ||
!M w w O INFORMATE MRV pg v. | |||
J | |||
!M w w O INFORMATE MRV | |||
pg v. | |||
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| Line 1,936: | Line 1,216: | ||
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04 i'r" PVTI" WT lexA -dad ' | 04 i'r" PVTI" WT lexA -dad ' | ||
SIGNATURE DT ISSUED: | SIGNATURE DT ISSUED: | ||
MARK NO.VJ.k.$dt 21 t8 C. 14 ! | MARK NO.VJ.k.$dt 21 t8 C. 14 ! | ||
| Line 1,951: | Line 1,228: | ||
o.s c. SUPV. @9/ # ' **re l . 8/M NO: REV. | o.s c. SUPV. @9/ # ' **re l . 8/M NO: REV. | ||
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''''#' '' "8 Docu=entation No. | ''''#' '' "8 Docu=entation No. | ||
* Location Approval ) | * Location Approval ) | ||
P.O. Installation 1 B/nl Deco File no. l TF.is APPliOVAL Sir:!T!!S TilAT transmittal Date vendor l TI:E "APPT.CED AS t;GTED* Engineering Approvea l As noted CGCf. TITS CY F 0ECT ElC:1. Approvea Ao noted Qua11ty Aeeurance Dir. | P.O. Installation 1 B/nl Deco File no. l TF.is APPliOVAL Sir:!T!!S TilAT transmittal Date vendor l TI:E "APPT.CED AS t;GTED* Engineering Approvea l As noted CGCf. TITS CY F 0ECT ElC:1. Approvea Ao noted Qua11ty Aeeurance Dir. | ||
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e _e / I I ; | e _e / I I ; | ||
&d.*//d ( Syntes Engineer | &d.*//d ( Syntes Engineer m' s T. l t 4 , | ||
m' s T. l t 4 , | |||
O O IC Proj. Director-Operations d / l j | O O IC Proj. Director-Operations d / l j | ||
,66 . . .l QA Prejoct Engineer | ,66 . . .l QA Prejoct Engineer | ||
| Line 1,966: | Line 1,239: | ||
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| Line 1,979: | Line 1,248: | ||
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| Line 2,018: | Line 1,270: | ||
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| Line 2,026: | Line 1,276: | ||
* M T y(y E l.E VAT ICnJ ',A A, | * M T y(y E l.E VAT ICnJ ',A A, | ||
$ =- r :r | $ =- r :r | ||
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g , - Au wCLOS PER 87 ;1 M A , | |||
WPstcoauutessQqac d3 - | WPstcoauutessQqac d3 - | ||
g Ma..B, kQ e - 3e s | g Ma..B, kQ e - 3e s | ||
| Line 2,037: | Line 1,283: | ||
.i , | .i , | ||
m | m | ||
' Y | ' Y Uf 'f O | ||
34 4 hl - I ecvdov R EBCidC .; | |||
Uf 'f O | c.rm ca e.PPL.Y A c.Tc Ie.et_ oTM?.P41D s . ou r- R4R. $$APS LccApcMEAd SIGNATURE DT ISSUED: | ||
34 4 | |||
hl - I ecvdov R EBCidC .; | |||
c.rm ca e.PPL.Y A c.Tc Ie.et_ oTM?.P41D s . ou r- R4R. $$APS | |||
LccApcMEAd SIGNATURE DT ISSUED: | |||
DE SIGN /DWG. ".:3C6/ O **d a 7 MARK NO.VJ.944 2n8 45 ; | DE SIGN /DWG. ".:3C6/ O **d a 7 MARK NO.VJ.944 2n8 45 ; | ||
cHa. | cHa. | ||
| Line 2,058: | Line 1,297: | ||
5tts. 7 l Ct. < lCLA 1 HCR. lSO:W P4 4 2nT3 1 Rev. A I | 5tts. 7 l Ct. < lCLA 1 HCR. lSO:W P4 4 2nT3 1 Rev. A I | ||
~ | ~ | ||
Dooucentation No. | |||
Location Approval P.O. - Installation B/W Deco File No. | |||
TF.S APPE0 VAL SIMi'JIIS T!!.iT trans=ittal Date vendor ' | TF.S APPE0 VAL SIMi'JIIS T!!.iT trans=ittal Date vendor ' | ||
i Tri "A7P;;CG AS I;GTE0" g g,,,3 3 ,,, g g, ,, g | i Tri "A7P;;CG AS I;GTE0" g g,,,3 3 ,,, g g, ,, g | ||
* Approved As Noted Quality Assurance Dir. | * Approved As Noted Quality Assurance Dir. | ||
c ., t , l | c ., t , l 1 k I/Is@ System Engineer 1 | ||
1 k I/Is@ System Engineer 1 | |||
' I D**D I I0 3 | ' I D**D I I0 3 | ||
IC Proj. Director-operations j l | IC Proj. Director-operations j l | ||
s@@ d . :n CA l Project Engineer Approved is Noted Rel. For Fab. Or Constr. | s@@ d . :n CA l Project Engineer Approved is Noted Rel. For Fab. Or Constr. | ||
| Line 2,075: | Line 1,309: | ||
..___a _. _. . - . - - -. - | ..___a _. _. . - . - - -. - | ||
Tile DETROIT LillSON CO. EhGINEERING IILPARTMENTS sus.N'a.; .e | |||
[.<t.' I OF. f . | [.<t.' I OF. f . | ||
L8 f,fy , ,''fi, DESCRIPTION n..,, ,, | L8 f,fy , ,''fi, DESCRIPTION n..,, ,, | ||
A s e,.,, | A s e,.,, | ||
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* L Gt . | * L Gt . | ||
2 | 2 B 2 L Z d2 A'/4 4 4 3/PLCs. A% | ||
B 2 L Z d2 A'/4 4 4 3/PLCs. A% | |||
Mh y 4 'uh..s | Mh y 4 'uh..s | ||
$ C d. P i pE t.,0 er 5 '/4 s'/2 W. 4 - | $ C d. P i pE t.,0 er 5 '/4 s'/2 W. 4 - | ||
U JW % - | U JW % - | ||
$ f.y . | $ f.y . | ||
| Line 2,097: | Line 1,323: | ||
la \ | la \ | ||
! , ,, e n o 10 0 fi g mw - | ! , ,, e n o 10 0 fi g mw - | ||
g Ib er%'2''1 LED COCUMW 6) | g Ib er%'2''1 LED COCUMW 6) u NAce-1SP % | ||
u NAce-1SP % | |||
y '/g '' | y '/g '' | ||
D ANO / | D ANO / | ||
| Line 2,112: | Line 1,336: | ||
}'t}S. . | }'t}S. . | ||
4 | 4 | ||
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| Line 2,124: | Line 1,345: | ||
f ft9=17, y 3- _ | f ft9=17, y 3- _ | ||
N | N | ||
,a 4 | ,a 4 | ||
-h wW p44r2176<iot u | -h wW p44r2176<iot u | ||
.ae l | .ae l | ||
Tce & | Tce & | ||
W-d t | W-d t | ||
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g ,g g,g-g,lT y~\ y4 | g ,g g,g-g,lT y~\ y4 p ig, i | ||
p ig, i | |||
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| Line 2,143: | Line 1,360: | ||
, w .(4) | , w .(4) | ||
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| Line 2,164: | Line 1,375: | ||
~ | ~ | ||
['.)octme.itstion No. Approval Location | ['.)octme.itstion No. Approval Location | ||
'P.O. Installation | 'P.O. Installation B/M MCo File No. | ||
B/M MCo File No. | |||
Ti'is APPE0 VAL S;S:GHS T!!AT | Ti'is APPE0 VAL S;S:GHS T!!AT | ||
* Transetttal pate vendor Ti'E "AFP;C'CD AS UGTED" Engineering Approved l As Noted CGCf.*.EttT5 CY F.T! CT E 102. Approved As noted quality Assurance Dir. | * Transetttal pate vendor Ti'E "AFP;C'CD AS UGTED" Engineering Approved l As Noted CGCf.*.EttT5 CY F.T! CT E 102. Approved As noted quality Assurance Dir. | ||
| Line 2,177: | Line 1,386: | ||
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5H I. 0F I | 5H I. 0F I IIII' Ul INI8II d os in i D. t' t.h e Sue.NO. | ||
IIII' Ul INI8II d os in i D. t' t.h e Sue.NO. | |||
E Sh t,iy go, DESCRIPTION isa,s 7 0 | E Sh t,iy go, DESCRIPTION isa,s 7 0 | ||
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A5304 | A5304 c i TS L w S * *3 $ 2 '5 x t'-nCW L% | ||
c i TS L w S * *3 $ 2 '5 x t'-nCW L% | |||
2 5 o 2 R. v2 e< c x 2 V4 A% | 2 5 o 2 R. v2 e< c x 2 V4 A% | ||
1 g E '/2 v. l'a x E ^% | 1 g E '/2 v. l'a x E ^% | ||
| Line 2,202: | Line 1,402: | ||
--~5 g , __ i_ pg . | --~5 g , __ i_ pg . | ||
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| Line 2,210: | Line 1,408: | ||
4y O__._ -- - | 4y O__._ -- - | ||
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6 3 | 6 3 | ||
| Line 2,216: | Line 1,413: | ||
u k | u k | ||
SJ | SJ | ||
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REF.*5 PPT,, pm%e 1 | |||
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A JUL 231930 , | A JUL 231930 , | ||
CONTROLLED 00CUW D Act wetos MR.WPS 7ecz b bg GES WM L'Ao (EA.,A PE) | CONTROLLED 00CUW D Act wetos MR.WPS 7ecz b bg GES WM L'Ao (EA.,A PE) | ||
F MS :: 14 S | F MS :: 14 S | ||
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g g" s | g g" s | ||
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* TPCMp(5e=tT.0 SIGN ATUR E DT ISSUED: MARK NO. W 744.Zn13,.$ l"[ | * TPCMp(5e=tT.0 SIGN ATUR E DT ISSUED: MARK NO. W 744.Zn13,.$ l"[ | ||
DE SIGN /OWG G DS / M .'.' f 4A PORTION OF THIS OWG IS A88 ECTED Bv | DE SIGN /OWG G DS / M .'.' f 4A PORTION OF THIS OWG IS A88 ECTED Bv j ' | ||
j ' | |||
ORIGINAL DCR/DCN. I OCR/DCN. | ORIGINAL DCR/DCN. I OCR/DCN. | ||
FIELO REVislON ST ATUS. /A\ | FIELO REVislON ST ATUS. /A\ | ||
| Line 2,274: | Line 1,449: | ||
Loostson Approval P.O. Installattoa 3/5 Deco P11e No. | Loostson Approval P.O. Installattoa 3/5 Deco P11e No. | ||
D**]D 3D 3 3 6 | D**]D 3D 3 3 6 | ||
' " "*2"*1 "*** ''***r | ' " "*2"*1 "*** ''***r g g , __ | ||
g g , __ | |||
Approved Engineering Approved l AsNote{ | Approved Engineering Approved l AsNote{ | ||
As Noted Quality Assurance Dir. | As Noted Quality Assurance Dir. | ||
l M /I/r/d,D , Systen Engineer E l IC Proj. Director-0perations aA t | |||
l M /I/r/d,D , Systen Engineer | |||
E l IC Proj. Director-0perations | |||
aA t | |||
. Projoet Engineer . | . Projoet Engineer . | ||
. Approved As Noted ' IBe1. For Feb. Or constr. | . Approved As Noted ' IBe1. For Feb. Or constr. | ||
.9Ac/wV | .9Ac/wV | ||
- - - ~ - -- - -- .. . | - - - ~ - -- - -- .. . | ||
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C t i.u. . .no l DESC".lPTION unit | C t i.u. . .no l DESC".lPTION unit | ||
^36 w?" | ^36 w?" | ||
| Line 2,302: | Line 1,467: | ||
6 2 R'/2x.2d 7'/4 O | 6 2 R'/2x.2d 7'/4 O | ||
% C i d */r x. t */s < 2 | % C i d */r x. t */s < 2 | ||
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g . - nw or a ., .1.._o | g . - nw or a ., .1.._o | ||
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g l'- 2 | g l'- 2 | ||
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'W | 'W l +r_u | ||
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: SE T{ , - - - - - - -------------j is M.G.642'-9 W | |||
u: <. # | u: <. # | ||
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(kSPok--t r- E e Im usme m n | |||
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+ | + | ||
p%- | p%- | ||
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f> e wan | f> e wan | ||
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a ggccv4 ( s.o n.0 bs ECW 32 6 E! JA.c-*cp9. | a ggccv4 ( s.o n.0 bs ECW 32 6 E! JA.c-*cp9. | ||
PPL.T ki2 6 t.OE' canip. M "iO | PPL.T ki2 6 t.OE' canip. M "iO | ||
| Line 2,376: | Line 1,502: | ||
, Engineering Approved l As Note _d l | , Engineering Approved l As Note _d l | ||
i L , ,J j Approved as Noted Quality areurance Dir. | i L , ,J j Approved as Noted Quality areurance Dir. | ||
I M //.' | I M //.' | ||
7 ,'[M > System Engineer E | 7 ,'[M > System Engineer E | ||
l IC Proj. Director-Operatto.s | l IC Proj. Director-Operatto.s u l 6 ProJoet higineer | ||
u l 6 ProJoet higineer | |||
. Apprevpd Ae Noted* Rel. For Feb. Or Cor.atr. | . Apprevpd Ae Noted* Rel. For Feb. Or Cor.atr. | ||
.9AtL4.~ | .9AtL4.~ | ||
. s u e. Ec. . | . s u e. Ec. . | ||
.. b oF i- Tile Dt.TROTT EDISON CO. ENGINEERING DEPARTMENTS l | .. b oF i- Tile Dt.TROTT EDISON CO. ENGINEERING DEPARTMENTS l 1,',7 ,, ,"& CESC:tPTION ,,,,g ,,, | ||
1,',7 ,, ,"& CESC:tPTION ,,,,g ,,, | |||
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5 a- | 5 a- | ||
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h :@e | h :@e | ||
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l h | l h | ||
o - W .(2)_ | o - W .(2)_ | ||
To BE A4CENT C~Co44E ? o. | To BE A4CENT C~Co44E ? o. | ||
87 " " -- h uindg* | 87 " " -- h uindg* | ||
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r' re . . . | r' re . . . | ||
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| Line 2,508: | Line 1,580: | ||
TFi$ AP''fiOVAL $;93!ES THAT Transmittal rate vendor TEE " APP;;CED t.3 f;0TED" gn,gn,,,,,, ,,,,,,,, g 3, ,,,,, | TFi$ AP''fiOVAL $;93!ES THAT Transmittal rate vendor TEE " APP;;CED t.3 f;0TED" gn,gn,,,,,, ,,,,,,,, g 3, ,,,,, | ||
CG.Tulis CY F:KCT EIC2. ,,,,,y,, 3, ,,g,, q,,31,, ,,,,,,,,, pg,, | CG.Tulis CY F:KCT EIC2. ,,,,,y,, 3, ,,g,, q,,31,, ,,,,,,,,, pg,, | ||
Ef.'.'' CE:t C:rfiPCMTED . | Ef.'.'' CE:t C:rfiPCMTED . | ||
c l | c l | ||
- > i 1kM | - > i 1kM Systes Engineer | ||
Systes Engineer | |||
* I D "'* *O* n r ' | * I D "'* *O* n r ' | ||
-I IC Pro). Director-0perations | -I IC Pro). Director-0perations | ||
) Jab W, ci QA l | ) Jab W, ci QA l | ||
'u,n l Q FLoject Engineer Approvod la Noted Rel. For Fab. Or Constr. | |||
'u,n l Q FLoject Engineer | |||
Approvod | |||
la Noted Rel. For Fab. Or Constr. | |||
( stDL H-34 | ( stDL H-34 | ||
= - | = - | ||
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| Line 2,538: | Line 1,599: | ||
Asc, 3 a F2 '/2 | Asc, 3 a F2 '/2 | ||
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| Line 2,553: | Line 1,607: | ||
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b ' | b ' | ||
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| Line 2,562: | Line 1,613: | ||
Au.wEtos wsgr.tyg | Au.wEtos wsgr.tyg | ||
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REV | |||
QAp /Wh he l 0.8.C. SUPV. HGR. ISO:(sM 744 Z176.) REV.M FIE LD F A8 ST ATUS: | |||
SEli I lCL C lCL A. I N" ** | SEli I lCL C lCL A. I N" ** | ||
~ Documentation No. | ~ Documentation No. | ||
Losetton Approval | Losetton Approval | ||
''~ | ''~ | ||
F.C. Installation | F.C. Installation E/B Deco File No. | ||
Transmittal Date fondor 99 Engineering Approved l &a Noted O h O le Boted QualityAssuranceDir7 Approved ggd (j g 3 _. | |||
E/B Deco File No. | |||
Transmittal Date fondor 99 | |||
Engineering Approved l &a Noted O h O le Boted QualityAssuranceDir7 Approved ggd (j g 3 _. | |||
I System Engineer M 8/r/DM 9 , | I System Engineer M 8/r/DM 9 , | ||
I E | I E | ||
IC Frej. Director-0peratior. | IC Frej. Director-0peratior. | ||
I | I | ||
- eA l | - eA l Froject Engineer apprevpd 1 | ||
As Noted' Be1. For Fab. Or constr | As Noted' Be1. For Fab. Or constr | ||
- - Mk- _ | - - Mk- _ | ||
mO SHT I cr I THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS DESCRIPTION T al'e o ~ | mO SHT I cr I THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS DESCRIPTION T al'e o ~ | ||
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FIELD p AS STATUS: SEtt | FIELD p AS STATUS: SEtt | ||
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,' Documentation No. | ,' Documentation No. | ||
Location Approval Installation P.O. | Location Approval Installation P.O. | ||
B/M DECO File No. | B/M DECO File No. | ||
Transmittal Dato Vcndor | Transmittal Dato Vcndor | ||
#ii r 9 rneinsering i,, roved I i. iioted | #ii r 9 rneinsering i,, roved I i. iioted | ||
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hp, /_or /_ THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | |||
1,ay go n DESCRIDTION m,1 , | |||
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SIGNATURE DT ISSUED-. | SIGNATURE DT ISSUED-. | ||
I RAARK NO.MM/ / # MM DE SIGN /DWG %/M <* | I RAARK NO.MM/ / # MM DE SIGN /DWG %/M <* | ||
| Line 2,847: | Line 1,803: | ||
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HGR. ISO: 6AW F44 s/OO-/ R E V. /A\. | HGR. ISO: 6AW F44 s/OO-/ R E V. /A\. | ||
FtELD F As ST ATUS SElk . I lCL ( lCLA I 70192 l | FtELD F As ST ATUS SElk . I lCL ( lCLA I 70192 l | ||
,' Documentation No. | ,' Documentation No. | ||
Approval Location i Installation P.O. I | Approval Location i Installation P.O. I B/M DECO File No. | ||
B/M DECO File No. | |||
i '3 '''"'*****' "*'* ''"*'" | i '3 '''"'*****' "*'* ''"*'" | ||
Approved l As Noted D 0 Engineering Approved As Noted Quality Ascut-ance Dir. | Approved l As Noted D 0 Engineering Approved As Noted Quality Ascut-ance Dir. | ||
a l | a l I | ||
t | |||
(!zei,#f@ S;utt.n En;i teor l | (!zei,#f@ S;utt.n En;i teor l | ||
E IC Proj. Director-Operationt-l QA Project Engineer | E IC Proj. Director-Operationt-l QA Project Engineer | ||
, Appraved f As Noted | , Appraved f As Noted Bel, For Fab. Or Constr. | ||
j 7N-b ~ - | |||
Bel, For Fab. Or Constr. | |||
j | |||
7N-b ~ - | |||
l | l | ||
_-- ~~ | _-- ~~ | ||
"J f -l 5HT OF l THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | "J f -l 5HT OF l THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | ||
'l'f affn DESCRIPTION | 'l'f affn DESCRIPTION | ||
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stGNATURE DT tsSutD; DE SIGNSWG WM b MARK NO WM hGot CH K. 9/W d2fn A PORTtON OF THIS DWG f5 AF FECTED 8v FIE LD RE VISION STATUS SUPV TR/8t/ aklM OR6GehAL DCR/DCN. { DCA/Oces I BM NO R F'' | stGNATURE DT tsSutD; DE SIGNSWG WM b MARK NO WM hGot CH K. 9/W d2fn A PORTtON OF THIS DWG f5 AF FECTED 8v FIE LD RE VISION STATUS SUPV TR/8t/ aklM OR6GehAL DCR/DCN. { DCA/Oces I BM NO R F'' | ||
FIELD FAB ST ATUS. ISEtt "I l Ct. C, lCLA .I HGR. tSO eWM PWYS82-8 REV A en 102 sev A | FIELD FAB ST ATUS. ISEtt "I l Ct. C, lCLA .I HGR. tSO eWM PWYS82-8 REV A en 102 sev A Documentation No. | ||
Documentation No. | |||
Loostion Approval P.O. Instal.lation w=. _ _3/E DECO Pile No. | Loostion Approval P.O. Instal.lation w=. _ _3/E DECO Pile No. | ||
' '"8'8 - | ' '"8'8 - | ||
fransmittal Date ~ Tendor Engineering Approved l As Noted | fransmittal Date ~ Tendor Engineering Approved l As Noted | ||
, Approved As Noted Quality Assuranos Dir | , Approved As Noted Quality Assuranos Dir | ||
~ | ~ | ||
i | i M 6 a *' | ||
M 6 a *' | |||
, c System .gineer IC Proj. D1 rector-operatfor.e | , c System .gineer IC Proj. D1 rector-operatfor.e | ||
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l | l | ||
+ - | + - | ||
Pros.et ng1n.or | Pros.et ng1n.or | ||
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w | w | ||
. sHT I cr I THE DETROIT EDISON CO. ENGINEERING DEPARTMEhTS s . | . sHT I cr I THE DETROIT EDISON CO. ENGINEERING DEPARTMEhTS s . | ||
O R M AT*L WT ___ | O R M AT*L WT ___ | ||
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M | M 3 i q | ||
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| Line 3,144: | Line 1,976: | ||
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| Line 3,178: | Line 1,998: | ||
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pn IDZ WV A Documentation 50. | pn IDZ WV A Documentation 50. | ||
. . _ . . . . . . . - - . . - 4oostion app %1 , | . . _ . . . . . . . - - . . - 4oostion app %1 , | ||
1 P.O. Instauntion | 1 P.O. Instauntion | ||
_3/3 -- | _3/3 -- | ||
Deco Pile No. | Deco Pile No. | ||
Transmittal Date Tender ao o g Engineering Approved l As Soted l s Approved As Noted Quality Assurance.Dir. | Transmittal Date Tender ao o g Engineering Approved l As Soted l s Approved As Noted Quality Assurance.Dir. | ||
oW c - J $ l N ///b */8 Systen Engineer | oW c - J $ l N ///b */8 Systen Engineer | ||
* I | * I | ||
- E - | - E - | ||
t l | t l | ||
- 1 | - 1 | ||
.O Pioj. Director-Operations | .O Pioj. Director-Operations e 8 | ||
, . M . _ l Projoet knaineer ' | |||
, . M . _ l | |||
Projoet knaineer | |||
s , , , Approvej , As Noted Es1. Por Pab. Or Constr. 3 QM[ | s , , , Approvej , As Noted Es1. Por Pab. Or Constr. 3 QM[ | ||
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3 . | 3 . | ||
_l- Or i THE DETROTT EDISON CO. ENGINEERING DEPARTMENTS Ii,f ca"e o DESCOsPTION m , ~ | |||
_l- Or i THE DETROTT EDISON CO. ENGINEERING DEPARTMENTS Ii,f | |||
ca"e o DESCOsPTION m , ~ | |||
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Fe 5/p tio y.t o Ag B | Fe 5/p tio y.t o Ag B | ||
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FIE LD P_A8 :TATUS: l Cl. C. | |||
70102 I | 70102 I | ||
,' Documentation No. | ,' Documentation No. | ||
| Line 3,301: | Line 2,059: | ||
//O'#,$ S; tt:s Erincer IJ , | //O'#,$ S; tt:s Erincer IJ , | ||
W . | W . | ||
l E | l E | ||
IC Eroj. Director-Operations cA I Project Engineer i | IC Eroj. Director-Operations cA I Project Engineer i | ||
| Line 3,307: | Line 2,064: | ||
t W,Td~ . | t W,Td~ . | ||
r | r | ||
M I 'OF 1 THE DETROTT EDISON CO. ENGINEERING DEPARTMENTS SHT | M I 'OF 1 THE DETROTT EDISON CO. ENGINEERING DEPARTMENTS SHT | ||
| Line 3,313: | Line 2,069: | ||
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I ' Tir. (4) Pt45. | I ' Tir. (4) Pt45. | ||
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asARK seo. W-PA4 85100- 608 onSecNiowa c,0. /W.R. 'Ma p, jg q, p A PORTM)N OF THIS OWC t$ AFFECTED ON FIE LD REvillON STATUS | asARK seo. W-PA4 85100- 608 onSecNiowa c,0. /W.R. 'Ma p, jg q, p A PORTM)N OF THIS OWC t$ AFFECTED ON FIE LD REvillON STATUS QR6 GIN AL DCR/DCh; 1 DCA/DCN. | ||
QR6 GIN AL DCR/DCh; 1 DCA/DCN. | |||
gUPV. T. M /LM. M h'h"4 - | gUPV. T. M /LM. M h'h"4 - | ||
l 8/M NO- - | l 8/M NO- - | ||
R E''. | R E''. | ||
FitLD F A5 STATUS: SEIS. ' I lCL C lRA 1 MC5L ISO 4WH.P44 9001 REV. A po, 10Z Rev A | FitLD F A5 STATUS: SEIS. ' I lCL C lRA 1 MC5L ISO 4WH.P44 9001 REV. A po, 10Z Rev A | ||
_h .- 12caumenta. tion 23. | _h .- 12caumenta. tion 23. | ||
gg. ___ __ __ __ | gg. ___ __ __ __ | ||
Installation l P.O. | Installation l P.O. | ||
B/)I DSCo File No. | B/)I DSCo File No. | ||
| Line 3,417: | Line 2,130: | ||
: , 'Q Approved f.:3 Noted Quality Assurance Dir. | : , 'Q Approved f.:3 Noted Quality Assurance Dir. | ||
J l Q' h . .i . | J l Q' h . .i . | ||
OM.,M i Syntt:5 Epincor _ | OM.,M i Syntt:5 Epincor _ | ||
11 E | 11 E | ||
\ l IC Proi. Director-Operatione CA l'' l Project Enginear | \ l IC Proi. Director-Operatione CA l'' l Project Enginear | ||
< Apprgvef,_ As Noted Be1. For Fab. Or Constr. | < Apprgvef,_ As Noted Be1. For Fab. Or Constr. | ||
| Line 3,426: | Line 2,137: | ||
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t | t | ||
l _=_ - -.. . | l _=_ - -.. . | ||
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THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | ||
; | ; | ||
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h* f. __ '&tcC. | h* f. __ '&tcC. | ||
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stGN ATUR E OT llSUED- h4 ARK NOJe//%4 5/OO-609 K. (P/ ( A #, 3 | stGN ATUR E OT llSUED- h4 ARK NOJe//%4 5/OO-609 K. (P/ ( A #, 3 | ||
,['ag [gh" d$g I I" FIE LD REVI5 TON STATUS / | ,['ag [gh" d$g I I" FIE LD REVI5 TON STATUS / | ||
Surv. TES /DC. iA7 EN No- REv F E LD F A8 8TATUS. SEli J lCL C lh7 NGR. ISOw. mad. SED- / REvd Pol 02 Documentatico Bo. . | Surv. TES /DC. iA7 EN No- REv F E LD F A8 8TATUS. SEli J lCL C lh7 NGR. ISOw. mad. SED- / REvd Pol 02 Documentatico Bo. . | ||
Laation Approval F.O. Installation O kl 4 @0 P 1 4 | Laation Approval F.O. Installation O kl 4 @0 P 1 4 gi 1[ Transmittal Date fonder O yj g Engineering Approved l As Noted Approved as Noted Quality Assurance Dir. | ||
gi 1[ Transmittal Date fonder | |||
1 M [f6/48 I System Engineer 8 i i IC FrsJ. Director-0perations GA / l Projoet haineer | 1 M [f6/48 I System Engineer 8 i i IC FrsJ. Director-0perations GA / l Projoet haineer | ||
. Apprevq$ , As Noted Rel. For Fab. Or Constr. | . Apprevq$ , As Noted Rel. For Fab. Or Constr. | ||
| Line 3,502: | Line 2,182: | ||
. I | . I | ||
gg7 / OF / THE DETROIT EDISON CO. ENGINEERING DEPARTME TS | gg7 / OF / THE DETROIT EDISON CO. ENGINEERING DEPARTME TS | ||
( 1:2 affo DESCRIPTION u ng.t A-M | ( 1:2 affo DESCRIPTION u ng.t A-M C' - | ||
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| Line 3,521: | Line 2,193: | ||
f | f | ||
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| Line 3,535: | Line 2,202: | ||
N - - | N - - | ||
l l | l l | ||
= c rz. u f-e" g \ _ ffg g i so L_" | |||
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rz. u f-e" g \ _ ffg g i so L_" | |||
y- M & . p fVp_ _ | y- M & . p fVp_ _ | ||
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ll I I aw d | |||
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h mawmmw~nt:w=W' OT SIGNATURE ISSUED. htARK NO.MAM 6tOO-6/O DEssGN/DWG #8/M6 CHK. (P/M' *** A PORTION OF THis DWG t$ AFFECTED BY FIELD REVislON STATUS URIG4N AL DCA/DCN. l DCR/DCN. | h mawmmw~nt:w=W' OT SIGNATURE ISSUED. htARK NO.MAM 6tOO-6/O DEssGN/DWG #8/M6 CHK. (P/M' *** A PORTION OF THis DWG t$ AFFECTED BY FIELD REVislON STATUS URIG4N AL DCA/DCN. l DCR/DCN. | ||
Surv. n5//:C " I * * * "'' | Surv. n5//:C " I * * * "'' | ||
| Line 3,580: | Line 2,232: | ||
l IC Proj. Director-Operations M l Projoot kgineer | l IC Proj. Director-Operations M l Projoot kgineer | ||
, Apprged f _ As Noted Be1. For Feb. Or Constr. I SSb5h-N $b a | , Apprged f _ As Noted Be1. For Feb. Or Constr. I SSb5h-N $b a | ||
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,s . | ,s . | ||
| Line 3,588: | Line 2,238: | ||
THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | ||
: m. m DESCRIPTION h Vf ,, eYn | : m. m DESCRIPTION h Vf ,, eYn | ||
-W 4 Y1" Ot A.V. S'/2- Lfa. PHILLtPS WCOGE Au CHO R , | -W 4 Y1" Ot A.V. S'/2- Lfa. PHILLtPS WCOGE Au CHO R , | ||
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| Line 3,596: | Line 2,245: | ||
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| Line 3,606: | Line 2,253: | ||
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%y 3l ' | %y 3l ' | ||
wru.Sek y | wru.Sek y | ||
SECTIOu B-B el I. l 3 | SECTIOu B-B el I. l 3 | ||
= 4 | = 4 K p. ..-cm - | ||
K p. ..-cm - | |||
i F-p l l DEST 6u t.oAos d | i F-p l l DEST 6u t.oAos d | ||
F y N E ET.h t 11 8 # | F y N E ET.h t 11 8 # | ||
A il ;1 i 1 F1 ( M-Sb i 710 # | A il ;1 i 1 F1 ( M-Sb i 710 # | ||
-l | -l | ||
- -- L- | - -- L- | ||
% u ..- . . _ | % u ..- . . _ | ||
| Line 3,670: | Line 2,291: | ||
> REF. StiPPORT w - P44. r>too. ses , | > REF. StiPPORT w - P44. r>too. ses , | ||
",V y U^D . UE | ",V y U^D . UE | ||
!5 o s**ne,.Et.<,,4r.(/ , - | !5 o s**ne,.Et.<,,4r.(/ , - | ||
k- I l *M ' | k- I l *M ' | ||
,n | ,n k .g 3 | ||
4.e = | |||
k .g | |||
h | h | ||
; e l .. .s l4h, le - - | ; e l .. .s l4h, le - - | ||
, ; (ia . rs Q | , ; (ia . rs Q u | ||
u | |||
: g. > 3 A,% 3sf ' 9 | : g. > 3 A,% 3sf ' 9 | ||
. . g g | . . g g | ||
gijc Mr. '.Tyr. 6 6 <=ce j _ | gijc Mr. '.Tyr. 6 6 <=ce j _ | ||
'N r." T v. | 'N r." T v. | ||
bMb 5h C + | bMb 5h C + | ||
SEC.T t o M A-A lL.0Caitou FLAN | SEC.T t o M A-A lL.0Caitou FLAN S | ||
E ECvJCol SL&PP LN 5N*/RETTatocho3L L&RAJ TO THERMM. REM:. torRs.C.oNet uGR ' | |||
_3 a 9 | _3 a 9 | ||
( . F AkJ L. Liut7 eu:A ,uutT'L - | ( . F AkJ L. Liut7 eu:A ,uutT'L - | ||
SIGN ATUR E DT- ISSUED. MARK seo W-P44 Stoo-Gil DEsicN Tmc c.e / W L Rh6 A PostTION OT THl3 DwG 15 aF FECTED 9V g* . | SIGN ATUR E DT- ISSUED. MARK seo W-P44 Stoo-Gil DEsicN Tmc c.e / W L Rh6 A PostTION OT THl3 DwG 15 aF FECTED 9V g* . | ||
FIE LD REVISION ST ATUS h OR4 GIN AL DCR/DCN l DCA/DCN SM NO Rf'' | |||
FIE LD REVISION ST ATUS h | |||
Rf'' | |||
T.R.D. /LM1M i | T.R.D. /LM1M i | ||
*- SUPV. HCR. ISO (,WM-r44-5d00-1 REV /A\, | *- SUPV. HCR. ISO (,WM-r44-5d00-1 REV /A\, | ||
| Line 3,712: | Line 2,317: | ||
Approval Location Installation P.O. | Approval Location Installation P.O. | ||
DECO File No. | DECO File No. | ||
~~B/M | ~~B/M p ''*"'"5''*2 "*** | ||
p ''*"'"5''*2 "*** | |||
0 *D'%' n Engineering Aporoved l As Noted I @g g .J 3 Approved A3 Noted Quality As:surance Dir. | 0 *D'%' n Engineering Aporoved l As Noted I @g g .J 3 Approved A3 Noted Quality As:surance Dir. | ||
l "c | l "c | ||
S;::tts En-inecr | S;::tts En-inecr Y M/se,M " l E | ||
Proj. Director-Operatio s IC I | Proj. Director-Operatio s IC I | ||
SA Project Engineer m Apprgved t is Noted Rel. For Fab. Or Constr. | SA Project Engineer m Apprgved t is Noted Rel. For Fab. Or Constr. | ||
| Line 3,724: | Line 2,326: | ||
'isi, , | 'isi, , | ||
,- _CF _ l THE DETROIT EDISON CO. ENGINEERING DEPARTMESTS DESCRIPTION *a a t.1L girt g (sy , ,w o, | ,- _CF _ l THE DETROIT EDISON CO. ENGINEERING DEPARTMESTS DESCRIPTION *a a t.1L girt g (sy , ,w o, t$' | ||
t$' | |||
-} 4 42" % es '/2 " PW' t L t 8:5 W EOcsE" AMCMOQS RIL-GG4 W u E ue. -3 't 2 " | -} 4 42" % es '/2 " PW' t L t 8:5 W EOcsE" AMCMOQS RIL-GG4 W u E ue. -3 't 2 " | ||
D As C - | D As C - | ||
g n K 9/4Ksotto | g n K 9/4Ksotto | ||
* A'2005 | * A'2005 | ||
. % M-8> t,312 S K ~-3 '-fa"L 6 , | . % M-8> t,312 S K ~-3 '-fa"L 6 , | ||
C l g e co v g 2. R */J., gl 2 3/A v 2 3/A AD 0 A D G-2 L 2 % 2 if '/4 X G" Ld:s . | C l g e co v g 2. R */J., gl 2 3/A v 2 3/A AD 0 A D G-2 L 2 % 2 if '/4 X G" Ld:s . | ||
p i L 2. % 2 % /4JC d'/2'L62 8 A% | p i L 2. % 2 % /4JC d'/2'L62 8 A% | ||
E ..., _fALE | E ..., _fALE | ||
_ g*ny, | _ g*ny, g 6 9 _ s h ' | ||
g 6 9 _ s | |||
h ' | |||
T~~ '/ | T~~ '/ | ||
= ]" ~-L _ | = ]" ~-L _ | ||
..''#:: et-1,4 4._s '/z'(c.o.) | ..''#:: et-1,4 4._s '/z'(c.o.) | ||
%%ecR4 1 | %%ecR4 1 | ||
Q | Q 5 | ||
5 | |||
\ | \ | ||
M y sp,. | M y sp,. | ||
E v m --' , -y 'rve w . . . | E v m --' , -y 'rve w . . . | ||
-LD'" s.gp- | -LD'" s.gp- | ||
| Line 3,767: | Line 2,348: | ||
!i rzz | !i rzz | ||
.E __ | .E __ | ||
i | i l l1; s 1- w 4 | ||
l l1; s 1- w 4 | |||
e e, y i 1 1.4...- | e e, y i 1 1.4...- | ||
- f -t T.::r | - f -t T.::r 1Et.;G4f.(; | ||
1Et.;G4f.(; | |||
1 | 1 | ||
'_f4Ybe'd une ug - - W.y% - | '_f4Ybe'd une ug - - W.y% - | ||
D @ @ | D @ @ | ||
O EIEVA' TJc4J WA" - | O EIEVA' TJc4J WA" - | ||
n? " | n? " | ||
.a Ed m.atr A Ah | .a Ed m.atr A Ah | ||
{y nween s zee' T"CE-40;flM 5 iln=' . | {y nween s zee' T"CE-40;flM 5 iln=' . | ||
QQ ,N u | QQ ,N u | ||
a $-2L ' | a $-2L ' | ||
| Line 3,798: | Line 2,372: | ||
_3 /5 Deco rile No. | _3 /5 Deco rile No. | ||
Tranentttal Date Tender oA m O $- Engineering Approved l As poted gg Approved As Noted Quality Assurance Dir | Tranentttal Date Tender oA m O $- Engineering Approved l As poted gg Approved As Noted Quality Assurance Dir | ||
_M []My M Systen Engineer | _M []My M Systen Engineer E l | ||
~ | ~ | ||
IC Proj. Director-operatione QA l Projoet hsineer | IC Proj. Director-operatione QA l Projoet hsineer | ||
, apprqvagt, As Noted Rel. For Feb. Or Constr. | , apprqvagt, As Noted Rel. For Feb. Or Constr. | ||
Y $ | Y $ | ||
l | l | ||
l---- | l---- | ||
sHT I or 1 THE DETROIT EI)1 SON CO. ENGINEERING DEPARTMENTS , | sHT I or 1 THE DETROIT EI)1 SON CO. ENGINEERING DEPARTMENTS , | ||
1 DESCR M M ,,,,g ,, | 1 DESCR M M ,,,,g ,, | ||
Yo aret | Yo aret | ||
@ 4 T2 " DI A4 S W" 16 PHILL)PS WEO6E tJ3C MoR | @ 4 T2 " DI A4 S W" 16 PHILL)PS WEO6E tJ3C MoR | ||
' c^ ' " *' *5 - '2 ' " ' | ' c^ ' " *' *5 - '2 ' " ' | ||
s'.''o"t.6.'2 " "*W "e>"""uotsd | s'.''o"t.6.'2 " "*W "e>"""uotsd 5 w/(4) rx. | ||
5 w/(4) rx. | |||
(s) .in =gN4 x s t- x Aw c) _i R. s/aa x 45/4- x O' - 43/4" t.A. (tmitL va-vsuT uos.s a2 O | (s) .in =gN4 x s t- x Aw c) _i R. s/aa x 45/4- x O' - 43/4" t.A. (tmitL va-vsuT uos.s a2 O | ||
.;_T.E 6 x 5* x -Va x W L(s . Asoo.e | .;_T.E 6 x 5* x -Va x W L(s . Asoo.e | ||
$ b) 21 (E'> -' 1 T.S. 3 " x 3 % 8/4" y O'-(s" 14. (FlEtJ) CLIT ro MIT') - go. g A% | $ b) 21 (E'> -' 1 T.S. 3 " x 3 % 8/4" y O'-(s" 14. (FlEtJ) CLIT ro MIT') - go. g A% | ||
4*% O'- 9 " 1.6 | 4*% O'- 9 " 1.6 | ||
.ft.1/2" y, l f3:) -1~ | .ft.1/2" y, l f3:) -1~ | ||
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| Line 3,834: | Line 2,395: | ||
5 la _m 5 . | 5 la _m 5 . | ||
t 5 y | t 5 y | ||
+ | + | ||
g .mr.<m mi y x ^ | g .mr.<m mi y x ^ | ||
| Line 3,841: | Line 2,401: | ||
+ uno u | + uno u | ||
~~ | ~~ | ||
4 | 4 | ||
+ ]~M 5 .I-StiffMT @ ,,,, | + ]~M 5 .I-StiffMT @ ,,,, | ||
: b. ,h : | : b. ,h : | ||
0 a | 0 a | ||
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,W, e | ,W, e a | ||
g srzr. :suecea:T w.e44-eico-son - ( l i | |||
srzr. :suecea:T w.e44-eico-son - ( l | |||
i | |||
6 / = w_ | 6 / = w_ | ||
.c_ | .c_ | ||
l__ g 'I | l__ g 'I 5 E n | ||
5 E n | |||
m !. . .. , , - - | m !. . .. , , - - | ||
l | l | ||
( | ( | ||
,ste | ,ste | ||
_b r M,Q5 ---- | _b r M,Q5 ---- | ||
=p_ ,, i y | =p_ ,, i y r i I secTion e-e | ||
r i I secTion e-e | |||
--- L- b-i. ' , | --- L- b-i. ' , | ||
[ | [ | ||
-m' j | -m' j | ||
8 bJ | 8 bJ | ||
; 4 E" l[] J | ; 4 E" l[] J l | ||
DESIGhl WD: | |||
FxtE-VI)d1409 4 - | FxtE-VI)d1409 4 - | ||
8 ! # ' | 8 ! # ' | ||
P g E mm. | P g E mm. | ||
st c,4 '-e n R l i -*, | st c,4 '-e n R l i -*, | ||
p e _ | p e _ | ||
4'-2 n 3 | 4'-2 n 3 | ||
= | = | ||
. . IA w. ' | . . IA w. ' | ||
l' ?a. | l' ?a. | ||
a D : .* - | a D : .* - | ||
'jhk , f;.. | 'jhk , f;.. | ||
4 h4 _II A- | 4 h4 _II A-s'tu-(D ' " | ||
s'tu-(D ' " | |||
c tve.~ Tyr. Tve.- wr. :.613 w | c tve.~ Tyr. Tve.- wr. :.613 w | ||
.1 | .1 g - . | ||
g - . | |||
0 -, | 0 -, | ||
gg S E( T i o N A-A C om o II | gg S E( T i o N A-A C om o II | ||
$d a S | $d a S | ||
- EECW MPPLT 4 RETT.1RN TO THERMA 1. R.ECAMOluGK | - EECW MPPLT 4 RETT.1RN TO THERMA 1. R.ECAMOluGK | ||
_T Au Coll Eu rT N'/"4 t OD B O'J1, KEAC.TbR C4.D(n .uutT*1 - | _T Au Coll Eu rT N'/"4 t OD B O'J1, KEAC.TbR C4.D(n .uutT*1 - | ||
stGNATURE DT ISSUED; MARK NO.VJ.pf4.gloc. GlS A PORTION OF TNis OWC f 3 AFFECTkD BN FIELD REVISION STATUS-DRIGIN AL DCA/DCN I DCA/DCN. | |||
stGNATURE DT ISSUED; MARK NO.VJ.pf4.gloc. GlS | |||
A PORTION OF TNis OWC f 3 AFFECTkD BN FIELD REVISION STATUS-DRIGIN AL DCA/DCN I DCA/DCN. | |||
b ~ | b ~ | ||
-at.o./M_ % ~ I BM No: R D'. | -at.o./M_ % ~ I BM No: R D'. | ||
| Line 3,930: | Line 2,450: | ||
FDELD FAB STATUS, J- - | FDELD FAB STATUS, J- - | ||
SEff6 1 - l Ct. - C lh 1 HGR. lSO:(,Wr444to.) REYd\ | SEff6 1 - l Ct. - C lh 1 HGR. lSO:(,Wr444to.) REYd\ | ||
Fo 602 Qv A | Fo 602 Qv A Documentation No. i | ||
_ h tton Approval D@00 l n '' E/M Ia't=22= stoa | |||
Documentation No. i | |||
_ h tton Approval | |||
D@00 l n '' E/M Ia't=22= stoa | |||
-l* (J Transmittal Date Deco File No. | -l* (J Transmittal Date Deco File No. | ||
Tendor l | Tendor l | ||
Engineering Approved l As Noted Approved As Noted Quality Assurance Dir~ | |||
Engineering Approved l As Noted | |||
Approved As Noted Quality Assurance Dir~ | |||
a ; | a ; | ||
~ | ~ | ||
I Oh'. N Systen Engineer . | I Oh'. N Systen Engineer . | ||
.E l IC Proj. Director-operatione | .E l IC Proj. Director-operatione | ||
* . m l 1 Project Engineer , | |||
* . m l | |||
..r- - | ..r- - | ||
. . m ApprJegdr As Noted ' 3el. For Fab. Or Constr. I ' | . . m ApprJegdr As Noted ' 3el. For Fab. Or Constr. I ' | ||
, 9,' $ .,, . . . . , . E4.sf - | , 9,' $ .,, . . . . , . E4.sf - | ||
g | g | ||
.r | .r | ||
sHT I 0F i THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS k ' | sHT I 0F i THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS k ' | ||
l'T . "8n DESCRIPTION u.n my E.-- A 2 L s"x% %~t 0-10~' '" lCUT10 S U *O A*% | l'T . "8n DESCRIPTION u.n my E.-- A 2 L s"x% %~t 0-10~' '" lCUT10 S U *O A*% | ||
u z B J L 2*aam 'm'r o'-2'LG A * * '" | u z B J L 2*aam 'm'r o'-2'LG A * * '" | ||
(, q ,g g ,, 5 O'-l~ t.A. . P pet.adnS [TRACEAELE MAT"d *A% C= B D E | (, q ,g g ,, 5 O'-l~ t.A. . P pet.adnS [TRACEAELE MAT"d *A% C= B D E | ||
!;; \ | !;; \ | ||
* i w s.a L- - - - _ - - - - tlV$wtol -, | * i w s.a L- - - - _ - - - - tlV$wtol -, | ||
| Line 3,976: | Line 2,475: | ||
1 e | 1 e | ||
o | o | ||
- - , ,41- | - - , ,41-i i 7, | ||
i i 7, | |||
l h--, l | l h--, l | ||
= | = | ||
7 | 7 | ||
[g | [g | ||
;=. | ;=. | ||
q l | q l | ||
l | l | ||
_l l_ _4 o -- l l1 4- 1tET. h)Pf0flT l _ | |||
_l l_ _4 | |||
o -- l l1 4- 1tET. h)Pf0flT l _ | |||
l- -- | l- -- | ||
T~" l WI I | T~" l WI I Jl | ||
Jl | |||
: W-944 5too Got (gyp) / %. | : W-944 5too Got (gyp) / %. | ||
I fise A__ _ _ _ | I fise A__ _ _ _ | ||
| Line 4,010: | Line 2,497: | ||
> $ l | > $ l | ||
* B l I | * B l I | ||
- e l1 V cw. i. yr,1T Gr40 ho r, i i | - e l1 V cw. i. yr,1T Gr40 ho r, i i 1l jj lF - | ||
1l jj lF - | |||
h_s'b_.= | h_s'b_.= | ||
c =rf a t. _ , , | c =rf a t. _ , , | ||
.= - - G _ _ a | .= - - G _ _ a | ||
| Line 4,026: | Line 2,508: | ||
, t , r. | , t , r. | ||
: s. gy.' | : s. gy.' | ||
g | g | ||
,~ | ,~ | ||
q) | q) | ||
- E g a {& \ | - E g a {& \ | ||
u g _s - | u g _s - | ||
h wood A-A u. w ' r*~1 4 s'N o NOTI. MAerTA.4 H Ad l[se,%9 ' i l I | |||
4 s'N o NOTI. MAerTA.4 H Ad l[se,%9 ' i l I | |||
@ Cmd L4AD'. g | @ Cmd L4AD'. g | ||
~p # | ~p # | ||
PAT. L.de Ca>(Q(($ As4D | PAT. L.de Ca>(Q(($ As4D | ||
* W T $JPPolllt STEEs.. - | * W T $JPPolllt STEEs.. - | ||
Q F(te-5)s t 24od p O_.2_ , | Q F(te-5)s t 24od p O_.2_ , | ||
i.i 1.d h( M 5uM ECTJ8d 1DT**e.ReJL. F.E4 4ibaseJr. F4N co+ L* rr slGNATURE DT ISSUED: MARK NO. N-P444. Snoo<,iq | i.i 1.d h( M 5uM ECTJ8d 1DT**e.ReJL. F.E4 4ibaseJr. F4N co+ L* rr slGNATURE DT ISSUED: MARK NO. N-P444. Snoo<,iq I RG AL DCR D RO SUPv. *fRP]3 g ifallii 8'M NO RF" FIE LO FA8 5TATUS: SEl$ I lCL C. lCL A I >+GR. eso WM hMioo 8 REVk pa 102 riev A Documentatien No. | ||
I RG AL DCR D RO | |||
SUPv. *fRP]3 g ifallii 8'M NO RF" FIE LO FA8 5TATUS: SEl$ I lCL C. lCL A I >+GR. eso WM hMioo 8 REVk pa 102 riev A | |||
Documentatien No. | |||
_ Location approval a | _ Location approval a | ||
F.O. _Ipetallataoo | F.O. _Ipetallataoo | ||
~~ ' * * * | ~~ ' * * | ||
* 3/M Deco File No. | |||
3/M Deco File No. | |||
Transmittal Date Fondor Bogineering Approved l As Noted OQ m \%. | Transmittal Date Fondor Bogineering Approved l As Noted OQ m \%. | ||
, D D Acorov a as sot d oualter se arane. cir.- | , D D Acorov a as sot d oualter se arane. cir.- | ||
@df c. , | @df c. , | ||
. M //Lf /[. N." i System Engineer - | . M //Lf /[. N." i System Engineer - | ||
t i i IC Proj. Director-operatione | t i i IC Proj. Director-operatione | ||
~ . | ~ . | ||
eA . - i. l rios.et mesa e ' | |||
eA . - i. l | |||
rios.et mesa e | |||
, . . APDryvendf As Noted Eel. For Feb. Or Constr. | , . . APDryvendf As Noted Eel. For Feb. Or Constr. | ||
. 'i- "[f g.ig-Q ~ ' | . 'i- "[f g.ig-Q ~ ' | ||
s | s | ||
\ | \ | ||
i THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | i THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS | ||
_ i_or DESCRIPTION u ,,.t ,, | _ i_or DESCRIPTION u ,,.t ,, | ||
?.d ,Te o | ?.d ,Te o TS 2 y 2 x 'i4 % O'-4"LG MIO)W & NENT NOLE A500 r,Re | ||
TS 2 y 2 x 'i4 % O'-4"LG MIO)W & NENT NOLE A500 r,Re | |||
-TC 1 A3G | -TC 1 A3G | ||
~ TG) 1 R v1 | ~ TG) 1 R v1 | ||
| Line 4,096: | Line 2,545: | ||
* V4 Y O'- S" t G A3G (n ) | * V4 Y O'- S" t G A3G (n ) | ||
L 2 X 2 # V4 X O '- t '+4 ^ L G A36 g) : | L 2 X 2 # V4 X O '- t '+4 ^ L G A36 g) : | ||
5 . | 5 . | ||
- DESIGN LOAD | - DESIGN LOAD s: | ||
s I VERT = t 225/ | s I VERT = t 225/ | ||
W LATR 1150* | W LATR 1150* | ||
0 [ , | 0 [ , | ||
Y | Y | ||
_a_ __ | _a_ __ | ||
d s | d s | ||
N . bict 'n . | N . bict 'n . | ||
4n 1-- ,, | 4n 1-- ,, | ||
(ryp) 'j i, J | (ryp) 'j i, J Orp) I, g | ||
Orp) I, g | |||
> o e | > o e | ||
C EL GSG' 6' T iu by = _ ._ {" T ",,_.% | C EL GSG' 6' T iu by = _ ._ {" T ",,_.% | ||
2 _ | 2 _ | ||
jg 4 3cygo -- ., | jg 4 3cygo -- ., | ||
& SUPPORT h W 944 Stoo Go4 4PLCS \ l o . y ap y (TYP) / kgV b | & SUPPORT h W 944 Stoo Go4 4PLCS \ l o . y ap y (TYP) / kgV b | ||
g SECTION- A-A g g | g SECTION- A-A g g | ||
| Line 4,129: | Line 2,568: | ||
y f | y f | ||
K (k n :. | K (k n :. | ||
I 4 .*' t I | I 4 .*' t I u | ||
u | |||
h C I h$$ | h C I h$$ | ||
DIV-I(H EECW .5UPPLY ( RETURN TO THfRMAL RfCOMBINEA - | DIV-I(H EECW .5UPPLY ( RETURN TO THfRMAL RfCOMBINEA - | ||
h (k FAN COIL UNIT REACTOR BLOG UNIT # 2 9:fy saanATURE ci ISSUED: MARK NO. W-P44 SIOO Gli A R t0N O T $ G $ ' | h (k FAN COIL UNIT REACTOR BLOG UNIT # 2 9:fy saanATURE ci ISSUED: MARK NO. W-P44 SIOO Gli A R t0N O T $ G $ ' | ||
FIELD REVislON STATUS . A | FIELD REVislON STATUS . A 3c .; , p DR surV. Tpd/.7 3 * ** D S/M NO- R E *' | ||
FIE LD FA5 STATUS. SEli I \CL C lCLA I HGR. ISOM N S/OO / REV /A mlDZ | |||
3c .; , p DR surV. Tpd/.7 3 * ** D S/M NO- R E *' | |||
FIE LD FA5 STATUS. SEli I \CL C lCLA I HGR. ISOM N S/OO / REV /A | |||
mlDZ | |||
,' Documentation No. | ,' Documentation No. | ||
Approval Location P.O. Instal _Intion DECO File No. | Approval Location P.O. Instal _Intion DECO File No. | ||
B/M Tran==itt=1 rato unaar D**, m - | B/M Tran==itt=1 rato unaar D**, m - | ||
Approved l As Noted | Approved l As Noted 3- Er.gineering Approved A3 Noted Quality As::urance Dir. | ||
3- Er.gineering Approved A3 Noted Quality As::urance Dir. | |||
0 WJ , | 0 WJ , | ||
St ., Ows., , S;utte EN ineer W s,mp. | St ., Ows., , S;utte EN ineer W s,mp. | ||
' l 1 | ' l 1 | ||
E Prbj. Director-0peratio[s IC GA / I Project Er.gineer 4pprtFeh f _ is Noted Re,1. For Fab. Or Constr. | E Prbj. Director-0peratio[s IC GA / I Project Er.gineer 4pprtFeh f _ is Noted Re,1. For Fab. Or Constr. | ||
9WW i | |||
9WW | |||
~q | ~q | ||
h'/oF _ - | h'/oF _ - | ||
/ THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS DENT'M -m vv g Vf ,ffo dB(p | / THE DETROIT EDISON CO. ENGINEERING DEPARTMENTS DENT'M -m vv g Vf ,ffo dB(p | ||
-j 2 L 8 t $v W W 6% d ''' | -j 2 L 8 t $v W W 6% d ''' | ||
8 ' ' ' ,''# | 8 ' ' ' ,''# | ||
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e | |||
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| Line 4,195: | Line 2,607: | ||
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s N r.dy dois OA// t MAC7DP BLEM W AWRE OT ISSUED: 94 ARK NO.M/'tE#.5/43C).6rJF l CTEDB) FIELD REVtslON STATUS | |||
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SEIL J ]CL C lCL C HGR. lSO4e#/4Id-5COV REV.4 DDCunentation No. | SEIL J ]CL C lCL C HGR. lSO4e#/4Id-5COV REV.4 DDCunentation No. | ||
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* *-"a d g" _3/$%1= .. - DECO File No. | * *-"a d g" _3/$%1= .. - DECO File No. | ||
_ Transuittal Date Tendor Engineering Approved l As Noted | _ Transuittal Date Tendor Engineering Approved l As Noted 9 Ipproved As Noted | ||
9 Ipproved As Noted | |||
* Quality Assurance Dir. | * Quality Assurance Dir. | ||
J[, TV D D O N | J[, TV D D O N | ||
: I bM ., | : I bM ., | ||
M /$//eM Systes Engineer | M /$//eM Systes Engineer I | ||
IC Proj. Dirootor-Operations QA s l | |||
QA s l | |||
ProJoet angineer Apprpvand, As Noted Rel. For Fab. Or Constr. | ProJoet angineer Apprpvand, As Noted Rel. For Fab. Or Constr. | ||
75 r$5 ' | 75 r$5 ' | ||
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| Line 4,279: | Line 2,661: | ||
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| Line 4,306: | Line 2,679: | ||
3Ric mat ocafocN ocR/ocN. FIELD REVISION STATUS \ | 3Ric mat ocafocN ocR/ocN. FIELD REVISION STATUS \ | ||
f tE LD FAB ST ATus. | f tE LD FAB ST ATus. | ||
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~ | ~ | ||
| Line 4,313: | Line 2,684: | ||
Documentation 30. - | Documentation 30. - | ||
Loostion Approval F.O. | Loostion Approval F.O. | ||
_B/N 4netallattoo pgco p h , go, O O ,, | |||
_B/N 4netallattoo pgco p h , go, | |||
O O , | |||
Transatttal Date Tendor ghj Engineering | Transatttal Date Tendor ghj Engineering | ||
. .3 Approved ! Approved l as Noted le Noted _ Ouality Assurance Dir | . .3 Approved ! Approved l as Noted le Noted _ Ouality Assurance Dir i | ||
.M /14).N Systen Engioser IC l QA Proj. Director-operatione i l ProJeet nagtneer m hPr, sed _ &a poted l 5ns lRel. For Feb. Or Constr. | |||
i | |||
.M /14).N Systen Engioser | |||
IC l QA Proj. Director-operatione i l ProJeet nagtneer m hPr, sed _ &a poted l 5ns lRel. For Feb. Or Constr. | |||
-Vo l | -Vo l | ||
1 l | 1 l | ||
- S | - S | ||
History (A30-00-G-900-SA-003) | |||
History | |||
(A30-00-G-900-SA-003) | |||
A30-06-0-000-SA-001 L H. i''CXSON .''?. | A30-06-0-000-SA-001 L H. i''CXSON .''?. | ||
AUG19 bou Title ! | AUG19 bou Title ! | ||
O DESIGN SPECIFICATION 1 NUCLEAR CLASS 2 & 3 SMALL PIPING AND TNRTRUMENT AND a)NTROL PIPING AND TUBING ENRICO FERMI POWER PLANT, UNIT 2 l | |||
O DESIGN SPECIFICATION 1 | |||
NUCLEAR CLASS 2 & 3 SMALL PIPING AND TNRTRUMENT AND a)NTROL PIPING | |||
AND TUBING | |||
ENRICO FERMI POWER PLANT, UNIT 2 | |||
l | |||
l l | l l | ||
Project l Design l Spec.fication | Project l Design l Spec.fication i : | ||
i : | |||
O ; | O ; | ||
i 1 | i 1 | ||
t Edison | t Edison | ||
\ | \ | ||
l | l 3071-525 Number Rev. A | ||
3071-525 Number Rev. A | |||
. O Date MARCH 1980 l-l -_. . . _ . - . L_ l | . O Date MARCH 1980 l-l -_. . . _ . - . L_ l | ||
Specificction 3071-525 Prsp rsd by Enrico Ferni II Project Management Organization Issued: 12-10-75 n | Specificction 3071-525 Prsp rsd by Enrico Ferni II Project Management Organization Issued: 12-10-75 n | ||
%J Rev. A: 3-21-80 DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING Enrico Fermi Atomic Power Plant - Unit 2 DATE WRITTEN BY: | %J Rev. A: 3-21-80 DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING Enrico Fermi Atomic Power Plant - Unit 2 DATE WRITTEN BY: | ||
| Line 4,377: | Line 2,711: | ||
CHECKED BY: / d'' / | CHECKED BY: / d'' / | ||
G' J [H. CASIGLIA - P.E. | G' J [H. CASIGLIA - P.E. | ||
O S ERV S NG NG R | O S ERV S NG NG R dA/2/7c7 ~/M | ||
dA/2/7c7 ~/M | |||
~ | ~ | ||
R. W. ' BARF & M. G. />IGETICH PROJECT SYSTEM f/ | R. W. ' BARF & M. G. />IGETICH PROJECT SYSTEM f/ | ||
/ , | / , | ||
ENGINEER: | ENGINEER: | ||
> W 7- 6 -80 D. F. LEHNERT, P.E. | > W 7- 6 -80 D. F. LEHNERT, P.E. | ||
9 gy | 9 gy h} 7 - 3. / - 70 T . H . DICK' SON , J R . | ||
REVIEWED: | REVIEWED: | ||
PROJECT ENGINEERING ASSURANCE ffIlb A. D. SMART ' | PROJECT ENGINEERING ASSURANCE ffIlb A. D. SMART ' | ||
| Line 4,409: | Line 2,739: | ||
l | l | ||
0 0 | 0 0 | ||
DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING ENRICO FERMI ATOMIC POWER PLANT UNIT 2 l | DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING ENRICO FERMI ATOMIC POWER PLANT UNIT 2 l | ||
l l | l l | ||
l l | l l | ||
| Line 4,426: | Line 2,754: | ||
I 1 | I 1 | ||
!O 3071-525A.3 i | !O 3071-525A.3 i | ||
_ _I | _ _I | ||
Specific.itien 3071-525 Prspared by Enrico F.tr=i II Projset :tnsgsment Organiza: ion Issued: 12-10-75 Rev. A: 3-21-80 0 | Specific.itien 3071-525 Prspared by Enrico F.tr=i II Projset :tnsgsment Organiza: ion Issued: 12-10-75 Rev. A: 3-21-80 0 | ||
DCRs and DCNs Cleared By Rev. A DCR I-0002 DCN 0219 DCR P-0563 DCN 0355 DCR P-0570 DCN 0469 DCN 0534 DCN 0566 DCN 1305 Rev.A Revision A Incorporates Addendum A Note: The above DCR's and DCN's are not retroactive. | DCRs and DCNs Cleared By Rev. A DCR I-0002 DCN 0219 DCR P-0563 DCN 0355 DCR P-0570 DCN 0469 DCN 0534 DCN 0566 DCN 1305 Rev.A Revision A Incorporates Addendum A Note: The above DCR's and DCN's are not retroactive. | ||
O | O I | ||
3071-525A 4 i | |||
I | I | ||
Sp;cificcticn 3071-525 Prsp red by , | |||
Sp;cificcticn 3071-525 | |||
Prsp red by , | |||
Enrico Ferni II i ProjIct Managsment l Organization i Issued: 12-10-75 ) | Enrico Ferni II i ProjIct Managsment l Organization i Issued: 12-10-75 ) | ||
,, Rev. A: 3-21-80 i | ,, Rev. A: 3-21-80 i | ||
\# | \# | ||
DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION | DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTR.UMENT AND CONTROL PIPING AND TUBING Enrico Fermi Atomic Power Plant - Unit 2 INDEX ARTICLE CODE ARTICLE PAGE | ||
FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTR.UMENT AND CONTROL PIPING AND TUBING Enrico Fermi Atomic Power Plant - Unit 2 INDEX ARTICLE CODE ARTICLE PAGE | |||
: 1. SCOPE .................................. NA-3250 .......... 1 | : 1. SCOPE .................................. NA-3250 .......... 1 | ||
: 2. CERTIFICATION .......................... NA-3250 .......... 1 | : 2. CERTIFICATION .......................... NA-3250 .......... 1 | ||
| Line 4,465: | Line 2,785: | ||
Sargent and Lundy Engineers 55 East Monroe Street Chicago, Illinois 60603 Attention: Mr. F. P. Tsai 2 Installer and Inspector: | Sargent and Lundy Engineers 55 East Monroe Street Chicago, Illinois 60603 Attention: Mr. F. P. Tsai 2 Installer and Inspector: | ||
General Contractor, EF2 Site Note: Uncontrolled copies may be distributed as needed. | General Contractor, EF2 Site Note: Uncontrolled copies may be distributed as needed. | ||
i | i 3071-525A.6 lh | ||
3071-525A.6 lh | |||
Specificcticn 3071-525 Prspersd by Enrico Ferci II Project Management Organization Issued: 12-10-75 | Specificcticn 3071-525 Prspersd by Enrico Ferci II Project Management Organization Issued: 12-10-75 | ||
^ Rev. A: 3-21-80 U | ^ Rev. A: 3-21-80 U | ||
| Line 4,476: | Line 2,793: | ||
" Nuclear Power Plant Components," for Nuclear Class 2 and 3 Small Piping and Instrumention and Control Tubing, to be install.e'. as part of the Nuclear Steata Supply System of the Enrico Fermi A'.omic Power Plant-Unit 2. | " Nuclear Power Plant Components," for Nuclear Class 2 and 3 Small Piping and Instrumention and Control Tubing, to be install.e'. as part of the Nuclear Steata Supply System of the Enrico Fermi A'.omic Power Plant-Unit 2. | ||
: 2. CERTIFICITION The undersigned registered Professional Engineer, competent in the field of design of piping and related nuclear energy system requirements, certifies th.2t this design specification together with the referenced documents complies with the requirements of Article NA-3250 of the ASME-Code, Section III and is correct and complete with respect to functions and operating conditions as required to provide a complete basis for design, construc-tion, and certified inspection in accordance with the code. | : 2. CERTIFICITION The undersigned registered Professional Engineer, competent in the field of design of piping and related nuclear energy system requirements, certifies th.2t this design specification together with the referenced documents complies with the requirements of Article NA-3250 of the ASME-Code, Section III and is correct and complete with respect to functions and operating conditions as required to provide a complete basis for design, construc-tion, and certified inspection in accordance with the code. | ||
Juar 9. M80 DATE 0% SIGNATgkE | Juar 9. M80 DATE 0% SIGNATgkE | ||
/ | / | ||
| Line 4,487: | Line 2,803: | ||
f4 / JOSEPH H. *., 4 CASfGLIA j c$ f i ce 2iEN 3i NO. G I /N E E R j eo '+, | f4 / JOSEPH H. *., 4 CASfGLIA j c$ f i ce 2iEN 3i NO. G I /N E E R j eo '+, | ||
3071-525A.7 Q'*..20842 | 3071-525A.7 Q'*..20842 | ||
......... , y OFESs\Ot | ......... , y OFESs\Ot f | ||
f | |||
Specificcticn 3071-525 Rs,v. A: 3-21-80 Pega 2 | Specificcticn 3071-525 Rs,v. A: 3-21-80 Pega 2 | ||
| Line 4,517: | Line 2,830: | ||
l | l | ||
Specificction 3071-525 R_v. A: 3-21-80 Pcg] 4 | Specificction 3071-525 R_v. A: 3-21-80 Pcg] 4 | ||
: 4. DOCUMEfffATION (cont 'd) | : 4. DOCUMEfffATION (cont 'd) | ||
| Line 4,542: | Line 2,854: | ||
Diagram - Reactor Water Clean-up, Reactor Bldg. (RWCU) 6M721-2047 Diagram - Reactor Water Clean-up, Filter /Demin., (RCiC) 6M721-2081 Diagram - Control Rod Drive System (CRD) 6M721-2082 Standby Liquid Control System 6M721-2083 Diagram - Residual Heat Removal (R.H.R. ) Division I 6M721-2084 Diagram - Residual Heat Removal (R.H.R.) Division II 6M721-2087 P&ID - Combustible Gas Control System 6M721-2088 Diagram - Reactor Water Clean-up Phase Separators 6M721-2089 Diagram - Nuclear Boiler System 6M721-2090 Diagram - Nuclear Boiler System 6M721-2833 Diagram - Reactor Recirculation System - Nuclear Boiler System 6M721-2985 , | Diagram - Reactor Water Clean-up, Reactor Bldg. (RWCU) 6M721-2047 Diagram - Reactor Water Clean-up, Filter /Demin., (RCiC) 6M721-2081 Diagram - Control Rod Drive System (CRD) 6M721-2082 Standby Liquid Control System 6M721-2083 Diagram - Residual Heat Removal (R.H.R. ) Division I 6M721-2084 Diagram - Residual Heat Removal (R.H.R.) Division II 6M721-2087 P&ID - Combustible Gas Control System 6M721-2088 Diagram - Reactor Water Clean-up Phase Separators 6M721-2089 Diagram - Nuclear Boiler System 6M721-2090 Diagram - Nuclear Boiler System 6M721-2833 Diagram - Reactor Recirculation System - Nuclear Boiler System 6M721-2985 , | ||
Diagram - Drips and Drains from | Diagram - Drips and Drains from | ||
* team Lines and Mair Turbine 6M721-3445 Diagram - Nitrogen Inerting Diagram 6M721N-2046 P&ID Diesel Generator System - Division I-R.H.R. Complex 6M721N-2047 P&ID Diesel Generator System - Division II-R.H.R. Complex 6M721N-2048 | * team Lines and Mair Turbine 6M721-3445 Diagram - Nitrogen Inerting Diagram 6M721N-2046 P&ID Diesel Generator System - Division I-R.H.R. Complex 6M721N-2047 P&ID Diesel Generator System - Division II-R.H.R. Complex 6M721N-2048 P&ID Diesel Fuel Oil System and Lube Oil System ' | ||
P&ID Diesel Fuel Oil System and Lube Oil System ' | |||
Division I - R.H.R. Complex 6M721N-2049 P&ID Diesel Fuel Oil System and Lube Oil System I Division II - R.H.R. Complex O | Division I - R.H.R. Complex 6M721N-2049 P&ID Diesel Fuel Oil System and Lube Oil System I Division II - R.H.R. Complex O | ||
3071-525A.11 1 -. | 3071-525A.11 1 -. | ||
| Line 4,566: | Line 2,876: | ||
O to 20 psig for 100 days at 200 F. | O to 20 psig for 100 days at 200 F. | ||
O a 1 tive n" taitF - iooz Radiation = 2.6 x 107 RADS (gamma) 7.4 System Fluid Those piping systems within the scope of this specification will l contain the following fluids. , | O a 1 tive n" taitF - iooz Radiation = 2.6 x 107 RADS (gamma) 7.4 System Fluid Those piping systems within the scope of this specification will l contain the following fluids. , | ||
l | l Media: demineralized water, steam, air, and nitrogen I | ||
Media: demineralized water, steam, air, and nitrogen I | |||
Radioactivity: 0.07 micro curie /mL at zero decay time ph 0 25 C: 6.0 to 8.5 ) | Radioactivity: 0.07 micro curie /mL at zero decay time ph 0 25 C: 6.0 to 8.5 ) | ||
Suspended Solids: <10 ppb Dissolved Oxygen: <200 ppb Halogens: <1.0 ppm | Suspended Solids: <10 ppb Dissolved Oxygen: <200 ppb Halogens: <1.0 ppm O | ||
3071-525A.13 | |||
Specifiestien 3071-525 Rev. A: 3-21-80 P g2 8 | Specifiestien 3071-525 Rev. A: 3-21-80 P g2 8 | ||
| Line 4,587: | Line 2,894: | ||
otherwise specified on the Piping Isometric Drawings. | otherwise specified on the Piping Isometric Drawings. | ||
3071-525A.14 | 3071-525A.14 | ||
Specificati n 3071-525 R2v. A: 3-21-80 Pcgs 9 | |||
: 8. SYSTEM DESIGN BASIS (cont'd) 8.4 Temperature Limits The metal and fluid temperature for cleaning, flushing, and decontaminating shall be above +60 F, but not exceeding 200 F for small piping systems. | : 8. SYSTEM DESIGN BASIS (cont'd) 8.4 Temperature Limits The metal and fluid temperature for cleaning, flushing, and decontaminating shall be above +60 F, but not exceeding 200 F for small piping systems. | ||
: 9. COMPONENT DESIGN BASIS 9.1 Equipment Nozzle Interface Loads 9.1.1 In the case where piping designed in accordance with this specification is connected to process connections (nozzles on pumps, heat exchangers, etc. ) consideration as to the maximum loading imposed upon the equipment is required. The maximum loadings for piping designed in accordance with this specification are given in Table I. The system Design Specification (Reference 1) for the system in question must be consulted and a determination made that the maximum loads from the piping do not exceed the allowable nozzle loads specified for the piece of equipment under consideration. | : 9. COMPONENT DESIGN BASIS 9.1 Equipment Nozzle Interface Loads 9.1.1 In the case where piping designed in accordance with this specification is connected to process connections (nozzles on pumps, heat exchangers, etc. ) consideration as to the maximum loading imposed upon the equipment is required. The maximum loadings for piping designed in accordance with this specification are given in Table I. The system Design Specification (Reference 1) for the system in question must be consulted and a determination made that the maximum loads from the piping do not exceed the allowable nozzle loads specified for the piece of equipment under consideration. | ||
9.1.2 In case of non process line small piping connections to equipment (i.e. instrument taps, bearing cooling water connections, etc.) the maximum loads imposed on the equipment are negligible, and need not be considered. | 9.1.2 In case of non process line small piping connections to equipment (i.e. instrument taps, bearing cooling water connections, etc.) the maximum loads imposed on the equipment are negligible, and need not be considered. | ||
9.2 Major Piping Connection Interface Loads In those cases where piping designed in the field, in accordance with this specification, connects to main process piping, the maximum probable loads imposed by the small piping will be considered in the design of the main process piping, and no further consideration of these effects is required. | 9.2 Major Piping Connection Interface Loads In those cases where piping designed in the field, in accordance with this specification, connects to main process piping, the maximum probable loads imposed by the small piping will be considered in the design of the main process piping, and no further consideration of these effects is required. | ||
9.3 Equipment Nozzle and Primary Containment Penetration Thermal Deflection Process equipment nozzles which connect to piping designed under this specification are considered as anchor points and are not subject to significant thermal deflection. | 9.3 Equipment Nozzle and Primary Containment Penetration Thermal Deflection Process equipment nozzles which connect to piping designed under this specification are considered as anchor points and are not subject to significant thermal deflection. | ||
| Line 4,597: | Line 2,904: | ||
307b 525A.15 | 307b 525A.15 | ||
Specificati:n 3071-525 R v. A: 3-21-80 P:ga 10 | Specificati:n 3071-525 R v. A: 3-21-80 P:ga 10 | ||
: 9. COMPONENT DESIGN BASIS (cont'd) | : 9. COMPONENT DESIGN BASIS (cont'd) | ||
O TABLE I MAXIMUM PIPING TERMINAL LOADS Pipe Size Schedule Moment Load (ft-lb) Shear Force (lb) 1/2 40 85 72 80 100 78 160 110 99 3/4 40 147 103 80 178 128 160 209 145 1 40 277 170 80 335 207 160 396 246 1-1/4 40 489 270 80 607 329 160 713 383 1-1/ 2 40 679 342 80 160 858 1060 427 529 lll 2 40 1170 536 80 1520 683 160 2040 912 2-1/2 40 2220 903 80 2790 1120 160 3410 1360 3 40 3590 1360 80 4630 1680 160 5990 2200 4 40 6690 2250 80 8890 2920 160 12300 3950 | O TABLE I MAXIMUM PIPING TERMINAL LOADS Pipe Size Schedule Moment Load (ft-lb) Shear Force (lb) 1/2 40 85 72 80 100 78 160 110 99 3/4 40 147 103 80 178 128 160 209 145 1 40 277 170 80 335 207 160 396 246 1-1/4 40 489 270 80 607 329 160 713 383 1-1/ 2 40 679 342 80 160 858 1060 427 529 lll 2 40 1170 536 80 1520 683 160 2040 912 2-1/2 40 2220 903 80 2790 1120 160 3410 1360 3 40 3590 1360 80 4630 1680 160 5990 2200 4 40 6690 2250 80 8890 2920 160 12300 3950 1 | ||
1 3071-525A.16 l | |||
3071-525A.16 l | |||
l | l | ||
Specificction 3071-525 Rev. A 3-21-80 Page 11 | |||
: 9. COMPONENT DESIGN BASIS (cont'd) | : 9. COMPONENT DESIGN BASIS (cont'd) | ||
C) | C) | ||
| Line 4,629: | Line 2,935: | ||
3071-525A.18 | 3071-525A.18 | ||
i | i Specificcticn 3071-525 l Rsv. A: 3-21-80 l Page 13 | ||
: 9. COMPONENT DESIGN BASIS (cont'd) | : 9. COMPONENT DESIGN BASIS (cont'd) | ||
[) | [) | ||
TABLE 2 SEISMIC DISPLACEMENTS OF j RECTOR / AUXILIARY BUILDING STRUCTURAL COMPONENTS | TABLE 2 SEISMIC DISPLACEMENTS OF j RECTOR / AUXILIARY BUILDING STRUCTURAL COMPONENTS I | ||
Component Seismic Displacements (2*0.B.E.) | |||
East-West North-South Up-Down l | East-West North-South Up-Down l | ||
1st Floor Slab 0.024 in. 0.024 in. 0.0032 in. | 1st Floor Slab 0.024 in. 0.024 in. 0.0032 in. | ||
| Line 4,656: | Line 2,958: | ||
9.6.3 Anchor Design Anchors, limit stops and rigid ties shall be provided for directing expansion away from equipment, control of line g behavior during temperature changes and for protection of elements in the system against excessive expansion travel. | 9.6.3 Anchor Design Anchors, limit stops and rigid ties shall be provided for directing expansion away from equipment, control of line g behavior during temperature changes and for protection of elements in the system against excessive expansion travel. | ||
Provision must be made to assure that the anchor, limit stop or rigid tie is designed and proportioned to resist the absolute sum of the forces and/or bending moments in the pipe at either side of the anchorage location. | Provision must be made to assure that the anchor, limit stop or rigid tie is designed and proportioned to resist the absolute sum of the forces and/or bending moments in the pipe at either side of the anchorage location. | ||
9.6.4 Structural Attachment 9.6.4.1 Wherever possible component support beam attachments shall be welded to major structural | 9.6.4 Structural Attachment 9.6.4.1 Wherever possible component support beam attachments shall be welded to major structural l | ||
steel or embedded steel plates as detailed on Detroit Edison Standard Drawing SP732 (see 9.7.8 for welding requirements). | |||
l l | l l | ||
i l | i l | ||
3071-525A.20 i | 3071-525A.20 i | ||
Specificcticn 3071-525 Rsv. A: 3-21-80 Page 15 | Specificcticn 3071-525 Rsv. A: 3-21-80 Page 15 | ||
() 9. COMPONENT DESIGN BASIS (cont'd) 9.6 PIPE SUPPORTS (cont'd) 9.6.4.2 Continuous Inserts (cont'd) | () 9. COMPONENT DESIGN BASIS (cont'd) 9.6 PIPE SUPPORTS (cont'd) 9.6.4.2 Continuous Inserts (cont'd) | ||
| Line 4,692: | Line 2,991: | ||
: 9. COMPONENT DESIGN BASIS (cont'd) 9.6 Pipe Supports (cont'd) 9.6.5 Variable Spring and Mechanical Snubber Design (cont'd) | : 9. COMPONENT DESIGN BASIS (cont'd) 9.6 Pipe Supports (cont'd) 9.6.5 Variable Spring and Mechanical Snubber Design (cont'd) | ||
Variable springs should have a spring variability factor equal to or less than the values shown in the table below: | Variable springs should have a spring variability factor equal to or less than the values shown in the table below: | ||
Spring Variability Selection Chart | Spring Variability Selection Chart | ||
~ | ~ | ||
| Line 4,723: | Line 3,021: | ||
t l | t l | ||
Specificatien 3071-525 Rev. A 3-21-80 Page 19 | Specificatien 3071-525 Rev. A 3-21-80 Page 19 | ||
() 9. COMPONENT DESIGN BASIS (Cont'd) 9.11 Dead Weight Analysis of Piping (Cont'd) | () 9. COMPONENT DESIGN BASIS (Cont'd) 9.11 Dead Weight Analysis of Piping (Cont'd) | ||
| Line 4,759: | Line 3,056: | ||
3071-525A.26 O | 3071-525A.26 O | ||
i i | i i | ||
Specificatien 3071-525 Rav. A 3-21-80 Pega 21 | |||
: 11. CLASSIFICATION OF CONDITIONS (cont'd) | : 11. CLASSIFICATION OF CONDITIONS (cont'd) | ||
O 11.2 Earthquake Loadings (cont'd) | O 11.2 Earthquake Loadings (cont'd) | ||
| Line 4,771: | Line 3,069: | ||
Hydronatic testing shall meet the requirements of ASME III Subsection NC-6200. Valve bodies shall be in accordance with ANSI B16.5 or MSS SP-66 for Class 2 and 3 valves. | Hydronatic testing shall meet the requirements of ASME III Subsection NC-6200. Valve bodies shall be in accordance with ANSI B16.5 or MSS SP-66 for Class 2 and 3 valves. | ||
The test pressures and temperatures shall be determined from the applicable system Design Specification (Reference 1). | The test pressures and temperatures shall be determined from the applicable system Design Specification (Reference 1). | ||
Prior to hydrostatic test, all system valves with leak off connections shall have the connections open-ended. Exercisable O 3071-525A.27 | Prior to hydrostatic test, all system valves with leak off connections shall have the connections open-ended. Exercisable O 3071-525A.27 l | ||
l | |||
Specificcticn 3071-525 Ra y. A 3-21-80 Pcg2 22 | Specificcticn 3071-525 Ra y. A 3-21-80 Pcg2 22 | ||
| Line 4,788: | Line 3,084: | ||
3071-525A.28 | 3071-525A.28 | ||
~ | ~ | ||
Specificati:n 3071-525 Rev. At 3-21-80 Page 23 | Specificati:n 3071-525 Rev. At 3-21-80 Page 23 | ||
| Line 4,804: | Line 3,099: | ||
\/ | \/ | ||
3071-525A.29 | 3071-525A.29 | ||
Specificsticn 3071-525 Ray. A: 3-21-80 Pego 24 | Specificsticn 3071-525 Ray. A: 3-21-80 Pego 24 | ||
: 14. REFERENCES (cont'd) | : 14. REFERENCES (cont'd) | ||
| Line 4,819: | Line 3,112: | ||
O 3071-525A.3C | O 3071-525A.3C | ||
O I | O I | ||
APPENDIX A ANSI Primary Pressure Rating, Materials and Dimensions for Nuclear Piping O | APPENDIX A ANSI Primary Pressure Rating, Materials and Dimensions for Nuclear Piping O | ||
O 3071-525A.31 | O 3071-525A.31 | ||
l | l | ||
. Al i | . Al i TABLE I | ||
() CARBON STEEL PIPING SYSTEMS ANSI ASTM ITEM PRESSURE RATING SIZE RATING TYPE SPECIFICATION Pipe 900 lbs 3" and Smaller Schedule 160 Seamless A106 Gr B 4" Schedule 120 Seamless A106 Cr B 600 lbs 3" and Smaller Schedule 160 Seamless A106 Cr B 4" Schedule 80 Seamless A106 Gr B 300 lbs 2" and Smaller Schedule 80 Seamless A106 Gr B 2-1/2" - 4" Schedule 40 Seamless A106 Cr B 150 lbs 2" and Smaller Schedule 80 Seamless A106 Gr B 2-1/2" - 4" Schedule 40 Seamless A106 Gr B Fittings 900 lbs 2" and Smaller 6000 lbs S.W. A234 Gr WPB - | |||
TABLE I | |||
() CARBON STEEL PIPING SYSTEMS ANSI ASTM ITEM PRESSURE RATING SIZE RATING TYPE SPECIFICATION Pipe 900 lbs 3" and Smaller Schedule 160 Seamless A106 Gr B 4" Schedule 120 Seamless A106 Cr B 600 lbs 3" and Smaller Schedule 160 Seamless A106 Cr B | |||
4" Schedule 80 Seamless A106 Gr B 300 lbs 2" and Smaller Schedule 80 Seamless A106 Gr B 2-1/2" - 4" Schedule 40 Seamless A106 Cr B 150 lbs 2" and Smaller Schedule 80 Seamless A106 Gr B 2-1/2" - 4" Schedule 40 Seamless A106 Gr B Fittings 900 lbs 2" and Smaller 6000 lbs S.W. A234 Gr WPB - | |||
2-1/2" - 4" Match Pipe Wall B.W. A234 Gr WPB | 2-1/2" - 4" Match Pipe Wall B.W. A234 Gr WPB | ||
( }) 600 lbs 2" and Smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 3" Schedule 160 B.W. A234 Gr WPB 4" Schedule 80 B.W. A234 Gr WPB 300 lbs 2" and smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 4" Schedule 40 B.W. A234 Gr WPB 150 lbs 2" and Smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 4" Schedule 40 B.W. A234 Gr WPB Valves 900 lbs 2" and Smaller 1500 lbs S.W. A105 2-1/2" - 4" 900 lbs B.W. A216 Gr B 600 lbs 2" and Smaller 600 lbs S.W. A105 600 lbs B.W. A216 Gr B 300 lbs 2" and Smaller 600 lbs S.W. A105 2-1/2" - 4" 300 lbs B.W. A216 Gr B 150 lbs 2" and smaller 600 lbs S.W. A105 2-1/2" - 4" 150 lbs B.W. A216 Gr B | ( }) 600 lbs 2" and Smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 3" Schedule 160 B.W. A234 Gr WPB 4" Schedule 80 B.W. A234 Gr WPB 300 lbs 2" and smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 4" Schedule 40 B.W. A234 Gr WPB 150 lbs 2" and Smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 4" Schedule 40 B.W. A234 Gr WPB Valves 900 lbs 2" and Smaller 1500 lbs S.W. A105 2-1/2" - 4" 900 lbs B.W. A216 Gr B 600 lbs 2" and Smaller 600 lbs S.W. A105 600 lbs B.W. A216 Gr B 300 lbs 2" and Smaller 600 lbs S.W. A105 2-1/2" - 4" 300 lbs B.W. A216 Gr B 150 lbs 2" and smaller 600 lbs S.W. A105 2-1/2" - 4" 150 lbs B.W. A216 Gr B | ||
| Line 4,842: | Line 3,128: | ||
Nuts All Caskets All Flexitallic Style CG 3071-525A.33 9 | Nuts All Caskets All Flexitallic Style CG 3071-525A.33 9 | ||
A3 TABLE 2 STAINLESS STEEL PIPING SYSTEMS | A3 TABLE 2 STAINLESS STEEL PIPING SYSTEMS | ||
~ | ~ | ||
| Line 4,852: | Line 3,137: | ||
Nuts All Gaskets All Flexitallic Style CG 3071-525A.35 i | Nuts All Gaskets All Flexitallic Style CG 3071-525A.35 i | ||
4 III | 4 III | ||
. = - . _. ,_ _. . - . . - _ _ . _ _ _ _ _ _ _ - _ _ _ | . = - . _. ,_ _. . - . . - _ _ . _ _ _ _ _ _ _ - _ _ _ | ||
m -m-o-o m-si-w3 . | m -m-o-o m-si-w3 . | ||
Title DERGENCY EQUIPMDIT COOLING WATER (EEI;W) SYSTEM | Title DERGENCY EQUIPMDIT COOLING WATER (EEI;W) SYSTEM ENRICO FERMI POWER PT ANT; MTT 2 Project Design Specification O | ||
Deholt Edison 3071-512 Including Addendum A Number DECDGER 1972 DECEMBER 1974 Date | |||
ENRICO FERMI POWER PT ANT; MTT 2 | |||
Project Design Specification O | |||
Deholt Edison | |||
3071-512 Including Addendum A Number | |||
DECDGER 1972 DECEMBER 1974 Date | |||
Specifiestion 3071-512 DETROIT EDISON Prripared By SPECIFICATION Enrico Fermi II ADDENDUM "A" 3*" "*9 " " | Specifiestion 3071-512 DETROIT EDISON Prripared By SPECIFICATION Enrico Fermi II ADDENDUM "A" 3*" "*9 " " | ||
Organization O' DESIGN SPECIFICATION nue : 11-15-74 FOR EMERGENCY EQUIPMENT COOLING WATER SYSTEM Enrico Fermi Atomic Power Plant Unit #2 i | Organization O' DESIGN SPECIFICATION nue : 11-15-74 FOR EMERGENCY EQUIPMENT COOLING WATER SYSTEM Enrico Fermi Atomic Power Plant Unit #2 i | ||
APPROVAL SHEET DATE | APPROVAL SHEET DATE | ||
^ | ^ | ||
j | j | ||
| Line 4,885: | Line 3,151: | ||
~ | ~ | ||
WRITTEN BY: ( . M 4 7U.O D. LEHNERT CHECKED BY: | WRITTEN BY: ( . M 4 7U.O D. LEHNERT CHECKED BY: | ||
. (v / 2 ' / { ! 7 8-/ | . (v / 2 ' / { ! 7 8-/ | ||
h F.El GREGOR -P.E. | h F.El GREGOR -P.E. | ||
| Line 4,891: | Line 3,156: | ||
,, LA-g EcJ / /2-G 74-v M. S IGET ICt+' | ,, LA-g EcJ / /2-G 74-v M. S IGET ICt+' | ||
I APPROVED: | I APPROVED: | ||
-[./ / | -[./ / | ||
ASSIST. PROJECT , | |||
ENGINEER, SYSTEMS f g //r /;.%f W.F. COLBERT-P.E. / / | ENGINEER, SYSTEMS f g //r /;.%f W.F. COLBERT-P.E. / / | ||
APPROVED: | APPROVED: | ||
EN R 2 , u /s/,2/7/ | EN R 2 , u /s/,2/7/ | ||
E.G.(gIPER-P.E. | E.G.(gIPER-P.E. | ||
O | O | ||
Specification 3071-512 Prepared By Enrico Fermi II Project Management Organization O Issued: 11-15-74 Addendum "A" P44 0-000 sA,002/ | Specification 3071-512 Prepared By Enrico Fermi II Project Management Organization O Issued: 11-15-74 Addendum "A" P44 0-000 sA,002/ | ||
DETROIT EDISON DESIGN SPECIFICATION FOR ENRICO FERMI ATOMIC POWER PLANT UNIT NO. 2 ADDENDUM "A" 0F DESIGN SPECIFICATION FOR EMERGENCY EQU1PMENT COOLING WATER SYSTEM DESIGN SPECIFICATION NO. 3071-512 o . | DETROIT EDISON DESIGN SPECIFICATION FOR ENRICO FERMI ATOMIC POWER PLANT UNIT NO. 2 ADDENDUM "A" 0F DESIGN SPECIFICATION FOR EMERGENCY EQU1PMENT COOLING WATER SYSTEM DESIGN SPECIFICATION NO. 3071-512 o . | ||
~ | ~ | ||
Specification 3071-512 Issurd: 11-15-74 O oeTao'T co'So" DESIGN SPECIFICATION ADDENDUM "A" EMERGENCY EQUIPMENT COOLING WATER SYSTEM | Specification 3071-512 Issurd: 11-15-74 O oeTao'T co'So" DESIGN SPECIFICATION ADDENDUM "A" EMERGENCY EQUIPMENT COOLING WATER SYSTEM | ||
: 1. On Page 2, delete Article 3. (h), | : 1. On Page 2, delete Article 3. (h), | ||
| Line 4,925: | Line 3,179: | ||
(4) - (5) - sPece cooiers: (i) aesideei seet aemevei (1) Core Spray and Reactor Core Isolation Cooling (1) Emergency Equipment Cooling Water Room (1) Hydrogen Control System or (1) High Pressure Cooling Injection (1) Core Spray (1) Residual Heat Removal (1) Emergency Equipment Cooling Water Room (1) Hydrogen Control System (1) Air Conditioning Equipment Unit for the Control Room (2) Switch Gear Room Space Coolers (1) Standby Control Air System (1) Standby Gas Treatment Room Space Cooler (7) Drywell Coolers. | (4) - (5) - sPece cooiers: (i) aesideei seet aemevei (1) Core Spray and Reactor Core Isolation Cooling (1) Emergency Equipment Cooling Water Room (1) Hydrogen Control System or (1) High Pressure Cooling Injection (1) Core Spray (1) Residual Heat Removal (1) Emergency Equipment Cooling Water Room (1) Hydrogen Control System (1) Air Conditioning Equipment Unit for the Control Room (2) Switch Gear Room Space Coolers (1) Standby Control Air System (1) Standby Gas Treatment Room Space Cooler (7) Drywell Coolers. | ||
O | O | ||
. Specification 3071-512 Issurd: 11-15-74 Addendum "A" Page 2 O 5- o# e 9 4. ^rtic' 5 r vis 4th P r ar P8 t= < d: | . Specification 3071-512 Issurd: 11-15-74 Addendum "A" Page 2 O 5- o# e 9 4. ^rtic' 5 r vis 4th P r ar P8 t= < d: | ||
The EECW system, supplying the above equipment, maintains a condensate de-sign temperature of 95 F by heat rejection loop heat exchangers, which are cooled by Emergency Equipment Service Water (see Design Specification 3071-517). | The EECW system, supplying the above equipment, maintains a condensate de-sign temperature of 95 F by heat rejection loop heat exchangers, which are cooled by Emergency Equipment Service Water (see Design Specification 3071-517). | ||
| Line 4,947: | Line 3,198: | ||
Piping of above category, which connects to EECW System piping inside the primary containment up to and including the first source valva is classi-fled as Class 2. Piping beyond the source valve up to and including the ter-minal or instrument is classified as Class 3. This piping shall be design and stress analyzed in accordance with Edison Design Specification 3071- 525 O | Piping of above category, which connects to EECW System piping inside the primary containment up to and including the first source valva is classi-fled as Class 2. Piping beyond the source valve up to and including the ter-minal or instrument is classified as Class 3. This piping shall be design and stress analyzed in accordance with Edison Design Specification 3071- 525 O | ||
. Sp;cification 3071-512 Issurd: 11-15-74 Addendum "A" Page 3 O II. On Page 8, revise Article 9.4 to read: | . Sp;cification 3071-512 Issurd: 11-15-74 Addendum "A" Page 3 O II. On Page 8, revise Article 9.4 to read: | ||
The pumps, heat exchangers and make-up tanks are classified as Class 3 components. Piping connections to these components shall be designed to limit reactions to the following limits: | The pumps, heat exchangers and make-up tanks are classified as Class 3 components. Piping connections to these components shall be designed to limit reactions to the following limits: | ||
| Line 4,957: | Line 3,206: | ||
No = the allowable value of M; when all forces are zero. | No = the allowable value of M; when all forces are zero. | ||
5 The values of Fo and No are given below: | 5 The values of Fo and No are given below: | ||
l OBE DBE Fo Ho Fo Mo Lbs. Ft-Lbs. Lbs Ft-Lbs Combined Resultant i168 2340 1500 3000 Suction Nozzle 875 , | l OBE DBE Fo Ho Fo Mo Lbs. Ft-Lbs. Lbs Ft-Lbs Combined Resultant i168 2340 1500 3000 Suction Nozzle 875 , | ||
1250 1125 , 1575 | 1250 1125 , 1575 Discharse Nozzle 1000 l 2000 l 1275 1 2550 (b) For the heat exchanger, the allowabie nozzle loads are given in the | ||
Discharse Nozzle 1000 l 2000 l 1275 1 2550 (b) For the heat exchanger, the allowabie nozzle loads are given in the | |||
'ollowing tables: | 'ollowing tables: | ||
NORMAL & UPSET CONDITION (OBE) | NORMAL & UPSET CONDITION (OBE) | ||
Service Water Service Water EECW EECW Inlet Outlet Inlet Outlet Div. I Div. II Div. I Div. II Div. I Div. II Div. I Div. II Fx 680 260 1600 1500 700 700 680 500 hrz 3800 2200 2400 600 175 770 1100 1300 1600 700 1000 400 550 200 400 200 Mx 3950 3400 2500 5500 3200 1300 700 500 My 2100 600 1100 6900 1000 800 1750 1000 Hz 2200 200 3850 7300 3500 3200 1500 400 | Service Water Service Water EECW EECW Inlet Outlet Inlet Outlet Div. I Div. II Div. I Div. II Div. I Div. II Div. I Div. II Fx 680 260 1600 1500 700 700 680 500 hrz 3800 2200 2400 600 175 770 1100 1300 1600 700 1000 400 550 200 400 200 Mx 3950 3400 2500 5500 3200 1300 700 500 My 2100 600 1100 6900 1000 800 1750 1000 Hz 2200 200 3850 7300 3500 3200 1500 400 | ||
Sp;cification 3071-512 Issu:d: 11-15-74 Addendum "A" Page 4 | |||
Addendum "A" Page 4 | |||
) EMERGENCY C0!4DITION (DBE) | ) EMERGENCY C0!4DITION (DBE) | ||
Service Water Service Water EECW EECW Inlet Outlet Inlet Outlet Div. I Div. II Div. I Div. II Div. I Div. II Div. I Div. II i | Service Water Service Water EECW EECW Inlet Outlet Inlet Outlet Div. I Div. II Div. I Div. II Div. I Div. II Div. I Div. II i | ||
| Line 4,991: | Line 3,233: | ||
O | O | ||
1 , | 1 , | ||
Sp;ci ficat ion 3071-512 Issued: 11-15-74 Addandum "A" Page 5 | |||
Sp;ci ficat ion 3071-512 | |||
: 14. On Page 12, Article 9.7, revise 4th paragraph to read: | : 14. On Page 12, Article 9.7, revise 4th paragraph to read: | ||
Class 2 and Class 3 piping 4" NPS and smaller shall be analyzed per Edison Speci ficat ion 3071- 525. ; | Class 2 and Class 3 piping 4" NPS and smaller shall be analyzed per Edison Speci ficat ion 3071- 525. ; | ||
| Line 5,013: | Line 3,250: | ||
For the Standby Control Compressor, (First Floor), | For the Standby Control Compressor, (First Floor), | ||
O Horizontal Displacement, OBE = .012 in. | O Horizontal Displacement, OBE = .012 in. | ||
DBE = .0172 in. | DBE = .0172 in. | ||
Vertical Displacement, OBE = .00156 In. | Vertical Displacement, OBE = .00156 In. | ||
| Line 5,029: | Line 3,265: | ||
Vertical Displacement, OBE = .00467 in. | Vertical Displacement, OBE = .00467 in. | ||
DBE = .00684 in. | DBE = .00684 in. | ||
O | O I | ||
I | |||
l i | l i | ||
.' l t' Spscificaticn 0071-512 Issurd: 11-15-74 l Addendum "A" | .' l t' Spscificaticn 0071-512 Issurd: 11-15-74 l Addendum "A" | ||
. Page 6 O 17. On Page 14, Article 9.9, revise the seismic displacements to read: (con t inued) | . Page 6 O 17. On Page 14, Article 9.9, revise the seismic displacements to read: (con t inued) | ||
| Line 5,047: | Line 3,278: | ||
i | i | ||
: 19. On Page 16, Article 11.1, Cooling Water Supply Line Temperature shall be 850F. j | : 19. On Page 16, Article 11.1, Cooling Water Supply Line Temperature shall be 850F. j | ||
: 20. On Page 17, Article 13 (1), revise to read: l Seismic Analysis of the Enrico Fermi #2 Reactor Buildirg, Sargent and Lundy Report #5L-2682. | : 20. On Page 17, Article 13 (1), revise to read: l Seismic Analysis of the Enrico Fermi #2 Reactor Buildirg, Sargent and Lundy Report #5L-2682. | ||
: 21. On Page 17, Article 13, add the following: | : 21. On Page 17, Article 13, add the following: | ||
| Line 5,054: | Line 3,284: | ||
4 (16) Certified Seismic Analysis Report of Crane Deming Horizontal Split Case Pump, Figure 5063 for Emergency Equipment Cooling Water Pump. | 4 (16) Certified Seismic Analysis Report of Crane Deming Horizontal Split Case Pump, Figure 5063 for Emergency Equipment Cooling Water Pump. | ||
O V | O V | ||
. O, s w | . O, s w | ||
J 5,,y,,, | J 5,,y,,, | ||
a mo 2o | a mo 2o | ||
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w/ | w/ | ||
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m .' | m .' | ||
c , | c , | ||
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As_.ie.st.rictqdaby__ lines (;l) | As_.ie.st.rictqdaby__ lines (;l) | ||
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| Line 5,152: | Line 3,339: | ||
:I- \:, | :I- \:, | ||
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\. ; ; allowable | \. ; ; allowable | ||
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j~f ; S - | j~f ; S - | ||
zonep \( Q - | zonep \( Q - | ||
t M | t M | ||
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1 .. | 1 .. | ||
| Line 5,176: | Line 3,355: | ||
. . .4. .. | . . .4. .. | ||
V | V | ||
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l' L . | l' L . | ||
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! 2.'.- . 2 d. ._. b. 2 4. . -1d \ . | ! 2.'.- . 2 d. ._. b. 2 4. . -1d \ . | ||
.8. .\.;: L. ' | .8. .\.;: L. ' | ||
| Line 5,191: | Line 3,367: | ||
:! 4 .' 28 . 3:! c:== | :! 4 .' 28 . 3:! c:== | ||
2N..,h....--.I.d 7.[20. : W | 2N..,h....--.I.d 7.[20. : W | ||
. . i .... 1 | . . i .... 1 i ! l LL_ \ ~!! Y L\ | ||
i ! l LL_ \ ~!! Y L\ | |||
1 | 1 | ||
@\ U! $ $ | @\ U! $ $ | ||
N \......'Y.g ~i ' | N \......'Y.g ~i ' | ||
| Line 5,203: | Line 3,375: | ||
l l ', | l l ', | ||
-( 10+3) m. l.-l.bs | -( 10+3) m. l.-l.bs | ||
" i | " i i ., | ||
i ., | |||
: c. -/-....! . | : c. -/-....! . | ||
.M g | .M g | ||
, m f - , | , m f - , | ||
i l . _ . _ ._ }' | i l . _ . _ ._ }' | ||
, l | , l | ||
.. y,. | .. y,. | ||
.i | .i | ||
:I 2. | :I 2. | ||
t | t | ||
. - ~./. | . - ~./. | ||
h ---- - | h ---- - | ||
'";.l!!" | '";.l!!" | ||
; i ', 11 .. .. | ; i ', 11 .. .. | ||
**; j | **; j t- ! j. I'.. ..... i * | ||
t- ! j. I'.. ..... i * | |||
/. . t q' . ._ . ;. j ... | /. . t q' . ._ . ;. j ... | ||
l' | l' | ||
.t .! .! ,.{ '. g. g | .t .! .! ,.{ '. g. g 1' . _ : . | ||
1' . _ : . | |||
_.1._. . ... .. ._ .~ . ..,.t. . .. | _.1._. . ... .. ._ .~ . ..,.t. . .. | ||
'' ""3 I | '' ""3 I | ||
_' 4:. l ', -":.l - :1!- l1; t-' | _' 4:. l ', -":.l - :1!- l1; t-' | ||
i 1 - | i 1 - | ||
:_ ' i. | :_ ' i. | ||
_g3 " | _g3 " | ||
p, __ _ | p, __ _ | ||
i | i o : t-i ! | ||
o : t-i ! | |||
:: : ... ; - | :: : ... ; - | ||
. _ .: . . .; . .; . ._. l ._ | . _ .: . . .; . .; . ._. l ._ | ||
: _.; . u. '. c. .u_. ..{. .;. | : _.; . u. '. c. .u_. ..{. .;. | ||
g g; p .p: 4 fi f. ;:. | g g; p .p: 4 fi f. ;:. | ||
.a . , | .a . , | ||
i ! Ficjure 7. i. Allowable;!!c zz- le Loadd.:P add M' . h in. 'li 4 iii! 8! , m u m j | i ! Ficjure 7. i. Allowable;!!c zz- le Loadd.:P add M' . h in. 'li 4 iii! 8! , m u m j | ||
, - - -- *- '''l . .. - .-- 1 .i ,. , I j... | |||
, - - -- *- '''l . .. - .-- 1 .i ,. , I | |||
j... | |||
't. .. | 't. .. | ||
,l... | ,l... | ||
..g l...a > | |||
..g | |||
l...a > | |||
.g. . | .g. . | ||
[a. .j'-*i i . , | [a. .j'-*i i . , | ||
., ., . i, . | ., ., . i, . | ||
.l . ..... .I... | .l . ..... .I... | ||
i.. | i.. | ||
8 u ! ._. .... ,.1..n .u. | 8 u ! ._. .... ,.1..n .u. | ||
.u L' L . ' 2.. u .. . u.: .1- Li' . ;. . | .u L' L . ' 2.. u .. . u.: .1- Li' . ;. . | ||
.n e"n L.. . . - . . . .. .... .... _. | .n e"n L.. . . - . . . .. .... .... _. | ||
' . . . . - .~ | ' . . . . - .~ | ||
; ; i | ; ; i j . 'p | ||
j . 'p | |||
: a . | : a . | ||
e lg.f. @i g. | e lg.f. @i g. | ||
p'fg_1- | p'fg_1- | ||
: ; | : ; | ||
2 1 | 2 1 | ||
y. | |||
hi- !I' $,. | hi- !I' $,. | ||
' [- Ii! ---?a | ' [- Ii! ---?a h. | ||
! . f l . . | ! . f l . . | ||
l ::" . -- | l ::" . -- | ||
-Y | -Y | ||
:1- ~ .,i t'.- ? | :1- ~ .,i t'.- ? | ||
~ ~ | ~ ~ | ||
.i | .i | ||
-t | -t | ||
"* - ~ ~ ~ -- | "* - ~ ~ ~ -- | ||
'g. ' - | 'g. ' - | ||
; | ; | ||
l l ,t ' j '. | l l ,t ' j '. | ||
. ..'. . j :. ! i'.j . '.t | . ..'. . j :. ! i'.j . '.t 1: | ||
o, l 4 | |||
1: | |||
o, | |||
l 4 | |||
;. - i | ;. - i | ||
, t ? | , t ? | ||
| Line 5,357: | Line 3,447: | ||
,. !!' , i l-* | ,. !!' , i l-* | ||
u, h.. | u, h.. | ||
te | te h. | ||
h. | |||
1 | 1 | ||
-- .i- . | -- .i- . | ||
N u'. | N u'. | ||
hj EI- yl + .i. . I a: .- | hj EI- yl + .i. . I a: .- | ||
- - - + | - - - + | ||
+---$ | +---$ | ||
e i if v. | |||
e i | |||
if v. | |||
, . + | , . + | ||
g' I 1 | g' I 1 | ||
_,,, 4 pm' +4 ... . . . .. | |||
_,,, 4 | |||
pm' +4 ... . . . .. | |||
' I I | ' I I | ||
i.i 1 | i.i 1 | ||
:l: | :l: | ||
t i' | t i' | ||
[I' l ! | [I' l ! | ||
l_ | l_ | ||
l l 6 | l l 6 | ||
. . _ . ri . . 1_ | . . _ . ri . . 1_ | ||
e '5 i | e '5 i | ||
m ,.,, g,,,, | m ,.,, g,,,, | ||
| Line 5,408: | Line 3,472: | ||
, /G i 15 Sowares so the siwh ,7 | , /G i 15 Sowares so the siwh ,7 | ||
[ | [ | ||
i v :v v | i v :v v l | ||
l | |||
i i .n. .:. . c : | i i .n. .:. . c : | ||
m , in ;pj ;. . | m , in ;pj ;. . | ||
..a | ..a | ||
'.u,.; ;h' - j; i. | '.u,.; ;h' - j; i. | ||
. . . . . :.. . .. .- .; | . . . . . :.. . .. .- .; | ||
. .. f _ . ... ;. . . ;;. !1d .. .; . ..; ;. Lh. p.... L;; . ; | . .. f _ . ... ;. . . ;;. !1d .. .; . ..; ;. Lh. p.... L;; . ; | ||
| Line 5,426: | Line 3,484: | ||
. ' . ' ;';a l . .-. | . ' . ' ;';a l . .-. | ||
: i. .. .. , ... | : i. .. .. , ... | ||
.it j ., | .it j ., | ||
gp , | gp , | ||
I" p ".,j 'p | I" p ".,j 'p | ||
. , ,;. | . , ,;. | ||
,. . t. ,, | ,. . t. ,, | ||
,'As-fcstricted-try-1-ine sM-5-)-.-e dd -N)l | ,'As-fcstricted-try-1-ine sM-5-)-.-e dd -N)l | ||
::/ | ::/ | ||
..! . for (PI p of 'Iable IV ! j. . ..I..' -. | ..! . for (PI p of 'Iable IV ! j. . ..I..' -. | ||
...J !. . | ...J !. . | ||
i, .. | i, .. | ||
:F | :F l | ||
,, 7 7 j i . I - | |||
l | |||
,, 7 7 | |||
j i . I - | |||
., P 1 | ., P 1 | ||
' [ | ' [ | ||
I | I | ||
-p' ri .. " h, ',, | -p' ri .. " h, ',, | ||
{ i i | { i i | ||
..\ %. ..o,. | ..\ %. ..o,. | ||
; , | ; , | ||
3.... .. j .i.. .. ,i . . . . . .e. . . . .. | 3.... .. j .i.. .. ,i . . . . . .e. . . . .. | ||
. .. . ; . . . . . an , u.. 1 . | . .. . ; . . . . . an , u.. 1 . | ||
.y i | .y i | ||
. "ul- - e | . "ul- - e t , 1 , ; | ||
t , 1 , ; | |||
o, ., ,' | o, ., ,' | ||
. l l. , , , . | . l l. , , , . | ||
' g. c c | ' g. c c | ||
, ; ; | , ; ; | ||
-- ;r , - | -- ;r , - | ||
. .t ,, | . .t ,, | ||
| Line 5,495: | Line 3,519: | ||
l .lc=D | l .lc=D | ||
:7 | :7 | ||
! l , i CO1'f ' | ! l , i CO1'f ' | ||
_.i 1 | _.i 1 | ||
| Line 5,506: | Line 3,528: | ||
.g. | .g. | ||
(.. i . | (.. i . | ||
. . .. . . t . .. . ._.. _.. | . . .. . . t . .. . ._.. _.. | ||
h ,i E,,d-o . ' | h ,i E,,d-o . ' | ||
\' | \' | ||
.._.'_ 'tk\. | .._.'_ 'tk\. | ||
\._. ( \ | \._. ( \ | ||
~:- 7 | ~:- 7 | ||
, al:.owable z o n.,_e._. i . | , al:.owable z o n.,_e._. i . | ||
r i Ni . | r i Ni . | ||
\ i . | \ i . | ||
| Line 5,527: | Line 3,540: | ||
\ | \ | ||
i, . i..1 , | i, . i..1 , | ||
__1_- . | __1_- . | ||
-l | -l | ||
. . . . . .__.l - | . . . . . .__.l - | ||
\,- \. | \,- \. | ||
11n,.J. i | 11n,.J. i | ||
. \_.. n .. .u t . 2. .. . .m . . . . . . . | . \_.. n .. .u t . 2. .. . .m . . . . . . . | ||
. i \ s . | . i \ s . | ||
\ , - - | \ , - - | ||
L' ._ ._1,\. ', | L' ._ ._1,\. ', | ||
,V 1 | |||
,V | |||
1 | |||
- 1. w | - 1. w | ||
\: l6 | \: l6 | ||
- - N. \ h: . | - - N. \ h: . | ||
7bN l !.-16..j.-14...12.! -10 b., -6.b.'.. 4\ .:.:.. 2.i 2 ). I. 4 6 .. | |||
7bN | |||
l !.-16..j.-14...12.! -10 b., -6.b.'.. 4\ .:.:.. 2.i | |||
2 ). I. 4 | |||
6 .. | |||
2 | 2 | ||
.1 0 .12. .' .1 4 16 @#g IITU=-ID' | .1 0 .12. .' .1 4 16 @#g IITU=-ID' | ||
; | ; | ||
..j . | ..j . | ||
i | i | ||
[ | [ | ||
~. | ~. | ||
j | j | ||
;. | ;. | ||
.1 .s... | .1 .s... | ||
1. | 1. | ||
L. | L. | ||
. J ., . ., . | . J ., . ., . | ||
( '_i~ ' | ( '_i~ ' | ||
fl | fl | ||
.. .. . . . . . .. . .-. . .;. . | .. .. . . . . . .. . .-. . .;. . | ||
.p: l:' | .p: l:' | ||
. . ,: ,. . , >+ | . . ,: ,. . , >+ | ||
; ; l 1 .- r N r + | ; ; l 1 .- r N r + | ||
| Line 5,598: | Line 3,576: | ||
:. P ( -- /.. Its ,.:i: : 11; .: ;;a ' | :. P ( -- /.. Its ,.:i: : 11; .: ;;a ' | ||
l:. ., : I't f[.'' '. 1 | l:. ., : I't f[.'' '. 1 | ||
'I':. ,!!:. | 'I':. ,!!:. | ||
L' _l' . ..N :M | L' _l' . ..N :M | ||
_. 1. ... l .' . .1- .... t , | _. 1. ... l .' . .1- .... t , | ||
.;gl:l: A.! l' .l . .: {. .' | .;gl:l: A.! l' .l . .: {. .' | ||
. .. . .l. .; ! . | . .. . .l. .; ! . | ||
.9 | .9 | ||
.;.. i.... .... . | .;.. i.... .... . | ||
_ . ... . .. .. . .-. . . . - . .J. | _ . ... . .. .. . .-. . . . - . .J. | ||
I;:;!. | I;:;!. | ||
:l * - | :l * - | ||
r .l: N. /. 1 | r .l: N. /. 1 | ||
' t.. ; t. l' ' l s '. ;: . | ' t.. ; t. l' ' l s '. ;: . | ||
, i 1 . . I .: 14 , | , i 1 . . I .: 14 , | ||
,3 | ,3 | ||
.. .,, .; | .. .,, .; | ||
n' | n' I 3 ' | ||
I 3 ' | |||
t , | t , | ||
,.e . ? ..,1 a; . Lc | ,.e . ? ..,1 a; . Lc | ||
. t li..;L:. i:, !. '; | . t li..;L:. i:, !. '; | ||
._L ;_. . . . . . . . . .. . . ... .n. .. . i .; . . . ._; ; ; .:.. . . . . .. .- . . ' d .! *! 4 .l. .. .1 .L - | ._L ;_. . . . . . . . . .. . . ... .n. .. . i .; . . . ._; ; ; .:.. . . . . .. .- . . ' d .! *! 4 .l. .. .1 .L - | ||
.I.. | .I.. | ||
. ::. : t. .t'!. .. .. | . ::. : t. .t'!. .. .. | ||
:r , i. . W | :r , i. . W | ||
: l l . . i ..: i , i:. p !! b;,l ip it: j!p i; : .: ; .;, o | : l l . . i ..: i , i:. p !! b;,l ip it: j!p i; : .: ; .;, o t- | ||
t- | |||
*4' 'I , , .., - . . .. | *4' 'I , , .., - . . .. | ||
I. "2 | I. "2 | ||
! j: ' | ! j: ' | ||
l lf.~L..j! 1.n l'i: | |||
l lf.~L..j! 1.n | |||
l'i: | |||
.l. 'l . . | .l. 'l . . | ||
. ' . ;;.! | . ' . ;;.! | ||
l | l | ||
. .;;. .'''' Ll.:! | . .;;. .'''' Ll.:! | ||
l''- *" | l''- *" | ||
:. :n.. . n. ..t} -. 4.1' p.: :.; g p- lp ; ;; ' ' ' | :. :n.. . n. ..t} -. 4.1' p.: :.; g p- lp ; ;; ' ' ' | ||
in. l!!!' r L.* | in. l!!!' r L.* | ||
. !.. _ ..: . n.; ..: . | . !.. _ ..: . n.; ..: . | ||
:j: l:". l .. .: | :j: l:". l .. .: | ||
; . ,. ; '2: | ; . ,. ; '2: | ||
pr !!! i;. | pr !!! i;. | ||
t- | t- | ||
. 11 : ;, , | . 11 : ;, , | ||
(If | (If | ||
'. a.' | '. a.' | ||
l :,. !: I; .;ii .!. I.I. . l''' ..I; ' | l :,. !: I; .;ii .!. I.I. . l''' ..I; ' | ||
O | O | ||
!ty ;J412. ;'i | !ty ;J412. ;'i | ||
_;. . 1. :L .a u. ... . .. c .i im I'!' j . ..4 ..n . L. . :h: in;. .' :.! a ..- a- J | _;. . 1. :L .a u. ... . .. c .i im I'!' j . ..4 ..n . L. . :h: in;. .' :.! a ..- a- J | ||
'.dp | '.dp | ||
....~1.. | ....~1.. | ||
..l.. : | ..l.. : | ||
un .4' . :.n :!1,. | un .4' . :.n :!1,. | ||
: e u | : e u | ||
.l. jn- | .l. jn-l u, : i. ,o; .o rh n-un . o :n- - | ||
l u, : i. ,o; .o rh n- | |||
un . o :n- - | |||
: i. u | : i. u | ||
; PlyUrb 6 . | ; PlyUrb 6 . | ||
j allOWallE- Nc zz1T5- Ec:IdE -P ~ : ar dC l:i; -[ ru .jp ..': j';i i.:j:. i . . | j allOWallE- Nc zz1T5- Ec:IdE -P ~ : ar dC l:i; -[ ru .jp ..': j';i i.:j:. i . . | ||
: c ;.! l.. ;,., . | : c ;.! l.. ;,., . | ||
:l . | :l . | ||
._i. . .. _.. . | ._i. . .. _.. . | ||
_.. p . ... . . . -. .... . . . .. ... . . i,,. .. .,.,, | _.. p . ... . . . -. .... . . . .. ... . . i,,. .. .,.,, | ||
.;1 | .;1 | ||
: 1. m; a .n. 4 . ... | : 1. m; a .n. 4 . ... | ||
; | ; | ||
-- . e | -- . e | ||
' g~~~ | ' g~~~ | ||
"""-Q b l | """-Q b l | ||
. g h M ! ' | . g h M ! ' | ||
i i | |||
i | |||
i | |||
\ .~ ' l . .*. * | \ .~ ' l . .*. * | ||
. L. p''. :'n. . j:: | . L. p''. :'n. . j:: | ||
y g l. | y g l. | ||
g .; . | g .; . | ||
.g. | .g. | ||
t | t 4 ,. .. . . .. . . | ||
4 ,. .. . . .. . . | |||
. . . ;.' . | . . . ;.' . | ||
m in. n i,: | m in. n i,: | ||
t l ! !' ' '' :f p: , | t l ! !' ' '' :f p: , | ||
- ''f! '!' ''' '' ' | - ''f! '!' ''' '' ' | ||
A Il7470 20 20 Seem en A incli | A Il7470 20 20 Seem en A incli | ||
' ,( ,/ i | ' ,( ,/ i | ||
.... m (-- ,/S3 . | .... m (-- ,/S3 . | ||
( \_/ | ( \_/ | ||
j '. j . ,l' i: .~ ,i. ;l'' .: 't!-. t: | j '. j . ,l' i: .~ ,i. ;l'' .: 't!-. t: | ||
lip idl::.;ib:. | lip idl::.;ib:. | ||
. i l i;;l l ' . ! . 1: i u.. | . i l i;;l l ' . ! . 1: i u.. | ||
!:g: '1!!i! .!!!i [lh..' !: .1 | !:g: '1!!i! .!!!i [lh..' !: .1 | ||
. _. ;.; _ . :. ! .n . I. ..n_. . .. . =.1 .. * | . _. ;.; _ . :. ! .n . I. ..n_. . .. . =.1 .. * | ||
'!!!l!' .L. u_ . ;': | '!!!l!' .L. u_ . ;': | ||
. uf . , .; | . uf . , .; | ||
:pj yjj jjjj j q !!N H; | :pj yjj jjjj j q !!N H; i h $; ; 4' ,~ | ||
i h $; ; 4' ,~ | |||
l l ! | l l ! | ||
: n. H, 'i; | : n. H, 'i; | ||
,, H ; "; t ... | ,, H ; "; t ... | ||
'j I-1 !' : :i; '' ' | |||
'j I- | |||
1 !' : :i; '' ' | |||
tl :!: I t: l l | tl :!: I t: l l | ||
. . . _ . . ..: . ., . ....... . .;. ;;.. . t. .. .n .; .. . ; .. nt .;.;; . . h j!:; g: . !'.. . p!l. 7 | . . . _ . . ..: . ., . ....... . .;. ;;.. . t. .. .n .; .. . ; .. nt .;.;; . . h j!:; g: . !'.. . p!l. 7 I : ''; | ||
I : ''; | |||
!; '' | !; '' | ||
;;; | ;;; | ||
l g l' I. ' ' ' | l g l' I. ' ' ' | ||
__.R g ._. | __.R g ._. | ||
I b 8 ,I ! '. .i!'-- '! l.i- 5II. '. ! j.fi I, i'' ' :a1. . ;; .. '!' ;! ni | I b 8 ,I ! '. .i!'-- '! l.i- 5II. '. ! j.fi I, i'' ' :a1. . ;; .. '!' ;! ni | ||
.._ i . . . . . . . . . . . . . . . . . . .l; . '.n;. _L; . .. . ' ' '' | .._ i . . . . . . . . . . . . . . . . . . .l; . '.n;. _L; . .. . ' ' '' | ||
*. . , t, a. . .. L;. .. . . . . ;;; . ... ._;. | *. . , t, a. . .. L;. .. . . . . ;;; . ... ._;. | ||
| Line 5,822: | Line 3,683: | ||
t .' ; p. -n;' !! | t .' ; p. -n;' !! | ||
. l :: - ' | . l :: - ' | ||
'. . . q+ '.l'; | '. . . q+ '.l'; | ||
il y: H"q F 8- r n: , | il y: H"q F 8- r n: , | ||
t | t | ||
! iI | ! iI | ||
'._.. . . .l _. . .._.l... . . . . | '._.. . . .l _. . .._.l... . . . . | ||
....l_l__.l... | ....l_l__.l... | ||
. .__ _; .... .: . .n ; . . . . | . .__ _; .... .: . .n ; . . . . | ||
N : .a | N : .a | ||
: 4. m. | : 4. m. | ||
. ;. . . . ; . . . . p l' ! ! F ^ ; | . ;. . . . ; . . . . p l' ! ! F ^ ; | ||
y + L w N:L n! g N | y + L w N:L n! g N | ||
: l. 4. | : l. 4. | ||
. . . _ l . . . .. . _ .. _ . . ..'._. o u;. .3 : f_ . y. q. l l. ... | . . . _ l . . . .. . _ .. _ . . ..'._. o u;. .3 : f_ . y. q. l l. ... | ||
. p,g; | . p,g; | ||
.Restracted by stre,sses - | .Restracted by stre,sses - | ||
l | l | ||
\ \ \ 4: %!\ k | \ \ \ 4: %!\ k | ||
. ~2 ~~'~~0~'' | . ~2 ~~'~~0~'' | ||
-h l.' | -h l.' | ||
h' k kk~ -^ | h' k kk~ -^ | ||
I | I dt su' pports. | ||
dt su' pports. | |||
~~' C | ~~' C | ||
. g , . . Q' i : ... - i ;i . | . g , . . Q' i : ... - i ;i . | ||
| Line 5,866: | Line 3,712: | ||
._.l.. . ., k. . / ,. . . C3 . ..l.uj allbwa[bl e. zone. i _. . . . . . . . . p,g) | ._.l.. . ., k. . / ,. . . C3 . ..l.uj allbwa[bl e. zone. i _. . . . . . . . . p,g) | ||
! ! . ..; i ' , | ! ! . ..; i ' , | ||
. A l\i if 3 ' | . A l\i if 3 ' | ||
d \. d\ ,; , | d \. d\ ,; , | ||
A , | A , | ||
_._. [_. | _._. [_. | ||
. _ - NN. -32 4 '.(' . ,2 0 l ',16 '.g "12.h :,. ;4.!.g.: ' [4 A .l8 16 | . _ - NN. -32 4 '.(' . ,2 0 l ',16 '.g "12.h :,. ;4.!.g.: ' [4 A .l8 16 | ||
. . . . . . ' .. 8.. | . . . . . . ' .. 8.. | ||
;. .. .. .. | ;. .. .. .. | ||
.hi.}:12 . | .hi.}:12 . | ||
3 .! | 3 .! | ||
; .20' S.2. , d. 2 . . . | ; .20' S.2. , d. 2 . . . | ||
t L\. | t L\. | ||
.' E(10 ,). in ?lbs \.p.,. .. . ' ' | .' E(10 ,). in ?lbs \.p.,. .. . ' ' | ||
q .q ._- .g.Mq g | q .q ._- .g.Mq g | ||
. . i | . . i | ||
,g - | ,g - | ||
; 3 _. | ; 3 _. | ||
_.4_.. | _.4_.. | ||
P | P l | ||
l | |||
; . . . Q l\ | ; . . . Q l\ | ||
l : | l : | ||
1 . ! | 1 . ! | ||
i, - | i, - | ||
~$ | ~$ | ||
_t 4:3 h. . | _t 4:3 h. . | ||
'( \ / l: .Restric d by | '( \ / l: .Restric d by | ||
[ | [ | ||
I stre ssel s-b | I stre ssel s-b | ||
! ! . l ; | ! ! . l ; | ||
. ' _.j ;_ - | . ' _.j ;_ - | ||
.n . | .n . | ||
:1: 'h " ([.2., . | :1: 'h " ([.2., . | ||
! A t...'sup . r.t.$., I_ | ! A t...'sup . r.t.$., I_ | ||
g' | g' | ||
: l. : 1:. .ll . l ,, ';, | : l. : 1:. .ll . l ,, ';, | ||
_. _. LLl '. | _. _. LLl '. | ||
.; .. _ . . _ . . . . .. . . .. ;_:.. ' | .; .. _ . . _ . . . . .. . . .. ;_:.. ' | ||
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| Line 6,121: | Line 3,854: | ||
THE DETR0li EDISON COMPANY :PecaicAfiO= 3071-512 sec,...- .. ::::::= ,, | THE DETR0li EDISON COMPANY :PecaicAfiO= 3071-512 sec,...- .. ::::::= ,, | ||
PROJtcT WAmAGEutu? | PROJtcT WAmAGEutu? | ||
ORG ANIZ Afl04 SYSTEM DESIGN SPECIFICATION Issued: 9-6-72 FOR EMERGENCY EQUIPMENT (X)0 LING WATER SYSTEM Enrico Femi Atomic Power Plant Unit #2 APPROVAL SHEET l | |||
l | l DATE l | ||
DATE l | |||
/Ib,162//7i/ J t ~b WRITTEN BY: ('N Di LEHNERT , | /Ib,162//7i/ J t ~b WRITTEN BY: ('N Di LEHNERT , | ||
CHECKED BY: 'tf W | CHECKED BY: 'tf W | ||
) .E. GREGOR hO# | ) .E. GREGOR hO# | ||
| Line 6,133: | Line 3,862: | ||
h-7 APPROVED: | h-7 APPROVED: | ||
PROJ. ENG'G Ih - | PROJ. ENG'G Ih - | ||
GROUP SUPERVISOR /'/M/hf.Y P.E. | GROUP SUPERVISOR /'/M/hf.Y P.E. | ||
M ~ N' b S.H1 NOIG!CZ V | M ~ N' b S.H1 NOIG!CZ V | ||
| Line 6,143: | Line 3,871: | ||
if a JLll \ k QM - N | if a JLll \ k QM - N | ||
* l- b /" | * l- b /" | ||
A. ALEXIOU APPROVED: | |||
PROJECT ENGINEER h)h. | PROJECT ENGINEER h)h. | ||
1 b ' 'y l 2 ~ h R.A. VAhCW.E . | 1 b ' 'y l 2 ~ h R.A. VAhCW.E . | ||
l . | l . | ||
; , ,- _ | ; , ,- _ | ||
;; _ . _ . _ _ _ _ _ _ . . | ;; _ . _ . _ _ _ _ _ _ . . | ||
- Specification No. 3071-512 , | - Specification No. 3071-512 , | ||
Iccued: 9-6-72 ) | Iccued: 9-6-72 ) | ||
l O | l O | ||
i P44-00C0CO&oo$ | i P44-00C0CO&oo$ | ||
THE DETROIT EDISON COMPANY r SPECIFICATION i | THE DETROIT EDISON COMPANY r SPECIFICATION i | ||
SYSTEM DESIGN SPECIFICATION FOR | |||
SYSTEM DESIGN SPECIFICATION | : EMERGENCY EQUIPMENT COOLING WATER SYSTEM l o- ENRICO FERMI ATOMIC POWER PIANT UNIT #2 I | ||
FOR | |||
: EMERGENCY EQUIPMENT COOLING WATER SYSTEM l o- ENRICO FERMI ATOMIC POWER PIANT UNIT #2 | |||
I | |||
i i | i i | ||
O | O | ||
-\ | -\ | ||
W . | W . | ||
THE DETROIT EDISON COMPANY settineAfion 3071-512 spaCIPICATION " fCo E isi si P90 JECT MANAGEMENT SYSTEM DESIGN SPECIFICATION '",*7' 7 *,'y'" 9-6 -72 FOR EMERGENCY EQUIPMENT COOLING WATER SYSTEM ENRICO FERMI ATOMIC POWER PIANT UNIT #2 INDEX Article Code Article Page | |||
THE DETROIT EDISON COMPANY settineAfion 3071-512 | |||
spaCIPICATION " fCo E isi si P90 JECT MANAGEMENT | |||
: 1. SC0PE.......................... NA-3250................ 1 2 CERTIFIO4 TION.................. NA-3250................ 1 | : 1. SC0PE.......................... NA-3250................ 1 2 CERTIFIO4 TION.................. NA-3250................ 1 | ||
: 3. C1 ASS IF ICATION . . . . . . . . . . . . . . . . . NA-2000................ 1 4 DOCUMENTATION . . . . . . . . . . . . . . . . . . NA-3256................ 2 | : 3. C1 ASS IF ICATION . . . . . . . . . . . . . . . . . NA-2000................ 1 4 DOCUMENTATION . . . . . . . . . . . . . . . . . . NA-3256................ 2 | ||
| Line 6,190: | Line 3,898: | ||
: 8. SYSTEM DESIGN BASIS...................................... 7 | : 8. SYSTEM DESIGN BASIS...................................... 7 | ||
: 9. COMPONENT DESIGN BASIS................................... 7 Os 1.0 COMPONENT CHARACTERISTICS................................ 14 | : 9. COMPONENT DESIGN BASIS................................... 7 Os 1.0 COMPONENT CHARACTERISTICS................................ 14 | ||
: 11. CIASSIFICATION OF CONDITIONS . . . . . NA-2140. . . . . . . . . . . . . . . . 16 | : 11. CIASSIFICATION OF CONDITIONS . . . . . NA-2140. . . . . . . . . . . . . . . . 16 12 HYDROSTATIC AND LEAK TESTS . . . . . . . NC-6000. . . . . . . . . . . . . . . . 16 | ||
: 13. REFERENCES............................................... 17 ATTACHMENTS: | : 13. REFERENCES............................................... 17 ATTACHMENTS: | ||
Process Diagram 6M721-2027 Systems Isometric (See References) | Process Diagram 6M721-2027 Systems Isometric (See References) | ||
| Line 6,200: | Line 3,907: | ||
I l | I l | ||
t | t | ||
^ | ^ | ||
Sptcification: 3071-512 Issued: 9-6-72 t | Sptcification: 3071-512 Issued: 9-6-72 t | ||
o THE DETROIT EDISON COMPANY d | o THE DETROIT EDISON COMPANY d | ||
| Line 6,214: | Line 3,917: | ||
with the Code. | with the Code. | ||
7- 3i- n DATE | 7- 3i- n DATE | ||
//tb n SIGNAIURE | //tb n SIGNAIURE Michigan - 18860 BRANCH REGISTRATION, STATE and NUMBER or SIAMP | ||
Michigan - 18860 BRANCH REGISTRATION, STATE and NUMBER or SIAMP | |||
: 3. CIASSIFICATION ( | : 3. CIASSIFICATION ( | ||
| Line 6,224: | Line 3,924: | ||
The Emergency Equipment Cooling Water (E.E.C.W.) System is divided into two classes. That portion of the E.E.C.W. System supply and return piping which is between the outboard containment isolation valve and the equipment inside the primary containment that requires cooling water shall be classified as a Class 2 system and shall be designed and constructed in accordance with the rules of Subsection NC of the ASME Code Section III,1971 Issue. | The Emergency Equipment Cooling Water (E.E.C.W.) System is divided into two classes. That portion of the E.E.C.W. System supply and return piping which is between the outboard containment isolation valve and the equipment inside the primary containment that requires cooling water shall be classified as a Class 2 system and shall be designed and constructed in accordance with the rules of Subsection NC of the ASME Code Section III,1971 Issue. | ||
.O- | .O- | ||
Speelfication: 3071-512 Icsued: 9-6-72 Page Two b_qk. 3. CIASSIFICATION ( | Speelfication: 3071-512 Icsued: 9-6-72 Page Two b_qk. 3. CIASSIFICATION ( | ||
| Line 6,248: | Line 3,943: | ||
~ | ~ | ||
, . l Specificatien; 3071-512 l Iscu:d: 9-6-72 l Page Three | , . l Specificatien; 3071-512 l Iscu:d: 9-6-72 l Page Three | ||
{ | { | ||
(f 4. DOCUMENTATION (Continued) 1 | (f 4. DOCUMENTATION (Continued) 1 | ||
: 4. The Enforcement Authority having jurisdiction at the location of the System is: | : 4. The Enforcement Authority having jurisdiction at the location of the System is: | ||
| Line 6,268: | Line 3,959: | ||
: 10. Upon completion of the contract each manufacturer and/or installer shall complete the appropriate certificate of Compliance and submit a copy of the Certificate to the Owner for inclusion in the Owner's Data Report Form N-3, (Article NA-3270). | : 10. Upon completion of the contract each manufacturer and/or installer shall complete the appropriate certificate of Compliance and submit a copy of the Certificate to the Owner for inclusion in the Owner's Data Report Form N-3, (Article NA-3270). | ||
{y, m | {y, m | ||
~ | ~ | ||
Specification: 3071-512 Issu:d: 9-6-72 Page Four | Specification: 3071-512 Issu:d: 9-6-72 Page Four | ||
()[ 5. GENERAL SYSTEM DESCRIPTION (This is a functional description and not a design requirement). | ()[ 5. GENERAL SYSTEM DESCRIPTION (This is a functional description and not a design requirement). | ||
The E.E.C.W. System consists of two redundant supply and return cooling loops, Division I and Division II. Each loop will consist of one e condensate circulating water pump of sufficient capacity to circulate water thru the system and return the cooling water to a full capacity t heat exchanger. | The E.E.C.W. System consists of two redundant supply and return cooling loops, Division I and Division II. Each loop will consist of one e condensate circulating water pump of sufficient capacity to circulate water thru the system and return the cooling water to a full capacity t heat exchanger. | ||
The E.E.C.W. System will be automatically operable upon a loss of A-C off-site power or may be manually initiated on system failure of the Reactor Building Closed Cooling Water System. | The E.E.C.W. System will be automatically operable upon a loss of A-C off-site power or may be manually initiated on system failure of the Reactor Building Closed Cooling Water System. | ||
| Line 6,288: | Line 3,973: | ||
l h V s | l h V s | ||
Specificction: 3071-512 Issurd: 9-6-72 Page Five | Specificction: 3071-512 Issurd: 9-6-72 Page Five | ||
[ 5. GENERAL SYSTEM DESCRIPTION (Continued) | [ 5. GENERAL SYSTEM DESCRIPTION (Continued) | ||
| Line 6,308: | Line 3,990: | ||
Neutron 140,000 N/CM - Sec. | Neutron 140,000 N/CM - Sec. | ||
t . | t . | ||
Specifiestion: 3071-512 Issu;d: 9-6-72 Page Six | Specifiestion: 3071-512 Issu;d: 9-6-72 Page Six h 7 DESIGN (Continued) 7.2 (Continued) | ||
h 7 DESIGN (Continued) 7.2 (Continued) | |||
All Class 2 components are insulated with an all metal reflective type insulation having a heat loss coefficient of approximately 0.15 BTU /HR/Sq. Ft/0 F/ Inch thickness. For the purpose of thermal analysis, this Insulation shall be assumed to be pe-fect (no heat loss). | All Class 2 components are insulated with an all metal reflective type insulation having a heat loss coefficient of approximately 0.15 BTU /HR/Sq. Ft/0 F/ Inch thickness. For the purpose of thermal analysis, this Insulation shall be assumed to be pe-fect (no heat loss). | ||
7.3 Faul ted Environmental Conditions in Drywell (or.e time only) | 7.3 Faul ted Environmental Conditions in Drywell (or.e time only) | ||
| Line 6,318: | Line 3,997: | ||
-2 to 56 PSIG for i minute at 340 F | -2 to 56 PSIG for i minute at 340 F | ||
-2 to 35 PSIG for 3 r.ours at 3400F , | -2 to 35 PSIG for 3 r.ours at 3400F , | ||
-2 to 35 PSIG for 6 hours at 3200F 0 to 25 PSIG for i day at 250 F j 0 to 20 PSIG for 100 days at 2000F Relative Humidity = 107/o Radiation = 2.6 x 107 RADS (gamma) 7.4 System Fluid The system will contain the following fluid: | |||
-2 to 35 PSIG for 6 hours at 3200F 0 to 25 PSIG for i day at 250 F j | |||
0 to 20 PSIG for 100 days at 2000F Relative Humidity = 107/o Radiation = 2.6 x 107 RADS (gamma) 7.4 System Fluid The system will contain the following fluid: | |||
( Medlum: Demineralized Water pH at 25 C: 6.5 to 7.5 Radioactivity: 0.7 Micro Curle/ml @ zero decay time Specific conductivity, mho/cm @ 250c <0.1 Chloride as Cl- <2 ppb Total metallic impurity <10 ppb Silicia as S102 <5 ppb ! | ( Medlum: Demineralized Water pH at 25 C: 6.5 to 7.5 Radioactivity: 0.7 Micro Curle/ml @ zero decay time Specific conductivity, mho/cm @ 250c <0.1 Chloride as Cl- <2 ppb Total metallic impurity <10 ppb Silicia as S102 <5 ppb ! | ||
l 7.5 Environmental Conditions of Secondary Containment The Class 3 portion of the system, situated in the secondary contain-ment will be subjected to the following conditions: | l 7.5 Environmental Conditions of Secondary Containment The Class 3 portion of the system, situated in the secondary contain-ment will be subjected to the following conditions: | ||
External Pressure = Atmospheric External Temperature = Winter Minimum of 400F Accidental Maximum of 1480F (for 8 hours) | External Pressure = Atmospheric External Temperature = Winter Minimum of 400F Accidental Maximum of 1480F (for 8 hours) | ||
Average Operating of 70 F | Average Operating of 70 F Relative Humidity = 50 to 9&4 Radia t Ion = 7 9 x 10 5RADS (gama - includes faulted dose) | ||
Relative Humidity = 50 to 9&4 | |||
Radia t Ion = 7 9 x 10 5RADS (gama - includes faulted dose) | |||
Specification: 3071-512 Issued: 9-6-72 P:;ge Ssven f 8. SYSTEM DESIGN BASIS t i V | Specification: 3071-512 Issued: 9-6-72 P:;ge Ssven f 8. SYSTEM DESIGN BASIS t i V | ||
8.1 Cold Springing Cold springing is not permitted in the design of the piping. In cases where mismatches due to fabrication tolerances exist during the instal!ation, the procedures for measuring and closing the gap giver in the syste:r. erection specification will be followed. | 8.1 Cold Springing Cold springing is not permitted in the design of the piping. In cases where mismatches due to fabrication tolerances exist during the instal!ation, the procedures for measuring and closing the gap giver in the syste:r. erection specification will be followed. | ||
| Line 6,355: | Line 4,022: | ||
.045 in | .045 in | ||
Specification: 3071-512 Issu;d: 9-6-72 Page Eight 9. | Specification: 3071-512 Issu;d: 9-6-72 Page Eight 9. | ||
( }{ COMPONENT DESIGN BASIS (Continued) 9.1 (Continued) | ( }{ COMPONENT DESIGN BASIS (Continued) 9.1 (Continued) | ||
In the accident condition the movement of the penetration assembly will be due to vertical and horizontal expansion from 700F to 3400F and pressure expansion from 0 to 56 psig of the primary containment. | In the accident condition the movement of the penetration assembly will be due to vertical and horizontal expansion from 700F to 3400F and pressure expansion from 0 to 56 psig of the primary containment. | ||
The movements shall be as follows: | The movements shall be as follows: | ||
Horizontal Displacement = | Horizontal Displacement = | ||
.539 in Vertical Displacement = | .539 in Vertical Displacement = | ||
| Line 6,369: | Line 4,031: | ||
The flued head anchor is subject to seismic displacements of the containment shield. | The flued head anchor is subject to seismic displacements of the containment shield. | ||
9.2 Class 2 System Line Valves and Isolation Valves All valves shall be designed, manufactured, tested and inspected in accordance with Edison's Valve Specification 3071-501 and 3071-12. | 9.2 Class 2 System Line Valves and Isolation Valves All valves shall be designed, manufactured, tested and inspected in accordance with Edison's Valve Specification 3071-501 and 3071-12. | ||
9.3 Piping of 3/4" NPS and Smaller and Instrument Piping Piping of above category, which connects to E.E.C.W. System piping | 9.3 Piping of 3/4" NPS and Smaller and Instrument Piping Piping of above category, which connects to E.E.C.W. System piping Inside the primary containment up to and including the first source valve is classified as Class 2 and shall be designed in accordance with A.S.M.E. Section III,1971 Edition. | ||
Inside the primary containment up to and including the first source valve is classified as Class 2 and shall be designed in accordance with A.S.M.E. Section III,1971 Edition. | |||
Piping beyond the source valve up to and including the ter-inal or instrument is classified as Class 3 and shall be designed in accordance with ANSI B31.1 " Power Piping", Paragraph 122.3, includ-Ing the application of ANSI B31 Code Case 78. | Piping beyond the source valve up to and including the ter-inal or instrument is classified as Class 3 and shall be designed in accordance with ANSI B31.1 " Power Piping", Paragraph 122.3, includ-Ing the application of ANSI B31 Code Case 78. | ||
Only seamless stainless steel or carbon steel tubine full stress relieved may be used for source connections. Cold forming, tending flaring etc. is not permitted. | Only seamless stainless steel or carbon steel tubine full stress relieved may be used for source connections. Cold forming, tending flaring etc. is not permitted. | ||
9.4 E.E.C.W. System Pumps, Heat Exchanger and Make-up Tanks The pumps, heat exchangers and make up tanks are classified as Class 3 components. Piping connections to these components shall be designed to limit reactions to the following limits: | 9.4 E.E.C.W. System Pumps, Heat Exchanger and Make-up Tanks The pumps, heat exchangers and make up tanks are classified as Class 3 components. Piping connections to these components shall be designed to limit reactions to the following limits: | ||
Based on the moment of inertia and the moment arm of reactions, the pump casing and the shell of the heat exchanger and the make-up tank are assuned to accept and transfer their respective loads | Based on the moment of inertia and the moment arm of reactions, the pump casing and the shell of the heat exchanger and the make-up tank are assuned to accept and transfer their respective loads to their anchor bolts, which present the weakest link. React ions are therefore limited based on the strength of the bolts. | ||
to their anchor bolts, which present the weakest link. React ions are therefore limited based on the strength of the bolts | |||
. | |||
Specification: 3071-512 Issu:d: 9-6-72 Page Nine i | Specification: 3071-512 Issu:d: 9-6-72 Page Nine i | ||
OJ' V ' | OJ' V ' | ||
: 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont'd) | : 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont'd) | ||
| Line 6,396: | Line 4,050: | ||
-My3 + Myql((Later) i l | -My3 + Myql((Later) i l | ||
l | l | ||
Specification: 3071-512 Issusd: 9-6-72 Page Ten | |||
: 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont'd) | : 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont'd) | ||
(2). Maximum Shear Moment (Cont'd) | (2). Maximum Shear Moment (Cont'd) | ||
| Line 6,417: | Line 4,067: | ||
Pr-m | Pr-m | ||
SpIcification: 3071-512 Issurd: 9-6-72 Page Eleven h 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont 'd ) | SpIcification: 3071-512 Issurd: 9-6-72 Page Eleven h 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont 'd ) | ||
Seismic displacements for the DBE are given in the gobal coordinate form where X is east, Z is south and Y is vertical . The three dis-placements components of the three mutually perpendicular directions of excitations are expressed in inches and represent the square root of the sum of the squares of the displacements of the vibratory modes. The displacements for the OBE are defined by multiplying the DBE displacements by 1/1.875. | Seismic displacements for the DBE are given in the gobal coordinate form where X is east, Z is south and Y is vertical . The three dis-placements components of the three mutually perpendicular directions of excitations are expressed in inches and represent the square root of the sum of the squares of the displacements of the vibratory modes. The displacements for the OBE are defined by multiplying the DBE displacements by 1/1.875. | ||
The pump, heat exchanger and make-up tank nozzle connections shall be rigid anchor points for piping. This equipment is subject to seismic displacements of the supporting floor slab. The anchor movements are as follows: | The pump, heat exchanger and make-up tank nozzle connections shall be rigid anchor points for piping. This equipment is subject to seismic displacements of the supporting floor slab. The anchor movements are as follows: | ||
Horizontal Displacement, OBE = . 042 in. , | Horizontal Displacement, OBE = . 042 in. , | ||
OBE = . 079 in. ; | OBE = . 079 in. ; | ||
| Line 6,433: | Line 4,078: | ||
All support structures for the E.E.C.W. System Class 2 and Class 3 1 components shall be designed for a Class I seismic criteria. Hangers and supports shall be located and spaced in a manner, to limit seismic accelerations for the line valves to 5.0g under DBE condi-tions. Seismic displacement of piping shall be limited to the clearance dimensions of piping where it passes through sleeves in walls and slabs to avoid impact. Anchor movements shall be de-termined from the applicable floor response spectra of the build-ing. | All support structures for the E.E.C.W. System Class 2 and Class 3 1 components shall be designed for a Class I seismic criteria. Hangers and supports shall be located and spaced in a manner, to limit seismic accelerations for the line valves to 5.0g under DBE condi-tions. Seismic displacement of piping shall be limited to the clearance dimensions of piping where it passes through sleeves in walls and slabs to avoid impact. Anchor movements shall be de-termined from the applicable floor response spectra of the build-ing. | ||
9.6 Insulation I All Class 3 components are insulated with insulation of approximately 1" thickness and a specific density of 15#/cu. f t. | 9.6 Insulation I All Class 3 components are insulated with insulation of approximately 1" thickness and a specific density of 15#/cu. f t. | ||
9.7 Seismic Analysis of Pipino l | 9.7 Seismic Analysis of Pipino l | ||
Class 2 and Class 3 piping 8 Inch NPS and larger shall be analyzed j by use of a multi-degree of freedom dynamic modal response method. I i | Class 2 and Class 3 piping 8 Inch NPS and larger shall be analyzed j by use of a multi-degree of freedom dynamic modal response method. I i | ||
The piping under seismic analysis shall be excited in each of three mutually perpendicular directions, two horizontal and one vertical . | The piping under seismic analysis shall be excited in each of three mutually perpendicular directions, two horizontal and one vertical . | ||
T* | T* | ||
m. | m. | ||
l u | l u | ||
Specification: 3071-512 Issu;d: 9-6-72 Page Twelve V[ | Specification: 3071-512 Issu;d: 9-6-72 Page Twelve V[ | ||
I~' 9. COMPONENT DESIGN BASIS (Continued) 9.7 Seismic Analysis of Piping (Cont 'd) | I~' 9. COMPONENT DESIGN BASIS (Continued) 9.7 Seismic Analysis of Piping (Cont 'd) | ||
| Line 6,458: | Line 4,098: | ||
Piping System. The pump movement i s as fol l ows : | Piping System. The pump movement i s as fol l ows : | ||
1.43 inches Down 0.265 inches East 1.06 inches South The connection weld between the E.E.C.W. System piping and the Drywell Cooler nozzles shall constitute a rigid anchor. This equipment is subject to seismic displacement of the supporting drywell steel. The anchor movements are as follows: | 1.43 inches Down 0.265 inches East 1.06 inches South The connection weld between the E.E.C.W. System piping and the Drywell Cooler nozzles shall constitute a rigid anchor. This equipment is subject to seismic displacement of the supporting drywell steel. The anchor movements are as follows: | ||
Specification: 3071-512 Issued: 9-6-72 Paga Thirtsen | Specification: 3071-512 Issued: 9-6-72 Paga Thirtsen | ||
[{ ~ | [{ ~ | ||
| Line 6,468: | Line 4,105: | ||
DBE = .0206 In. | DBE = .0206 In. | ||
Vertical Displacement OBE = .0034 in. | Vertical Displacement OBE = .0034 in. | ||
DBE = . 016 in. | DBE = . 016 in. | ||
9.9 Piping Class 3. E.E.C.W. System Equipment Interfaces The connection weld between the E.E.C.W. System piping out side the primary containment and the equipment (as listed in Section 5) nozzles shall constitute a rigid anchor. This equipment is sub-ject to seismic displacement of the supporting floor slab. The anchor movements are as follows: | 9.9 Piping Class 3. E.E.C.W. System Equipment Interfaces The connection weld between the E.E.C.W. System piping out side the primary containment and the equipment (as listed in Section 5) nozzles shall constitute a rigid anchor. This equipment is sub-ject to seismic displacement of the supporting floor slab. The anchor movements are as follows: | ||
For the Core Spray System and Residual Heat f.emovat System Pump Motors; the Core Spray and Reactor Core Isolation Coolant and High Pressure Cooling Injection Space Coolers, (sub-ba s ement ) , | For the Core Spray System and Residual Heat f.emovat System Pump Motors; the Core Spray and Reactor Core Isolation Coolant and High Pressure Cooling Injection Space Coolers, (sub-ba s ement ) , | ||
Horizontal Displacement OBE = .0128 in. | Horizontal Displacement OBE = .0128 in. | ||
| Line 6,482: | Line 4,117: | ||
DBE = . 031'In. | DBE = . 031'In. | ||
Vertical Displacement OBE = .0096 in. | Vertical Displacement OBE = .0096 in. | ||
DBE = . 018 In. | DBE = . 018 In. | ||
For the Switch Gear Room Space Coolers (Second floor), | For the Switch Gear Room Space Coolers (Second floor), | ||
| Line 6,489: | Line 4,123: | ||
Vertical Displacement ODE = .0096 in. | Vertical Displacement ODE = .0096 in. | ||
DBE = . 018 in. | DBE = . 018 in. | ||
Or uA. ' | Or uA. ' | ||
t. | t. | ||
. Specification: 3071-512 Issurd: 9-6-72 Paga Fourteen | . Specification: 3071-512 Issurd: 9-6-72 Paga Fourteen | ||
: 9. COMPONENT DESIGN BASIS (Continued) 9.9 Piping Class 3. E.E.C.W. System Equipment Interfaces (Cont 'd ) | : 9. COMPONENT DESIGN BASIS (Continued) 9.9 Piping Class 3. E.E.C.W. System Equipment Interfaces (Cont 'd ) | ||
For the Switch Gear Room Space Coolers and the Hydrogen Control System (Third floor), | For the Switch Gear Room Space Coolers and the Hydrogen Control System (Third floor), | ||
Horizontal Displacement OBE = . 056 in. | Horizontal Displacement OBE = . 056 in. | ||
DBE = .106 in. | DBE = .106 in. | ||
| Line 6,514: | Line 4,142: | ||
Material See Appendix "A", Table 7 Dimensions i", li", 2", 2}", 3", 4", 6", 8' & 10" Sch . LO 10.2 Valves As per Valve Specification, Valve List and Valve Design Specif1-cation 3071-501 & 3071-12. | Material See Appendix "A", Table 7 Dimensions i", li", 2", 2}", 3", 4", 6", 8' & 10" Sch . LO 10.2 Valves As per Valve Specification, Valve List and Valve Design Specif1-cation 3071-501 & 3071-12. | ||
10.3 Pumps Specific pump data is given in Detroit Edison Specification 3071-85 Specific Design Data is as follows: | 10.3 Pumps Specific pump data is given in Detroit Edison Specification 3071-85 Specific Design Data is as follows: | ||
Cl | Cl l | ||
e- | |||
---~ . , | ---~ . , | ||
4 | 4 | ||
+ | + | ||
f | f | ||
~$R;9pp | ~$R;9pp | ||
/// | /// | ||
f(M>+$/ * %d'7,$ | f(M>+$/ * %d'7,$ | ||
| Line 6,531: | Line 4,155: | ||
TEST TARGET (MT-3) | TEST TARGET (MT-3) | ||
; | ; | ||
; | ; | ||
l.0 5 a j!22 rap 3Ipl=2.2 E l?A U l,l $# h_N_ | l.0 5 a j!22 rap 3Ipl=2.2 E l?A U l,l $# h_N_ | ||
11 1.25 1.4 1.6 | 11 1.25 1.4 1.6 l | ||
4 6" y MICROCOPY RESOLUTION TEST CH ART mtv d#4, wyr, i | |||
/f4* | /f4* | ||
+.3 %a4 m ,f 4 | +.3 %a4 m ,f 4 | ||
,ee 4 +, , | ,ee 4 +, , | ||
O ' | O ' | ||
/-- | /-- | ||
8' | 8' | ||
~~~ | ~~~ | ||
l | l Specification: 3071-512 Issusd: 9-6-72 Paga Fifteen I | ||
Specification: 3071-512 Issusd: 9-6-72 Paga Fifteen I | |||
10 COMPONENT CHARACTERISTICS (Continued) | 10 COMPONENT CHARACTERISTICS (Continued) | ||
[' | [' | ||
10.3 Pumps (Cont'd) | 10.3 Pumps (Cont'd) | ||
Design Pressure 120 PSIG | Design Pressure 120 PSIG Design Temperature 120 F Pump Casing Material A216 WCB Cast Steel Discharge Capacity 1450 GPM Discharge Head 158 Ft. @ 51 Ft. NPSH @ 95 F 10.4 Heat Exchangers Specific heat exchanger data is given in Detroit Edison Specifi- | ||
Design Temperature 120 F Pump Casing Material A216 WCB Cast Steel | |||
Discharge Capacity 1450 GPM Discharge Head 158 Ft. @ 51 Ft. NPSH @ 95 F 10.4 Heat Exchangers Specific heat exchanger data is given in Detroit Edison Specifi- | |||
, cation 3071-88. | , cation 3071-88. | ||
- Specific Design Data is as follows: | - Specific Design Data is as follows: | ||
Shell Side Tube Side Design Pressure 120 PSIG 175 PSIG Dest gn Temperature 1200F 1200F Mate rial A-515 Grade 70 Admiralty SB-lli Fluid Condensate RHR Service Water I Quantity 1600 GPM 1450 GPM Temp-In ll00F (890) | Shell Side Tube Side Design Pressure 120 PSIG 175 PSIG Dest gn Temperature 1200F 1200F Mate rial A-515 Grade 70 Admiralty SB-lli Fluid Condensate RHR Service Water I Quantity 1600 GPM 1450 GPM Temp-In ll00F (890) | ||
Temp-Out 950F 102.60F 10.5 Make-up Tanks Specific make-up tank data is given in Detroit Edison Bill of | Temp-Out 950F 102.60F 10.5 Make-up Tanks Specific make-up tank data is given in Detroit Edison Bill of Material S20-17M. | ||
Material S20-17M. | |||
Specific Design Data is as follows: | Specific Design Data is as follows: | ||
Design Pressure 100 PSIG Design Temperature 120 F Material for Shall and Head A-515 Grade 70 Capaci ty 600 Gallons 10.6 Overpressure Protection The E.E.C.W. heat exchangers and make-up tanks are equipped with relief valves. | Design Pressure 100 PSIG Design Temperature 120 F Material for Shall and Head A-515 Grade 70 Capaci ty 600 Gallons 10.6 Overpressure Protection The E.E.C.W. heat exchangers and make-up tanks are equipped with relief valves. | ||
.m, | .m, Q | ||
Q | |||
-- . .n . _ . _ | -- . .n . _ . _ | ||
~ | ~ | ||
Specificat ion: 3071-512 Issurd: 9-6-72 Page Sixteen | Specificat ion: 3071-512 Issurd: 9-6-72 Page Sixteen | ||
| Line 6,591: | Line 4,195: | ||
: 12. HYDROSTATIC AND LEAK TESTS Hydrostatic testing shall meet the requirements of NC-6200, except that the valve bodies shall be tested by the manufacturer in accordance | : 12. HYDROSTATIC AND LEAK TESTS Hydrostatic testing shall meet the requirements of NC-6200, except that the valve bodies shall be tested by the manufacturer in accordance | ||
{ | { | ||
with ANSI Bl6.5 or MSS SP-66 for Class 2 and Class 3 valves. | with ANSI Bl6.5 or MSS SP-66 for Class 2 and Class 3 valves. | ||
Specifiestion: 3071-512 Issurd: 9-6-72 Page Seventeen 12 HYDROSTATIC AND LEAK TESTS (Continued) | |||
Prior to the hydrostatic test, all valve stem leak-off connections shall be open ended. All line valves, sMil be in the open position, but not bachseated, to provide full differential pressure across the stem pack-Ings. | Prior to the hydrostatic test, all valve stem leak-off connections shall be open ended. All line valves, sMil be in the open position, but not bachseated, to provide full differential pressure across the stem pack-Ings. | ||
During hydrostatic test, examination for leakage shall be made. There | During hydrostatic test, examination for leakage shall be made. There shall be absolutely no visible leakage ,on any of the pressure retaining components, including valve stem packings and check valve exercising devices. | ||
shall be absolutely no visible leakage ,on any of the pressure retaining components, including valve stem packings and check valve exercising | |||
devices. | |||
The test medium shall be demineralized water. | The test medium shall be demineralized water. | ||
The hydrostatic test pressure for the system shall be 188 PSIG @ 70 0F. | The hydrostatic test pressure for the system shall be 188 PSIG @ 70 0F. | ||
| Line 6,620: | Line 4,215: | ||
(II). Edison Specification 3071-85, ti.c E.E.C .W. System Pumps . | (II). Edison Specification 3071-85, ti.c E.E.C .W. System Pumps . | ||
i (12). Edison Specification 3071-88, the E.E.C.sf. Heat F;. changers. | i (12). Edison Specification 3071-88, the E.E.C.sf. Heat F;. changers. | ||
(13) . Emergency Equipment Cooling Water System Isometric Drawings: | (13) . Emergency Equipment Cooling Water System Isometric Drawings: | ||
6M721-3672 6M721-3368 3351 3337 rs 3347 3336 Q' 3679 3666 | 6M721-3672 6M721-3368 3351 3337 rs 3347 3336 Q' 3679 3666 | ||
Specification: 3071-512 Issutd: 9-6-72 Page Eighteen | Specification: 3071-512 Issutd: 9-6-72 Page Eighteen | ||
(( 13. REFERENCES (Cont inued) | (( 13. REFERENCES (Cont inued) | ||
(13). Emergency Equipment Cooling Vater System Isometric Drawings: (Con 6 *d) 6H721 -3657 6H721-3348 3340 3346 3656 3345 3362 3667 3189 3368 3672 3084 | (13). Emergency Equipment Cooling Vater System Isometric Drawings: (Con 6 *d) 6H721 -3657 6H721-3348 3340 3346 3656 3345 3362 3667 3189 3368 3672 3084 1-O g | ||
1-O | |||
g | |||
([)F- | ([)F- | ||
. n. . | . n. . | ||
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! !: .. ; ,. | ! !: .. ; ,. | ||
pm :vum twasm w-:s. | pm :vum twasm w-:s. | ||
a m)-l. . | a m)-l. . | ||
i l | |||
i | i f - - | ||
f - | |||
. f . i ~ | . f . i ~ | ||
si.g.g r | si.g.g r | ||
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j | j s | ||
(m) r,stl . s : : en .-.yu ~ " - - , | |||
r,stl . s : : en .-.yu ~ " - - , | |||
8I $ '' | 8I $ '' | ||
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1v!rlN | |||
. l MM*HI! | . l MM*HI! | ||
g | |||
'%g id. . .; ' | '%g id. . .; ' | ||
- <y' w : | - <y' w : | ||
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1-po-(-) | 1-po-(-) | ||
l | l | ||
, i h . ,'. . | , i h . ,'. . | ||
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:=. | :=. | ||
r ' | r ' | ||
; 1 | ; 1 | ||
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g ' | g ' | ||
e | e | ||
; ,' | ; ,' | ||
i | i | ||
. 4 Y' 1: . ! | . 4 Y' 1: . ! | ||
1 | 1 1 a a, | ||
1 a a, | |||
' ~ | ' ~ | ||
o ; i prl ! - | o ; i prl ! - | ||
i( i s 5 - f3 | i( i s 5 - f3 e | ||
0 L. .A.; | |||
L. .A.; | |||
i.l.Uf.,.m.n h a i | i.l.Uf.,.m.n h a i | ||
;s o. | ;s o. | ||
,N I | ,N I | ||
,e .s p i.. | ,e .s p i.. | ||
d :, ,, | d :, ,, | ||
% s tl O*- l ii s s ii c 1 :: a '[ i.i = .<. .v. | |||
% s tl O*- l ii | |||
s s ii | |||
c 1 :: a '[ i.i = .<. .v. | |||
; | ; | ||
j s , | j s , | ||
o l' | o l' | ||
j' y !Y | j' y !Y | ||
: a. , - | : a. , - | ||
m . | m . | ||
.,f. -I | .,f. -I i | ||
i | |||
! i * * | ! i * * | ||
/ , J...- yu | / , J...- yu | ||
,. m , | ,. m , | ||
u, o o l , - | u, o o l , - | ||
p,.y.....u.............-3 /. | p,.y.....u.............-3 /. | ||
4.----4...:l- , | 4.----4...:l- , | ||
o , d , | o , d , | ||
a 4 ., | a 4 ., | ||
4. | 4. | ||
~ .. | ~ .. | ||
!. }l l,,/,,s' e 0,. n | !. }l l,,/,,s' e 0,. n n | ||
! ' [T r = - - - - | |||
n | |||
! ' [T | |||
r = - - - - | |||
f i,, i. A | f i,, i. A | ||
( - | ( - | ||
L 4 " | L 4 " | ||
j, j l g' y) i r 3h_ - | |||
i r 3h_ - | |||
v | v | ||
" p. L tr i J - | " p. L tr i J - | ||
A s s | A s s | ||
. h wy r :, : | . h wy r :, : | ||
! p 's_ t.f a . | ! p 's_ t.f a . | ||
y u | |||
y | 4 se [1 22 rI - E,; | ||
a,.F.. 1 } ' L_. .i I | a,.F.. 1 } ' L_. .i I | ||
*9 Ir b' ( ,f | |||
*9 | |||
Ir | |||
*?t (3.. C' | *?t (3.. C' | ||
'? | '? | ||
l, lt m o | |||
l, lt | |||
m o | |||
, I .~.1 | , I .~.1 | ||
: m m 3 ; : :, - | : m m 3 ; : :, - | ||
| Line 6,838: | Line 4,307: | ||
,1 | ,1 | ||
. :r r | . :r r | ||
i pi rp | i pi rp j gy o , , , | ||
j gy | |||
o , , , | |||
o | o | ||
'g* : t | 'g* : t | ||
,J [jl5 | ,J [jl5 h.,-... . ql, .................... " . , | ||
h.,-... . ql, .................... " . , | |||
),,.~.' . , | ),,.~.' . , | ||
S | S | ||
= ^;* | = ^;* | ||
: n. .-e - | : n. .-e - | ||
u *, r = , W | u *, r = , W | ||
,, l 3 | |||
,, l | 1' | ||
[ y. . | [ y. . | ||
, f., | , f., | ||
4.s7 y ll 11;1j ! ' (.<c -a.g e.h . | 4.s7 y ll 11;1j ! ' (.<c -a.g e.h . | ||
. v i ! | . v i ! | ||
3 1: | 3 1: | ||
3:. %- | 3:. %- | ||
; | ; | ||
3_ j .. q!e-: a; ,g ' < | 3_ j .. q!e-: a; ,g ' < | ||
, r 1- . ., , | , r 1- . ., , | ||
I'~~Uo ~ | I'~~Uo ~ | ||
n | n | ||
.b l -f'~ | .b l -f'~ | ||
tf.5o) e U,.}1 | tf.5o) e U,.}1 o - - - | ||
o - - - | |||
," e , | ," e , | ||
s_; | s_; | ||
~ | ~ | ||
n - | n - | ||
w) s n - --- - - - - > | w) s n - --- - - - - > | ||
| Line 6,901: | Line 4,341: | ||
> ',,e ;- | > ',,e ;- | ||
^ | ^ | ||
;p | ;p N | ||
: e. _ n es l' ID l gggm l f g | |||
N | J u | ||
: e. _ n es l' ID l gggm | |||
l f g | |||
J | |||
u | |||
'. ~ * | '. ~ * | ||
~ LOCAL COORDINATE SYSTEM O _AND SIGN CONVENTION Y | |||
~ LOCAL COORDINATE SYSTEM O _AND SIGN CONVENTION | |||
Y | |||
........_........:.- ] | ........_........:.- ] | ||
. F | . F | ||
. _ _ _ _ _.__. . ... .. _._ i )y | . _ _ _ _ _.__. . ... .. _._ i )y | ||
, - - . . - - - - . - 3 . | , - - . . - - - - . - 3 . | ||
l | l | ||
. 8 | . 8 | ||
?"e 4$ | ?"e 4$ | ||
- ',/,/ - | - ',/,/ - | ||
| Line 6,938: | Line 4,359: | ||
~. ,, 1 \ | ~. ,, 1 \ | ||
''f' | ''f' | ||
..,; Myz . | ..,; Myz . | ||
,'y4 4 Fyg | ,'y4 4 Fyg | ||
, / ; | , / ; | ||
@ . Jw ' | @ . Jw ' | ||
.e . .._ .. | .e . .._ .. | ||
a @ 6) % | a @ 6) % | ||
Mx af\ - ~ - ~ | Mx af\ - ~ - ~ | ||
Z ez. _ . _ . . . _ _ _ _ . _ . _ _ . | Z ez. _ . _ . . . _ _ _ _ . _ . _ _ . | ||
ex X | ex X Mx =._._. . - | ||
Mx =._._. . - | |||
TORSIONAL MOMENT inch # | TORSIONAL MOMENT inch # | ||
Myz = VMy'+ Mz' = BENDING MOMENT inch ti EX = | Myz = VMy'+ Mz' = BENDING MOMENT inch ti EX = | ||
= AxlL FORCE N Fyz = VFy' + Fr * = LATERAL FORCE # | |||
= AxlL FORCE N | tg4M = My/Mz = >dM Dee, tg4F = Fy/ Fz = >4F Des. | ||
Fyz = VFy' + Fr * = LATERAL FORCE # | |||
tg4M = My/Mz = >dM Dee, | |||
tg4F = Fy/ Fz = >4F Des | |||
FI G. 42 a b .. | FI G. 42 a b .. | ||
6 4 | 6 4 | ||
A n | A n | ||
O 4 | |||
O | |||
4 | |||
APPENDIX A ANSI Primary pressure rating, materials and dimensions for Nuclear Piping. | APPENDIX A ANSI Primary pressure rating, materials and dimensions for Nuclear Piping. | ||
O . | O . | ||
J l | |||
l t | |||
J | 1 O l l | ||
O l l | |||
l l | l l | ||
. t 1ABLE 1 900 LBS ANSI PRESSURE RATING CARBON STEEL PIPING SYSTEMS O | |||
. t | ASIM Trem Size Ratine Tvoc~ Socciffeation Pipe 3" and Smaller Sch 160 Seamless - | ||
A106 Gr. | A106 Gr. | ||
* 4" thru 10" SCH 120 Seamless A106 Gr. B | * 4" thru 10" SCH 120 Seamless A106 Gr. B | ||
| Line 7,021: | Line 4,392: | ||
Valves 2" and Smaller 1500 lbs. SW' A105 | Valves 2" and Smaller 1500 lbs. SW' A105 | ||
* all 2 1/2" thru 24" 900 lbs. BW A216 Gr. WCB* | * all 2 1/2" thru 24" 900 lbs. BW A216 Gr. WCB* | ||
Types | Types Fittings 2" and. Smaller 6000 lbs. SW A234 Gr. WPB* | ||
2 1/2" and 10" Match pipe wall BW A234 Gr. WPB* | 2 1/2" and 10" Match pipe wall BW A234 Gr. WPB* | ||
12"' thru 14" Sch 100 BW A234 Gr. WPB* | 12"' thru 14" Sch 100 BW A234 Gr. WPB* | ||
,16" and Larger Sch 80 BW A234 C;r. WPB* | ,16" and Larger Sch 80 BW A234 C;r. WPB* | ||
() - | () - | ||
F1&nge 2" and Smaller 2 1/2" and Larger 1500 Lbs. | F1&nge 2" and Smaller 2 1/2" and Larger 1500 Lbs. | ||
| Line 7,032: | Line 4,401: | ||
SW, RF WN, RF A105* | SW, RF WN, RF A105* | ||
A105* | A105* | ||
( | ( | ||
Bolts Bolt Studs A193 Gr. B7* | Bolts Bolt Studs A193 Gr. B7* | ||
Nuts Hex A194 Gr. 2H3 Class Gaskets Flexitallic Style CG | Nuts Hex A194 Gr. 2H3 Class Gaskets Flexitallic Style CG | ||
* For ASME Code Class I the materials must be impact tested per NB-2300 at a temperature of +10 F O | * For ASME Code Class I the materials must be impact tested per NB-2300 at a temperature of +10 F O | ||
e | e | ||
TABLE 2 900 LBS' ANSI PRESSURE RATING STAINIESS STEEL PIPING SYSTEMS ASTM Item Size Ratine Tvoe Soecification PIPE 2" and Smaller Sch 160 S Seamless A312 TP304 2 1/2" and 3" Sch 160 S Seamless A376 TP304 4" and thru 6 " Sch 120 S or Seamweld A358 TP304 8" thru 24" Sch 100 S Valves 2" and Smaller 1500 lbs. SW A182 Gr. F304 , | |||
all 2 1/2" and Larger 900 Lbs. BW A351 Gr. CF8M Types Fittings 2" and. Smaller 3000 Lbs. SW A182 Gr. F304 2 1/2" and 3" Sch 160 S BW A403 Gr. WP304 4" thru 6" Sch 120 S BW A403 Gr. WP304 ' | |||
TABLE 2 | |||
900 LBS' ANSI PRESSURE RATING STAINIESS STEEL PIPING SYSTEMS | |||
ASTM Item Size Ratine Tvoe Soecification PIPE 2" and Smaller Sch 160 S Seamless A312 TP304 2 1/2" and 3" Sch 160 S Seamless A376 TP304 4" and thru 6 " Sch 120 S or Seamweld A358 TP304 8" thru 24" Sch 100 S Valves 2" and Smaller 1500 lbs. SW A182 Gr. F304 , | |||
all 2 1/2" and Larger 900 Lbs. BW A351 Gr. CF8M | |||
Types Fittings 2" and. Smaller 3000 Lbs. SW A182 Gr. F304 2 1/2" and 3" Sch 160 S BW A403 Gr. WP304 4" thru 6" Sch 120 S BW A403 Gr. WP304 ' | |||
8" thru 24" Sch 100 S BW A403 Gr. WP304 | 8" thru 24" Sch 100 S BW A403 Gr. WP304 | ||
~ | ~ | ||
(:)- l g Flanges 2" and Smaller 1500 lbs. SW, R.F. A182 Gr. F304 ) | (:)- l g Flanges 2" and Smaller 1500 lbs. SW, R.F. A182 Gr. F304 ) | ||
~ | ~ | ||
2 1/2" and Larger 903 Lbs. WN, R.F. A182 Gr. F304 1 Bolts Bolt Studs A193 GR. B7 l | |||
2 1/2" and Larger 903 Lbs. WN, R.F. A182 Gr. F304 1 | , l l | ||
Nuts Hex A194 Gr. 2H. | |||
Bolts Bolt Studs A193 GR. B7 l | l Gaskets Flexitallic Style CG O | ||
, l | d | ||
l | |||
Gaskets Flexitallic Style CG | |||
I TABLE 3 ) | I TABLE 3 ) | ||
l l | l l | ||
| Line 7,086: | Line 4,425: | ||
~~ | ~~ | ||
,.. .. \ | ,.. .. \ | ||
Pipe 3" and Smaller Sch 160- Seamless A106 Gr. B 4" and Larger l Sch 80 Seamless A106 Gr. B Valves 2" and Smaller 600 lbs. SW A105 all 2 1/2" and larger 600 lbs. BW A216 Gr. WCB | Pipe 3" and Smaller Sch 160- Seamless A106 Gr. B 4" and Larger l Sch 80 Seamless A106 Gr. B Valves 2" and Smaller 600 lbs. SW A105 all 2 1/2" and larger 600 lbs. BW A216 Gr. WCB Fittings 2" and Smaller 3000 Lbs SW A234 Gr. B l | ||
Fittings 2" and Smaller 3000 Lbs SW A234 Gr. B l | |||
. 2 1/2"*thru 3" | . 2 1/2"*thru 3" | ||
* Sch 160 BW A234 Gr. B 4" and larger Sch 80 BW A234 Gr. B | * Sch 160 BW A234 Gr. B 4" and larger Sch 80 BW A234 Gr. B Flanges 2" and Smaller 600 Lbs SW, R.F. A105 - | ||
Flanges 2" and Smaller 600 Lbs SW, R.F. A105 - | |||
21/2" and larger 600 Lbs BW, R.F. A105 Bolting , | 21/2" and larger 600 Lbs BW, R.F. A105 Bolting , | ||
Bolt Studs A193 Gr. B7 Nuts Hex A194 Gr. 2H,' | Bolt Studs A193 Gr. B7 Nuts Hex A194 Gr. 2H,' | ||
Gaskets Flexitallic Style CG | Gaskets Flexitallic Style CG 4 | ||
4 | |||
9 | 9 | ||
.O- | .O- | ||
; 6 l | |||
; 6 | l - | ||
- l | - l | ||
TABLE 4 rQ . | |||
600 LBS ANSI PRESSURE RATING STAINLESS STEEL PIPING SYSTEMS ASIM Iten Size Ratine Tvoe Sneciffeation Pipe 2" and Smaller Sch 80 S Seamless A312 TP304 2 1/2" thru 12" Sch 80 S Seamless or A376 TP304 or 14" and larger Sch 60 S Seamweld A358 TP304 Valves 2" and Smaller 600 lbs. SW A182 Gr. F316 all 21/2" and larger 600 Lbs. BW A351 Gr. .CF8;; | |||
600 LBS ANSI PRESSURE RATING STAINLESS STEEL PIPING SYSTEMS | |||
ASIM Iten Size Ratine Tvoe Sneciffeation Pipe 2" and Smaller Sch 80 S Seamless A312 TP304 | |||
2 1/2" thru 12" Sch 80 S Seamless or A376 TP304 or 14" and larger Sch 60 S Seamweld A358 TP304 Valves 2" and Smaller 600 lbs. SW A182 Gr. F316 all 21/2" and larger 600 Lbs. BW A351 Gr. .CF8;; | |||
Sizes | Sizes | ||
. Fittings 2" and Smaller 3000 Lbs. SW A182 Gr. F304 2 1/2"'thru 12" Sch 80 S BW A403 Gr. WP304 14" and larger Sch 60 S BW A403 Gr. WP304 0 - . | . Fittings 2" and Smaller 3000 Lbs. SW A182 Gr. F304 2 1/2"'thru 12" Sch 80 S BW A403 Gr. WP304 14" and larger Sch 60 S BW A403 Gr. WP304 0 - . | ||
( Flanges 2" and Smaller 600 lbs. SW, R.F. A182 Gr. F316 | ( Flanges 2" and Smaller 600 lbs. SW, R.F. A182 Gr. F316 21/2" au1 Iarger 600 Lbs. WN, R.F. A182 Gr. F316 Bolting Bolt Studs A193 Gr. B7 Nuts Rex A194, Gr. 2H, Gaskets Flexitallic Style CG e | ||
21/2" au1 Iarger 600 Lbs. WN, R.F. A182 Gr. F316 Bolting Bolt Studs A193 Gr. B7 | |||
Nuts Rex A194, Gr. 2H, | |||
Gaskets Flexitallic Style CG | |||
e | |||
O. | O. | ||
IABLE 5 300 LBS ANSI PRESSUPI RATING CARBON STEEL PIPING SYSTDIS Item ASIM Size Ratine Tvoo Snecification Pipe 2" and Smaller Sch 80 Seamless A106 Gr. B 2 1/2" and Large r Sch 40 Seamless A10s Gr. B Valves 2" and Smaller 600 Lbs. SW A105 all 2 1/2" and Larger 300 lbs. BW A216 Gr. WCB | |||
IABLE 5 | |||
300 LBS ANSI PRESSUPI RATING CARBON STEEL PIPING SYSTDIS | |||
Item ASIM Size Ratine Tvoo Snecification Pipe 2" and Smaller Sch 80 Seamless | |||
A106 Gr. B 2 1/2" and Large r Sch 40 Seamless A10s Gr. B Valves 2" and Smaller 600 Lbs. SW A105 all 2 1/2" and Larger 300 lbs. BW A216 Gr. WCB | |||
, Types Fittings 2" and smaller 3000 lbs SW A234 Gr. B 2 1/2" and Larger Sch 40 BW A234 Gr. B | , Types Fittings 2" and smaller 3000 lbs SW A234 Gr. B 2 1/2" and Larger Sch 40 BW A234 Gr. B | ||
) Flanges 2" and Smaller 300 Lbs. Sw, R.F. A105 2 1/2" ar.4 Larger 300 lbs. WN, R. F. A105 Bolting Bolt Studs A193 Gr. B7 Nuts Hex A194 Gr. 2H | ) Flanges 2" and Smaller 300 Lbs. Sw, R.F. A105 2 1/2" ar.4 Larger 300 lbs. WN, R. F. A105 Bolting Bolt Studs A193 Gr. B7 Nuts Hex A194 Gr. 2H Gaskets Flexitallic** | ||
Gaskets Flexitallic** | |||
Style CG | Style CG | ||
** For non-nuclear piping systems (Group 't") use 1/16" cranite rings (ANSI B31.I). | ** For non-nuclear piping systems (Group 't") use 1/16" cranite rings (ANSI B31.I). | ||
9 e | 9 e | ||
i 1 | |||
TABLE 6 l | TABLE 6 l | ||
; | ; | ||
O - - | O - - | ||
| Line 7,176: | Line 4,459: | ||
300 LBS ANSI PRESSURE RATING STAINLESS STEEL PIPING SYSID1S | 300 LBS ANSI PRESSURE RATING STAINLESS STEEL PIPING SYSID1S | ||
: s. ASIM Item Size Ratine Tvoo , | : s. ASIM Item Size Ratine Tvoo , | ||
Specification Pipe 2" and Smaller Sch 40S Seamless A312 Gr. TP304 2 1/2" thru 10" Seamless or A376 Gr. TP304 c | Specification Pipe 2" and Smaller Sch 40S Seamless A312 Gr. TP304 2 1/2" thru 10" Seamless or A376 Gr. TP304 c Sch 40S 12" and Larger Std 3/8" Wall Seamwelded A358 Gr. TP304 Valves 2" and Smaller 300 Lbs SW' A182 Gr. F316 all 2 1/2" and larger 300 Lbs BW A351 Gr. CF8M Types Fittings 2" and Smaller | ||
Sch 40S 12" and Larger Std 3/8" Wall Seamwelded A358 Gr. TP304 Valves 2" and Smaller 300 Lbs SW' A182 Gr. F316 all 2 1/2" and larger 300 Lbs BW A351 Gr. CF8M Types Fittings 2" and Smaller | |||
* 2000 Lbs SW A182 Gr. F304 | * 2000 Lbs SW A182 Gr. F304 | ||
) | ) | ||
2 1/2"'thru.10" Sch 40S BW A403 Gr. WP304 12" and Iarger Std 3/8" Wall BW A403 Gr. WP304 | 2 1/2"'thru.10" Sch 40S BW A403 Gr. WP304 12" and Iarger Std 3/8" Wall BW A403 Gr. WP304 | ||
~ ~~ | ~ ~~ | ||
O Flanges 2" and Smaller 300 Lbs. SW, R.F. A182 Gr. F316 | O Flanges 2" and Smaller 300 Lbs. SW, R.F. A182 Gr. F316 | ||
( , | ( , | ||
21/2" and larger 300 Lbs. WN, R.F. A182 Gr. F316 Bolting Bolt Studs A193 Gr. B7 | 21/2" and larger 300 Lbs. WN, R.F. A182 Gr. F316 Bolting Bolt Studs A193 Gr. B7 Nuts Hex A194Gr.2N' Gaskets Flexitallic Style CG | ||
Nuts Hex A194Gr.2N' Gaskets Flexitallic Style CG | |||
. O. | . O. | ||
I | I | ||
l 1 | |||
l | 1 TABLE 7 O - | ||
150 LBS ANSI PRESSURE RATING CARBON STEEL PIPING SYSTEMS ASDi Item Size Ratine Tvoe Soecification Pipe 2" and Smaller Sch 80 Seamless A106 Gr. B 2 1/2" thru 10" Sch 40 Seamless A106 Gr. B 12" thru 24" Std 3/8" Wall Seamless A106 Gr. B 26" and larger Std 3/8" Wall Welded A155 Gr. KCF 70 | |||
* Valves 2" and Smaller 600 Lbs. SW A105 all 2 1/2" and Larger 150 Lbs. BW A216 Gr. WCB Types Fittings 2" and' Smaller 3000 Lbs SW A234 Gr. B 2 1/2" thru 10" Sch 40 BW A234 Gr. B ! | |||
TABLE 7 | |||
O - | |||
150 LBS ANSI PRESSURE RATING CARBON STEEL PIPING SYSTEMS ASDi Item Size Ratine Tvoe Soecification Pipe 2" and Smaller Sch 80 Seamless A106 Gr. B | |||
2 1/2" thru 10" Sch 40 Seamless A106 Gr. B 12" thru 24" Std 3/8" Wall Seamless A106 Gr. B 26" and larger Std 3/8" Wall Welded A155 Gr. KCF 70 | |||
* Valves 2" and Smaller 600 Lbs. SW A105 all 2 1/2" and Larger 150 Lbs. BW A216 Gr. WCB Types | |||
Fittings 2" and' Smaller 3000 Lbs SW A234 Gr. B 2 1/2" thru 10" Sch 40 BW A234 Gr. B ! | |||
12" and Larger Std 3/8" Wall BW A234 Gr. B 1 l | 12" and Larger Std 3/8" Wall BW A234 Gr. B 1 l | ||
. . , . i | . . , . i O " | ||
O " | |||
Flanges 2" and Smaller 150 Lb. SW,I.F. . A105 1 | Flanges 2" and Smaller 150 Lb. SW,I.F. . A105 1 | ||
( , | ( , | ||
2 1/2" and Larger 150 Lb. WN, R.F. A105 Bolts , | 2 1/2" and Larger 150 Lb. WN, R.F. A105 Bolts , | ||
Bolt Studs A193 Gr. B7 | Bolt Studs A193 Gr. B7 Nuts Hex A194 2H Gaskets FlexItal1 Ic ** | ||
Nuts Hex A194 2H Gaskets FlexItal1 Ic ** | |||
Style CG | Style CG | ||
* Butterfly valves 4" and larger also used within this pressure range. | * Butterfly valves 4" and larger also used within this pressure range. | ||
** For non-nuclear piping systems (Group "D) use 1/16" cranite rings (ANSI B31.1). | ** For non-nuclear piping systems (Group "D) use 1/16" cranite rings (ANSI B31.1). | ||
O. - | O. - | ||
I | I | ||
TABI2 8 | TABI2 8 | ||
. 150 LBS ANSI PRESSURE - RATING STAINLESS STEEL PIPING SYSEMS AS'Di . | . 150 LBS ANSI PRESSURE - RATING STAINLESS STEEL PIPING SYSEMS AS'Di . | ||
Item Size Ratine Tvoe Soecificotfor Pipe 2" and Smaller Sch 40S Seamless A312 TP304 2 1/2" thru 12" Sch 10S Seamless or 4376 TP304 or 14" and larger Sch 10S Seamwelded A358 TP304 Valves 2" and Smaller 150 lbs. SW. A351 Gr. CF8M all 2 1/2" and Larger 150 Lbs. BW A351 Gr. CF8M Types Fittings 2" and Smaller 2000 Lbs SW A182 Gr. F304 | Item Size Ratine Tvoe Soecificotfor Pipe 2" and Smaller Sch 40S Seamless A312 TP304 2 1/2" thru 12" Sch 10S Seamless or 4376 TP304 or 14" and larger Sch 10S Seamwelded A358 TP304 Valves 2" and Smaller 150 lbs. SW. A351 Gr. CF8M all 2 1/2" and Larger 150 Lbs. BW A351 Gr. CF8M Types Fittings 2" and Smaller 2000 Lbs SW A182 Gr. F304 | ||
. 2 1/2" and Larger Sch.10S BW A403 Gr. WP 304 | . 2 1/2" and Larger Sch.10S BW A403 Gr. WP 304 O Flanges 2" and Smaller 150 Lbs SW, R.F. A182 Gr'. F316 l | ||
O Flanges 2" and Smaller 150 Lbs SW, R.F. A182 Gr'. F316 l | |||
( 21/2" and larger 150 lbs WN, R. F. A182 Gr. F316 i | ( 21/2" and larger 150 lbs WN, R. F. A182 Gr. F316 i | ||
Bolting Bolt Studs A193 Gr. B7 e . | |||
Bolting Bolt Studs | Nuts Hex A194 Gr. '2H Gaskets Flexitallic Style CG , | ||
1 O. | |||
4 e | |||
A193 Gr. B7 | |||
Nuts Hex A194 Gr. '2H | |||
Gaskets Flexitallic Style CG , | |||
1 | |||
O. | |||
4 | |||
e | |||
. TABII 9 900 LBS ANSI PRESSURE RATING, CARSON STEEL PIPING SYSTEMS (BRITILE FRACTURE CONTROL) | |||
. TABII 9 | |||
900 LBS ANSI PRESSURE RATING, CARSON STEEL PIPING SYSTEMS (BRITILE FRACTURE CONTROL) | |||
"SIM A - | "SIM A - | ||
Item Size Ratine Tvoe Soccificatior Pipe- 3" and Smaller Sch 160 Seamlers A333 Gt . 6 4" thru 10" Sch 120 Seamless A333 Gr. 6* ! | Item Size Ratine Tvoe Soccificatior Pipe- 3" and Smaller Sch 160 Seamlers A333 Gt . 6 4" thru 10" Sch 120 Seamless A333 Gr. 6* ! | ||
12" thru 14" Sch 100 A333 Gr. 6* 1 16" and larger Sch 80 ** - A333 Gr. 6* l | 12" thru 14" Sch 100 A333 Gr. 6* 1 16" and larger Sch 80 ** - A333 Gr. 6* l | ||
. L_ | . L_ | ||
Vilves 2" and Smaller 1500 Lbs SW A350 Gr. LF2 ' | Vilves 2" and Smaller 1500 Lbs SW A350 Gr. LF2 ' | ||
s.nd 2 1/2" and larger 900 Lbs BW A352 Gr. LCB Types - | s.nd 2 1/2" and larger 900 Lbs BW A352 Gr. LCB Types - | ||
or A216 Gr. WCC Fittings 2" and Smaller 6000 Lbs SW A420 Gr. WPL 2 1/2" thru.10" March pipe wall BW A420 Gr. WPI 12" thru 14" Sch 100 3W A420 Gr. WPI | or A216 Gr. WCC Fittings 2" and Smaller 6000 Lbs SW A420 Gr. WPL 2 1/2" thru.10" March pipe wall BW A420 Gr. WPI 12" thru 14" Sch 100 3W A420 Gr. WPI 16" and Larger Sch 80** BW A420 Gr. WP1 Flanges 2" and Smaller 1500 Lbs SW, R.F. A350 Gr. LF2 I 2 1/2" and larger 900 Lbs. WN, R.F. A350 Gr. LF2 Bolts 1" Dia and Smaller Bolt Studs A193 Gr. B7 1 1/8" and larger Bolt Studs A320 Gr. L7* | ||
16" and Larger Sch 80** BW A420 Gr. WP1 | |||
Flanges 2" and Smaller 1500 Lbs SW, R.F. A350 Gr. LF2 I 2 1/2" and larger 900 Lbs. WN, R.F. A350 Gr. LF2 Bolts 1" Dia and Smaller Bolt Studs A193 Gr. B7 1 1/8" and larger Bolt Studs A320 Gr. L7* | |||
Nuta 2" and Smaller Hex A194 Gr. 2H Gaskets Flexitallic Style CG | Nuta 2" and Smaller Hex A194 Gr. 2H Gaskets Flexitallic Style CG | ||
* Materials must be impact tested per ASME Code Section III, Article NB-2300 at a temperature of (-) 200F. | |||
* Materials must be impact tested per ASME Code Section III, | |||
Article NB-2300 at a temperature of (-) 200F. | |||
I | I | ||
** 20" Feedwater system piping to be schedule 100 , | ** 20" Feedwater system piping to be schedule 100 , | ||
-'- ' - ~ ~ ~ ~ | -'- ' - ~ ~ ~ ~ | ||
. l '- | . l '- | ||
~ ~ | ~ ~ | ||
TABLE 10 O f 1500 LBS ANSI PRESSURE RATING STAIN 1ESS SIEEL PIPING SYSTEMS ASIM Item Size Ratin? Tvee Soecification Pipe 2" and Smaller Sch 160 Seamless A312 TP304 2 1/2" and 3" Sch 160 Seamless or A376 TP304 Valves 2" and Smaller 1500 Lbs SW A182 Gr. 3N 2 1/2" and 3" 1500 lbs BW A351 Gr. CFI Fittings 2" and Smaller 3000 Lbs SW A182 Gr.304 2 1/2" and 3" Sch 160 LW A403 Gr. WP 304 | |||
TABLE 10 O f 1500 LBS ANSI PRESSURE RATING STAIN 1ESS SIEEL PIPING SYSTEMS | |||
ASIM Item Size Ratin? Tvee Soecification Pipe 2" and Smaller Sch 160 Seamless A312 TP304 2 1/2" and 3" Sch 160 Seamless or A376 TP304 | |||
Valves 2" and Smaller 1500 Lbs SW A182 Gr. 3N 2 1/2" and 3" 1500 lbs BW A351 Gr. CFI Fittings 2" and Smaller 3000 Lbs SW A182 Gr.304 2 1/2" and 3" Sch 160 LW A403 Gr. WP 304 | |||
..3 k , | ..3 k , | ||
Flanges 2" and Smaller 1500 lbs SW, R.F. A182 Gr.304 | Flanges 2" and Smaller 1500 lbs SW, R.F. A182 Gr.304 2 1/2" and 3" 1500 lbs BW, R.F. A182 Gr. 304 1 | ||
2 1/2" and 3" 1500 lbs BW, R.F. A182 Gr. 304 1 | |||
Bolts . | Bolts . | ||
Bolts, Studs A193 Gr. B7 l | Bolts, Studs A193 Gr. B7 l 1 | ||
1 | |||
1 Nuts Hex -A194 Gr. 2H i | 1 Nuts Hex -A194 Gr. 2H i | ||
Gaskets Flexital.lic Style CG l e | |||
Gaskets Flexital.lic Style CG l | |||
e | |||
D - | D - | ||
t | t | ||
,; e.. | ,; e.. | ||
. .. v.. . a.s, | . .. v.. . a.s, | ||
.. ;: . .C w e - | .. ;: . .C w e - | ||
.:.2.x..:a:- | .:.2.x..:a:- | ||
-W~ ,=.1 .f , - | -W~ ,=.1 .f , - | ||
OCUWNT CONTR01 | OCUWNT CONTR01 n. | ||
n. | |||
. - - . .. . . 2. .s. | . - - . .. . . 2. .s. | ||
3oW-e .w-n.+s7, | 3oW-e .w-n.+s7, x . | ||
x | |||
; lllC . | ; lllC . | ||
, NUCLEAR SAFETY RELATCD | , NUCLEAR SAFETY RELATCD AUG5 1977 | ||
AUG5 1977 | |||
. a, | . a, | ||
.s. :: ~ -- | .s. :: ~ -- | ||
| Line 7,369: | Line 4,538: | ||
. - .c. . | . - .c. . | ||
rma swus F . | rma swus F . | ||
C. | C. | ||
,s ., | ,s ., | ||
)_ _ - | )_ _ - | ||
CO.- | CO.- | ||
LTR. NO. A | LTR. NO. A | ||
;*= | ;*= | ||
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e | e J ' .- | ||
J ' .- | |||
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.t.w-., .we..=..,. | .t.w-., .we..=..,. | ||
. . .. ;. . - . SMALL-PIPING DESIGN STANDARD . | . . .. ;. . - . SMALL-PIPING DESIGN STANDARD . | ||
e.u. .': . c . . w . . - . . | e.u. .': . c . . w . . - . . | ||
TU,. | TU,. | ||
,, . '.F;.NRICO FERMI ATOMIC POWER PLANT - U,IVIT 2 | ,, . '.F;.NRICO FERMI ATOMIC POWER PLANT - U,IVIT 2 3 | ||
3 | |||
g . s s | g . s s | ||
3 . 9, | 3 . 9, | ||
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i - | i - | ||
ry.c.-- *~. .Wy: : ' * .- -' | ry.c.-- *~. .Wy: : ' * .- -' | ||
B, .M. | B, .M. | ||
N. ,. '. e M Y.M,.. . y . . REPORT PREPARED FOR ;:..: m;:-- - - - - - | N. ,. '. e M Y.M,.. . y . . REPORT PREPARED FOR ;:..: m;:-- - - - - - | ||
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, w . | , w . | ||
v.e.; p:.TM% @,OETROIT4DISON COM P.A. N Y m.. .. . n m m . | |||
.n 7.. W. 1 m : | |||
v.e.; p:.TM% @,OETROIT4DISON COM P.A. N | |||
Y m.. .. . n m m | |||
.n | |||
7.. W. 1 m : | |||
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..,:.. w | |||
n..w w g W s.m. - | |||
: v. . . . , . . . . . ..:.n. sn. ., .,.. ,,., | : v. . . . , . . . . . ..:.n. sn. ., .,.. ,,., | ||
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N. . . N.,'/., 3 4..?.3.T W P:,w . p.it';.WA".-r.-we F Md. .wp.U .y..h.s.,.w..t.v.e.#.r | N. . . N.,'/., 3 4..?.3.T W P:,w . p.it';.WA".-r.-we F Md. .wp.U .y..h.s.,.w..t.v.e.#.r | ||
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y, f,y;g . . | |||
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M''*ij:yMQ'P'%,.yW$f*M,'V.w *Q'Q ;. ' 'b. '. a. . . .. w ' .;s D W m ,G ' X W w .T- | M''*ij:yMQ'P'%,.yW$f*M,'V.w *Q'Q ;. ' 'b. '. a. . . .. w ' .;s D W m ,G ' X W w .T- | ||
& '' 0 W[:2R..W . 7''.= :%r::'ER!i.#12:nWNN D. f.i N.k W:h',hk:&. | & '' 0 W[:2R..W . 7''.= :%r::'ER!i.#12:nWNN D. f.i N.k W:h',hk:&. | ||
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| Line 7,554: | Line 4,622: | ||
4 .. | 4 .. | ||
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NUCLEAR SAFETY RELATED O | NUCLEAR SAFETY RELATED O | ||
SMALL PIPING DESIGN STANDARD ENRICO FliRMI ATOMIC POWER PLANT - UNIT 2 REPORT PREPARED FOR DETROIT EDISON COMPANY O | SMALL PIPING DESIGN STANDARD ENRICO FliRMI ATOMIC POWER PLANT - UNIT 2 REPORT PREPARED FOR DETROIT EDISON COMPANY O | ||
REPORT SL-3150 REVISION 1, JULY 29,19T, SA" GENT &LUNDY O ~~~~~~~ - | |||
REPORT SL-3150 REVISION 1, JULY 29,19T, | |||
SA" GENT &LUNDY O ~~~~~~~ - | |||
- a | - a | ||
O TABLE OF CONTENTS Rev.1, 7-29-77 PAGE I INTRODUCTION 1 | O TABLE OF CONTENTS Rev.1, 7-29-77 PAGE I INTRODUCTION 1 | ||
A. Description B. Relationship to ASME Code Requirements C. Scope II DESIGN PRINCIPLES 2 i A. General I | A. Description B. Relationship to ASME Code Requirements C. Scope II DESIGN PRINCIPLES 2 i A. General I | ||
B. Weight Analysis O C. Dermal Analysis | B. Weight Analysis O C. Dermal Analysis D. Seismic Analysis III ASME CODE REQUIREMENTS l | ||
7 i A. Sustained Losds i | |||
D. Seismic Analysis III ASME CODE REQUIREMENTS | 1 B. Occasional Loads C. Dermal Expansion IV CONCLUSION 11 A. Stresses B. Nozzle Loads O | ||
1 B. Occasional Loads C. Dermal Expansion IV CONCLUSION 11 A. Stresses | |||
B. Nozzle Loads O | |||
11 SL-3159 | 11 SL-3159 | ||
Rev.1, 7-29-77 V REFERENCES 14 APPENDICES Appendix A - Calculations and Equation Derivations Appendix B - Weight Support System Design Appendix C - Seismic Support System Design i | Rev.1, 7-29-77 V REFERENCES 14 APPENDICES Appendix A - Calculations and Equation Derivations Appendix B - Weight Support System Design Appendix C - Seismic Support System Design i | ||
Appendix D - Flexibility Support System Design Appendix E - Small Piping Design Worksheet | Appendix D - Flexibility Support System Design Appendix E - Small Piping Design Worksheet t | ||
O l | |||
1 s | |||
O 111 SL-3159 l TL | |||
111 SL-3159 | |||
l TL | |||
. -..~ __ _. . - _ _ . _ . . . . _ . . _ - - - - - - - | . -..~ __ _. . - _ _ . _ . . . . _ . . _ - - - - - - - | ||
SARGENT & LUNDY ENGINEERS cmcac Rev.1, 7-29-77 O SMAU_ MPING DESIGN STANDARD ENRICO FERMI ATOMIC POWER PLANT - UNIT 2 DETROIT EDISON COMPANY I INTRODUCTION A. Description The Small-Piping Design Standard presents genc al guidelines and specific rules which are to be applied to the design of piping subsystems to locate weight i supports and seismic restraints and to guarantee adequate flexibility for 1 accommodation of thermal expansion and anchor movements. De recommenda- ! | SARGENT & LUNDY ENGINEERS cmcac Rev.1, 7-29-77 O SMAU_ MPING DESIGN STANDARD ENRICO FERMI ATOMIC POWER PLANT - UNIT 2 DETROIT EDISON COMPANY I INTRODUCTION A. Description The Small-Piping Design Standard presents genc al guidelines and specific rules which are to be applied to the design of piping subsystems to locate weight i supports and seismic restraints and to guarantee adequate flexibility for 1 accommodation of thermal expansion and anchor movements. De recommenda- ! | ||
tions of the standard are based on weight, thermal expansion and seismic analysis i of simple beams, which represent elements of the piping subsystem. The assumptions used in the analyses insure conservative results: the estimates of stresses and loads for a given design environment exceed the values which could exist in the actual system. | tions of the standard are based on weight, thermal expansion and seismic analysis i of simple beams, which represent elements of the piping subsystem. The assumptions used in the analyses insure conservative results: the estimates of stresses and loads for a given design environment exceed the values which could exist in the actual system. | ||
| Line 7,872: | Line 4,797: | ||
_ ___ _ M | _ ___ _ M | ||
SARGENT a LUNDY ENGINEER $ | SARGENT a LUNDY ENGINEER $ | ||
occaco Rev.1, 7-29-77 O | occaco Rev.1, 7-29-77 O | ||
11 DESIGN PRINCIPLES A. General A piping system design represents a compromise t'etween two competing design' requirements: 1) the system must be adequately restrained to prevent overstress | 11 DESIGN PRINCIPLES A. General A piping system design represents a compromise t'etween two competing design' requirements: 1) the system must be adequately restrained to prevent overstress due to weight and seismic loads and; 2) it must be flexible enough to accommodate thermal expansion and nozzle movements. Unnecessary or poorly located restraints restrict thermal expansion and nozzle movements and so should be avoided, but enough restraints must be used to limit seismic and weight stresses to allowable values. Recommended spans for seismic and weight supports are given in the Tables of Appendices B and C. To increase the flexibility of a system in a given direction, pipe must be added perpendicular to that direction. The length of perpendicular pipe which is required to accommodate thermal expansion and nozzle movements under various conditions is given in the Tables of Appendix D. | ||
due to weight and seismic loads and; 2) it must be flexible enough to accommodate thermal expansion and nozzle movements. Unnecessary or poorly located restraints restrict thermal expansion and nozzle movements and so should be avoided, but enough restraints must be used to limit seismic and weight stresses to allowable values. Recommended spans for seismic and weight supports are given in the Tables of Appendices B and C. To increase the flexibility of a system in a given direction, pipe must be added perpendicular to that direction. The length of perpendicular pipe which is required to accommodate thermal expansion and nozzle movements under various conditions is given in the Tables of Appendix D. | |||
B. Weight Analysis | B. Weight Analysis | ||
'Ihe standard procedure for designing a weight support system .n colves the use of recommended span lengths to limit the weight-induced bending stress. The requirements of ASME Code may be satisfied by this approach even though the governing equations do not directly indicate an allowable weight stress level. | |||
'Ihe standard procedure for designing a weight support system .n colves the use of recommended span lengths to limit the weight-induced bending stress. The | |||
requirements of ASME Code may be satisfied by this approach even though the governing equations do not directly indicate an allowable weight stress level. | |||
It is only necessary to determine what fraction of the allowable combined stress the weight load should contribute. Recommenaed spans baseJ on this allowable stress can then be calculated by elementary bending theory (See Appendix A). | It is only necessary to determine what fraction of the allowable combined stress the weight load should contribute. Recommenaed spans baseJ on this allowable stress can then be calculated by elementary bending theory (See Appendix A). | ||
The span recommendations are listed in Tabic ". I cf Appah il for fluid filled and empty pipes. The effect of the weight of standard insulation for 300"F has also been considered. The recommended span length is given by span (ft) = d 2000Z _y l | The span recommendations are listed in Tabic ". I cf Appah il for fluid filled and empty pipes. The effect of the weight of standard insulation for 300"F has also been considered. The recommended span length is given by span (ft) = d 2000Z _y l | ||
l O | l O | ||
-i SL-3159 | -i SL-3159 | ||
{ | { | ||
| Line 7,900: | Line 4,818: | ||
As previously stated, flexibility in one direction is dependent upon the amount of pipe which is perpendicular to that direction. For instance, c component of nozzle movement in the X-direelion can be accommodated if the nozzle is separated from the first X-direction restraint by enough piping in the Y- and Z-directions (See Figure 1). | As previously stated, flexibility in one direction is dependent upon the amount of pipe which is perpendicular to that direction. For instance, c component of nozzle movement in the X-direelion can be accommodated if the nozzle is separated from the first X-direction restraint by enough piping in the Y- and Z-directions (See Figure 1). | ||
It is the bending stress in the perpenaicular legs, B and D, that must be examined. These may be conservatively modeled as a beam with guided ends subjected to a displacement, 6 ,(Sec Figure 2). The model is conservative since it ignores the flexibility of the elbows and imposes more rigid end conditions than the actual supports. | It is the bending stress in the perpenaicular legs, B and D, that must be examined. These may be conservatively modeled as a beam with guided ends subjected to a displacement, 6 ,(Sec Figure 2). The model is conservative since it ignores the flexibility of the elbows and imposes more rigid end conditions than the actual supports. | ||
SL-3159 | SL-3159 | ||
; L l | ; L l | ||
SARGENT c LUNDY ENGINEERS cmcaco REV.1. 7-29-77 A | |||
SARGENT c LUNDY ENGINEERS cmcaco REV.1. 7-29-77 | E | ||
~ | ~ | ||
g s '/ | g s '/ | ||
C 1, | C 1, | ||
/B D jt | /B D jt | ||
| Line 7,919: | Line 4,831: | ||
I | I | ||
: s. K H I- H l- l I | : s. K H I- H l- l I | ||
c- x l l | c- x l l | ||
l ; | l ; | ||
/ | / | ||
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FIGURE 2 i | FIGURE 2 i | ||
y/: m O itthe etio edie stressis isooo psi the2easta or erneaaieuiereine n re9uiredto accommodate the component of nozzle movement is 1 1 = 1245 r. r. = outside radius - | y/: m O itthe etio edie stressis isooo psi the2easta or erneaaieuiereine n re9uiredto accommodate the component of nozzle movement is 1 1 = 1245 r. r. = outside radius - | ||
'Ihe recommended lengths for various values of 6 and r. are listed in Table D-1 | 'Ihe recommended lengths for various values of 6 and r. are listed in Table D-1 | ||
; | ; | ||
| Line 7,941: | Line 4,847: | ||
1 See Appendix A for derivations of the equations in this section. | 1 See Appendix A for derivations of the equations in this section. | ||
D* | D* | ||
O - | O - | ||
]D *]D | ]D *]D | ||
| Line 7,947: | Line 4,852: | ||
SL-3159 1 | SL-3159 1 | ||
SARGENT c LUNDY ENGINEER 5 cmcaco REV. 1, 7-29-77 2 25 | SARGENT c LUNDY ENGINEER 5 cmcaco REV. 1, 7-29-77 2 25 | ||
(, | (, | ||
''1 11 t | ''1 11 t | ||
2 05 7 | 2 05 7 | ||
6 1 85 | 6 1 85 5 | ||
( 58 1.65 . | |||
5 | |||
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4 n | 4 n | ||
-4 1.45 l | -4 1.45 l O I 1.25 . . | ||
3 t | |||
0 'l s 1.05 . | |||
O I | |||
1.25 . . | |||
3 | |||
19 I . | 19 I . | ||
18 0.85 | |||
\ L'Q | \ L'Q | ||
.5 2!3 s4 '; A 7 0.0 0.5 10 1.5 2.0 25 DEFLECTION FIGURE 3 O. OFFSET REQUIRED TO ACCOMMODATE NOZZLE MOVEMENTS SL-3159 | .5 2!3 s4 '; A 7 0.0 0.5 10 1.5 2.0 25 DEFLECTION FIGURE 3 O. OFFSET REQUIRED TO ACCOMMODATE NOZZLE MOVEMENTS SL-3159 w | ||
w | |||
SARGENT a LUNDY EN[NEERs REV 1, 7-29-77 4 | SARGENT a LUNDY EN[NEERs REV 1, 7-29-77 4 | ||
p*----...,,__ 9_uide i f | p*----...,,__ 9_uide i f l | ||
FIGURE 4 r7777 The length of pipe required to accommodate the expansion of the length t' , is 1 = 1.475 Y t r. Values for various lengths and radii are listed in Table D-2 of Appendix D. If nozzle movement and pipe expansion occur simultaneously, the total length of perpendicular pipe required is the sum of the lengths required for l | |||
1 = 1.475 Y t r. Values for various lengths and radii are listed in Table D-2 of Appendix D. If nozzle movement and pipe expansion occur simultaneously, the total length of perpendicular pipe required is the sum of the lengths required for l | |||
each. ' | each. ' | ||
D. Seismic Analysis An adequate number of properly located restraints must be provided to limit the stress and deflection due to seismic excitation to allowable values. Location of supports requires determination of the maximum span (distance between parallel restraints) in each direction, for which the system response is acceptable. To assure satisfaction of ASME Code requiremen's a response shall be considered 2 | D. Seismic Analysis An adequate number of properly located restraints must be provided to limit the stress and deflection due to seismic excitation to allowable values. Location of supports requires determination of the maximum span (distance between parallel restraints) in each direction, for which the system response is acceptable. To assure satisfaction of ASME Code requiremen's a response shall be considered 2 | ||
acceptable if the total stress ( x2y22)l due to bending and torsional moments does not exceed 7000 psi for OBE an,d 14,000 psi for SSE, and the total deflection ( x +y +z) does not exceed two inches. | acceptable if the total stress ( x2y22)l due to bending and torsional moments does not exceed 7000 psi for OBE an,d 14,000 psi for SSE, and the total deflection ( x +y +z) does not exceed two inches. | ||
; | ; | ||
To estimate a system's seismic response it is assumed thrit each section of pipe l | To estimate a system's seismic response it is assumed thrit each section of pipe l 3 | ||
between two parallel restraints acts as a simple beam. For the deflection - | |||
estimate the beam is assumed to be simply supported and for the natural frequency estimate it is assumed to have one fixed and one simply supported end. - | estimate the beam is assumed to be simply supported and for the natural frequency estimate it is assumed to have one fixed and one simply supported end. - | ||
This assures a conservative estimate of the respor.se. | This assures a conservative estimate of the respor.se. | ||
O SL-3159 | O SL-3159 I | ||
l' | |||
SARGENT & LUNDY ENGINEERS Rev.1, 7-29-77 O Using the assumed model, seismic deflection versus span length curves are generated. These are based on appropriatt response acceleration spectra. | SARGENT & LUNDY ENGINEERS Rev.1, 7-29-77 O Using the assumed model, seismic deflection versus span length curves are generated. These are based on appropriatt response acceleration spectra. | ||
Superimposed on each deflection ( x, y, z) versus span curve is a curve which indicates the deflection at which the stress for each span is 4000 psi. The intersection of these curves indicates the longest span for which the anticipated deflection does not exceed the allowed deflection (See Figures 5 and 6). Note that the deflection is limited to two inches regardless of the stress. The span values taken from these curves are summarized in the span versus pipe size Table C-1 of Appendix C. | Superimposed on each deflection ( x, y, z) versus span curve is a curve which indicates the deflection at which the stress for each span is 4000 psi. The intersection of these curves indicates the longest span for which the anticipated deflection does not exceed the allowed deflection (See Figures 5 and 6). Note that the deflection is limited to two inches regardless of the stress. The span values taken from these curves are summarized in the span versus pipe size Table C-1 of Appendix C. | ||
'Ihe seismic stresses are determined by using the computer program SIPDA (Sargent & Lundy Document No. 09-5-047-2.0). This program was developed by Mr. E. B. Branch and Mr. M. Nopola of Sargent & Lundy to: | 'Ihe seismic stresses are determined by using the computer program SIPDA (Sargent & Lundy Document No. 09-5-047-2.0). This program was developed by Mr. E. B. Branch and Mr. M. Nopola of Sargent & Lundy to: | ||
: 1) Enable selection of maximum spans so that the stresses due to each seismic excitation (i.e., N-S, Ver., E-W) are 4000 psi or less for OBE, 8000 psi or less for SSE. | : 1) Enable selection of maximum spans so that the stresses due to each seismic excitation (i.e., N-S, Ver., E-W) are 4000 psi or less for OBE, 8000 psi or less for SSE. | ||
: 2) Provide seismic restraint design loads. I | : 2) Provide seismic restraint design loads. I | ||
: 3) Assure that seismic deflections do not exceed two inches. ' | : 3) Assure that seismic deflections do not exceed two inches. ' | ||
III ASME CODE REQUIREMENTS 1 l | III ASME CODE REQUIREMENTS 1 l | ||
Class 2 and 3 Systems | Class 2 and 3 Systems | ||
) | ) | ||
In the following subsections it is shown that the stress limits which are established by the design rules of this standard satisfy the ASME Code requirements for Class 2 and l 3 piping. | In the following subsections it is shown that the stress limits which are established by the design rules of this standard satisfy the ASME Code requirements for Class 2 and l 3 piping. | ||
A. Sustained Loads | A. Sustained Loads | ||
'Ihe effects of sustained mechanical loads must satisfy equation (8) of NC-3652.1: | 'Ihe effects of sustained mechanical loads must satisfy equation (8) of NC-3652.1: | ||
P, Do+ .751 M, 3 4t n Z t, = wall thickness | P, Do+ .751 M, 3 4t n Z t, = wall thickness | ||
( M, = weight induced bending moment Sh = all wable stress in the hot condition. | ( M, = weight induced bending moment Sh = all wable stress in the hot condition. | ||
SL-3159 l | SL-3159 l | ||
SARGENT & LUNDY ENGINEERS REV. 1, 7-29-77 CHICACO SAMPLE SESIMIC DESIGN CURVE SPAN vs DEFLECTION RIGID _ 33 SIR ___ | |||
SARGENT & LUNDY ENGINEERS REV. 1, 7-29-77 CHICACO SAMPLE SESIMIC DESIGN CURVE SPAN vs DEFLECTION | |||
RIGID _ 33 SIR ___ | |||
FLEXI3LE _ | FLEXI3LE _ | ||
MAX AL'E.Va_E DEFLECTICN j j l O | |||
2- / | |||
MAX AL'E.Va_E DEFLECTICN j j l | |||
s. | s. | ||
M ' | M ' | ||
g1 | g1 U | ||
ta MAX MID-SRAN CEFLECTION 10 20 ..- v 00 | |||
10 20 ..- v 00 | |||
; . .- a i . , r :3 FIGURE 5 | ; . .- a i . , r :3 FIGURE 5 | ||
! SEISMIC DESIGN CURVES 1 IMPLY SUPPORTED PIPE O | ! SEISMIC DESIGN CURVES 1 IMPLY SUPPORTED PIPE O | ||
SL-3159 l | SL-3159 l | ||
a | a | ||
SARGENT a LUNDY | SARGENT a LUNDY | ||
'"[ "5 REV. 1, 7-29-77 SAMPLE | '"[ "5 REV. 1, 7-29-77 SAMPLE O 13 . | ||
O 13 . | |||
SEISMIC DESIGN CURVE-SPAN vs REACTION p RIGID 72.3"? - | SEISMIC DESIGN CURVE-SPAN vs REACTION p RIGID 72.3"? - | ||
FLEXIE13 _ | FLEXIE13 _ | ||
11 < | 11 < | ||
10 . | 10 . | ||
2 64 6 | 2 64 6 | ||
4 7 | 4 7 | ||
: u. . | : u. . | ||
b O 6 | b O 6 4 | ||
3 2 | |||
2 | |||
i i f 1- : | i i f 1- : | ||
._y , | ._y , | ||
8 10 15 20 30 e so LETETH IN FEET FIGURE 6 SEISMIC DESIGN CURVES SIMPLY SUPPORTED PIPE O | 8 10 15 20 30 e so LETETH IN FEET FIGURE 6 SEISMIC DESIGN CURVES SIMPLY SUPPORTED PIPE O | ||
SL-3159 | SL-3159 | ||
~ | ~ | ||
s SARGENT C 1. UNDY E >lCIN E E R S c>ucAco Rev.1, 7-29-77 O For pipes of 4 inches nominal diameter or less and subject to pressure not exceeding 1750 psi (or the recommended value from Sargent & Lundy Mechanical Engineering Specifications if that value is lower), the first term has a maximum | s SARGENT C 1. UNDY E >lCIN E E R S c>ucAco Rev.1, 7-29-77 O For pipes of 4 inches nominal diameter or less and subject to pressure not exceeding 1750 psi (or the recommended value from Sargent & Lundy Mechanical Engineering Specifications if that value is lower), the first term has a maximum | ||
~ | ~ | ||
| Line 8,096: | Line 4,940: | ||
I or equation (11) from NC-3652.3 is satisfied. | I or equation (11) from NC-3652.3 is satisfied. | ||
IM | IM | ||
[ 1 S, (10) l l M,/Z is the bending stress due to thermal expansion and anchor movements, so | [ 1 S, (10) l l M,/Z is the bending stress due to thermal expansion and anchor movements, so | ||
' O 1.532 (15000) = 22980 psi SL-3159 | ' O 1.532 (15000) = 22980 psi SL-3159 | ||
:1 | :1 | ||
SARGENT a LUNDY ENGINEERS CHICACO Rev.1, 7-29-77 O | SARGENT a LUNDY ENGINEERS CHICACO Rev.1, 7-29-77 O | ||
But S, = (1.25S, + .25Sh) = (1.25 15000 + .25 15000) = 22500 psi. | But S, = (1.25S, + .25Sh) = (1.25 15000 + .25 15000) = 22500 psi. | ||
| Line 8,108: | Line 4,949: | ||
PD M M 4tn + .751 Y +1 j 1 Sh+8a IIII 5000 + .75 (1.532) (3000) + 1.532 (15000) = | PD M M 4tn + .751 Y +1 j 1 Sh+8a IIII 5000 + .75 (1.532) (3000) + 1.532 (15000) = | ||
31427 psi 137500 psi So equation (11) is satisfied. | 31427 psi 137500 psi So equation (11) is satisfied. | ||
i IV CONCLUSION | i IV CONCLUSION For systems within the scope of this standard, application of iis design rules assures satisfaction of the requirements of NC-3650 of the ASME Code. I* | ||
For systems within the scope of this standard, application of iis design rules assures satisfaction of the requirements of NC-3650 of the ASME Code. I* | |||
These systems must have the fo!!owing characteristics: - | These systems must have the fo!!owing characteristics: - | ||
Pipe class: 2 and 3 | Pipe class: 2 and 3 Nominal pipe size: 4 inches and smaller Maxinium operating pressure: 1750 psi Maximum operating temperature: 300*F Allowable stress: Sh > 15000 psi S, 2.15000 psi A. Stresses | ||
Nominal pipe size: 4 inches and smaller | |||
Maxinium operating pressure: 1750 psi Maximum operating temperature: 300*F Allowable stress: Sh > 15000 psi S, 2.15000 psi A. Stresses | |||
'Ihe stresses in a system designed accordin;- to t" - ytendard arc limited to the following values: | 'Ihe stresses in a system designed accordin;- to t" - ytendard arc limited to the following values: | ||
Moment loading Max stress (psi) seismic OBE 7000 weight 3000 thermal expansion plus nozzle movements 15000 0 | Moment loading Max stress (psi) seismic OBE 7000 weight 3000 thermal expansion plus nozzle movements 15000 0 | ||
SL-3159 rt | SL-3159 rt | ||
SARGENT a LUNDY ENGINEERS CHICACO Rev.1, 7-29-77 O TABLE 1 NOZZLE ALLOWABLES CR AMCHoA RE%TIO M Pipe Size Schedule Moment Load ( ft-lb) Shear Force (Ib) 1/2 40 85 72 80 100 78 160 110 99 3/4 40 147 103 80 178 128 160 209 145 1 40 277 170 80 335 207 160 396 246 1-1/4 40 489 270 . | SARGENT a LUNDY ENGINEERS CHICACO Rev.1, 7-29-77 O TABLE 1 NOZZLE ALLOWABLES CR AMCHoA RE%TIO M Pipe Size Schedule Moment Load ( ft-lb) Shear Force (Ib) 1/2 40 85 72 80 100 78 160 110 99 3/4 40 147 103 80 178 128 160 209 145 1 40 277 170 80 335 207 160 396 246 1-1/4 40 489 270 . | ||
80 607 329 160 713 383 : | 80 607 329 160 713 383 : | ||
1-1/2 40 679 342 80 858 O 160 1060 427 529 j 2 40 1170 536 80s 1520 683 160 2040 912 | 1-1/2 40 679 342 80 858 O 160 1060 427 529 j 2 40 1170 536 80s 1520 683 160 2040 912 t | ||
2-1/2 40 2220 903 80 2790 1120 160 3410 1360 3 40 3590 1360 80 4630 1680 - | |||
160 3410 1360 3 40 3590 1360 80 4630 1680 - | |||
160 5990 2200 3-1/2 40 6690 2250 80 6540 2240 XXS 10300 3490 4 40 6600 2250 80 8890 2920 160 12300 3950 0 | 160 5990 2200 3-1/2 40 6690 2250 80 6540 2240 XXS 10300 3490 4 40 6600 2250 80 8890 2920 160 12300 3950 0 | ||
SL-3159 | SL-3159 | ||
| Line 8,135: | Line 4,965: | ||
b l SARGENT e LUNDY | b l SARGENT e LUNDY | ||
- E NCIN E E RS | - E NCIN E E RS Rev.1, 7-29-77 B. Nozzle Loads | ||
Rev.1, 7-29-77 | |||
B. Nozzle Loads | |||
'Ihe loads imposed on nozzles by piping which is designed according to this standard do not exceed the values listed in Table 1. | 'Ihe loads imposed on nozzles by piping which is designed according to this standard do not exceed the values listed in Table 1. | ||
Sargent & Lundy | Sargent & Lundy Prepared by: e. - , .?ev. 1, 7-29-77 P. Ivy, g Project Engineer, Engineering Mechanics Division Reviewed by: b Rev.1, 7-29-77 | ||
Prepared by: e. - , .?ev. 1, 7-29-77 P. Ivy, g | |||
Project Engineer, Engineering Mechanics Division Reviewed by: b Rev.1, 7-29-77 | |||
. . . Hart, F ineering Analyst, Engineering Mechanics Division O ME. B. Branen, aev 1. 7-29-77 Head, Engineering Mechanics Division | . . . Hart, F ineering Analyst, Engineering Mechanics Division O ME. B. Branen, aev 1. 7-29-77 Head, Engineering Mechanics Division | ||
( sw_ = | ( sw_ = | ||
Approved by: Rev.1, 7-29-77 R. F.' Scheibel, Project Director O | Approved by: Rev.1, 7-29-77 R. F.' Scheibel, Project Director O | ||
SL-3159 | SL-3159 | ||
5ARCENT A LUNDY l E N GIN E E R S Rev.1, 7-29-77 | |||
[O V REFERENCES l | |||
5ARCENT A LUNDY | ASME Boiler and Pressure Vessel Code, Section III,1974 ed. New York: American Society of Mechanical Engineers,1974. | ||
l E N GIN E E R S Rev.1, 7-29-77 | |||
[O V REFERENCES | |||
l | |||
ASME Boiler and Pressure Vessel Code, Section III,1974 ed. New York: American | |||
Society of Mechanical Engineers,1974. | |||
3 Kellogg, M.W. and Company. Design of Piping Systems. Revised 2nd ed. New York: | 3 Kellogg, M.W. and Company. Design of Piping Systems. Revised 2nd ed. New York: | ||
John Wiley and Sons, Inc.1965. | John Wiley and Sons, Inc.1965. | ||
| Line 8,170: | Line 4,981: | ||
] | ] | ||
d D Ae, ORNL-TM-3645. Oak Ridge: Oak Ridge National Laboratory, Feb.1572. | d D Ae, ORNL-TM-3645. Oak Ridge: Oak Ridge National Laboratory, Feb.1572. | ||
Roark, Raymond J., Formulas for Stress and Strain. 4th ed. New York: McGraw- l | Roark, Raymond J., Formulas for Stress and Strain. 4th ed. New York: McGraw- l 11111 Book Company,1965. 1 L Timoshewko, S. and D.11. Young, Elements of Strength of Materiah. 5th ed. Princeton: | ||
11111 Book Company,1965. 1 L Timoshewko, S. and D.11. Young, Elements of Strength of Materiah. 5th ed. Princeton: | |||
1968. | 1968. | ||
[ | [ | ||
l - | l - | ||
1 0 | 1 0 | ||
SL-3159 | SL-3159 | ||
h.4 z._a 2 m. , e ., 4 2 w - -' - - - -- - - | h.4 z._a 2 m. , e ., 4 2 w - -' - - - -- - - | ||
| Line 8,190: | Line 4,994: | ||
l | l | ||
, I l | , I l | ||
i l | i l o | ||
o | |||
; | ; | ||
9 4 | 9 4 | ||
i | i 1 | ||
O 1 | |||
1 | |||
m - .- _ | m - .- _ | ||
Cf ROENT O LUNDY ENGINEEDS APPENDIX A CHICAGO sL-3159 l R E V. 1, 7-29--77 i O 'cAucut ions ^~o EauxTion oERiv4Tions A-1 Weight The recommended weight support spans are based on the following analysis: l The pipe elements between two weight supports may be j l | Cf ROENT O LUNDY ENGINEEDS APPENDIX A CHICAGO sL-3159 l R E V. 1, 7-29--77 i O 'cAucut ions ^~o EauxTion oERiv4Tions A-1 Weight The recommended weight support spans are based on the following analysis: l The pipe elements between two weight supports may be j l | ||
conservatively represented by a simply supported, uniformly loaded beam (fig. lA.). | conservatively represented by a simply supported, uniformly loaded beam (fig. lA.). | ||
f 1 | f 1 | ||
IY1J 1 V 1 1 i fl 1 1 1 A A g ' | IY1J 1 V 1 1 i fl 1 1 1 A A g ' | ||
x :I fig.1 A 2 fig.1B From symmetry and squilibrium considerations the bending moment at' a cross section X t' nits from A is: | x :I fig.1 A 2 fig.1B From symmetry and squilibrium considerations the bending moment at' a cross section X t' nits from A is: | ||
O M: Xdx : @ (x I-X' ) R,- p , a : 1incar weight dersity X-f"xo | O M: Xdx : @ (x I-X' ) R,- p , a : 1incar weight dersity X-f"xo 1 | ||
1 | |||
This is a maximum at X = f/2 y - m max- 2 '.!*_ [4,- | This is a maximum at X = f/2 y - m max- 2 '.!*_ [4,- | ||
62 _ sfe | 62 _ sfe | ||
* The stress due to this moment is 5: *= ^l , 2: se ction m o du'us If S a is the allowable stress sa : a l*/BZ ,so l= fB y ' | * The stress due to this moment is 5: *= ^l , 2: se ction m o du'us If S a is the allowable stress sa : a l*/BZ ,so l= fB y ' | ||
1 is the maximum span for which the allowable stress is not ! | 1 is the maximum span for which the allowable stress is not ! | ||
exceeded. j | exceeded. j O | ||
l A-1 l | |||
A-1 l | |||
w-_ - -- -- - | w-_ - -- -- - | ||
'l | 'l | ||
| Line 8,235: | Line 5,021: | ||
For 2 given in (inches) ,3 / in feet, and ee- in lb/ft j = 20032' w g,; ) | For 2 given in (inches) ,3 / in feet, and ee- in lb/ft j = 20032' w g,; ) | ||
to allow a construction tolerance of one foot without exceeding the allowable stress, the recommended span is one foot less than indicated by equation (A-1). | to allow a construction tolerance of one foot without exceeding the allowable stress, the recommended span is one foot less than indicated by equation (A-1). | ||
y: 20,. W -1 m.2) l | y: 20,. W -1 m.2) l The maximum support load is calculated assuming that l:fs +1 is used as the span length. Thus LOAD = feu (A-3) | ||
The maximum support load is calculated assuming that l:fs +1 is used as the span length. Thus LOAD = feu (A-3) | |||
This is not the reaction, R,a of fig. 1D. It is the total weight of a full span and represeits the load which would be imposed on an intermediate support of a continuous multi-support system. | This is not the reaction, R,a of fig. 1D. It is the total weight of a full span and represeits the load which would be imposed on an intermediate support of a continuous multi-support system. | ||
() | () | ||
l l | l l | ||
A-2 l | A-2 l | ||
l | l | ||
3 CARGENT& LUNDY E N C. I N E E N s | 3 CARGENT& LUNDY E N C. I N E E N s | ||
> ' " ' " " APPENDIX A SL-3159 | > ' " ' " " APPENDIX A SL-3159 | ||
:o REV.1, 7-29-77 | :o REV.1, 7-29-77 A-1 Weight (continued) | ||
A-1 Weight (continued) | |||
Span Reduction for Concentrated Weights The maximum total bending moment for a span of length f,, | Span Reduction for Concentrated Weights The maximum total bending moment for a span of length f,, | ||
) | ) | ||
subject to distributed weight, s , and centrally located concentrated weight, W, e is Mmax= + * ,' '' | subject to distributed weight, s , and centrally located concentrated weight, W, e is Mmax= + * ,' '' | ||
For a given pipe the allowable maximum moment is where 8 is the recommended span length without the concentrated load. Therefore w8 S. + $ g M S' 4 6 If one half of the recommended span length is used the safe value for We can be obtained. | |||
For a given pipe the allowable maximum moment is where | |||
8 is the recommended span length without the concentrated load. Therefore | |||
w8 S. + $ g M S' 4 6 If one half of the recommended span length is used the safe value for We can be obtained. | |||
M it?) .y we tit o) S MA' | M it?) .y we tit o) S MA' | ||
* 8 4 8 | * 8 4 8 | ||
| Line 8,270: | Line 5,042: | ||
( | ( | ||
l A-3 | l A-3 | ||
8 l | |||
8 | CARGENTQ LUNDY EN08NEED9 APPENDIX A g cmcaco SL-3159 r RE V. 1, 7-2 9-7 4 | ||
['O A-1 Weight (continued) | ['O A-1 Weight (continued) | ||
Span Reduction for Concentrated Weights So, for a concentrated weight of less than 10% of the normal span weight a 10% reduction in span would keep the weight stress below 3000 psi. | |||
normal span weight a 10% reduction in span would keep the weight stress below 3000 psi. | |||
For a very short span (say 10% of the normal span) a similar analysis shows that a concentrated weight of 2.5 times the normal span support load can be accommodated. | For a very short span (say 10% of the normal span) a similar analysis shows that a concentrated weight of 2.5 times the normal span support load can be accommodated. | ||
Since such concentrated weights are usually very rigid compared to the piping, the length of the concentrated | Since such concentrated weights are usually very rigid compared to the piping, the length of the concentrated | ||
| Line 8,289: | Line 5,056: | ||
A-4 | A-4 | ||
{ | { | ||
CARGENT O LUNDY ENoNEERS C M 6C# GO APPENDIX A SL-3159 | CARGENT O LUNDY ENoNEERS C M 6C# GO APPENDIX A SL-3159 | ||
~ | ~ | ||
REV.1, 7-29--77 t' | |||
REV.1, 7-29--77 | A-2 Expansion and Nozzle Movements (continued) 9 The recommendedc offset lengths are based on the following I | ||
t' A-2 Expansion and Nozzle Movements (continued) 9 The recommendedc offset lengths are based on the following I | |||
analysis: | analysis: | ||
i All segments of pipe in the offset direction are assumed | i All segments of pipe in the offset direction are assumed to act as a single guided cantilever. The flexibility of i intermediate elbows and pipes is ignored (see Fig. 2) b-s l "i 's i i , | ||
to act as a single guided cantilever. The flexibility of i intermediate elbows and pipes is ignored (see Fig. 2) b-s | |||
l "i 's i i , | |||
bl #2. - - | bl #2. - - | ||
S | S | ||
* 5 F I G. 2 Suppose a deflection,d,is caused by a load, W. . | * 5 F I G. 2 Suppose a deflection,d,is caused by a load, W. . | ||
W | W | ||
: n. ;r | : n. ;r | ||
' ~ - - - aa-u W | ' ~ - - - aa-u W | ||
M Rs U A B | M Rs U A B IF: | ||
IF: | |||
j O Q R:W IM:ox 0 > Wf-M a-Mb=O but Ma Mb 50 f-( I Mb ds aW ' M(n) 2 x M*)WY -Wf/ 2 :W( x - f / 2.' | j O Q R:W IM:ox 0 > Wf-M a-Mb=O but Ma Mb 50 f-( I Mb ds aW ' M(n) 2 x M*)WY -Wf/ 2 :W( x - f / 2.' | ||
v 8: | v 8: | ||
| Line 8,325: | Line 5,077: | ||
W IX* fmai p, | W IX* fmai p, | ||
Q Y EII'G 4 [+ , y:O at x: O s o C': 0 A-5 | Q Y EII'G 4 [+ , y:O at x: O s o C': 0 A-5 | ||
CARGENTO LUNDY E N GIN E E AS | CARGENTO LUNDY E N GIN E E AS | ||
""''' APPENDIX A SL-3159 o REV. 1, 7-29-77 J | ""''' APPENDIX A SL-3159 o REV. 1, 7-29-77 J | ||
A-2 Expansion and Nozzle Movements ! | A-2 Expansion and Nozzle Movements ! | ||
(cont'nued) . | (cont'nued) . | ||
Thus -W y :EI | Thus -W y :EI i | ||
G M\4 j is the deflection at a distance X from the anchored end. | |||
M\4 j is the deflection at a distance X from the anchored end. | |||
1 Since Y = -f at X = f - 6.Ef_ | 1 Since Y = -f at X = f - 6.Ef_ | ||
i E1 4 _A.',i 4 l W l' , | i E1 4 _A.',i 4 l W l' , | ||
g _12EI - or w:_12SE1 J* | g _12EI - or w:_12SE1 J* | ||
] | ] | ||
The stress due to the defeletion, d , is , | The stress due to the defeletion, d , is , | ||
r 5 :r.M/t : Wfr- 12 f cI r. | r 5 :r.M/t : Wfr- 12 f cI r. | ||
JQ 21 | JQ 21 29'I | ||
29'I | |||
- 9d r. E_ , r. : c u te r radio, f* | - 9d r. E_ , r. : c u te r radio, f* | ||
If this deflection is the resultant of three equal orthoganal deflections, E' , S: 65 r. E 8:h(S'*) | If this deflection is the resultant of three equal orthoganal deflections, E' , S: 65 r. E 8:h(S'*) | ||
f | f R' | ||
t | |||
R' t | = _G66 r.E g GTT 4'r,.r /t 5 5 For an allowable stress of 15000 psi the offset length must be ll _ [ GT3 3 010* r,f'' | ||
= _G66 r.E g GTT 4'r,.r /t 5 5 | |||
For an allowable stress of 15000 psi the offset length must be ll _ [ GT3 3 010* r,f'' | |||
Y2 . | Y2 . | ||
- l 15000 -44(I' 2. ' or ' 2 h , ! r e t ' | |||
- l | |||
15000 -44(I' 2. ' or ' 2 h , ! r e t ' | |||
! I tor r, and E in inches L. | ! I tor r, and E in inches L. | ||
1 i | 1 i | ||
s | s O | ||
O | |||
) A-6 | ) A-6 | ||
i CARGENT O LUNDY ENGINEERS ! | i CARGENT O LUNDY ENGINEERS ! | ||
C"'C"' APPENDIX A I SL- 3159 m RE V. 1, 7-29-77 U i | C"'C"' APPENDIX A I SL- 3159 m RE V. 1, 7-29-77 U i | ||
.A-2 Expansion and Nozzle Movements (continued) | .A-2 Expansion and Nozzle Movements (continued) | ||
The def?ection due to pipe expansion is handled in a similar manner except that the imposed deflection is i | The def?ection due to pipe expansion is handled in a similar manner except that the imposed deflection is i | ||
| Line 8,382: | Line 5,112: | ||
l | l | ||
; | ; | ||
* l For' expansion of a length A' | * l For' expansion of a length A' l 0 l 2 | ||
l 0 l 2 | |||
j = f' A A T : ( .0261 in/f t )f' for austenitic stee: 70* to 3 O O | j = f' A A T : ( .0261 in/f t )f' for austenitic stee: 70* to 3 O O | ||
* F | * F O e f:9.129 @ | ||
O e f:9.129 @ | |||
a R> | a R> | ||
1 29.1291r, (.0 2 51 ) f" | 1 29.1291r, (.0 2 51 ) f" | ||
' i 77F - ! | ' i 77F - ! | ||
f :1. 4751 r. J' ~' for / and [in fee t , r. in inches O | f :1. 4751 r. J' ~' for / and [in fee t , r. in inches O | ||
l Note that the flexibility of the leng th j and the elbow i | |||
l | |||
Note that the flexibility of the leng th j and the elbow i | |||
I is ignored. 1 6 ! | I is ignored. 1 6 ! | ||
Free Ends: The bending moment cannot_ c::cced thi t for a l | Free Ends: The bending moment cannot_ c::cced thi t for a l | ||
| Line 8,412: | Line 5,133: | ||
~ | ~ | ||
CARGENTOLUNDY E"fj,",EE"5 | CARGENTOLUNDY E"fj,",EE"5 | ||
. APPENDIX A SL-3159 REV 1, 7-29-77 | . APPENDIX A SL-3159 REV 1, 7-29-77 | ||
| Line 8,421: | Line 5,141: | ||
] | ] | ||
T | T | ||
] | ] | ||
TO | TO | ||
| Line 8,427: | Line 5,146: | ||
[ | [ | ||
r ; | r ; | ||
l l | l l I | ||
o A-8 e | |||
A-8 e | |||
CAGOENT O LUNDY E"fle",E"#8 | CAGOENT O LUNDY E"fle",E"#8 | ||
,o APPENDIX A SL-3159 R E V. 1, 7-29-77 | ,o APPENDIX A SL-3159 R E V. 1, 7-29-77 | ||
| Line 8,441: | Line 5,155: | ||
{ action of weight, thermal, and seismic loading. That value is 3000 + 15000 + 7000 = 25000 psi. The | { action of weight, thermal, and seismic loading. That value is 3000 + 15000 + 7000 = 25000 psi. The | ||
[ , | [ , | ||
bending moment corresponding to this stress is | bending moment corresponding to this stress is Z 25000 psi l M= = 2083 Z ft.lb. | ||
Z 25000 psi l M= = 2083 Z ft.lb. | |||
I 12 in/ft , | I 12 in/ft , | ||
[ where 2 = section modulus (in ) 3 | [ where 2 = section modulus (in ) 3 The shear force due to weight is one half the maximum ' | ||
The shear force due to weight is one half the maximum ' | |||
lJ weight support load from table B-1, Appendix B. | lJ weight support load from table B-1, Appendix B. | ||
7 The shear force due to seismic loading may be estimated ; | |||
by assuming that it is in the same proportion to the ii | by assuming that it is in the same proportion to the ii | ||
) | ) | ||
weight shear force as the seismic stress is to the weight ', | weight shear force as the seismic stress is to the weight ', | ||
i stress. | i stress. | ||
seismic shear = 7000 weight shear 3000 seismic shear = 2.33 weight shear . | seismic shear = 7000 weight shear 3000 seismic shear = 2.33 weight shear . | ||
The shear due to bending moments is estimated by assuming that it is equal to the force required to cause a 15000 psi bending stress with a moment arm equal to the minimum allowed offset from table D-2. | The shear due to bending moments is estimated by assuming that it is equal to the force required to cause a 15000 psi bending stress with a moment arm equal to the minimum allowed offset from table D-2. | ||
l l | l l | ||
O A-9 | O A-9 | ||
] SARGENT Q LUNDY ENGINFLH% | ] SARGENT Q LUNDY ENGINFLH% | ||
i .m a . .. . | i .m a . .. . | ||
| Line 8,482: | Line 5,182: | ||
. tions shown here and enveloped seismic response spectra covering all elevations in the Reactor, Turbine, and RHR Complex Buildings. For each of the Buildings, separate responses were calculated for the East-West, North-South, and Vertical Direction Excita.. . . . | . tions shown here and enveloped seismic response spectra covering all elevations in the Reactor, Turbine, and RHR Complex Buildings. For each of the Buildings, separate responses were calculated for the East-West, North-South, and Vertical Direction Excita.. . . . | ||
: a. .f at exci tation in any one building the allowabic deficction of the pipe | : a. .f at exci tation in any one building the allowabic deficction of the pipe | ||
. segment modeled and analyzed was based on a 4030 psi bending | . segment modeled and analyzed was based on a 4030 psi bending | ||
~ | ~ | ||
stress. This criteria limits the maximum bending stress due | stress. This criteria limits the maximum bending stress due | ||
(] to excitation in all three directions simultaneously to A-10 | |||
(] to excitation in all three directions simultaneously to | |||
A-10 | |||
-a, e | -a, e | ||
CARGENTQLUNDY EN NEERS | CARGENTQLUNDY EN NEERS c,co APPENDIX A SL-3159 RE V.1, 7-29-77 | ||
c,co APPENDIX A SL-3159 RE V.1, 7-29-77 | |||
]O 4000 h psi using the square root of the sum of the squares to combine the responses in accordance with NRC Regulatory Guide 1.92. | ]O 4000 h psi using the square root of the sum of the squares to combine the responses in accordance with NRC Regulatory Guide 1.92. | ||
A-4.2 Derivation of Equations Figure A-4.2a Models and Nomenclature | A-4.2 Derivation of Equations Figure A-4.2a Models and Nomenclature | ||
] o i | ] o i | ||
3 e f = | 3 e f = | ||
o =X | o =X g g | ||
g g | |||
.. om ex x, umir ''"""' | .. om ex x, umir ''"""' | ||
Cons &t EX, D, or | Cons &t EX, D, or | ||
| Line 8,511: | Line 5,201: | ||
4= 1 = | 4= 1 = | ||
3 | 3 | ||
, Consfant EI,D3m-Model Used for Natural Frcqucncy Det.crminations I | |||
, Consfant EI,D3m-Model Used for Natural Frcqucncy Det.crminations | |||
. 11 3 | . 11 3 | ||
_. . . _ -- a | _. . . _ -- a | ||
( | ( | ||
CARGENTO LUNDY EN N RS | CARGENTO LUNDY EN N RS APPENDIX A SL-3159 RE V. 1, 7-2 E-77 lo A-4.2 Nomenclature 60' = weight per unit length of beam a | ||
APPENDIX A SL-3159 RE V. 1, 7-2 E-77 lo A-4.2 Nomenclature 60' = weight per unit length of beam a | |||
E = Youngs modulus k = | E = Youngs modulus k = | ||
I Area Moment of Inertia of Pipe Cross-section D = Outside Diameter of pipe - | I Area Moment of Inertia of Pipe Cross-section D = Outside Diameter of pipe - | ||
| Line 8,530: | Line 5,214: | ||
, T}g = Modal Participation Factor of mode n y(t) = Beam deflection relative to supports M (x, t) = Moment at beam cross sections V (x, t)= She;.r at beam cross sections ee | , T}g = Modal Participation Factor of mode n y(t) = Beam deflection relative to supports M (x, t) = Moment at beam cross sections V (x, t)= She;.r at beam cross sections ee | ||
][ = Absolute acceleration A-4.2-1 Solution The equation of motion, using Euler Bernoulli Beam Theory and neglecting Shear Effects on curvature and Rotary Inertia can be written as follows for a beam segment | ][ = Absolute acceleration A-4.2-1 Solution The equation of motion, using Euler Bernoulli Beam Theory and neglecting Shear Effects on curvature and Rotary Inertia can be written as follows for a beam segment | ||
(]) between two supports. | (]) between two supports. | ||
A-12 | A-12 4 | ||
4 | |||
q CARGENTQ LUNDY J | q CARGENTQ LUNDY J | ||
""L',c"[,,E"5 APPENDlX A SL-3159 | ""L',c"[,,E"5 APPENDlX A SL-3159 | ||
'] A-4.2-1 RE V. 1, 7-29-77 I+- '" | '] A-4.2-1 RE V. 1, 7-29-77 I+- '" | ||
l l = 0 | l l = 0 | ||
.] The absolute acceleration of any point on the beam | .] The absolute acceleration of any point on the beam can be rewritten as: | ||
can be rewritten as: | |||
J y = @) + y;a) (2) | J y = @) + y;a) (2) | ||
T j where f h*@ | T j where f h*@ | ||
g = the acceleration of any point on the beam relative to the supports. The equation of motion | g = the acceleration of any point on the beam relative to the supports. The equation of motion may then be rewritten as: | ||
may then be rewritten as: | |||
Y =~ 5 b) (3) | Y =~ 5 b) (3) | ||
[O { | [O { | ||
| Line 8,564: | Line 5,237: | ||
A-13 | A-13 | ||
a l CARGENTO LUNDY E N G1N EE Rs c mc ac, APPENDIX A SL-3159 RE V. 1, 7-29-77 and sum over the m index J ll9? +'DWYy}~q-; =-%>f-~y | a l CARGENTO LUNDY E N G1N EE Rs c mc ac, APPENDIX A SL-3159 RE V. 1, 7-29-77 and sum over the m index J ll9? +'DWYy}~q-; =-%>f-~y | ||
:) | :) | ||
| Line 8,571: | Line 5,243: | ||
j t 1 O (7) | j t 1 O (7) | ||
.. ee k C-3(f) [ k 2. d,X | .. ee k C-3(f) [ k 2. d,X | ||
,=31 | ,=31 Integration: | ||
Integration: | |||
-] | -] | ||
I O m #m | I O m #m 44.nt> %1YX (a) | ||
44.nt> %1YX (a) | |||
A M rnTfx A | A M rnTfx A | ||
Q=) \ | Q=) \ | ||
| Line 8,586: | Line 5,253: | ||
+ ( gw and the index on the right side can be changed to n. The equation can then be rewritte n as: | + ( gw and the index on the right side can be changed to n. The equation can then be rewritte n as: | ||
i 9 ., | i 9 ., | ||
This will be satisfied if, for all n, Y b h [ | This will be satisfied if, for all n, Y b h [ | ||
/ | / | ||
5 A-14 | 5 A-14 | ||
CARGENTO LUNDY EN INE RS g,,, APPENDIX A SL-3159 A-4.2-1 | CARGENTO LUNDY EN INE RS g,,, APPENDIX A SL-3159 A-4.2-1 | ||
:} | :} | ||
A. | A. | ||
REV. 1, 7-29-77 i | REV. 1, 7-29-77 i | ||
| Line 8,608: | Line 5,270: | ||
} [+ k(* g= - | } [+ k(* g= - | ||
k(OM | k(OM | ||
, Using the standard spectral analysis technique bb l VCT4 | , Using the standard spectral analysis technique bb l VCT4 h (d x2 n. (12) where Y ( Ts ) is the response spectra acceleration. | ||
h (d x2 n. (12) where Y ( Ts ) is the response spectra acceleration. | |||
Therefore:. | Therefore:. | ||
-e 1 | -e 1 | ||
| Line 8,617: | Line 5,277: | ||
l ** .. | l ** .. | ||
4 | 4 | ||
=. t Z T 4. Y (T ,d p wwx i | =. t Z T 4. Y (T ,d p wwx i | ||
4:s 4 TT'2 y | 4:s 4 TT'2 y | ||
) 2/ (14) | ) 2/ (14) | ||
O ' % Mn | O ' % Mn 71 = I )=ydu = f, 4 o | ||
71 = I )=ydu = f, 4 o | |||
I, g 9 %. M Substitute: | I, g 9 %. M Substitute: | ||
=f{M M W3 (TN d 9t.#"X (15) n=1, 3, 5... | =f{M M W3 (TN d 9t.#"X (15) n=1, 3, 5... | ||
L I | L I | ||
| Line 8,635: | Line 5,291: | ||
} * * $j "do'" APPENDlX A SI..-3159 FE V. 1, 7-2 9--77 Calculation of Shear Distribution | } * * $j "do'" APPENDlX A SI..-3159 FE V. 1, 7-2 9--77 Calculation of Shear Distribution | ||
] | ] | ||
3 v_=*El p=tavcu = *nx n = 1, 3, 5... | 3 v_=*El p=tavcu = *nx n = 1, 3, 5... | ||
} The maximum shear occurs at x = 0 and x = 1 Vmax 2 1- q2T{y(Tw) (18) | } The maximum shear occurs at x = 0 and x = 1 Vmax 2 1- q2T{y(Tw) (18) n=1, 3, 5... | ||
n=1, 3, 5.. | |||
} The maximum moment is calculated considering the first mode only. | } The maximum moment is calculated considering the first mode only. | ||
M max 1 TI (T8} OI 7 # (19) | M max 1 TI (T8} OI 7 # (19) | ||
T EL g max _ M o _ EDTF V(td | T EL g max _ M o _ EDTF V(td g (19a) ) | ||
g (19a) ) | |||
The maximum deflection is also calculated considering the first mode only. | The maximum deflection is also calculated considering the first mode only. | ||
ymM ' d T# ~ | ymM ' d T# ~ | ||
g (20) 7T3 | g (20) 7T3 Considering Equations 19 and 20 ' | ||
Considering Equations 19 and 20 ' | |||
3 | 3 | ||
~ frE E D Aas = 2 12 Y""# | ~ frE E D Aas = 2 12 Y""# | ||
7O | 7O A-16 l | ||
A-16 l | |||
CARGENT O LUNDY | CARGENT O LUNDY | ||
' " $ c"."c,o* " " APPENDIX A SL-3159 | ' " $ c"."c,o* " " APPENDIX A SL-3159 | ||
| Line 8,677: | Line 5,320: | ||
= | = | ||
/ | / | ||
s scle f O | |||
s scle f | e Y | ||
m s \ | |||
) | ) | ||
t O r | t O r | ||
= | = | ||
.e A-17 | .e A-17 | ||
CARGENTOLUNDY O | CARGENTOLUNDY O | ||
E N GIN E E R S CMtC&t O APPENDIX A SL 3159 | E N GIN E E R S CMtC&t O APPENDIX A SL 3159 REV.1, 7 29 77 A-4.2-1 Equation 18 may be conaervatively rewritten as: | ||
l EI . . (24) | |||
J by = 7g Yed) E x^re n=1, 3, 5... | |||
REV.1, 7 29 77 A-4.2-1 Equation 18 may be conaervatively rewritten as: | |||
l | |||
EI . . (24) | |||
J by = 7g Yed) E x^re | |||
n=1, 3, 5... | |||
This equation is used to calculate the Restraint Reaction Curves. | This equation is used to calculate the Restraint Reaction Curves. | ||
The natural frequencies of the fixed - simple beam | The natural frequencies of the fixed - simple beam shown in figure A-4.2a are accurately approximated by: | ||
shown in figure A-4.2a are accurately approximated by: | |||
(25) a)x : (x+%t)*TT* fy ay JL n = 1, 2, 3... | (25) a)x : (x+%t)*TT* fy ay JL n = 1, 2, 3... | ||
l Therefore, | l Therefore, | ||
| Line 8,716: | Line 5,342: | ||
the design curves. | the design curves. | ||
(21) fE Y allowable = 2.(h E TT,a v | (21) fE Y allowable = 2.(h E TT,a v | ||
for the allowable en.relope | for the allowable en.relope a | ||
(23) Y actual = T'1 Y(Ti) for the actual dis-O placement "3 | |||
A .o P | A .o P | ||
] CARGENT Q LUNDY | ] CARGENT Q LUNDY | ||
, E N GIN F E R S APPENDIX A SL-3159 REV. !, 7-29-77 (24) Vmax = CD) MT for the restraint loads due to 1 span | , E N GIN F E R S APPENDIX A SL-3159 REV. !, 7-29-77 (24) Vmax = CD) MT for the restraint loads due to 1 span n = 1, 3, 5... | ||
These values should be doubled to calculate restraint loads because there are generally two adjacent spans being restrained by any one restraint. | |||
n = 1, 3, 5... | |||
These values should be doubled to calculate restraint | |||
loads because there are generally two adjacent spans being restrained by any one restraint. | |||
(25) ! for the natural Tx = Ot+%d Tf V E l | (25) ! for the natural Tx = Ot+%d Tf V E l | ||
} periods. | } periods. | ||
]O I | ]O I | ||
l' O | l' O | ||
I | I | ||
:o b | :o b | ||
LO . | LO . | ||
s A-19 f ~ Final | s A-19 f ~ Final | ||
._ .._. _ _ _ . - ___.__.u- - _. u - - - - | ._ .._. _ _ _ . - ___.__.u- - _. u - - - - | ||
----------.n_---- | ----------.n_---- | ||
CARGENTO LUNDY ENG1NEERS C HIC AGO APPENDIX B SL-3159 RE V. 1, 7-29-77 weiowTsueeoaTs | CARGENTO LUNDY ENG1NEERS C HIC AGO APPENDIX B SL-3159 RE V. 1, 7-29-77 weiowTsueeoaTs | ||
}O B-1 Procedure for Weight Support System Design Starting from a convenient point (nozzle, structural anchor, header connection, etc.) the piping is traversed in steps, called half-spans, of length equal to one half the recommended span from Table B-1 (normal l | }O B-1 Procedure for Weight Support System Design Starting from a convenient point (nozzle, structural anchor, header connection, etc.) the piping is traversed in steps, called half-spans, of length equal to one half the recommended span from Table B-1 (normal l | ||
| Line 8,757: | Line 5,366: | ||
3 one ste;p is made at a time and each is assigned a unique ; | 3 one ste;p is made at a time and each is assigned a unique ; | ||
integer label which is marked on an isometric of system. | integer label which is marked on an isometric of system. | ||
The isometric is included in the system design | The isometric is included in the system design | ||
] documentation along with the weight support system design | ] documentation along with the weight support system design | ||
| Line 8,763: | Line 5,371: | ||
} work sheets (see sample problems). These worksheets list alJ steps nuvarico11y and include a description of the | } work sheets (see sample problems). These worksheets list alJ steps nuvarico11y and include a description of the | ||
] elements in each step, the length and recommended supports | ] elements in each step, the length and recommended supports | ||
, for each step,and the rules which govern the design l decisions. The worksheet. is t. sci as an ..id to system design and as documentation to show that the requirements l ' | |||
, for each step,and the rules which govern the design l | |||
decisions. The worksheet. is t. sci as an ..id to system | |||
design and as documentation to show that the requirements | |||
l ' | |||
; of the standard have been met. Enough information should ! | ; of the standard have been met. Enough information should ! | ||
be presented to show that the designer has considered ! | be presented to show that the designer has considered ! | ||
" i all relevant system characteristi ;. | " i all relevant system characteristi ;. | ||
| Line 8,783: | Line 5,382: | ||
CARGENTG LUNDY E N G I N E E *t 9 | CARGENTG LUNDY E N G I N E E *t 9 | ||
*"'' " APPENDIX B SL-3159 RE V. 1, 7- 29-- 77 B-1 Procedure for Weicht Support System Design (continued) | *"'' " APPENDIX B SL-3159 RE V. 1, 7- 29-- 77 B-1 Procedure for Weicht Support System Design (continued) | ||
The steps are made in a consistent direction and branch lines are traversed only after an end point of the main run is reached. Each step has two ends, A and B, where A to B is the direction of traversing. The support | The steps are made in a consistent direction and branch lines are traversed only after an end point of the main run is reached. Each step has two ends, A and B, where A to B is the direction of traversing. The support system is completely defined by specifying the length m | ||
system is completely defined by specifying the length m | |||
of each step and the ends which require support. Note | of each step and the ends which require support. Note | ||
) | ) | ||
that end A of one step is end B of the preceeding step, but each support is listed only once on the worksheet. | that end A of one step is end B of the preceeding step, but each support is listed only once on the worksheet. | ||
That is, if a given step must be supported on end A, it | That is, if a given step must be supported on end A, it | ||
_Qb | _Qb | ||
]- | ]- | ||
is not necessary to indicate that end B of the previous | is not necessary to indicate that end B of the previous step is supported. Similarly, if a support at end B is ; | ||
step is supported. Similarly, if a support at end B is ; | |||
required, it is not necessary to indicate tl.at a support l | required, it is not necessary to indicate tl.at a support l | ||
is required at end A of the following step. The | is required at end A of the following step. The | ||
[ ! | [ ! | ||
| Line 8,812: | Line 5,404: | ||
6 | 6 | ||
- . . . . ~ . _ | - . . . . ~ . _ | ||
. CARGENT eLUNDY ENGINEERS APPENDIX B | . CARGENT eLUNDY ENGINEERS APPENDIX B | ||
- SL 3159 REV.1, 7 29 77 | |||
- SL 3159 | .O B-1 Procedure for Weight Support System Design (continued) | ||
: 3. Examine the components within this step and determine which ends of the section require support and whether or not a shortening of the span is required by the weight support system design rules. | |||
REV.1, 7 29 77 | - 4. Mark the end point of the step on the isometric and number the step. (Number steps with consecutive integers.) | ||
.O | Indicate the type and location of supports on the isometric. | ||
: 3. Examine the components within this step and determine | |||
which ends of the section require support and | |||
whether or not a shortening of the span is required | |||
by the weight support system design rules. | |||
- 4. Mark the end point of the step on the isometric and | |||
number the step. (Number steps with consecutive integers.) | |||
Indicate the type and location of supports on the | |||
isometric. | |||
~ | ~ | ||
: 5. Enter all pertinent information on the worksheet. | : 5. Enter all pertinent information on the worksheet. | ||
: 6. Starting from the end point of this step, go to 2 above and continue this procedure until all lines and branches have been covered. | |||
: 6. Starting from the end point of this step, go to 2 above and continue this procedure until all lines | |||
and branches have been covered | |||
. O 4 | . O 4 | ||
r e | r e | ||
I | I 3 l l | ||
3 l l | |||
i i | i i | ||
c l | |||
c | |||
l | |||
*I | *I | ||
| Line 8,867: | Line 5,426: | ||
-() B-2 Rules for Locating Weight Supports | -() B-2 Rules for Locating Weight Supports | ||
'3 | '3 | ||
: 1. A half-span of plain pipe must have a vertical support J at one end. | : 1. A half-span of plain pipe must have a vertical support J at one end. | ||
: 2. A half-span which includes an elbow must have a vertical | : 2. A half-span which includes an elbow must have a vertical | ||
:] | :] | ||
J support at both e,nds. | J support at both e,nds. | ||
.] 3. The length of a half-span which includes a J concentrated weight of less than 10% of the normal span load (Table B-1) should not exceed 40% of the | .] 3. The length of a half-span which includes a J concentrated weight of less than 10% of the normal span load (Table B-1) should not exceed 40% of the | ||
'] normal span length. It must have a vertical support J on one side. - | '] normal span length. It must have a vertical support J on one side. - | ||
| Line 8,883: | Line 5,440: | ||
: 6. A concentrated weight which exceeds 250s of the ncrmal | : 6. A concentrated weight which exceeds 250s of the ncrmal | ||
] | ] | ||
span load should be supported directly rather tha:. | span load should be supported directly rather tha:. | ||
by the piping to which it is attached. | by the piping to which it is attached. | ||
} 7. The length of a half-span with one free end should not exceed 50% of the normal span length. | } 7. The length of a half-span with one free end should not exceed 50% of the normal span length. | ||
I | I | ||
: 8. A halt-span with a concentrated w,ight should not have a free end. | : 8. A halt-span with a concentrated w,ight should not have a free end. | ||
: 9. Supports not required by taese rules should not be used. | : 9. Supports not required by taese rules should not be used. | ||
M m | M m | ||
l L (~) - | |||
l | |||
L (~) - | |||
7 r | 7 r | ||
i h B-4 l | i h B-4 l | ||
| Line 8,906: | Line 5,455: | ||
CARGENTO LUNDY E N G 1 N E E R *' | CARGENTO LUNDY E N G 1 N E E R *' | ||
C H K At*U APPENDIX B l SL 3159 REV.1. 7 - 29 77 | C H K At*U APPENDIX B l SL 3159 REV.1. 7 - 29 77 | ||
_ Tabic B-1 | _ Tabic B-1 RECOMMENDEO se SPA!!3 FOlt DEAD W1:IGi!T SUPI'OltTS NOM. S'"O | ||
RECOMMENDEO se SPA!!3 FOlt DEAD W1:IGi!T SUPI'OltTS NOM. S'"O | |||
* WATER-FILLED GAS-FILLED ROD DIAM, j | * WATER-FILLED GAS-FILLED ROD DIAM, j | ||
_SCH. S PA_!!* LO-\D (LB) SPAN | _SCH. S PA_!!* LO-\D (LB) SPAN | ||
| Line 8,917: | Line 5,464: | ||
] 3/4 40 80 7'-7" 7'-11" 16 20 8'-4" 8'-4" 16 18 3/8 3/8 i | ] 3/4 40 80 7'-7" 7'-11" 16 20 8'-4" 8'-4" 16 18 3/8 3/8 i | ||
I 160 7'-10" 22 8'-1" 22 1 40 9'-0" 26 9'-10" 24 80 9'-2" 32 9'-10" 20 ) | I 160 7'-10" 22 8'-1" 22 1 40 9'-0" 26 9'-10" 24 80 9'-2" 32 9'-10" 20 ) | ||
160 3/8 l 38 | 160 3/8 l 38 9'-2" 9'-6" 38 ! | ||
l-1/4 40 10'-5" 42 11'-7" 38 80 10'-9" 50 46 160 11*-6" 3/8 10'-10" 58 11'-5" 56 1-1/2 40 11'-4" 57 12*-1C" 48 80 11'-9* 64 12*-30" 58 160 3/8 , | |||
9'-2" 9'-6" 38 | a 11'-10" 60 12'-6" 76 2 40 12'-9" 82 14'-9" | ||
l-1/4 40 10'-5" 42 11'-7" 38 80 10'-9" 50 46 160 11*-6" 3/8 10'-10" 58 11'-5" 56 1-1/2 40 11'-4" 57 12*-1C" 48 | |||
80 11'-9* 64 12*-30" 58 160 3/8 , | |||
a 11'-10" 60 12'-6" 76 | |||
2 40 12'-9" 82 14'-9" | |||
~ | ~ | ||
7: | 7: | ||
80 13'-2" 102 | 80 13'-2" 102 | ||
, 160 14'-9" 94 3/8 13'-6"s . 136 14'-4" 128 | , 160 14'-9" 94 3/8 13'-6"s . 136 14'-4" 128 2-1/2 40 14'-6" 138 16'-9" 120 80 15'-0" 168 152 160 16'-7' 1/2 15'-1" 202 16'-2" 190 1 | ||
3 40 15'-6" 210 la'-)" 199 80 16'-2" 248 18'-1" 232 160 1/2 16'-7" 326 17'-10" 306 j 3-1/2 40 16'-7" 272 19'-9" 232 80 17'-5" 340 19'-9" 302 XXS 5/8 17'-11" 520 18 ' - 11 '' 496 i | |||
2-1/2 40 14'-6" 138 16'-9" 120 80 15'-0" 168 152 | |||
160 16'-7' 1/2 15'-1" 202 16'-2" 190 1 | |||
3 40 15'-6" 210 la'-)" 199 80 16'-2" 248 18'-1" 232 160 1/2 16'-7" 326 17'-10" 306 | |||
j 3-1/2 40 16'-7" 272 19'-9" 232 80 17'-5" 340 19'-9" 302 XXS 5/8 17'-11" 520 18 ' - 11 '' 496 i | |||
4 4 40 17'-7" 346 21'-2" 290 80 18*-7" 436 21'-3" 394 | 4 4 40 17'-7" 346 21'-2" 290 80 18*-7" 436 21'-3" 394 | ||
~ | ~ | ||
160 5/8 | 160 5/8 19'-2" 584 20'-6" 542 The actual span should not exceed the recommended value by more than 1 foot. | ||
I B-5 a c) _ _ | |||
19'-2" 584 20'-6" 542 | |||
I | |||
B-5 | |||
a c) _ _ | |||
f CARGENTO LUNDY E N G1N E E RS B-3 Sample Problem emeno APPENDIX B SL-3159 RE V. 1, 7-29-77 o _ | f CARGENTO LUNDY E N G1N E E RS B-3 Sample Problem emeno APPENDIX B SL-3159 RE V. 1, 7-29-77 o _ | ||
_f /A' . | _f /A' . | ||
D' | D' | ||
; | ; | ||
"f'.'-f. | "f'.'-f. | ||
@~ @ | @~ @ | ||
.b | .b | ||
) ! | ) ! | ||
l | l | ||
] | ] | ||
Fig. B-1. | Fig. B-1. | ||
O I Pipe Size I/" Sch. 40 2 | O I Pipe Size I/" Sch. 40 2 | ||
| Line 8,975: | Line 5,495: | ||
1 0 | 1 0 | ||
]o / "". _ | ]o / "". _ | ||
e*e , | e*e , | ||
e . | e . | ||
o g r. e | o g r. e e y 20th 1 H 51b ! | ||
e y 20th 1 H 51b ! | |||
l Figure B-1 is an isometric of sampic probl'em one. It includes labels for all steps, marks to indicate the end-points of steps, and symbols ( ) to indicate su.pport locations. The worksheet for this system is attached a44d should be | l Figure B-1 is an isometric of sampic probl'em one. It includes labels for all steps, marks to indicate the end-points of steps, and symbols ( ) to indicate su.pport locations. The worksheet for this system is attached a44d should be | ||
-1 tua. tea with the following discussion. | -1 tua. tea with the following discussion. | ||
1 | 1 H | ||
H | |||
Step one is a hal::-span of plain pipe nupported at end A by the header. By rule one a support is required at one end. Since the i L ' | Step one is a hal::-span of plain pipe nupported at end A by the header. By rule one a support is required at one end. Since the i L ' | ||
} | } | ||
support at end A is provided by the header no actual hanger is 1 | |||
support at end A is provided by the header no actual hanger is | L q needed, so the worksheet indicates no required supports. The l | ||
]: U y step length is'one half the normal span. The span load may be B-6 | |||
]: U | |||
y step length is'one half the normal span. The span load may be B-6 | |||
'O e | 'O e | ||
CAR 2ENT O LUNDY ENGINEERS APPENDIX B | CAR 2ENT O LUNDY ENGINEERS APPENDIX B | ||
**'*^'' | **'*^'' | ||
| Line 9,007: | Line 5,513: | ||
.} B-3 (continued) REV. 1, 7-29-77 11 ted on the worx deet, but is oa1r 1 gorteat for comgerieoa | .} B-3 (continued) REV. 1, 7-29-77 11 ted on the worx deet, but is oa1r 1 gorteat for comgerieoa | ||
]O with concentrated weights. Rule 9 is always used implicitly: | ]O with concentrated weights. Rule 9 is always used implicitly: | ||
it is not indicated on the worksheet. | it is not indicated on the worksheet. | ||
Step two is also a plain half-span, but it is not supported at end A. Therefore, it must be supported at end B as is indicated | Step two is also a plain half-span, but it is not supported at end A. Therefore, it must be supported at end B as is indicated | ||
) on the worksheet. Si:.ce a support at end A is unnecessary it | ) on the worksheet. Si:.ce a support at end A is unnecessary it is not recommended. | ||
is not recommended. | |||
Step three contains an elbow and so must be supported on both sides (Rule 2). The step length is measured along the tangent | Step three contains an elbow and so must be supported on both sides (Rule 2). The step length is measured along the tangent | ||
] lines of the elbow, | ] lines of the elbow, 1 | ||
1 | |||
lo Step four is plain pipe and is supported at end A (step three end B) so no additional support is required. | lo Step four is plain pipe and is supported at end A (step three end B) so no additional support is required. | ||
Step five must be supported at one end. End B is choseri e,ince support at end A would put an unnecessary support on step four at end B. | Step five must be supported at one end. End B is choseri e,ince support at end A would put an unnecessary support on step four at end B. | ||
] | ] | ||
Step six is also plain pipe and the support 2.t end B of section five satisfies the support requirexr.u. | Step six is also plain pipe and the support 2.t end B of section five satisfies the support requirexr.u. | ||
Step seven includes an elbow so it must be supported at both ends. | Step seven includes an elbow so it must be supported at both ends. | ||
] Notice that this puts a support at end B of step six so that | ] Notice that this puts a support at end B of step six so that | ||
, step six is a half-span of plain pipe supported at both ends. The B suggert is unnecessary for steg six dut neceesery for steg seven, | , step six is a half-span of plain pipe supported at both ends. The B suggert is unnecessary for steg six dut neceesery for steg seven, o] | ||
o] | |||
1 | 1 | ||
CARGENT O LUNDY E N G1N E E A5 C"'C " APPENDIX D SL-3159 RE V. 1, 7-29-77 A | CARGENT O LUNDY E N G1N E E A5 C"'C " APPENDIX D SL-3159 RE V. 1, 7-29-77 A | ||
V B-3 Sample Problem (continued) so rule 9 is not violated. | V B-3 Sample Problem (continued) so rule 9 is not violated. | ||
| Line 9,043: | Line 5,538: | ||
;) ' | ;) ' | ||
] | ] | ||
0 1 | 0 1 | ||
] n-8 | ] n-8 | ||
9 | 9 CARGENTO LUNDY E N GIN E EDS APPENDIX B I C"'C^' | ||
SL-3159 REV.1. 7-29-77 i | |||
CARGENTO LUNDY E N GIN E EDS APPENDIX B I C"'C^' | WEIGHT SUPPORT SYSTEM DESIGN WORKSHEET | ||
SL-3159 REV.1. 7-29-77 | |||
] | ] | ||
Line Identification Information WEIGHT SAMPLE #1 STEP SPAN PIPING ELEMENT S U PPOR'l STEP DESIGN SO. l NORMAL SPAN l LOADDESCRIPTION A 13 LENGTH RULES | Line Identification Information WEIGHT SAMPLE #1 STEP SPAN PIPING ELEMENT S U PPOR'l STEP DESIGN SO. l NORMAL SPAN l LOADDESCRIPTION A 13 LENGTH RULES | ||
. I 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 | . I 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 2 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 3 11' - 4" 52 lb. Elbow X X 5' - 8" 2 4 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 5 11' - 4" 52 lb. Plain Pipe X 5' - 8" 1 6 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 7 11' - 4" 52 lb. Elbow X X S' - 8" 2 8 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 9 11' - 4" 52 lb. Plain Pipe X S' - 8" | ||
2 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 | |||
3 11' - 4" 52 lb. Elbow X X 5' - 8" 2 | |||
4 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 5 11' - 4" 52 lb. Plain Pipe X 5' - 8" 1 6 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 7 11' - 4" 52 lb. Elbow X X S' - 8" 2 8 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 | |||
9 11' - 4" 52 lb. Plain Pipe X S' - 8" | |||
- 1 10 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 | - 1 10 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 | ||
_ 11 11' - 4" 52 lb. Plain Pipe X 5' - 8" 1 | _ 11 11' - 4" 52 lb. Plain Pipe X 5' - 8" 1 | ||
] 12 11' - 4" 52 lb. | ] 12 11' - 4" 52 lb. | ||
Plain Pipe 5' - 8" I n 13 11' - 4" 52 lb. 20 lb. Vnive ' | |||
Plain Pipe 5' - 8" I | \ \ 5' - 8" 4 g 1 14 11' - 4" 52 lb. Plain Pipe 5' - 8" I h 15 11' - 4" 52 lb. Plain Pipe X 5' - 8" I c | ||
n 13 11' - 4" 52 lb. 20 lb. Vnive ' | |||
\ \ 5' - 8" 4 g 1 | |||
14 11' - 4" 52 lb. Plain Pipe 5' - 8" I h 15 11' - 4" 52 lb. Plain Pipe X 5' - 8" I c | |||
16 11' - 4" 52 lb. Free end Cone. wt X 5' - 8" 8 | 16 11' - 4" 52 lb. Free end Cone. wt X 5' - 8" 8 | ||
[O , | [O , | ||
I B ') | I B ') | ||
b Final e. | b Final e. | ||
t | t | ||
CARGENT Q LUNDY E N GIN E Eno APPENDIX C SL-3159 REV.1. 7-29-77 13 SEISMIC SUPPORTS SYSTEM DESIGN The nature of seismic loading is similar to that of weight loading: a distributed force acts upon each element of a piping system in proportion to its mass. However, the seismic loading is horizontal as well as vertical. Therefore, a procedure similar to that which is used for locating weight supports may be used to locate seismic support.< | |||
CARGENT Q LUNDY E N GIN E Eno | |||
APPENDIX C SL-3159 REV.1. 7-29-77 13 SEISMIC SUPPORTS SYSTEM DESIGN The nature of seismic loading is similar to that of weight loading: a distributed force acts upon each element of a piping system in proportion to its mass. However, the seismic loading is horizontal as well as vertical. Therefore, a procedure similar to that which is used for locating weight supports may be used to locate seismic support.< | |||
if provision is made for including horizontal restraints at these locations. | if provision is made for including horizontal restraints at these locations. | ||
Regarding vertical seismie loading, one set of restrainte enn serse as both weight supports and vertical scismic restraints. Choose the shorter of the weight span and , | Regarding vertical seismie loading, one set of restrainte enn serse as both weight supports and vertical scismic restraints. Choose the shorter of the weight span and , | ||
vertical seismic span for_the building in which the, system is locate.d. | vertical seismic span for_the building in which the, system is locate.d. | ||
Once the system is adequately restrained to resist vertical seismic loading, the system must be restrained for the two horizontal scismic loadings. For vertical pipe | Once the system is adequately restrained to resist vertical seismic loading, the system must be restrained for the two horizontal scismic loadings. For vertical pipe | ||
] runs, two orthogonallateral supports are required at each r_estraint location (choose | ] runs, two orthogonallateral supports are required at each r_estraint location (choose the shor'.er of the E-W and N-S spans). For horbntal runs, one horizontal restraint is l | ||
the shor'.er of the E-W and N-S spans). For horbntal runs, one horizontal restraint is | |||
l | |||
required at each location. The following procedure is recommended for location of : | required at each location. The following procedure is recommended for location of : | ||
O LJ these horizontal scismic restraints. | O LJ these horizontal scismic restraints. | ||
C-1 Procedure for Seismic Support System Des ,7 Starting from a convenient point (nozzle, st ntural anchor her der connection, etc.) the piping is traversed in steps, called balf-spans, of len, th equal to one half the recommended span from Tatle C-1 (normal seismic ! >an). Th" steps l 3 may be shortened to accommodate special piping componen s and must be | C-1 Procedure for Seismic Support System Des ,7 Starting from a convenient point (nozzle, st ntural anchor her der connection, etc.) the piping is traversed in steps, called balf-spans, of len, th equal to one half the recommended span from Tatle C-1 (normal seismic ! >an). Th" steps l 3 may be shortened to accommodate special piping componen s and must be | ||
,J supported on one or both sides according to the rules given be civ. Only one | ,J supported on one or both sides according to the rules given be civ. Only one l | ||
step is made at a time and each ir asched a ' nig te in'.cger abel which 13 | |||
,,, marked on an isometric of the system. The isomety is included in the system design documentation along with the se's'nic support -" stem design orks'ieets (see sample problems). These worksheets lis* all steps numeric: illy and include a description of the elements in each step, the length and rceommended supports for each step, and the rules which govern the design decisions. The worksheet is used as an aid to system design and as documentation to show that the requirements of the standard have been met. Enough information should be | |||
,,, marked on an isometric of the system. The isomety is included in the system design documentation along with the se's'nic support -" stem design orks'ieets (see sample problems). These worksheets lis* all steps numeric: illy and include a | |||
description of the elements in each step, the length and rceommended supports for each step, and the rules which govern the design decisions. The worksheet is | |||
used as an aid to system design and as documentation to show that the | |||
requirements of the standard have been met. Enough information should be | |||
!= presented to show that the designer has considered all relevant system O enaiacteristics. | != presented to show that the designer has considered all relevant system O enaiacteristics. | ||
1 < | 1 < | ||
c-1 b | c-1 b | ||
CARGENTO LUNDY | CARGENTO LUNDY | ||
, ENGINEER 9 | , ENGINEER 9 | ||
***^* | ***^* | ||
APPENDlX C | APPENDlX C SL-3159 REV.1. 7-29--77 | ||
'Ihe steps are made in a consistent direction, and branch lines are traversed only after an end point of the main run is rehehed. Each step has two ends, A and F, where A to B is the direction of traversing. The support system is completely defined by specifying the length of each step, the ends which require support, and the support types. Note that end A of one step is end B of the preceding step, btit each support is listed only once on the worksheet. That is, if a given I step mi.st be supported on end A, it is not necessary to indicate that a support is J | |||
SL-3159 REV.1. 7-29--77 | |||
'Ihe steps are made in a consistent direction, and branch lines are traversed only after an end point of the main run is rehehed. Each step has two ends, A and F, | |||
where A to B is the direction of traversing. The support system is completely defined by specifying the length of each step, the ends which require support, and the support types. Note that end A of one step is end B of the preceding | |||
step, btit each support is listed only once on the worksheet. That is, if a given I step mi.st be supported on end A, it is not necessary to indicate that a support is J | |||
required at end A of the following step. The worksheet only indicates additional supports, which are required due to the characteristics of each successive ste[. | required at end A of the following step. The worksheet only indicates additional supports, which are required due to the characteristics of each successive ste[. | ||
A summary of this procedure follows. | A summary of this procedure follows. | ||
| Line 9,141: | Line 5,593: | ||
l l | l l | ||
C-2 Rules for Locating Seismic Supports | C-2 Rules for Locating Seismic Supports | ||
] 1. A horizontal half-span must have a horizontal, lateral restraint at one | ] 1. A horizontal half-span must have a horizontal, lateral restraint at one end. | ||
end. | |||
] 2. A ~ vertical half-span must have two orthogonal, horizontal restraints at one end. | ] 2. A ~ vertical half-span must have two orthogonal, horizontal restraints at one end. | ||
: 3. A ha f-span which includes a bend and lies in a vertical plane must be | : 3. A ha f-span which includes a bend and lies in a vertical plane must be | ||
! g suppcrted at both ends--a horizontal, lateral support at the horizontal end | ! g suppcrted at both ends--a horizontal, lateral support at the horizontal end | ||
. and two orthogonal, lateral supports on the vertical end (see rule 14). i e | . and two orthogonal, lateral supports on the vertical end (see rule 14). i e | ||
1 c-2 . | |||
1 | 1 | ||
- - m ,-- ---- | - - m ,-- ---- | ||
CARGENT O LUNDY ENGlNEER5 CMsCAGO APPENDIX C SL-3159 RE V. 1, 7 77 o 4. A straight, horizontal section of pipe which is less than 4/10 of the normal span in length requires no horizontal restraints. It is treated as a concentrated weight in its axial direction. | CARGENT O LUNDY ENGlNEER5 CMsCAGO APPENDIX C SL-3159 RE V. 1, 7 77 o 4. A straight, horizontal section of pipe which is less than 4/10 of the normal span in length requires no horizontal restraints. It is treated as a concentrated weight in its axial direction. | ||
: 5. A horizontal section of pipe whose length exceeds 4/10 of the normal span | : 5. A horizontal section of pipe whose length exceeds 4/10 of the normal span must be restrained along its axis. | ||
must be restrained along its axis. | |||
: 6. A half-span which contains a concentrated weight of less than 10% of the normal seismic-span weight should not exceed 40% of the normal-span length. It should be supported on one side with horizontal restraints. | : 6. A half-span which contains a concentrated weight of less than 10% of the normal seismic-span weight should not exceed 40% of the normal-span length. It should be supported on one side with horizontal restraints. | ||
: 7. A half-span which includes a concentrated weight of from 10% to 75% of the normal seismic-span weight must be supported on both ends with | : 7. A half-span which includes a concentrated weight of from 10% to 75% of the normal seismic-span weight must be supported on both ends with | ||
] 8. | ] 8. | ||
horizontal restraints. | horizontal restraints. | ||
The length of a half-span which includes a concentrated weight of more tnan 75% but less than 250% of the normal seismic-span weight should not exceed 10% of the normal span (exclusive of the actual length of the | The length of a half-span which includes a concentrated weight of more tnan 75% but less than 250% of the normal seismic-span weight should not exceed 10% of the normal span (exclusive of the actual length of the | ||
~ j concentrated weight). This half-span should be supported on both ends by | ~ j concentrated weight). This half-span should be supported on both ends by | ||
| Line 9,173: | Line 5,614: | ||
] 9. A concentrated weight which exceeds 250% of the normal scismic-span weight should be supported directly, rather than by the piping to which it is attached. Horizontal support i.; required at the center of gravity. | ] 9. A concentrated weight which exceeds 250% of the normal scismic-span weight should be supported directly, rather than by the piping to which it is attached. Horizontal support i.; required at the center of gravity. | ||
] 10. In general, motor operators fo valves should be restrained in three | ] 10. In general, motor operators fo valves should be restrained in three | ||
] orthogonal directions. For vertically mounted operators, only horizontal, . | ] orthogonal directions. For vertically mounted operators, only horizontal, . | ||
lateral support is required. i 2 | lateral support is required. i 2 | ||
: 11. A half-span with a concentrated weight shou ~ not have a free end: hori- i 3 zontal, lateral support should be provided. | : 11. A half-span with a concentrated weight shou ~ not have a free end: hori- i 3 zontal, lateral support should be provided. | ||
| Line 9,184: | Line 5,621: | ||
. hangers. | . hangers. | ||
14.' 'As an alternative to rule 3, a half-span which includes an elbow may end at the elbow and be supported at a tangent point. | 14.' 'As an alternative to rule 3, a half-span which includes an elbow may end at the elbow and be supported at a tangent point. | ||
O | O 1 | ||
l E I | |||
1 | 1 | ||
? 1 | ? 1 | ||
'1 w CARGENTQ LUNDY E N G 1 N E E C7 8 c .cac.o APPENDIX C SL-3159 REV.1, 7-29-77 | |||
'1 w CARGENTQ LUNDY | |||
E N G 1 N E E C7 8 | |||
c .cac.o APPENDIX C SL-3159 REV.1, 7-29-77 | |||
'30 i. | '30 i. | ||
TABLE C-1 REACTOR BUILDING RECOMMENDED SPANS FOR SEISMIC SUPPORTS 1 | TABLE C-1 REACTOR BUILDING RECOMMENDED SPANS FOR SEISMIC SUPPORTS 1 | ||
N O Al . N ORTH-SO U TH EAST-W EST \ ERTIC A L DI A M . Scil. SPAN LOAD SPAN LOAD SPAN LOAD | N O Al . N ORTH-SO U TH EAST-W EST \ ERTIC A L DI A M . Scil. SPAN LOAD SPAN LOAD SPAN LOAD 3/8 | ||
3/8 | |||
: 0. 9 q_ 7 1.25 7 1.25 4 1.0 1/2 160 10 16.75 9 9.50 6 15.5 | : 0. 9 q_ 7 1.25 7 1.25 4 1.0 1/2 160 10 16.75 9 9.50 6 15.5 | ||
: 5. og8a" s, e 3.0 e 4.25 e 4.50 3 | : 5. og8a" s, e 3.0 e 4.25 e 4.50 3 | ||
3/4 160 11 14.25 11 22.0 7 24.0 Q 1 160 13 33.0 12 23.0 8 38.5 ' | 3/4 160 11 14.25 11 22.0 7 24.0 Q 1 160 13 33.0 12 23.0 8 38.5 ' | ||
il 160 15 51.5 14 40.0 l 10 63.25 | il 160 15 51.5 14 40.0 l 10 63.25 il 160 16 58.0 47.75 | ||
il 160 16 58.0 47.75 | |||
_15 10 79.25 | _15 10 79.25 | ||
] 2 160 18 91.0 17 81.75 12 141.25 24 160 20 133.0 19 126.75 13 205.0 l | ] 2 160 18 91.0 17 81.75 12 141.25 24 160 20 133.0 19 126.75 13 205.0 l | ||
3 160 - 22 178.0 21 185.5 14 271.25 34 80XS 24 265.5 23 26i.0 15 317.75 4 120 26 441 24 299.5 16 423.25 UNITS: NOMINAL DIAMETER - IN. | 3 160 - 22 178.0 21 185.5 14 271.25 34 80XS 24 265.5 23 26i.0 15 317.75 4 120 26 441 24 299.5 16 423.25 UNITS: NOMINAL DIAMETER - IN. | ||
SPANS - FT. | SPANS - FT. | ||
| Line 9,217: | Line 5,641: | ||
I | I | ||
; o . | ; o . | ||
C-4 | C-4 | ||
f, CARGENTQLUNDY ENGINEERS APPENDIX C a ** ' ! | f, CARGENTQLUNDY ENGINEERS APPENDIX C a ** ' ! | ||
SL-3159 REV.1. 7-29-77 | SL-3159 REV.1. 7-29-77 1 | ||
b' TABLE C-2 TURBINE BL'ILDit!G RECOMMENDED SPANS FOR SEISMIC SUPPORTS r | |||
NOM. NORTH-SOUTH E AST-W EST DIAM . SCll. VERTICAL SPAN LOAD SPAN LOAD SPAN LOA { | NOM. NORTH-SOUTH E AST-W EST DIAM . SCll. VERTICAL SPAN LOAD SPAN LOAD SPAN LOA { | ||
0 9 3/8 5 0.75 6 1.75 4 1.0 1 1/2 160 7 8.25 8 15.75 5 8.0 5/8 | 0 9 3/8 5 0.75 6 1.75 4 1.0 1 1/2 160 7 8.25 8 15.75 5 8.0 5/8 | ||
| Line 9,238: | Line 5,658: | ||
: n. C-5 l J ! | : n. C-5 l J ! | ||
t T*' CARGENTQ LUNDY cuosuceno APPENDIX C | t T*' CARGENTQ LUNDY cuosuceno APPENDIX C SL-3159 REV.1. 7-29-77 h | ||
SL-3159 REV.1. 7-29-77 h | |||
[] | [] | ||
TABLE C-3 RHR COMPLEX RECOMMENDED SPANS FOR | TABLE C-3 RHR COMPLEX RECOMMENDED SPANS FOR | ||
| Line 9,250: | Line 5,667: | ||
SPANS - FT. | SPANS - FT. | ||
] LOADS - LBS. | ] LOADS - LBS. | ||
t o | t o | ||
, C-6 l | , C-6 l | ||
u | u e | ||
e | |||
._,. car 2 GENT O LUNDY E N GIN E E Rs APPENDIX C c .cao SL - 3159 REV.1. 7- 29 77 C-3 Sample Problem Following is an isometric of a system for which horizontal seismic restraint locations have been chosen according to the seismic support system design rules. The isometric is marked as required by the procedure and the worksheet is completed. Certain characteristics of the support system cannot be defined g without consideration of thermal expansion and anchor movements. These J include locations where snubbers rather than rigid restraints are to be used and preferred locations for axial restraints. | ._,. car 2 GENT O LUNDY E N GIN E E Rs APPENDIX C c .cao SL - 3159 REV.1. 7- 29 77 C-3 Sample Problem Following is an isometric of a system for which horizontal seismic restraint locations have been chosen according to the seismic support system design rules. The isometric is marked as required by the procedure and the worksheet is completed. Certain characteristics of the support system cannot be defined g without consideration of thermal expansion and anchor movements. These J include locations where snubbers rather than rigid restraints are to be used and preferred locations for axial restraints. | ||
] The support description includes the end which is supported, the number of restraints and the restraint orientation. "B-2-liOR-LAT" means two horizontal, lateral supports are required at end B. | ] The support description includes the end which is supported, the number of restraints and the restraint orientation. "B-2-liOR-LAT" means two horizontal, lateral supports are required at end B. | ||
s Jo | s Jo 3 | ||
3 | |||
] | ] | ||
] | ] | ||
| Line 9,269: | Line 5,679: | ||
} . | } . | ||
J 1 | J 1 | ||
1 | 1 | ||
} | } | ||
LO8 | LO8 | ||
> C-7 l | > C-7 l | ||
l | l | ||
-- yg- ---- wm r n 1 M W &~ O' Y W & W % | -- yg- ---- wm r n 1 M W &~ O' Y W & W % | ||
O O O fY W | O O O fY W | ||
,,. ;-=. N' = | ,,. ;-=. N' = | ||
! le e s? | ! le e s? | ||
/ | / | ||
l] :.8; 2s a | l] :.8; 2s a | ||
: s. . | : s. . | ||
es h ft fe, | es h ft fe, | ||
'r ' F 4 a. z' , / ,,. | 'r ' F 4 a. z' , / ,,. | ||
| Line 9,301: | Line 5,701: | ||
'A ? A_ F,, | 'A ? A_ F,, | ||
.. : cc\ ir =. | .. : cc\ ir =. | ||
c F | c F | ||
s ,, | s ,, | ||
160 lb. 2 ' ler.g g 3 | 160 lb. 2 ' ler.g g 3 0 | ||
f i | |||
(< | (< | ||
P1 Y | P1 Y | ||
x* | x* | ||
L_3 , | L_3 , | ||
| Line 9,316: | Line 5,713: | ||
NORMAL SPAN W ICPT: '90 l b. | NORMAL SPAN W ICPT: '90 l b. | ||
- mm> | - mm> | ||
Qc==a | Qc==a ISOMETRIC FOR SAMPLE SEISMIC PROBLEM .mm Y -. G 2 | ||
=9 p o b 7 d | =9 p o b 7 d | ||
~; | ~; | ||
f | f CARGENT' O LUNDY j ENGINEERS APPENDIX C | ||
CARGENT' O LUNDY j ENGINEERS APPENDIX C | |||
, c mu.c." | , c mu.c." | ||
SL- 3159 REV.1. 7-29-77 p | SL- 3159 REV.1. 7-29-77 p | ||
'd SEISMIC SUPPORT SYSTEM -DESIGN WORKSHEET I | 'd SEISMIC SUPPORT SYSTEM -DESIGN WORKSHEET I | ||
s l 5.P NORMAL SP/ N SUPPOR'l% S i l l' IHNii s N jN O. SPAN W EPdlT PlPING El,LMEN r 1)ESt:RIPflON A 18 1.ENilTil ItUI.IN t 'OM M I N IN | s l 5.P NORMAL SP/ N SUPPOR'l% S i l l' IHNii s N jN O. SPAN W EPdlT PlPING El,LMEN r 1)ESt:RIPflON A 18 1.ENilTil ItUI.IN t 'OM M I N IN Fixed at End A g i 20' 190 10. Vert. with 281b. valve B-2-l!OR-LAT 10' T- , | ||
Fixed at End A g i 20' 190 10. Vert. with 281b. valve B-2-l!OR-LAT 10' T- , | |||
2 , Bend in Vertical Plane B-1-ilO R-L A I 3 f l 3 Plain Pipe ; i l l | 2 , Bend in Vertical Plane B-1-ilO R-L A I 3 f l 3 Plain Pipe ; i l l | ||
4 ; Plain Pipe Il- 1 -llO R-i- A I I l l | 4 ; Plain Pipe Il- 1 -llO R-i- A I I l l 5 Plain Pipe I l l 14 190 R-l. 41' l l j b Plain Pipe Ending at Elbow li- % \ l l 5 l | ||
5 Plain Pipe I l | |||
l 14 190 R-l. 41' l l j b Plain Pipe Ending at Elbow li- % \ l l 5 l | |||
j 3 ' 7 Plain hoc I LAT. Suppori at 7A Acts al Plain ISpc Endung ut Elbow ll- t -ilO R- LA I I,5 Axistly Plain Pipe Elbow in | j 3 ' 7 Plain hoc I LAT. Suppori at 7A Acts al Plain ISpc Endung ut Elbow ll- t -ilO R- LA I I,5 Axistly Plain Pipe Elbow in | ||
, 9 Horizontal Plane I lbl-HOR-L AT g | , 9 Horizontal Plane I lbl-HOR-L AT g | ||
10 j Plain Pipe Ends at Elbow 11- A Al 14,5 l | 10 j Plain Pipe Ends at Elbow 11- A Al 14,5 l | ||
l11 l Plain Pipe (vertical) l 2 l | l11 l Plain Pipe (vertical) l 2 l | ||
I /-~jl2 l f Section Ends at Tee l B-t-liOR-LA I 5' | I /-~jl2 l f Section Ends at Tee l B-t-liOR-LA I 5' | ||
l 2 l l | l 2 l l IJ Plain Pipe H-2-HOH-L A r 10' i ! i | ||
IJ Plain Pipe H-2-HOH-L A r 10' i ! i | |||
{ | { | ||
g 14 Plain Pipe witti Lit >ow Il- 1 -ilOR-L A I 3 15 Plain Pipe 1 in Plain Pipe it-i-HOR-L AT I I; Pinin Pape I lia \ l les l'inin Pym l.'nel, nl 1.ltam li ? !!Oli 84 I 3. 5 u f 19 Plam ISpc l l l I h I 20 Pemt in Vertical Pirene it-I flor-l.? ! I n' 14 l l f 21 Plain Pipe 1 7' | |||
g 14 Plain Pipe witti Lit >ow Il- 1 -ilOR-L A I 3 15 Plain Pipe 1 | |||
in Plain Pipe it-i-HOR-L AT I I; Pinin Pape I | |||
lia \ l les l'inin Pym l.'nel, nl 1.ltam li ? !!Oli 84 I 3. 5 u f 19 Plam ISpc | |||
l l l I h I 20 Pemt in Vertical Pirene it-I flor-l.? ! I n' 14 l l f 21 Plain Pipe 1 7' | |||
l 1 l l | l 1 l l | ||
: e. .iuiH. A i | : e. .iuiH. A i | ||
' , Suppict Motor 22 l~ 160 lp. valve iH - HO R-L A T 4' ! 8,10 | ' , Suppict Motor 22 l~ 160 lp. valve iH - HO R-L A T 4' ! 8,10 | ||
, Opere tor 2J ' | , Opere tor 2J ' | ||
f Plain Pipe Fixed at End 11 '- | f Plain Pipe Fixed at End 11 '- | ||
| Line 9,373: | Line 5,745: | ||
, %ertical Plain Pipe 26 Fased at End H | , %ertical Plain Pipe 26 Fased at End H | ||
, 10' g,1 V( | , 10' g,1 V( | ||
h | h | ||
~ | ~ | ||
C-9 Final j | C-9 Final j | ||
CARGENTQLUNDY EN GIN E E R s APPENDIX D c nc^" | CARGENTQLUNDY EN GIN E E R s APPENDIX D c nc^" | ||
SL-3159 FLEXIBILITY SUPPORT SYSTEM DESIGN REV. f, 7-29-77 | SL-3159 FLEXIBILITY SUPPORT SYSTEM DESIGN REV. f, 7-29-77 D-1 Procedure O | ||
D-1 Procedure O | |||
Starting at a convenient point (e.g., equipment nozzle, r | Starting at a convenient point (e.g., equipment nozzle, r | ||
structural anchor, header connection) traverse the entire | structural anchor, header connection) traverse the entire | ||
.1 system once for each orthogonal direction of thermal move-ment, following the steps below for each successive pair | .1 system once for each orthogonal direction of thermal move-ment, following the steps below for each successive pair of adjacent parallel (i.e., acting in the same direction) restraints. | ||
1 i On the thermal worksheet, identify the restraint pair 1. | |||
of adjacent parallel (i.e., acting in the same direction) restraints. | |||
1 i On the thermal worksheet, identify the restraint pair | |||
1. | |||
, and direction, l | , and direction, l | ||
: 2. Determine the total expanding length of pipe in the restraint direction between the pair and enter it on the worksheet. If one of the restraints is a header or equipment nozzle with thermal movement in the restraint direction, enter this movement on the work-sheet. | : 2. Determine the total expanding length of pipe in the restraint direction between the pair and enter it on the worksheet. If one of the restraints is a header or equipment nozzle with thermal movement in the restraint direction, enter this movement on the work-sheet. | ||
| Line 9,401: | Line 5,761: | ||
-O k 4. Determine the actual existing offset - total length of D-1 | -O k 4. Determine the actual existing offset - total length of D-1 | ||
] | ] | ||
g gg g g g M M M M M h h h M M h M U \ | g gg g g g M M M M M h h h M M h M U \ | ||
| Line 9,412: | Line 5,771: | ||
1-1/4 Sft 6in 7ft 9ir m3 9ft 61n 30ft 11in 12ft 32n 13ft Sin 14ft 61n 15ft 6in 16ft Sin 17ft 41n 2 O y 1-1/2 Sft loin Bft no m 3i-10ft 2in Ilft 91n 13ft !in 14ft 4in 15ft 61n 16ft '* in 17ft 6in l'Jf t 61D - | 1-1/4 Sft 6in 7ft 9ir m3 9ft 61n 30ft 11in 12ft 32n 13ft Sin 14ft 61n 15ft 6in 16ft Sin 17ft 41n 2 O y 1-1/2 Sft loin Bft no m 3i-10ft 2in Ilft 91n 13ft !in 14ft 4in 15ft 61n 16ft '* in 17ft 6in l'Jf t 61D - | ||
2 6ft 61n 9ft 3i 11tt 4in 13ft lin 14ft */ i n 16ft 'in 17ft 41n 18ft sin 19ft 7in 20ft Bin 2-1/2 7ft 2in 10ft 2. | 2 6ft 61n 9ft 3i 11tt 4in 13ft lin 14ft */ i n 16ft 'in 17ft 41n 18ft sin 19ft 7in 20ft Bin 2-1/2 7ft 2in 10ft 2. | ||
a r-12ft 6in 34ft 41n 16ft Iin 17ft 3in 19ft Oin 20ft lin 21ft 71n 22ft 91n *Cz 3 7ft 111, 11ft 3i- O 13ft 91n 15ft loin 17ft 9fn 19ft 5in 21ft Oin 22ft iin 23ft loin 25ft lin "< | a r-12ft 6in 34ft 41n 16ft Iin 17ft 3in 19ft Oin 20ft lin 21ft 71n 22ft 91n *Cz 3 7ft 111, 11ft 3i- O 13ft 91n 15ft loin 17ft 9fn 19ft 5in 21ft Oin 22ft iin 23ft loin 25ft lin "< | ||
3-1/2 Hft 6in 12f t Oi 14'' | 3-1/2 Hft 6in 12f t Oi 14'' | ||
sin 17ft Oin 19ft Oin 20ft 91n 22ft 61n 24ft 'in 25ft 61n 26ft loin 4 9ft nin 12ft 9i .Sft 7in left Oin 20ft ;in 22ft Oin 23ft loin 25ft ein 27ft Oin 28ft 61n | sin 17ft Oin 19ft Oin 20ft 91n 22ft 61n 24ft 'in 25ft 61n 26ft loin 4 9ft nin 12ft 9i .Sft 7in left Oin 20ft ;in 22ft Oin 23ft loin 25ft ein 27ft Oin 28ft 61n (a)This is the minimum lenti th ni piae which is installed perpendicular to the Sirection of no zie move nent between the nozzle and the firsi. r. | ||
(a)This is the minimum lenti th ni piae which is installed perpendicular to the Sirection of no zie move nent between the nozzle and the firsi. r. | |||
considered. traint wht-5 acts in that direction. Movements in three orthw onal directions are' | considered. traint wht-5 acts in that direction. Movements in three orthw onal directions are' | ||
:D (/) > | :D (/) > | ||
M f~ T bk2 | M f~ T bk2 y eO i X | ||
y eO i X | |||
~ | ~ | ||
O T | O T | ||
0 | 0 | ||
mm-N | mm-N W tomt N O M $ W W E U E E | ||
W tomt N O M $ W W E U E E | |||
) | ) | ||
O - | O - | ||
O TABLE D-2 MINIMUM OFFSET REQUIRED TO ACCOMMODATE THERMAL EXPANSION OF PIPING, FEET EXPANDING LENGTH OF PIPE., FEET | O TABLE D-2 MINIMUM OFFSET REQUIRED TO ACCOMMODATE THERMAL EXPANSION OF PIPING, FEET EXPANDING LENGTH OF PIPE., FEET N)minal ,, | ||
N)minal ,, | |||
Diam?ter, i; Inch f | Diam?ter, i; Inch f | ||
! 10 15 20 25 30 b 35 40 45 50 I 3/8(tubs) 1*-11" 2'-9" 3*-4" 3'-1C" 4'-3" 4'-8" 5'-1" I 5'-5" 5'-9" 6'-1" 1/2 U 2'-2" 3'-0" 3'-8" 4*-3" 4'-9" 5'-3" 5'-8" 6'-1" 6*-5" 6'-9" M ; | ! 10 15 20 25 30 b 35 40 45 50 I 3/8(tubs) 1*-11" 2'-9" 3*-4" 3'-1C" 4'-3" 4'-8" 5'-1" I 5'-5" 5'-9" 6'-1" 1/2 U 2'-2" 3'-0" 3'-8" 4*-3" 4'-9" 5'-3" 5'-8" 6'-1" 6*-5" 6'-9" M ; | ||
| Line 9,443: | Line 5,790: | ||
6'-5" 6'-10" 7'-2" j ,3 'l 3/4 2'-5' 3 '-5 ' 4'-2" 4'-9" 1 2 0 m | 6'-5" 6'-10" 7'-2" j ,3 'l 3/4 2'-5' 3 '-5 ' 4'-2" 4'-9" 1 2 0 m | ||
e 5'-4* 5'-10" 6'-4" 6*-9" 7*-2" '7'-7" s no Z u 1 2'-t' 3'-9" 4'-8" 5'-4" 6*-;" 6*-7" 7'-1" 7'-7" z_d 5 | e 5'-4* 5'-10" 6'-4" 6*-9" 7*-2" '7'-7" s no Z u 1 2'-t' 3'-9" 4'-8" 5'-4" 6*-;" 6*-7" 7'-1" 7'-7" z_d 5 | ||
i 3'-C" 8'-5" g ,zg, ' | i 3'-C" 8'-5" g ,zg, ' | ||
1-1/4 3'-;" 4'-3" 5'-2" 6'-O" 6'-3" 7'-4" 7'-11" On 8'-6" 9'-0" 9'-6" ah 1-1/2 3 -3* 4'-7' 5'-7" 6'-5" 7'-2" 7'-11" 8'-6" 9'-1" 9'-9" | 1-1/4 3'-;" 4'-3" 5'-2" 6'-O" 6'-3" 7'-4" 7'-11" On 8'-6" 9'-0" 9'-6" ah 1-1/2 3 -3* 4'-7' 5'-7" 6'-5" 7'-2" 7'-11" 8'-6" 9'-1" 9'-9" | ||
*Z 10'-2" D | *Z 10'-2" D | ||
=2 3'-7" 5'-1" 6*-3" 7*-2" 8'-5" 8'-10" ' | =2 3'-7" 5'-1" 6*-3" 7*-2" 8'-5" 8'-10" ' | ||
9'-S" 10*-2" 10'-9" 11'-4" 2-1/2 3'-11" 5'-7" 6'-10" 7'-11" a*-10" 9'-9" 10'-5" 11'-2" 11*-10" 12'-6" | 9'-S" 10*-2" 10'-9" 11'-4" 2-1/2 3'-11" 5'-7" 6'-10" 7'-11" a*-10" 9'-9" 10'-5" 11'-2" 11*-10" 12'-6" | ||
| Line 9,454: | Line 5,799: | ||
% (A > , | % (A > , | ||
m r" T | m r" T | ||
<lT l | <lT l w rfl | ||
w rfl | |||
. ~n 2 y=2 1 X ro T | . ~n 2 y=2 1 X ro T | ||
u M | u M | ||
k CARGENTOLUNDY ENG1NEERS APPENDIX D c.ucaso SL-3159 1 pipe in the two directions perpendicular to the REV 1, 7-29-77 O | |||
k CARGENTOLUNDY ENG1NEERS APPENDIX D c.ucaso SL-3159 1 pipe in the two directions perpendicular to the REV 1, 7-29-77 | |||
O | |||
,I restraint direction between the restraint pair. | ,I restraint direction between the restraint pair. | ||
: 5. Check whether the actual offset exceeds the required offset. For restraint pairs with both expanding | : 5. Check whether the actual offset exceeds the required offset. For restraint pairs with both expanding 1ength and header or equipment nozzle thermal movement, the actual offset must exceed the sum of the associated t required offsets. If the actual offset exceeds the | ||
~I required offset, move onto the next restraint pair. | ~I required offset, move onto the next restraint pair. | ||
If the actual offset is less than the required offset, one of the rigid restraints must be changed to a snubber | If the actual offset is less than the required offset, one of the rigid restraints must be changed to a snubber | ||
| Line 9,477: | Line 5,814: | ||
I Replace w. | I Replace w. | ||
snubber and S>rino l . | snubber and S>rino l . | ||
~ | ~ | ||
10' _ __ | 10' _ __ | ||
g JT .75 2 ' MA | g JT .75 2 ' MA | ||
, ,3. . | , ,3. . | ||
~ | ~ | ||
10 C_,L 15' anch >rF l /as 3. S' / D 2p EC i O~ . | |||
10 C_,L 15' anch >rF l /as 3. S' / D 2p EC | . C .N change to snubber ' | ||
i O~ . | |||
. C .N | |||
change to snubber ' | |||
D-4 | D-4 | ||
l. | l. | ||
CARGENTC LUNDY APPENDIX D E N GIN E E R 5 CHICAGO SL-3159 REV. 1, 7-29-77 The above system will be checked for thermal flexibility; pertinent data will be entered on the thermal worksheet. | CARGENTC LUNDY APPENDIX D E N GIN E E R 5 CHICAGO SL-3159 REV. 1, 7-29-77 The above system will be checked for thermal flexibility; pertinent data will be entered on the thermal worksheet. | ||
The global X-direction will be considered first. Starting at the header, the first X-direction restraint pair is identified as A-C. The X-direction expanding length is the 10' from A to B; from Table D-2, the offset required for 10' is 5'1". The X-direction header movement of 0.25" must also be considered for restraint pair A-C - the offset required from Table D-1 is 6'6,". The amount of actual offset available (total length of pipe perpendicular to the X-direction) is the 10 f t. from B to C Since 10 f t. is less than the total 11'7" offset required, the C rigid i strut is changed to a snubber. | The global X-direction will be considered first. Starting at the header, the first X-direction restraint pair is identified as A-C. The X-direction expanding length is the 10' from A to B; from Table D-2, the offset required for 10' is 5'1". The X-direction header movement of 0.25" must also be considered for restraint pair A-C - the offset required from Table D-1 is 6'6,". The amount of actual offset available (total length of pipe perpendicular to the X-direction) is the 10 f t. from B to C Since 10 f t. is less than the total 11'7" offset required, the C rigid i strut is changed to a snubber. | ||
, i f Since the restraint at C is now a snubber, X-direction I restraint pair A-E is considered. The 25' (10' frcm A to B | , i f Since the restraint at C is now a snubber, X-direction I restraint pair A-E is considered. The 25' (10' frcm A to B plus 15' from C1 to E) expanding length requires an 53'0" offset. The 0.25" header mcvement requitec 6'6". The | ||
plus 15' from C1 to E) expanding length requires an 53'0" offset. The 0.25" header mcvement requitec 6'6". The | |||
}I total actual offset, 15 ', (i . e . , 10' from B to C plus 5' from C to C1) exceeds the total 14'6"~ required, thus accom-modating the X-direction thermal movement. | }I total actual offset, 15 ', (i . e . , 10' from B to C plus 5' from C to C1) exceeds the total 14'6"~ required, thus accom-modating the X-direction thermal movement. | ||
Considering thermal movement in the Y-direction, restraint pair A-B is examined first. Since there is no Y-direction i piping between A and B, no accommodation for piping expansion a | |||
Considering thermal movement in the Y-direction, restraint | |||
pair A-B is examined first. Since there is no Y-direction i piping between A and B, no accommodation for piping expansion a | |||
l D-5 | l D-5 | ||
CARGENTQLUNDY E N G I N ER ERS APPENDIX D | CARGENTQLUNDY E N G I N ER ERS APPENDIX D SL-3159 REV.1, 7-29 77 | ||
SL-3159 REV.1, 7-29 77 | |||
.O I is required. The Y-direction header movement at A, 0.75", | .O I is required. The Y-direction header movement at A, 0.75", | ||
requires 11'4" of offset. The actual offset available is the 10' from A to B. Since 10' is less than the required 11'4", the rigid strut at B.- hich provided both weight support and seismic restraint - is replaced with a variable | requires 11'4" of offset. The actual offset available is the 10' from A to B. Since 10' is less than the required 11'4", the rigid strut at B.- hich provided both weight support and seismic restraint - is replaced with a variable | ||
' hanger at B and a Y-direction snubber in the immediate vicinity of B or C. Next, restraint pair A-D is checked. | ' hanger at B and a Y-direction snubber in the immediate vicinity of B or C. Next, restraint pair A-D is checked. | ||
'I The expanding 10 ' from B to C requires 5 '1" offset. The 0.75" | 'I The expanding 10 ' from B to C requires 5 '1" offset. The 0.75" Y-direction header movement requires 11'4". The existing | ||
Y-direction header movement requires 11'4". The existing | |||
. offset, 17' (i.e., 10' from A to B plus 5' from C to Cl plus | . offset, 17' (i.e., 10' from A to B plus 5' from C to Cl plus | ||
.10 2' from Cl to D) exceeds the total offset required, 16'5", | .10 2' from Cl to D) exceeds the total offset required, 16'5", | ||
and is therefore adequate. Regarding restraint pair D-E, no l l d Y-direction anchor movement or piping e xpansion exists. | and is therefore adequate. Regarding restraint pair D-E, no l l d Y-direction anchor movement or piping e xpansion exists. | ||
Ig Regarding Z-direction movement, restraint pair A-D is l | Ig Regarding Z-direction movement, restraint pair A-D is l | ||
| Line 9,533: | Line 5,848: | ||
n-6 | n-6 | ||
CARGENTO LUNDY NEERS APPENDIX D E N Gj,g SL-3159 RE V. 1, 7-29-77 THERMAL EXPANSION WORKSHEET Restraint Expanding Nozzle Required Actual Pair Dir. Length,ft. Movement,in. Offset, ft. Offset,ft. Recommendation A-C X 10 25 5'1" 6'6" 10 Change to snubber A-E X 25 .25 8'0" 6'6" 15 ok A-B Y 0 .75 0 11'4" 10 Replace w, snubber and spring A-D Y 10 .75 5'1" 11'4" 17 ok D-E Y 0 0 0 0 13 I A-D Z 5 1.5 3'7" 16'0" 22 ok ok D-E Z 0 0 0 0 13 ok 10 J-I | |||
CARGENTO LUNDY NEERS APPENDIX D E N Gj,g SL-3159 RE V. 1, 7-29-77 | |||
THERMAL EXPANSION WORKSHEET Restraint Expanding Nozzle Required Actual Pair Dir. Length,ft. Movement,in. Offset, ft. Offset,ft. Recommendation A-C X 10 25 5'1" 6'6" 10 Change to snubber A-E X 25 .25 8'0" 6'6" 15 ok A-B Y 0 .75 0 11'4" 10 Replace w, snubber and spring A-D Y 10 .75 5'1" 11'4" 17 ok D-E Y 0 0 0 0 13 I A-D Z 5 1.5 3'7" 16'0" 22 ok ok D-E Z 0 0 0 0 13 ok 10 J- | |||
I | |||
~I J | ~I J | ||
l 1 | l 1 | ||
| Line 9,544: | Line 5,854: | ||
. D-7 Final E . | . D-7 Final E . | ||
CARGENT O LUNDY ENGlNEE20 CHICAGO APPENDIX E SL-3159 N | CARGENT O LUNDY ENGlNEE20 CHICAGO APPENDIX E SL-3159 N | ||
f (o REV.1, 7 77 SMALL PIPING DESIGN WORK SHEETS sI WEIGHT SUPPORT SYSTEM DESIGN WORKSHEET | f (o REV.1, 7 77 SMALL PIPING DESIGN WORK SHEETS sI WEIGHT SUPPORT SYSTEM DESIGN WORKSHEET | ||
'l I Sm NO | 'l I Sm NO SPAN ee-LOAD e1P1- E-DESCRIPTION e-A b eTEe LENGTH Deem. | ||
SPAN ee-LOAD e1P1- E-DESCRIPTION e-A b eTEe LENGTH Deem. | |||
RULED i | RULED i | ||
I LI | I LI | ||
,1 i | ,1 i | ||
l | l | ||
:10 I | :10 I | ||
I 1 , | I 1 , | ||
j , | j , | ||
me -M-- | me -M-- | ||
wg | wg | ||
_ ; | _ ; | ||
I o | I o | ||
Il m\ | Il m\ | ||
| Line 9,572: | Line 5,872: | ||
:' l!I ll , l | :' l!I ll , l | ||
,',t i' | ,',t i' n>2 zd D rCZU<. | ||
m*@2mmDO QEEo >1k2ExM ur wGS - | |||
mm . wi"T M | |||
S r | |||
n>2 zd D rCZU<. | M f f | ||
m*@2mmDO QEEo >1k2ExM | |||
ur wGS - | |||
mm . wi"T | |||
E t | E t | ||
m o | m o | ||
C . | C . | ||
| Line 9,595: | Line 5,886: | ||
r r | r r | ||
W d n | W d n | ||
B S S . | B S S . | ||
K T R R O | K T R R O | ||
| Line 9,602: | Line 5,892: | ||
P I | P I | ||
G U I S S A E | G U I S S A E | ||
D | D a | ||
T S ! | |||
S ! | |||
Y ! | Y ! | ||
O S I T T R P I | O S I T T R P I | ||
| Line 9,613: | Line 5,900: | ||
l E 5 | l E 5 | ||
S L E = | S L E = | ||
!G M t I | !G M t I | ||
P I | P I | ||
| Line 9,620: | Line 5,906: | ||
l H AG PI SE W | l H AG PI SE W | ||
L AN MA | L AN MA | ||
!P 0S 1 | !P 0S 1 | ||
t | t | ||
. ! I- | . ! I-P . | ||
E0 1 T1 S . | |||
P . | |||
E0 1 | |||
T1 S . | |||
il sb W r i | il sb W r i | ||
y | y | ||
=3 SARGENTO LUNDY ENGINEERS | =3 SARGENTO LUNDY ENGINEERS | ||
| Line 9,644: | Line 5,924: | ||
:I o | :I o | ||
E-3 l- Final | E-3 l- Final | ||
DOCU V'i = | DOCU V'i = | ||
M i | M i 2 | ||
2 | |||
PAGE _ | PAGE _ | ||
B U-- ' | B U-- ' | ||
A\ O. smwose NO. OF PAGES 8 YnoLFS REASON-O PAGE ILLEGIBLE: | A\ O. smwose NO. OF PAGES 8 YnoLFS REASON-O PAGE ILLEGIBLE: | ||
PDR CF l O HARD COPY FILED AT: ) | PDR CF l O HARD COPY FILED AT: ) | ||
| Line 9,665: | Line 5,935: | ||
O BETTER COPi' REQUESTED ON O PAGE 100 LARGE TO FILM. | O BETTER COPi' REQUESTED ON O PAGE 100 LARGE TO FILM. | ||
PDR CF O HARD COPV FILED AT: l OTHER l | PDR CF O HARD COPV FILED AT: l OTHER l | ||
0 FILMED ON APERTURE CARD NO. k Foo9AL/o S/J-[9 | 0 FILMED ON APERTURE CARD NO. k Foo9AL/o S/J-[9 I | ||
I | |||
l EF- 2-FSAR | l EF- 2-FSAR | ||
. .,Y | . .,Y | ||
[ DRYWELL ELEV. 662'-b" FLANGE PRESSURE VESSEL FLANGE STABILIZER TRUSS | [ DRYWELL ELEV. 662'-b" FLANGE PRESSURE VESSEL FLANGE STABILIZER TRUSS | ||
\ ELEV. 647'-6" | \ ELEV. 647'-6" ll 4 t | ||
ll 4 t | |||
,. REACTOR , | ,. REACTOR , | ||
, PRESSURE , | , PRESSURE , | ||
.$ VESSEL I r, i. | .$ VESSEL I r, i. | ||
,, i y ,8 SHIELD WALL | ,, i y ,8 SHIELD WALL e t< | ||
e t< | |||
l, DRYWELL VESSEL | l, DRYWELL VESSEL | ||
,'., i | ,'., i 5 ' | ||
S 5 PLATFORM ELEV. 607'-0" E i >r -- _.1 I '; ' I | |||
5 ' | |||
S 5 PLATFORM ELEV. 607'-0" | |||
E i >r -- _.1 | |||
I '; ' I | |||
} , | } , | ||
'' /8 l | '' /8 l | ||
: s. ,,, .N | : s. ,,, .N | ||
..., g,"v. | ..., g,"v. | ||
*4 REACTOR | *4 REACTOR | ||
,, SUPPORT ,e PLATFORM | ,, SUPPORT ,e PLATFORM | ||
\ - | \ - | ||
; PEDESTAL f | ; PEDESTAL f | ||
/ | / | ||
ELEV. 585'-3 7 /8" | ELEV. 585'-3 7 /8" | ||
.* ,I ,. | .* ,I ,. | ||
'' t | '' t | ||
.i, | .i, ELEV. 572'-1" | ||
ELEV. 572'-1" | |||
.',9 /* < ',' te e , , , | .',9 /* < ',' te e , , , | ||
*. l,/,, :, ,f . .',.s | *. l,/,, :, ,f . .',.s | ||
-t ,* .'s , .. %, ' | -t ,* .'s , .. %, ' | ||
l ,* * * $ , | l ,* * * $ , | ||
ENRICO FERMI ATOMIC POWER PLANT UNIT 2 | ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT , | ||
FINAL SAFETY ANALYSIS REPORT , | |||
I .. | I .. | ||
FIGURE 3.7-14 SECTION THROUGH LENTER LINE OF DRYWELL | FIGURE 3.7-14 SECTION THROUGH LENTER LINE OF DRYWELL | ||
| Line 9,742: | Line 5,972: | ||
l . | l . | ||
/ | / | ||
EF- 2-FSAR | EF- 2-FSAR | ||
?. | ?. | ||
s ..'h 6 9 | s ..'h 6 9 | ||
CONTAINMENT SHIELD s | CONTAINMENT SHIELD s | ||
. . . . . . . 18 9 DRYWELL BELLOWS | . . . . . . . 18 9 DRYWELL BELLOWS | ||
, 27 9 I | , 27 9 I | ||
X - DIRECTION 4 93 ' | |||
X - DIRECTION 4 | |||
93 ' | |||
REFUELING BELLOWS ONLY 25g[// | REFUELING BELLOWS ONLY 25g[// | ||
CONTAINMENT 17 i s VESSEL 3 16 ' 24 s', 32 | |||
CONTAINMENT 17 i s VESSEL | |||
3 16 ' 24 s', 32 | |||
.......( ) . . . . g . . 3. , ; , "ll STABILIZER i 23,', i 31 4 g SACRIFICAL 15f22h I | .......( ) . . . . g . . 3. , ; , "ll STABILIZER i 23,', i 31 4 g SACRIFICAL 15f22h I | ||
* I SHIELD 2 | * I SHIELD 2 | ||
| Line 9,772: | Line 5,991: | ||
=.......( ) 19 28js | =.......( ) 19 28js | ||
- ; | - ; | ||
12 C' l | 12 C' l | ||
l l | l l | ||
| Line 9,778: | Line 5,996: | ||
//O///ON$/OJ/////////////$/ i ENRICO FERMI ATOMIC POWER PLANT UNIT 2 | //O///ON$/OJ/////////////$/ i ENRICO FERMI ATOMIC POWER PLANT UNIT 2 | ||
. FINAL SAFETY ANALYSIS REPORT ' | . FINAL SAFETY ANALYSIS REPORT ' | ||
FIGURE 3.7-15 | FIGURE 3.7-15 REACTOR / AUXILIARY BUILDING HORIZONTAL DYNAMIC MODEL SARGENT & LUNDY REPORT NO. SL-2682 - | ||
REACTOR / AUXILIARY BUILDING HORIZONTAL DYNAMIC MODEL SARGENT & LUNDY REPORT NO. SL-2682 - | |||
l EF- 2-FS AR TABLE 3.7-8 REACTOR / AUXILIARY BUILDING PROBABLE MAXIMUM DISPLACEMENTS Horizontal Displacements, " ft OBE SSE Mass X-Excit. Y-Excit. X-Excit. Y-Excit. | l EF- 2-FS AR TABLE 3.7-8 REACTOR / AUXILIARY BUILDING PROBABLE MAXIMUM DISPLACEMENTS Horizontal Displacements, " ft OBE SSE Mass X-Excit. Y-Excit. X-Excit. Y-Excit. | ||
No. X-Disp 1.,ft_ Y-Disp 1.,ft X-Disp 1.,ft Y-Disp 1.,ft 1 0.00110 0.00095 0.00157 0.00136 2 0.00257 0.00245 0.00366 0.00349 3 0.00376 0.00260 0.00535 0.00469 4 0.00430 0.00376 0.00611 0.00534 5 0.00483 0.00340 0.00686 0.00594 6 0.03502 0.03240 0.05082 0.04623 7 0.00149 0.00117 0.00209 0.00164 8 0.00330 0.00143 0.00465 0.00201 9 0.00491 0.00500 0.00692 0.00705 10 0.03500 0.02780 0.05080 0.04040 11 0.00490 0.00310 0.00689 0.00465 12 0.00070 0.00040 0.00094 0.00060 13 0.00110 0.00070 0.00157 0.00102 14 0.00250 0.00160 0.00357 0.00252 15 0.00310 0.00210 0.00436 0.00322 16 0.00380 0.00270 0.00536 0.00419 17 0.00430 0.00320 0.00610 0.00485 18 0.00480 0.00390 0.00689 0.00600 19 0.00090 0.00060 0.00126 0.00086 20 0.00150 0.00100 0.00208 0.00152 | No. X-Disp 1.,ft_ Y-Disp 1.,ft X-Disp 1.,ft Y-Disp 1.,ft 1 0.00110 0.00095 0.00157 0.00136 2 0.00257 0.00245 0.00366 0.00349 3 0.00376 0.00260 0.00535 0.00469 4 0.00430 0.00376 0.00611 0.00534 5 0.00483 0.00340 0.00686 0.00594 6 0.03502 0.03240 0.05082 0.04623 7 0.00149 0.00117 0.00209 0.00164 8 0.00330 0.00143 0.00465 0.00201 9 0.00491 0.00500 0.00692 0.00705 10 0.03500 0.02780 0.05080 0.04040 11 0.00490 0.00310 0.00689 0.00465 12 0.00070 0.00040 0.00094 0.00060 13 0.00110 0.00070 0.00157 0.00102 14 0.00250 0.00160 0.00357 0.00252 15 0.00310 0.00210 0.00436 0.00322 16 0.00380 0.00270 0.00536 0.00419 17 0.00430 0.00320 0.00610 0.00485 18 0.00480 0.00390 0.00689 0.00600 19 0.00090 0.00060 0.00126 0.00086 20 0.00150 0.00100 0.00208 0.00152 | ||
| Line 9,791: | Line 6,003: | ||
Elevation OBE SSE Elev. 583 ft, 6 in. 0.00013 0.00020 (1st Floor) | Elevation OBE SSE Elev. 583 ft, 6 in. 0.00013 0.00020 (1st Floor) | ||
Elev. 613 ft, 6 in. 0.00026 0.00039 (2nd Floor) | Elev. 613 ft, 6 in. 0.00026 0.00039 (2nd Floor) | ||
Elev. 641 ft, 6 in 0.00035 0.00052 | Elev. 641 ft, 6 in 0.00035 0.00052 (3rd Floor) | ||
(3rd Floor) | |||
Elev. 659 ft, 6 in 0.00039 0.00057 (4th Floor) | Elev. 659 ft, 6 in 0.00039 0.00057 (4th Floor) | ||
Elev. 684 ft, 6 in. 0.00044 0.00064 (5th Floor) | Elev. 684 ft, 6 in. 0.00044 0.00064 (5th Floor) | ||
O (a, Displacements are relative to the base of the structure. | O (a, Displacements are relative to the base of the structure. | ||
l 3.7-75 | l 3.7-75 I . | ||
s 0 | s 0 | ||
EF-2-FSAR i | EF-2-FSAR i | ||
F R EQUENCY, CPS | F R EQUENCY, CPS 90 33 20 10 SA 3.3 2A 1A 05 | ||
## -liII lill l I I I I I IilI I l li liII Illi i l I I I l l l ll lilh= | |||
90 33 20 10 SA 3.3 2A 1A 05 | |||
## -liII | |||
lill l I I I I I IilI I l li liII Illi i l I I I l l l ll lilh= | |||
~ | ~ | ||
15A , _ | 15A , _ | ||
10D _ | 10D _ | ||
~ | ~ | ||
SA _ ; | SA _ ; | ||
~ | ~ | ||
IS - | IS - | ||
6A _ | 6A _ | ||
4D _ | 4D _ | ||
E : | E : | ||
3.0 _ | 3.0 _ | ||
2 h% DAMPING - | 2 h% DAMPING - | ||
~ ~ | ~ ~ | ||
' 1% DAMPlNG h | ' 1% DAMPlNG h | ||
h - , 2% DAMPlNG jg - / r 5% DAMPlNG | h - , 2% DAMPlNG jg - / r 5% DAMPlNG | ||
- : / 2 s IS | - : / 2 s IS | ||
/ | / | ||
| Line 9,844: | Line 6,037: | ||
5 Ir-51 \ / | 5 Ir-51 \ / | ||
O " | O " | ||
r-< //,-LAA - | r-< //,-LAA - | ||
W | W | ||
/- \ /// \\\ | /- \ /// \\\ | ||
] - | ] - | ||
/# | /# | ||
//_J | //_J | ||
| Line 9,858: | Line 6,046: | ||
/// /\\\ | /// /\\\ | ||
//// | //// | ||
m s y | |||
m s | 0, y - | ||
y - | |||
\q : | \q : | ||
/)/ -\ah s w : | /)/ -\ah s w : | ||
0 10 | 0 10 | ||
# y s y | # y s y | ||
w : | w : | ||
: /g w\% : | : /g w\% : | ||
0.10 - | 0.10 - | ||
| Line 9,884: | Line 6,062: | ||
~ | ~ | ||
0.06 | 0.06 | ||
,,, 7 III IIII I I I i 1 1 IIII IIII IIII Ill1 I I I I I I I INW l I l' O 02 0.03 0.04 0.06 0.06 0.00 0.1 0.15 0.2 0.3 0.4 05 0.8 02 1A 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 | ,,, 7 III IIII I I I i 1 1 IIII IIII IIII Ill1 I I I I I I I INW l I l' O 02 0.03 0.04 0.06 0.06 0.00 0.1 0.15 0.2 0.3 0.4 05 0.8 02 1A 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-32 HORIZONTAL FLOOR RESPONSE SPECTRA | ||
FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-32 HORIZONTAL FLOOR RESPONSE SPECTRA | |||
''~ | ''~ | ||
OPERATING BASIS EARTHOUAKE ELEVATION - | OPERATING BASIS EARTHOUAKE ELEVATION - | ||
583'-6" (SLAB NO.1) REACTOR / AUXILIARY BUILDING NORTH - SOUTH COMPONENT SARGENT & LUNDY REPORT NO. SL-2682 | 583'-6" (SLAB NO.1) REACTOR / AUXILIARY BUILDING NORTH - SOUTH COMPONENT SARGENT & LUNDY REPORT NO. SL-2682 | ||
EF-2-FSAR FREOVENCY, CPS | |||
EF-2-FSAR | |||
FREOVENCY, CPS | |||
/ 50 33 20 10 SA 3.3 2A 1A 05 | / 50 33 20 10 SA 3.3 2A 1A 05 | ||
/ 20A _;;gg ggg, , g g g y ; ; ggg g g gg gg3g 3:33 g 3 g g 1 y g;3g gigy | / 20A _;;gg ggg, , g g g y ; ; ggg g g gg gg3g 3:33 g 3 g g 1 y g;3g gigy | ||
~ | ~ | ||
C 1sb _ | C 1sb _ | ||
10A g - | 10A g - | ||
~ | ~ | ||
SD - _ | SD - _ | ||
00 _ | |||
_ | |||
Eb _ | Eb _ | ||
eb ,_ | eb ,_ | ||
~ | ~ | ||
2 | 2 2 | ||
3.0 - | |||
- 1% DAMPlNts - | - 1% DAMPlNts - | ||
~ | ~ | ||
| Line 9,926: | Line 6,086: | ||
10% DAMPlNG | 10% DAMPlNG | ||
_ f { | _ f { | ||
/ | / | ||
xy - | xy - | ||
g'A G | g'A G | ||
jK A 1 ll l \ | |||
jK A 1 | |||
ll l \ | |||
I - | I - | ||
II / / \ li , | II / / \ li , | ||
| Line 9,948: | Line 6,096: | ||
3 - \ 1 | 3 - \ 1 | ||
\\ | \\ | ||
0 - | 0 - | ||
//// \ L W ** '' | //// \ L W ** '' | ||
// // \ \ \\ ~ | // // \ \ \\ ~ | ||
.3 " | .3 " | ||
//g )_A \\ - | //g )_A \\ - | ||
x | x i /// \\ \' E ; | ||
i /// \\ \' E ; | |||
: p s % | : p s % | ||
N | N r \N N A i | ||
: N N N '%s h 0.10 _ | |||
r \N N | |||
A i | |||
: N N N '%s h | |||
0.10 | |||
_ | |||
~ ~ | ~ ~ | ||
0.0s _ | 0.0s _ | ||
0.06 | 0.06 | ||
,, 11II IIIi i I i i l I IIII IIII IIII IIII I i 1. 1 I I IIII I I I l' 022 0.03 0.04 0.06 0.06 0.00 0.1 0.15 0.2 0.3 OA 05 0.6 OA 1.0 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-93 | ,, 11II IIIi i I i i l I IIII IIII IIII IIII I i 1. 1 I I IIII I I I l' 022 0.03 0.04 0.06 0.06 0.00 0.1 0.15 0.2 0.3 OA 05 0.6 OA 1.0 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-93 | ||
~ | ~ | ||
VERTICAL RESPONSE SPECTRA SAFE SHUTDOWN (A '; EARTHQUAKE REACTOR BUILD!NG SLAB EL. 583'-6'', 613'-6" SARGENT & LUNDY REPORT NO. SL-2682 | VERTICAL RESPONSE SPECTRA SAFE SHUTDOWN (A '; EARTHQUAKE REACTOR BUILD!NG SLAB EL. 583'-6'', 613'-6" SARGENT & LUNDY REPORT NO. SL-2682 | ||
EFo 2-FSAR t | EFo 2-FSAR t | ||
F R EOUENCY. CPS 10 5.0 3.3 2D 1.0 05 60 33 20 | F R EOUENCY. CPS 10 5.0 3.3 2D 1.0 05 60 33 20 | ||
-1lll lll1 l l I I I I IIII I I Il IIII Illl I I I I I I IIII IIIb | -1lll lll1 l l I I I I IIII I I Il IIII Illl I I I I I I IIII IIIb 1sm _ | ||
1sm _ | |||
_ ~ | _ ~ | ||
- ~ | - ~ | ||
10A ,_ ~ | 10A ,_ ~ | ||
SD _ | SD _ | ||
nmus CD _ | nmus CD _ | ||
52 , | 52 , | ||
~ | ~ | ||
;g %% DAMPING _, | ;g %% DAMPING _, | ||
~ | ~ | ||
} p ,1% DAMPING | } p ,1% DAMPING | ||
~ / / 2% DAMPlNG C ! j/ 5% DAMPlNG E / // '*-- | ~ / / 2% DAMPlNG C ! j/ 5% DAMPlNG E / // '*-- | ||
2n y _ , | 2n y _ , | ||
I' ,/ ( | I' ,/ ( | ||
D 1h , | D 1h , | ||
I I / 7 5 2 / / h - | I I / 7 5 2 / / h - | ||
G 'D - j r \ | G 'D - j r \ | ||
I - lj / ( (\i\ - | I - lj / ( (\i\ - | ||
= 08 - lii! \ \ \\ - | = 08 - lii! \ \ \\ - | ||
//// t \\\ | //// t \\\ | ||
\ \\\ | \ \\\ | ||
U *~' - | U *~' - | ||
//// | //// | ||
e ,j s. | e ,j s. | ||
0A yg xxxw | |||
0A | |||
yg xxxw | |||
\ g 3 | \ g 3 | ||
; | ; | ||
0.3 b y \\ s Mk E E | 0.3 b y \\ s Mk E E | ||
0.2 | 0.2 | ||
_ r s Ng gg | _ r s Ng gg | ||
%\\ : | %\\ : | ||
E / | E / | ||
0.10 V | 0.10 V | ||
%A \ ggg s | %A \ ggg s | ||
_ % \\ | _ % \\ | ||
0.08 _ | 0.08 _ | ||
| Line 10,067: | Line 6,156: | ||
. FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-84 l | . FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-84 l | ||
._ . VERTICAL RESPONSE SPECTRA OPERATING BASIS EARTHOUAKE RE ACTOR O, | ._ . VERTICAL RESPONSE SPECTRA OPERATING BASIS EARTHOUAKE RE ACTOR O, | ||
l BUILDING SLAB EL. 583'-6**. 613'-6" SARGENT & LUNDY REPORT NO. SL-2682 | l BUILDING SLAB EL. 583'-6**. 613'-6" SARGENT & LUNDY REPORT NO. SL-2682 | ||
i l | |||
i | EF- 2-FS AR t, | ||
l | |||
EF- 2-FS AR | |||
t, | |||
,, FREQUENCY, CPS | ,, FREQUENCY, CPS | ||
?% | ?% | ||
Q ,) 60 33 _ | Q ,) 60 33 _ | ||
20 10 ED 3.3 2B 1D 05 | 20 10 ED 3.3 2B 1D 05 | ||
-l I I i 11ll l l I l 1 l l 311 I l 11 11ll lill I l l l l l llll Ill | -l I I i 11ll l l I l 1 l l 311 I l 11 11ll lill I l l l l l llll Ill 15A ~ | ||
15A ~ | |||
~ | ~ | ||
~ - | ~ - | ||
10A ,_ | 10A ,_ | ||
~ | ~ | ||
$D | $D SD 4A ,, | ||
2 3.0 ~ | |||
SD | |||
4A ,, | |||
2 | |||
3.0 ~ | |||
2 | 2 | ||
~ - | ~ - | ||
2.0 | 2.0 | ||
= p 1% DAMPING h a 93 - 2% DAMPf NG - | = p 1% DAMPING h a 93 - 2% DAMPf NG - | ||
= [ / 5% DAMPING [ | = [ / 5% DAMPING [ | ||
[ | [ | ||
Q | Q Z ,# | ||
Z ,# | |||
I 1\ / / | I 1\ / / | ||
f10% DAMPANG | f10% DAMPANG r - | ||
fr -s\ /s 5 - | |||
r - | |||
fr -s\ /s | |||
5 - | |||
// \X / - | // \X / - | ||
0 - | 0 - | ||
r/ /\'/ , - | r/ /\'/ , - | ||
U .) | U .) | ||
# 46 % \ - I O 0. | # 46 % \ - I O 0. | ||
c -- | c -- | ||
' // / /N NN - | ' // / /N NN - | ||
\ | \ | ||
03 | 03 2 | ||
2 | |||
/ | / | ||
y sw | y sw x\w \\\h 5 | ||
x\w \\\h | |||
5 | |||
- j /, Ng N% | - j /, Ng N% | ||
W = | W = | ||
= | = | ||
j N h : | j N h : | ||
0.10 - - | 0.10 - - | ||
~ | ~ | ||
| Line 10,160: | Line 6,201: | ||
0.Os - | 0.Os - | ||
T - | T - | ||
0.06 0.05 | 0.06 0.05 | ||
~IIII IIII I I I I I I IIII IIII IIII IllI I I I I I I IIIl I I l l' Oh2 0.03 0.04 0.06 0.06 0.08 0.1 0.15 02 0.3 0.4 05 OA 02 14 1A 2.0 PERIOD. SECONO ENRICO FERMI ATOMIC POWER PL NT ' | ~IIII IIII I I I I I I IIII IIII IIII IllI I I I I I I IIIl I I l l' Oh2 0.03 0.04 0.06 0.06 0.08 0.1 0.15 02 0.3 0.4 05 OA 02 14 1A 2.0 PERIOD. SECONO ENRICO FERMI ATOMIC POWER PL NT ' | ||
UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-57 | UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-57 HORIZONTAL FLOOR RESPONSE SPECTRA SAFE SHUTDOWN EARTHOUAKE ELEVATION - 583*-6" O- (SLAB NO.1) KEACTOR/ AUXILIARY BUILDING EAST - WEST COMPONENT SARGENT & LUNDY REPORT NO. SL-2682 | ||
HORIZONTAL FLOOR RESPONSE SPECTRA SAFE SHUTDOWN EARTHOUAKE ELEVATION - 583*-6" O- (SLAB NO.1) KEACTOR/ AUXILIARY BUILDING EAST - WEST COMPONENT SARGENT & LUNDY REPORT NO. SL-2682 | |||
l 1 | l 1 | ||
l 1 | l 1 | ||
EF- 2-FS AR : | EF- 2-FS AR : | ||
\ , | \ , | ||
i | i | ||
.. FREQUENCY, CPS | .. FREQUENCY, CPS | ||
% so 33 to 10 En 33 2D 12 05 | % so 33 to 10 En 33 2D 12 05 | ||
-iiii iiii i i i i i i isii i i ii iiii iiii : i i i i i iiii siih 1sm _ _ | |||
-iiii iiii i i i i i i isii i i ii iiii iiii : i i i i i iiii siih | |||
1sm | |||
_ _ | |||
10n _ _ | 10n _ _ | ||
l | l | ||
- -~ | - -~ | ||
so | so SD sa - | ||
SD | |||
sa - | |||
42 _ | 42 _ | ||
~ | ~ | ||
~~ | ~~ | ||
3.0 | 3.0 1% DAMPlNG 2 2.0 g _ ' 2s DAMPING - | ||
1% DAMPlNG 2 2.0 g _ ' 2s DAMPING - | |||
g 3 la | g 3 la | ||
[/f o% DAMPING ~ | [/f o% DAMPING ~ | ||
5% DAMPING | 5% DAMPING | ||
~ | ~ | ||
,/- | ,/- | ||
_ l | _ l | ||
~ | ~ | ||
: I : | : I : | ||
!; '" - | !; '" - | ||
I i x/s | I i x/s | ||
// - | // - | ||
c - | c - | ||
I.' Ai - | I.' Ai - | ||
c- // /\N - | c- // /\N - | ||
/_ \ / /N X - | /_ \ / /N X - | ||
// | // | ||
\\ | \\ | ||
// | // | ||
// // N N - | // // N N - | ||
8, -- .\\ /// /\ ' | 8, -- .\\ /// /\ ' | ||
\' s - | \' s - | ||
| Line 10,245: | Line 6,245: | ||
~~ | ~~ | ||
Y \ | Y \ | ||
// | // | ||
y- y y xxxs | y- y y xxxs | ||
\5NN, | \5NN, 02 | ||
[7 3 3 3 _ | |||
02 | |||
[7 | |||
3 3 3 _ | |||
0.15 E \\% \\ | 0.15 E \\% \\ | ||
E | E N _ | ||
0.10 Ng : | |||
N _ | |||
0.10 | |||
Ng : | |||
0.Os _ _ | 0.Os _ _ | ||
~ ~ | ~ ~ | ||
| Line 10,272: | Line 6,258: | ||
, UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-56 | , UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-56 | ||
.. HORIZONTAL FLOOR RESPONSE SPECTRA SAFE SHUTDOWN EARTHQUAKE ELEVATION - 583'-6'' | .. HORIZONTAL FLOOR RESPONSE SPECTRA SAFE SHUTDOWN EARTHQUAKE ELEVATION - 583'-6'' | ||
O | O (SLAB NO.1) REACTOR / AUXILIARY BUILDING NORTH - SOUTH COMPONENT SARGENT & LUNDY REPORT NO. SL-2882 l | ||
(SLAB NO.1) REACTOR / AUXILIARY BUILDING NORTH - SOUTH COMPONENT SARGENT & LUNDY REPORT NO. SL-2882 l | |||
f I | f I | ||
I EF-2-FSAR 1 | |||
I | |||
i . | i . | ||
l FREOUENCY. CPS y .. | l FREOUENCY. CPS y .. | ||
i $ 50 33 20 to 50 33 20 10 0.5 | i $ 50 33 20 to 50 33 20 10 0.5 | ||
'# * -IIII till i I I I I I I III I l li iiIi till i I I I I I IIII li t h | '# * -IIII till i I I I I I I III I l li iiIi till i I I I I I IIII li t h | ||
~ | ~ | ||
15A , | 15A , | ||
10.0 _, _ | 10.0 _, _ | ||
8.0 _ _ | 8.0 _ _ | ||
6.0 _ | 6.0 _ | ||
5.0 _ | 5.0 _ | ||
4.0 _ | 4.0 _ | ||
~ | ~ | ||
30 - | 30 - | ||
~. _- | ~. _- | ||
Y m 2.0 | Y m 2.0 r '% UAMYING t - 1% DAMPlNG ; | ||
r '% UAMYING t - 1% DAMPlNG ; | |||
p "" | p "" | ||
$ 93 ,2% DAMPING | $ 93 ,2% DAMPING | ||
. 2 [ 5% DAMPING | . 2 [ 5% DAMPING z' - | ||
z' - | |||
~ | ~ | ||
/ | / | ||
/ / | / / | ||
/ | / | ||
~ | ~ | ||
9 g ,o y - f/// - | 9 g ,o y - f/// - | ||
02 j e a* | 02 j e a* | ||
e v - | e v - | ||
e - g A\ - | e - g A\ - | ||
Q // - | Q // - | ||
[ | [ | ||
'\\\ | '\\\ | ||
0, | 0, r | ||
m- | |||
/// \\\% N - | /// \\\% N - | ||
h m \ \^ ~ | h m \ \^ ~ | ||
?- | ?- | ||
| Line 10,351: | Line 6,300: | ||
E 0.15 g _- | E 0.15 g _- | ||
/ \ Z 0.10 | / \ Z 0.10 | ||
_ j y _ | _ j y _ | ||
# ~ | # ~ | ||
0 08 _ | 0 08 _ | ||
_ g _ | _ g _ | ||
0 06 og l11I IIII I I i l l I IIII IIll 1llI Iill I I I I I ! IIl\ 11Il' 0 02 0 03 0 04 0.05 006 0 08 0.1 0.15 0.2 0.3 0.4 0.5 06 OS 1.0 1.5 2.0 PERIOD. SE COND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 | 0 06 og l11I IIII I I i l l I IIII IIll 1llI Iill I I I I I ! IIl\ 11Il' 0 02 0 03 0 04 0.05 006 0 08 0.1 0.15 0.2 0.3 0.4 0.5 06 OS 1.0 1.5 2.0 PERIOD. SE COND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-33 HORIZONTAL FLOOR RESPONSE SPECTRA | ||
FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-33 HORIZONTAL FLOOR RESPONSE SPECTRA | |||
-- - OPERATING BASIS EARTHQUAKE ELEVATION - | -- - OPERATING BASIS EARTHQUAKE ELEVATION - | ||
O SARGENT & LUNDY REPORT NO. SL-2682 583'-6** (SLAB NO.1) RE ACTOR /AUXILI ARY BUILDING EAST - WEST COMPONENT | O SARGENT & LUNDY REPORT NO. SL-2682 583'-6** (SLAB NO.1) RE ACTOR /AUXILI ARY BUILDING EAST - WEST COMPONENT | ||
8 EFo 2-FS AR 4 | 8 EFo 2-FS AR 4 | ||
FREOUENCY,CP5 s | FREOUENCY,CP5 s | ||
'/ s0 as 20 10 sm 3.3 2m im Os | '/ s0 as 20 10 sm 3.3 2m im Os | ||
'' 8 | '' 8 | ||
_IIii 11ll l : ii i i I IIII I I II IIII Illi i i i I I I IIII IIIS | _IIii 11ll l : ii i i I IIII I I II IIII Illi i i i I I I IIII IIIS 1ss _ _ | ||
1ss _ _ | |||
10A _ | 10A _ | ||
- ~ | - ~ | ||
sm ,_ | sm ,_ | ||
so _ ,q s.O 4D ,_ | |||
so _ ,q | |||
s.O | |||
4D ,_ | |||
~ | ~ | ||
3D | 3D | ||
, 1% DAMPlNG - | , 1% DAMPlNG - | ||
- 2% DAMPING ~ | - 2% DAMPING ~ | ||
2A _ r' gf , 5% DAMPING - | 2A _ r' gf , 5% DAMPING - | ||
_ = J j # 10% DAMPlNG r - | _ = J j # 10% DAMPlNG r - | ||
l , | l , | ||
3 15 _ :r - | 3 15 _ :r - | ||
: / : | : / : | ||
8 - / - | 8 - / - | ||
c 'n s' / a | c 'n s' / a 11 - | ||
11 | |||
JI i / \ \\ ~ | JI i / \ \\ ~ | ||
'8 / \ - | '8 / \ - | ||
| Line 10,411: | Line 6,333: | ||
// / \\ | // / \\ | ||
0 '' | 0 '' | ||
// / / \ \\ - | // / / \ \\ - | ||
W - | W - | ||
// / / n \\ - | // / / n \\ - | ||
') [ | ') [ | ||
/// / \\\% - | /// / \\\% - | ||
0, E /F \\MN \ | 0, E /F \\MN \ | ||
E | E | ||
'2 | '2 | ||
~_ | ~_ | ||
_ z | _ z | ||
| Line 10,430: | Line 6,346: | ||
/" s | /" s | ||
\ s | \ s | ||
: N NN N : | : N NN N : | ||
0.15 | 0.15 | ||
: x\ NN3 : | : x\ NN3 : | ||
N3N N : | N3N N : | ||
0.10 A- _ | |||
0.10 | |||
A- _ | |||
~ ~ | ~ ~ | ||
Om _ - | Om _ - | ||
0.06 0.05 | 0.06 0.05 O.02 ' ' .0 0 3 0.04 ODS 0.06 0.08 0.1 0.15 0.2 0.3 OA 05 0.6 OA 1.0 1.5 2 .0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER Pl ANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-94 VERTICAL RESPONSE SPECTRA SAFE SHUTDOWN EARTHQUAKE REACTOR BUILDING O. SLAB EL. 641*- 6", 669'- 6" & 684'-6" SARGENT & LUNDY REPORT NO. SL-2682 | ||
O.02 ' ' .0 0 3 0.04 ODS 0.06 0.08 0.1 0.15 0.2 0.3 OA 05 0.6 OA 1.0 1.5 2 .0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER Pl ANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-94 | |||
VERTICAL RESPONSE SPECTRA SAFE SHUTDOWN EARTHQUAKE REACTOR BUILDING | |||
O. SLAB EL. 641*- 6", 669'- 6" & 684'-6" SARGENT & LUNDY REPORT NO. SL-2682 | |||
e EF o 2-FS AR 4 | e EF o 2-FS AR 4 | ||
F REQUENCY, CPS | F REQUENCY, CPS | ||
| Line 10,463: | Line 6,363: | ||
2 | 2 | ||
~ | ~ | ||
i 10A _ | i 10A _ | ||
1 | 1 sh _ Z | ||
sh _ Z | |||
_ ~ | _ ~ | ||
ah ! | ah ! | ||
bA - | bA - | ||
%% DAMPING 44 - 1% DAMPING - | %% DAMPING 44 - 1% DAMPING - | ||
b / 2% DAMPING b 3S j ( / $% DAMPING | b / 2% DAMPING b 3S j ( / $% DAMPING | ||
/ - | / - | ||
I | I | ||
/ | / | ||
//// / Z | //// / Z 2D / | ||
2D / | |||
E 5 | E 5 | ||
~ | ~ | ||
5 5 15 / | 5 5 15 / | ||
9 33 | 9 33 | ||
= | = | ||
lIf / | lIf / | ||
A | A | ||
= | = | ||
Q IlL.-. / 1 \\ - | |||
Q | |||
IlL.-. / 1 \\ - | |||
e - | e - | ||
III F \\ ~ | III F \\ ~ | ||
88 / //r | 88 / //r i l\\ ! | ||
i l\\ ! | |||
O | O | ||
*S | *S i/// \\ \\ - 1 W | ||
i/// \\ \\ - 1 W | |||
/f/ \\\\ - | /f/ \\\\ - | ||
p' - | p' - | ||
i | i | ||
/# \\ Y5 - | /# \\ Y5 - | ||
r | r | ||
# \\ M % | # \\ M % | ||
E | E 0.15 r | ||
%\\ i 0 10 \ | |||
0.15 r | |||
%\\ i | |||
0 10 \ | |||
%\ ,- | %\ ,- | ||
O 'U* ' | O 'U* ' | ||
| Line 10,542: | Line 6,401: | ||
0.06 | 0.06 | ||
_ g . | _ g . | ||
~llll llll I I I I l l llll llll l lll llII l l ll ll !: 1 1 ll ll 11 l l' OA2 0.03 0.04 0.05 006 0.08 0.1 0.15 OJ 0.3 0.4 05 0.6 03 1A 1.5 2.0 PERIOD, SECOND l | ~llll llll I I I I l l llll llll l lll llII l l ll ll !: 1 1 ll ll 11 l l' OA2 0.03 0.04 0.05 006 0.08 0.1 0.15 OJ 0.3 0.4 05 0.6 03 1A 1.5 2.0 PERIOD, SECOND l | ||
l ENRICO FERMI ATOMIC POWER PLANT UNIT 2 l | l ENRICO FERMI ATOMIC POWER PLANT UNIT 2 l | ||
\ | \ | ||
FINAL RAcf.TY ANALYSIS REPORT FIGURE 3.7-85 l | FINAL RAcf.TY ANALYSIS REPORT FIGURE 3.7-85 l | ||
-- - VERTICAL RESPONSE SPECTRA OPERATING | -- - VERTICAL RESPONSE SPECTRA OPERATING BASIS EARTHOUAKE REACTOR BUILDING l l O'- SLAB EL. 641'- 6", 659'- 6" & 684*-6" ! | ||
BASIS EARTHOUAKE REACTOR BUILDING l l O'- SLAB EL. 641'- 6", 659'- 6" & 684*-6" ! | |||
SARGENT & LUNDY REPORT NO. SL-2682 l l | SARGENT & LUNDY REPORT NO. SL-2682 l l | ||
EF- 2-FS AR | |||
\ | \ | ||
3 FREOUENCY, CPS | 3 FREOUENCY, CPS | ||
. 50 33 20 to 5.0 33 2D 1.0 05 g | . 50 33 20 to 5.0 33 2D 1.0 05 g | ||
| Line 10,563: | Line 6,415: | ||
~ | ~ | ||
ISD | ISD | ||
~ | ~ | ||
10D | 10D | ||
| Line 10,576: | Line 6,425: | ||
~ | ~ | ||
j 1% DAMPING - | j 1% DAMPING - | ||
f 2% DAMPING - | f 2% DAMPING - | ||
0 | 0 M | ||
8 | |||
/ 5% D AMPING 10% DAMPlNG 20 | |||
/ 5% D AMPING 10% DAMPlNG | |||
20 | |||
! ,, E 8dxW 5 5,D - | ! ,, E 8dxW 5 5,D - | ||
/// | /// | ||
/ r | / r | ||
/ x x3\x ! | / x x3\x ! | ||
Q - | Q - | ||
r g3 /// / \ \ \\ - | r g3 /// / \ \ \\ - | ||
U - | U - | ||
| Line 10,600: | Line 6,442: | ||
#// \\\\ - | #// \\\\ - | ||
~ | ~ | ||
0.4 $ 1 | 0.4 $ 1 sr % % - | ||
0.3 E | |||
sr % % - | |||
0.3 | |||
E | |||
: gN | : gN | ||
~ | ~ | ||
02 _ | 02 _ | ||
0.15 | 0.15 | ||
= | = | ||
~ | ~ | ||
3w E | 3w E | ||
- Z 0.10 _ | - Z 0.10 _ | ||
~ | ~ | ||
~ | ~ | ||
0 06 - | 0 06 - | ||
~ | ~ | ||
~ | ~ | ||
0.06 og l111 1111 l i I l l I Iili lill Itil 111ll l l l l 1 I l l 1l 11 l l' O.02 0.03 0.04 0.05 0.06 0.08 0.1 0.15 02 0.3 0.4 05 0.6 OD 1.0 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT | 0.06 og l111 1111 l i I l l I Iili lill Itil 111ll l l l l 1 I l l 1l 11 l l' O.02 0.03 0.04 0.05 0.06 0.08 0.1 0.15 02 0.3 0.4 05 0.6 OD 1.0 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-63 HORIZONTAL FLOOR RESPONSE SPECTRA SAFE O SHUTDOWN E ARTHOUAKE ELEVATION - 659 -0" (SLAB NO. 4) REACTOR / AUXILIARY BUILDING EAST - WEST COMPONENT SARGENT Si LUNDY REPORT NO. S 2682 | ||
UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-63 | |||
HORIZONTAL FLOOR RESPONSE SPECTRA SAFE O SHUTDOWN E ARTHOUAKE ELEVATION - 659 -0" (SLAB NO. 4) REACTOR / AUXILIARY BUILDING EAST - WEST COMPONENT SARGENT Si LUNDY REPORT NO. S 2682 | |||
1 EF-2-FSAR | |||
1 | |||
EF-2-FSAR | |||
\ | \ | ||
FREQUEM:Y, CPS | FREQUEM:Y, CPS | ||
) 50 33 20 l | ) 50 33 20 l | ||
10 l lll SA lIII 3.3 IIll I 2A I I I I I 1.0 IIII 05 | 10 l lll SA lIII 3.3 IIll I 2A I I I I I 1.0 IIII 05 | ||
-IIII | -IIII llll 1 I l l l l l Il IIIh | ||
llll 1 I l l l l l Il IIIh | |||
~ | ~ | ||
15A _ j | 15A _ j | ||
) | ) | ||
: I 10A ,_ - | : I 10A ,_ - | ||
- 1 sA - _ | - 1 sA - _ | ||
- l | - l SA ~ | ||
SA ~ | |||
1% DAMPING | 1% DAMPING | ||
_ 2% DAMPING - | _ 2% DAMPING - | ||
j | j 4A 5% DAMPING - | ||
3.0 _ | 3.0 _ | ||
{ ,10% DAMPING f | { ,10% DAMPING f | ||
E_ | E_ | ||
- J p - | |||
- J | |||
p - | |||
2.0 - ' | 2.0 - ' | ||
g ,_ _ | g ,_ _ | ||
3 12 | 3 12 | ||
= | = | ||
!/Af r \ - | !/Af r \ - | ||
= | = | ||
. : / \ C 5 '# | |||
. : / \ C | |||
5 '# | |||
/; ; s E - // / / \\ \\ - | /; ; s E - // / / \\ \\ - | ||
I - /// / \\ \\ - | I - /// / \\ \\ - | ||
OA ffff N N NN - | OA ffff N N NN - | ||
3 _ | 3 _ | ||
WK - | WK - | ||
AV \\\\ - | AV \\\\ - | ||
,] | ,] | ||
~ = | ~ = | ||
_ p Ng - | _ p Ng - | ||
| Line 10,711: | Line 6,497: | ||
= f y y\ N < | = f y y\ N < | ||
5 03 _- s 3 _. | 5 03 _- s 3 _. | ||
\ | \ | ||
n = = | n = = | ||
0.15 mh'h = | 0.15 mh'h = | ||
0.10 ,_ 3 - | 0.10 ,_ 3 - | ||
0.08 _ | 0.08 _ | ||
0.06 O.05 1111 till l l l l l 1 1IIi 1111 1III Illl I l l I I _It ! I I 1 111 l' 0.02 0.03 0.04 0.06 0.06 0.06 0.1 0.15 0.2 03 0.4 05 0.6 OA 1.0 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-62 HORIZONTAL FLOOR RESPONSE SPECTRA SAFE | |||
0.06 O.05 1111 till l l l l l 1 1IIi 1111 1III Illl I l l I I _It ! I I 1 111 l' 0.02 0.03 0.04 0.06 0.06 0.06 0.1 0.15 0.2 03 0.4 05 0.6 OA 1.0 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 | |||
FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-62 HORIZONTAL FLOOR RESPONSE SPECTRA SAFE | |||
~~~ | ~~~ | ||
SHUTDOWN E ARTHOUAKE ELEVATION - 659'-0" (SLAB NO. 4) REACTOR / AUXILIARY BUILDING O. NORTH - SOUTH COMPONENT sfRGENT & LUNDY REPORT NO. SL-2682 i | SHUTDOWN E ARTHOUAKE ELEVATION - 659'-0" (SLAB NO. 4) REACTOR / AUXILIARY BUILDING O. NORTH - SOUTH COMPONENT sfRGENT & LUNDY REPORT NO. SL-2682 i | ||
EF-2-FS AR FREOUENCY, CPS I' to 33 20 10 5A 3.3 2A 14 05 20A ,,,, ,,,, , , , , , , ,,, ,,,, y,,, ,,,, , , , , , , ,i,, ii,, | |||
EF-2-FS AR FREOUENCY, CPS | |||
I' to 33 20 10 5A 3.3 2A 14 05 | |||
20A ,,,, ,,,, , , , , , , ,,, ,,,, y,,, ,,,, , , , , , , ,i,, ii,, | |||
= | = | ||
ISA [ _ | ISA [ _ | ||
10A _ _ | 10A _ _ | ||
~ | ~ | ||
SA _ | SA _ | ||
SA ~ | SA ~ | ||
ED | ED | ||
-- 1% DAMPlNG | -- 1% DAMPlNG 4A _ | ||
4A _ | |||
[ 2% DAMPlNG | [ 2% DAMPlNG | ||
' 5% DAMPING - | ' 5% DAMPING - | ||
3 e 10% DAMPING h 3.0 f _ | 3 e 10% DAMPING h 3.0 f _ | ||
: / | : / | ||
r, / - | r, / - | ||
! '" E D tb _ | ! '" E D tb _ | ||
| Line 10,776: | Line 6,524: | ||
ll y N _ | ll y N _ | ||
~ | ~ | ||
//// \\\ \ - | //// \\\ \ - | ||
g //// \\ \\ - | g //// \\ \\ - | ||
", 02 _ fffj gg g\ _ | ", 02 _ fffj gg g\ _ | ||
N// \\ N N - | N// \\ N N - | ||
//// \ N \\ - | //// \ N \\ - | ||
Q ' | Q ' | ||
- 47 \'N'sN - | - 47 \'N'sN - | ||
i # 4' M% E | i # 4' M% E | ||
: NNNN : | : NNNN : | ||
a2 | a2 | ||
= | = | ||
NN\xs s | NN\xs s | ||
= | = | ||
0.15 | 0.15 | ||
: N gw\g | : N gw\g | ||
= | = | ||
Z Z 0.10 _ q _ | Z Z 0.10 _ q _ | ||
0.08 [ [ | 0.08 [ [ | ||
0.06 0.05 OS2 0.03' ' '0 .040.06 0.06 0.08 0 ' .1 0.15 02 0.3 OA 03 0.6 OE 1.0 1.5 2.0 PERIOD. SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY AN ALYSIS REPORT FIGURE 3.7-61 HORIZONTAL FLOOP RESPONSE SPECTRA SAFE | |||
0.06 0.05 | |||
OS2 0.03' ' '0 .040.06 0.06 0.08 0 ' .1 0.15 02 0.3 OA 03 0.6 OE 1.0 1.5 2.0 PERIOD. SECOND | |||
ENRICO FERMI ATOMIC POWER PLANT UNIT 2 | |||
FINAL SAFETY AN ALYSIS REPORT FIGURE 3.7-61 HORIZONTAL FLOOP RESPONSE SPECTRA SAFE | |||
. . . SHUTDOWN EARTHOUAKE ELEVATION - 641*-6" | . . . SHUTDOWN EARTHOUAKE ELEVATION - 641*-6" | ||
. (SLAB NO. 3) REACTOR /AUXlLIAR / BUILDING d.D EAST - WEST COMPONEAT SARGENT & LUNDY REPORT NO. SL-2682 l | . (SLAB NO. 3) REACTOR /AUXlLIAR / BUILDING d.D EAST - WEST COMPONEAT SARGENT & LUNDY REPORT NO. SL-2682 l | ||
EF- 2-FS AR | EF- 2-FS AR | ||
% FREOUENCY, CPS | % FREOUENCY, CPS | ||
*\ 20 10 5A 3.3 2A 1A OA to 33 k.) 20A _ , , , , - -,,,, ,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,g | *\ 20 10 5A 3.3 2A 1A OA to 33 k.) 20A _ , , , , - -,,,, ,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,,g | ||
= | = | ||
~ | ~ | ||
162 - | 162 - | ||
_ = | _ = | ||
10A _ - | 10A _ - | ||
~ | ~ | ||
GA - _ | GA - _ | ||
~ | ~ | ||
sA - | sA - | ||
, 1% DAMPING S.0 - | , 1% DAMPING S.0 - | ||
4A | 4A | ||
[ 2% DAMPING C | [ 2% DAMPING C | ||
_ j | _ j | ||
| Line 10,853: | Line 6,568: | ||
y | y | ||
"" = | "" = | ||
11 | 11 | ||
// / m)(\ | // / m)(\ | ||
E | E a 1.s . | ||
a 1.s . | |||
\ - | \ - | ||
= 2 I K | = 2 I K | ||
| Line 10,872: | Line 6,584: | ||
//// \ \\ \ - | //// \ \\ \ - | ||
l | l | ||
//// \ \ \\ - | //// \ \ \\ - | ||
l | l sW NW - | ||
sW NW - | |||
O. w \s\x h OA s = | O. w \s\x h OA s = | ||
E I + : | E I + : | ||
e-I MQ NN s n E | |||
e- | |||
I MQ NN s n E | |||
c2 | c2 | ||
= | = | ||
q E 0.15 _ | |||
q E | |||
0.15 _ | |||
^ \ - | ^ \ - | ||
C ~ | C ~ | ||
0.10 ,_ | 0.10 ,_ | ||
T - | T - | ||
0.08 ~_ - | 0.08 ~_ - | ||
l | l GA6 OAS OA2 ' ' '0 .03 0.04 0.06 0.06 0.00 0 ' .1 0.15 0 .2 0.3 0.4 0.5 0.6 OA L1.0' ' ' ' .5 1 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-60 i | ||
GA6 | |||
OAS OA2 ' ' '0 .03 0.04 0.06 0.06 0.00 0 ' .1 0.15 0 .2 0.3 0.4 0.5 0.6 OA L1.0' ' ' ' .5 1 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT | |||
FIGURE 3.7-60 i | |||
HORIZONTAL FLOOR RESPONSE SPECTRA SAFE SHUTDOWN E ARTHOUAKE ELEVATION - 641-6" O . | HORIZONTAL FLOOR RESPONSE SPECTRA SAFE SHUTDOWN E ARTHOUAKE ELEVATION - 641-6" O . | ||
(SLAB NO. 3) REACTOR / AUXILIARY BUILOING NORTH - SOUTH COMPONENT l SARGENT & LUNDY REPORT NO. SL-2682 l | (SLAB NO. 3) REACTOR / AUXILIARY BUILOING NORTH - SOUTH COMPONENT l SARGENT & LUNDY REPORT NO. SL-2682 l | ||
.m - _ _ _ _ _ _ _ - - | .m - _ _ _ _ _ _ _ - - | ||
r -- | r -- | ||
l EF-2-FSAR t | l EF-2-FSAR t | ||
FREQUENCY, CPS , | FREQUENCY, CPS , | ||
50 33 20 10 5A 3.3 2.0 1A 05 | 50 33 20 10 5A 3.3 2.0 1A 05 | ||
;I l ll llll l I I I I I I III IIll l IIi 1113 I l l I I I IIII lilh ISA 3 b ( | ;I l ll llll l I I I I I I III IIll l IIi 1113 I l l I I I IIII lilh ISA 3 b ( | ||
10A _ 2 , | 10A _ 2 , | ||
- 1 SA , - | - 1 SA , - | ||
- ~ | - ~ | ||
SA , h% DAMPING | SA , h% DAMPING | ||
/ 1% DAMPlNG j '2% DAMPlNC 4A - | |||
/ 1% DAMPlNG j '2% DAMPlNC | |||
4A - | |||
/ r | / r | ||
$% DAMPING = | $% DAMPING = | ||
3D 5 | 3D 5 | ||
/ // = | / // = | ||
; | ; | ||
( | ( | ||
c ** = | c ** = | ||
| Line 10,947: | Line 6,623: | ||
G '# - | G '# - | ||
I/f/ \ \\ \ - | I/f/ \ \\ \ - | ||
$ 08 | $ 08 II// \ \\ \ - | ||
II// \ \\ \ - | |||
5 - | 5 - | ||
//h \\\ \ - | //h \\\ \ - | ||
0 5 | 0 5 | ||
/#/ \\\\ i W - | |||
/#/ \\\\ i | |||
W - | |||
// \\\\ I - | // \\\\ I - | ||
O' - | O' - | ||
# V h - | # V h - | ||
, = | , = | ||
~ | ~ | ||
/ | / | ||
/ m\ \ i E | / m\ \ i E | ||
| Line 10,970: | Line 6,638: | ||
02 _ y-- 3 3 _ | 02 _ y-- 3 3 _ | ||
7 \\xN E a" | 7 \\xN E a" | ||
xw xNs : | xw xNs : | ||
0.10 s s \ | 0.10 s s \ | ||
3 y y3 _ | 3 y y3 _ | ||
~ ~ | ~ ~ | ||
| Line 10,981: | Line 6,645: | ||
_ i _ | _ i _ | ||
0.06 | 0.06 | ||
,, lIIi 1111 1 I I I 1 i iiii till Ii11 till i I i g_I IIi til r 0#2 0.03 0.04 0.05 006 0.08 0.1 0.15 0.2 0.3 0A 05 0.6 0A 14 15 2.0 PERIOD, SECOND | ,, lIIi 1111 1 I I I 1 i iiii till Ii11 till i I i g_I IIi til r 0#2 0.03 0.04 0.05 006 0.08 0.1 0.15 0.2 0.3 0A 05 0.6 0A 14 15 2.0 PERIOD, SECOND ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPOPT FIGURE 3.7-39 | ||
ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPOPT FIGURE 3.7-39 | |||
~ | ~ | ||
HORIZONTAL FLOOR RESPONSE SPECTRA OPERATING BASIS EARTHQUAKE ELEVATION - 659'-0" (SLAB NO. 4) REACTOR / | HORIZONTAL FLOOR RESPONSE SPECTRA OPERATING BASIS EARTHQUAKE ELEVATION - 659'-0" (SLAB NO. 4) REACTOR / | ||
C AUXILIARY BUILDING EAST-WEST COM"ONENT SARGENT & LUNDY REPORT NO. SL-2682 | C AUXILIARY BUILDING EAST-WEST COM"ONENT SARGENT & LUNDY REPORT NO. SL-2682 | ||
EF 2-FSAR s | EF 2-FSAR s | ||
FREOUENCY, CPS 4 | FREOUENCY, CPS 4 | ||
SO 33 20 10 5A 3.3 2A 1A 05 | SO 33 20 10 5A 3.3 2A 1A 05 | ||
/ | / | ||
-1lll ll1I I I I I I I i 11 I I I ll l l 3l lll3 I I I I I I IIII IIIh | |||
-1lll | |||
ll1I I I I I I I i 11 I I I ll l l 3l lll3 I I I I I I IIII IIIh | |||
~ | ~ | ||
= | = | ||
15A _ | 15A _ | ||
~ | ~ | ||
10A _ | 10A _ | ||
8A _ ,,,, | 8A _ ,,,, | ||
SA - h% DAMPlNG _ | SA - h% DAMPlNG _ | ||
~ | ~ | ||
| Line 11,018: | Line 6,666: | ||
= p% //,. 5% D AMPING 2% DAMPlNG C 3A | = p% //,. 5% D AMPING 2% DAMPlNG C 3A | ||
: I / | : I / | ||
g - | g - | ||
- .2 - | - .2 - | ||
i | i | ||
| Line 11,028: | Line 6,673: | ||
~ | ~ | ||
E o | E o | ||
1E i , | 1E i , | ||
i | i | ||
| Line 11,036: | Line 6,680: | ||
P - | P - | ||
//// \\\ \ | //// \\\ \ | ||
I '8 | I '8 | ||
/// / \\\ \ | /// / \\\ \ | ||
w - N/ / \\\ \ | w - N/ / \\\ \ | ||
//// \\\ \ - | //// \\\ \ - | ||
N"" - | N"" - | ||
#// \\\ ( - | #// \\\ ( - | ||
l | l Q '' | ||
Q '' | |||
//U M - | //U M - | ||
i f Vk E f xg - | i f Vk E f xg - | ||
\g\NN | \g\NN | ||
/ : 1 g , / gNK g 0.is _ gg 3 _ | / : 1 g , / gNK g 0.is _ gg 3 _ | ||
0.10 | 0.10 | ||
: ss\ g \ s | : ss\ g \ s | ||
_ y y 3g _ | _ y y 3g _ | ||
- NX X\ - | - NX X\ - | ||
\\\\ - ; | \\\\ - ; | ||
\\\\ l 0.06 1 | \\\\ l 0.06 1 | ||
,, 11II lill I I I I l l ll ll 1Ill l IIi 1111 l I I I I I I I IN i l I l' ) | ,, 11II lill I I I I l l ll ll 1Ill l IIi 1111 l I I I I I I I IN i l I l' ) | ||
OA2 0.03 0.04 0.06 0.06 0.08 0.1 C.15 0.2 0.3 OA 05 0.6 OA 14 15 2.0 1 PERIOD, $ECOND ENRICO FERMI ATOMIC POWER PLANT 1 | OA2 0.03 0.04 0.06 0.06 0.08 0.1 C.15 0.2 0.3 OA 05 0.6 OA 14 15 2.0 1 PERIOD, $ECOND ENRICO FERMI ATOMIC POWER PLANT 1 UNIT 2 l FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-38 | ||
UNIT 2 l FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-38 | |||
.__. HORIZONTAL FLOOR RESPONSE SPECTRA | .__. HORIZONTAL FLOOR RESPONSE SPECTRA | ||
. OPERATING BASIS EARTHQUAKE ELEVATION - | . OPERATING BASIS EARTHQUAKE ELEVATION - | ||
659'-0'' (SLAB NO. 41 RE ACTOR /AUXILI ARY | 659'-0'' (SLAB NO. 41 RE ACTOR /AUXILI ARY | ||
( BUILOING NORTH - SOUTH COMPONENT l SARGENT & LUNDY REPORT NO. SL-2682 l | ( BUILOING NORTH - SOUTH COMPONENT l SARGENT & LUNDY REPORT NO. SL-2682 l | ||
EF- 2-FS AR FR EQUE NCY, CPS so 33 20 10 sA 3.3 2D 1.0 05 zos ,,,, | |||
EF- 2-FS AR FR EQUE NCY, CPS so 33 20 10 sA 3.3 2D 1.0 05 | |||
zos ,,,, | |||
~ | ~ | ||
Isa _ | Isa _ | ||
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| Line 11,113: | Line 6,721: | ||
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a's | |||
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N\ sq g | |||
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l 0.06 | l 0.06 NM - | ||
l OD5 0 02 0 03 0.04 0.05 0.06 0.08 0.1 0.15 0.2 0.3 0.4 05 0.6 02 1A 15 2.0 PERIOD, SECOND l | |||
NM - | ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-37 l HORIZONTAL FLOOR RESPONSE SPECTRA | ||
l | |||
OD5 0 02 0 03 0.04 0.05 0.06 0.08 0.1 0.15 0.2 0.3 0.4 05 0.6 02 1A 15 2.0 PERIOD, SECOND l | |||
ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-37 | |||
. -- . OPERATING BASIS EARTHQUAKE ELEVATION - | . -- . OPERATING BASIS EARTHQUAKE ELEVATION - | ||
641*-6" (SLAB NO. 3) REACTOR / AUXILIARY l BUILDING E AST - WEST COMPONENT l | 641*-6" (SLAB NO. 3) REACTOR / AUXILIARY l BUILDING E AST - WEST COMPONENT l | ||
SARGENT & LUNDY REPORT NO. SL-2882 | SARGENT & LUNDY REPORT NO. SL-2882 | ||
EF 2-FSAR F RE OUE NCY, CPS P 50 33 20 10 50 33 20 to 05 | |||
EF 2-FSAR | |||
F RE OUE NCY, CPS P 50 33 20 10 50 33 20 to 05 | |||
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ng ~1111 1111 1 1 1 1 l L _LJ l 1 11ll IIli i111 . I I I i 1 1 IIii l i i l' 0 02 0 03 0 03 00's006 0 08 01 0 15 02 0.3 04 05 06 08 10 1.5 20 PE RIOD. SE COND l | ng ~1111 1111 1 1 1 1 l L _LJ l 1 11ll IIli i111 . I I I i 1 1 IIii l i i l' 0 02 0 03 0 03 00's006 0 08 01 0 15 02 0.3 04 05 06 08 10 1.5 20 PE RIOD. SE COND l | ||
ENRICO FERMI ATOMIC POWER PLANT UNIT 2 FINAL SAFETY ANALYSIS REPORT - | |||
ENRICO FERMI ATOMIC POWER PLANT UNIT 2 | |||
FINAL SAFETY ANALYSIS REPORT - | |||
FIGURE 3.7-36 HORIZONTAL FLOOR RESPONSE SPECTRA | FIGURE 3.7-36 HORIZONTAL FLOOR RESPONSE SPECTRA | ||
. _ _ OPERATING BASIS EARTHOUAKE ELEVATION - | . _ _ OPERATING BASIS EARTHOUAKE ELEVATION - | ||
''N . 641'-6" (SLAB NO. 3) REACTOR / AUXILIARY l | ''N . 641'-6" (SLAB NO. 3) REACTOR / AUXILIARY l BUILDING NORTH - SOUTH COMPONENT SARGENT & LUNDY REPORT NO. SL-2SS2 | ||
BUILDING NORTH - SOUTH COMPONENT SARGENT & LUNDY REPORT NO. SL-2SS2 | |||
~ | ~ | ||
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GSE 2 0 0 .008 AlorES : | GSE 2 0 0 .008 AlorES : | ||
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mm wmi.u.u,: | mm wmi.u.u,: | ||
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| Line 11,351: | Line 6,849: | ||
REQUEST (DESICN) f @/47 g - | REQUEST (DESICN) f @/47 g - | ||
DATE REQD. & OR SCHD. IMPACT | DATE REQD. & OR SCHD. IMPACT | ||
$ LOCATION & OR SYSTEM NSAdTOk EST. COST (IF IOJOWN) 8[.Ob Sd8'N5dY d | $ LOCATION & OR SYSTEM NSAdTOk EST. COST (IF IOJOWN) 8[.Ob Sd8'N5dY d | ||
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BI- FE | |||
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DOCUMENTS Td( - P4lISED.- Re\/ f I '18A- l - | DOCUMENTS Td( - P4lISED.- Re\/ f I '18A- l - | ||
DVE | DVE DESCRIPTION t ncBq^ JA ~WI M O1 HAAlGER.S G O S M ) AAfD OV - | ||
DESCRIPTION t ncBq^ JA ~WI M O1 HAAlGER.S G O S M ) AAfD OV - | |||
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KEASON . Ti4ER E I.S AN O PGN IA)G IA) THE u/AlI AT YOR PRESEA T .L OCATicAl fMh Alo PLAT & rb ArrkH CilANGE: s.J A AI G E G A RA% PLA TE JArrE)2FEA2&VM tAl ITf4 l AI AW I t Ch C/ fr2Pk A L 5]M YL1 blC . | KEASON . Ti4ER E I.S AN O PGN IA)G IA) THE u/AlI AT YOR PRESEA T .L OCATicAl fMh Alo PLAT & rb ArrkH CilANGE: s.J A AI G E G A RA% PLA TE JArrE)2FEA2&VM tAl ITf4 l AI AW I t Ch C/ fr2Pk A L 5]M YL1 blC . | ||
Written By: M.MAMU b _. | Written By: M.MAMU b _. | ||
/ A $ ., Dat. 7- f - 80 DarUel Discipline Engr. bM'[ =1 Date "'b 7 - M Authority For Work To Proceed: M Y. M/d44.M e Date Y-f"NO Edison Verbal Concurrence BIL L Affil8HAA) / WIM Pkd(w I'OORM Date . 'T- f ~FC Edison Field Engr. p /j_) M d m 2a Eh _ -__ 8 - | / A $ ., Dat. 7- f - 80 DarUel Discipline Engr. bM'[ =1 Date "'b 7 - M Authority For Work To Proceed: M Y. M/d44.M e Date Y-f"NO Edison Verbal Concurrence BIL L Affil8HAA) / WIM Pkd(w I'OORM Date . 'T- f ~FC Edison Field Engr. p /j_) M d m 2a Eh _ -__ 8 - | ||
Date 8-/- 6 2dison Field Project Engr. | Date 8-/- 6 2dison Field Project Engr. | ||
| Line 11,378: | Line 6,869: | ||
SKETCH AND/OR ADDITIONALINFORMATION ggTERNg ff .,. | SKETCH AND/OR ADDITIONALINFORMATION ggTERNg ff .,. | ||
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Revision as of 15:32, 31 January 2020
| ML19332B088 | |
| Person / Time | |
|---|---|
| Site: | Fermi  |
| Issue date: | 09/22/1980 |
| From: | DETROIT EDISON CO. |
| To: | |
| Shared Package | |
| ML19332B085 | List: |
| References | |
| NUDOCS 8009240513 | |
| Download: ML19332B088 (275) | |
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History (A30-00-G-900-SA-003) A30-06-0-000-SA-001 L H. iCXSON .?. AUG19 bou Title ! O DESIGN SPECIFICATION 1 NUCLEAR CLASS 2 & 3 SMALL PIPING AND TNRTRUMENT AND a)NTROL PIPING AND TUBING ENRICO FERMI POWER PLANT, UNIT 2 l l l Project l Design l Spec.fication i : O ; i 1 t Edison
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l 3071-525 Number Rev. A . O Date MARCH 1980 l-l -_. . . _ . - . L_ l
Specificction 3071-525 Prsp rsd by Enrico Ferni II Project Management Organization Issued: 12-10-75 n
%J Rev. A: 3-21-80 DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING Enrico Fermi Atomic Power Plant - Unit 2 DATE WRITTEN BY:
~
, f 80 R . J . ADLER /
CHECKED BY: / d / G' J [H. CASIGLIA - P.E. O S ERV S NG NG R dA/2/7c7 ~/M
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ENGINEER:
> W 7- 6 -80 D. F. LEHNERT, P.E.
9 gy h} 7 - 3. / - 70 T . H . DICK' SON , J R . REVIEWED: PROJECT ENGINEERING ASSURANCE ffIlb A. D. SMART ' SPECIFICATION CONTROL . LJ // f/ 6 /VO GENERATION ENGINEERINM DEPARTMENT - STAFF SPECIFICATION CONTROL - Generation Engineering Department - Staff t O 3071-525A.1 i l
MpecSUSectSen 27/h-kn3 Prcp;r:d by Enrico FGrmi 11 Proj:ct Managsment Organization Issued: 12-10-75 Rev. A: 3-21-80 DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING Summary of Revision A Section Description of Revision Effective Date
- 3. Revised to incorporate Addendum A 10-31-79 and changed temperature limitation from 300 F to 575 F.
8.1.A Revised to agree with Specifica- 3-01-76 tion 3071-032 Revison B. 9.3 Second paragraph on design thermal 3-21-80 and pressure displacements. 9.4.1 Revised to incorporate Addendum A 10-31-77 g and operating temperation condi- W tions. 9.4.2 Revised to incorporate Addendum A. 3-01-78 9.6 Changed section title to pipe 10-31-77 supports. 9.6.1 Revised second paragraph to 10-31-77 incorporate Addendum A. 9.6.4.3 Revised reference from 9.7.5.1 and 1-22-80 97.5.2 to 9.6.4.1 and 9.6.4.1. Changed means of attaching plates from Phillips Red to wedge anchor. 9.6.4.7 Removed entire article 10-31-77 9.6.4.8 Renumbered to 9.6.4.7 due to N/A deletion of old section 9.6.4.7. I I 3071-525A.2 l l
0 0 DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING ENRICO FERMI ATOMIC POWER PLANT UNIT 2 l l l l l l l 3071-525A.0 O
MjosROMOGIFGi1DXl/H937#
- Pr:parcd by Enrico Farmi 11 Project Managtment Organization Issued: 12-10-75 Rev. A: 3-21-80 DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING Summary of Revision A Section Description of Revision Effective Date 9.6.5 Added new section on variable 5-01-78 spring and mechanical snubber design.
9.6.6 Changed section of article from 10-31-77 10.3 and revised second paragraph to incorporate Addendum A. 9.10 Changed title of article, rewrote 3-31-80 paragraph on flexibility require-ments. . 9.11 Added paragraph five on maximum 2-09-78 allowable span for vertical pipe runs. 10.1.B Revised design temperature 10-31-77 10.2.B Revised design temperature 10-31-77 10.2.C Revised material specifications 3-02-78 10.3 Changed to article 9.6.6. N/A 14.1 Added to References, Specification 4-16-79 3071-527, 3071-528, and 3071-529 14.12, 14.13, 14.4 Additions to References. I 1 !O 3071-525A.3 i _ _I
Specific.itien 3071-525 Prspared by Enrico F.tr=i II Projset :tnsgsment Organiza: ion Issued: 12-10-75 Rev. A: 3-21-80 0 DCRs and DCNs Cleared By Rev. A DCR I-0002 DCN 0219 DCR P-0563 DCN 0355 DCR P-0570 DCN 0469 DCN 0534 DCN 0566 DCN 1305 Rev.A Revision A Incorporates Addendum A Note: The above DCR's and DCN's are not retroactive. O I 3071-525A 4 i I
Sp;cificcticn 3071-525 Prsp red by , Enrico Ferni II i ProjIct Managsment l Organization i Issued: 12-10-75 )
,, Rev. A: 3-21-80 i
\# DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTR.UMENT AND CONTROL PIPING AND TUBING Enrico Fermi Atomic Power Plant - Unit 2 INDEX ARTICLE CODE ARTICLE PAGE
- 1. SCOPE .................................. NA-3250 .......... 1
- 2. CERTIFICATION .......................... NA-3250 .......... 1
- 3. CLASSIFICATION ......................... NA-2000 .......... 2
- 4. DOCUMENTATION .......................... NA-3256 .......... 2
- 5. DESCRIPTION ............................ NA-3252 (a).......... 4
(]) 6. APPLICABLE DOCUMENTS ................... NA-3254 .......... 4
- 7. DESIGN ................................. NA-3252 (b).......... 6
- 8. SYSTEM DESIGN BAS IS . . . . . . . . . . . . . . . . . . . . NB-3111 .......... 8
- 9. COMPONENT DESIGN BASIS ................. NB-3112 .......... 9
- 10. COMPONENT CHARACTERISTICS .............. NB-3112 .......... 19
- 11. CLASSIFICATION ......................... NB-2140 .......... 20
- 12. HYDROSTATIC AND LEAK TESTS . . . . . . . . . . . . . NB-6000 .......... 21
- 13. IN-SERVICE INSPECTION .................. 10CRF50 .......... 22
- 14. REFERENCES ........................................................ 23 Attachment Appendix A, ANSI-Rating, Material Table 3071-525A.5 O
Specificction 3071-525 Issu:d: 12-10-75 R2v. A: 3-21-80 A30-00-G-900-SA-00 DISTRIBUTION OF CONTROLLED COPI"S OF SPECIFICATION 3071-525 lll No. of Copies Recipient 1 A. Alexiou, QA for Transmittal to State of Michigan 1 Documentation Control, Fermi 2 1 Fermi 2 Site, W. M. Everett 1 Project Engineer, E. G. Sliper 1 (ea.) Originacors: R. J. Adler, J. H. Casiglia 1 Reviewer of Stress Report and Certifying Professional Engineer: J. H. Casiglia 1 Enc,ineering Organization: Sargent and Lundy Engineers 55 East Monroe Street Chicago, Illinois 60603 Attention: Mr. F. P. Tsai 2 Installer and Inspector: General Contractor, EF2 Site Note: Uncontrolled copies may be distributed as needed. i 3071-525A.6 lh
Specificcticn 3071-525 Prspersd by Enrico Ferci II Project Management Organization Issued: 12-10-75
^ Rev. A: 3-21-80 U
DETROIT EDISON SPECIFICATION DESIGN SPECIFICATION FOR NUCLEAR CLASS 2 AND 3 SMALL PIPING AND INSTRUMENT AND CONTROL PIPING AND TUBING
- 1. SCOPE This document constitutes the Design Specification required by Article NA-3200 of ASME Boiler and Pressure Vessel Code, Section III,1971 issue,
" Nuclear Power Plant Components," for Nuclear Class 2 and 3 Small Piping and Instrumention and Control Tubing, to be install.e'. as part of the Nuclear Steata Supply System of the Enrico Fermi A'.omic Power Plant-Unit 2.
- 2. CERTIFICITION The undersigned registered Professional Engineer, competent in the field of design of piping and related nuclear energy system requirements, certifies th.2t this design specification together with the referenced documents complies with the requirements of Article NA-3250 of the ASME-Code, Section III and is correct and complete with respect to functions and operating conditions as required to provide a complete basis for design, construc-tion, and certified inspection in accordance with the code.
Juar 9. M80 DATE 0% SIGNATgkE
/
1 d ' l
$2C/Af//WM.
BRANCH ZG$/2 WMEW t REGISTRATION', STATE , and NUMBER or STAMP .
% l
."..,1 j
f4 / JOSEPH H. *., 4 CASfGLIA j c$ f i ce 2iEN 3i NO. G I /N E E R j eo '+, 3071-525A.7 Q'*..20842
......... , y OFESs\Ot f
Specificcticn 3071-525 Rs,v. A: 3-21-80 Pega 2
- 3. CLASSIFICATION h The piping systems referred to in this specification are limited to Nuclear Class 2 and 3 piping and Instrument and Control System Piping and tubing 4 inches and smaller in nominal diameter.
Process and Instrumentatien and Control piping systems whose designs are controlled by this specification are divided into two distinct classifica-tions. Those piping systems 4" and less in noninal diameter with design temperatures of 575 F or less and with design pressures of 1750 psig or less , which are connected to the pressure boundary 'at piping systems or equipment classified as Clase 2, are also classified as Class 2. These systems shall be designed in accordance with the requirements of the ASME III Code, Subsection NC, 1971 issue, including addenda thru Winter 1971. Those piping systems 4" and less in nominal diameter with design temperatures of 575 F or less and design pressures of 1750 psig or less, which are connected to the pressure boundary of piping systems or equipment classified as Class 3, are also classified Class 3. These piping systems shall be designed in accordance with the requirements of ASME III, Subsection ND, 1971 issue, including addenda thru Wihter 1971. In those cases where field designed small piping connects to systems or equipment of different code classifications, the more stringent design requirements will be applied out to the first anchor or normally closed g valve on the small pipe line. All Nuclear Class 1 and that Nuclear Class 2 and 3 sinall piping whosa design temperature exceeds 575 F and/or design pressure exceeds 1750 psig is not within the scope of this specification, and must be designed to the criteria specified by the System Design Specification for the system under consideration. (Reference 1)
- 4. DOCUMENTATION
- 1. The Owner and User of the system will be: -
Detroit Edison 2000 Second Avenue Detroit, Michigan 48226 3071-525A.8 l
Specificoticn 3071-525 R v. A: 3-21-80 Pcgs 3
- 4. DOCUMENTATION (cont'd)
- 2. The piping will be installed in the ENRICO FERMI ATOMIC POWER PLANT-UNIT 2 6400 N. Dixie Highway Stony Creek, Monroe County, Michigan - 48166 (P.O. Newport, Michigan)
- 3. The installer of the system will be designated by the Owner.
- 4. The enforcement authority having jurisdiction ht the location of the piping systems is:
l THE STATE OF MICHIGAN I DEPARTMENT OF LABOR BUREAU OF SAFETY AND REGULATION DEPARTMENT OF LABOR BUILDING 300 E. Ifichigan Avenue Lansing, Michigan 48913
- 5. Communications between the installer or manufacturer and the enforcement authority will be through the Owner unless specifically required by the code to be otherwise. In the latter case, prior approval r ' obtained and advance copies of the correspondence directed ,wner's documentation of fice and the cerfifying Professu . Engineer (s) of this document.
- 6. The Owner will comply with Article NA-3256 in filing a copy of this design specification with the enforcement authority before the piping is placed in service.
- 7. The manufacturer and/or installer shall identify the authorized inspection agency to the Owner on or before the contract date and shall provide the inspection agency with all required documentation, including the Quality Assurance Manual and this~ design specification.
- 8. A design report will be prepared for the piping systems within the scope of this specification. This report will be reviewed by those responsible for the design specification. The design report will be prepared by the Owner or his designated agent. The design methods, procedures, and records required by this specification and its attachments and references will form the basis for the preparation of the design report.
O l 3071-525A.9 ,_ l
Specificction 3071-525 R_v. A: 3-21-80 Pcg] 4
- 4. DOCUMEfffATION (cont 'd)
- 9. Each manufacturer and/or installer shall furnish the Owner with a copy of the appropriate certificate of authorization not later than the date of contract, (Article NA-3330).
- 10. Upon completion of the contract each manufacturer and/or installer shall complete the appropriate certificate of compliance and submit a copy of the certificate to the Owner for inclusion in the Owner's data report form N-3, (Article NA-3270)
- 5. DESCRIPTION (This is a functional description and not a code requirement.)
The field designed small piping within the scope of this specification is grouped into two general categories. 5.1 Instrumentation and Control Piping and Tubing The instrumentation and control piping and tubing is used to convey pressure signals and/or fluid samples from the process lines to the instrumentation for subsequent measurement or analysis. It is also used to convey a control medium (air, water, nitrogen) to an actuating device such as a hydraulic or pneumatic operator, hydraulic cylinder or diaphragm operator. Although the instrumentation and control piping and tubing may be connected to the process piping g pressure boundary, it is not considered to be functionally part of the process stream. 5.2 Small Process Piping The small process piping typically serves as an interconnection between a main process pipe header and an individual piece or small group of equipment or components. A typical example of a small process pipe is the interconnecting pipe between a main cooling water header and a locally mounted compartment fan-coil cooler. The small process piping constitutes an extension of the system process boundary.
- 6. APPLICABLE DOCUMENTS The design, material, fabrication, installation, inspection, and testing of the system and the system components shall be in accordance with the following:
O 3071-525A.10
Specificati:n 3071-525 R3v. A: 3-21-80 Page 5 () 6. APPLICABLE DOCUMENTS (cont'd)
- 1. This specification with the attachments.
- 2. The System Process and Instrumentation Diagrams 6M721-2000 Index and Legend of Abbreviations 6M721-2001 Legend of Symbols and Instr. Ident. for Plant System Diagrams 6M721-2002 Diagram - Main and Reheat Steam Systems 6M721-2015 Diagram - Station and Control Air - Unit 2 6M721-2017-1 Diagram - Off Gas Process System, Recombiner Chains I and II, Sheet 1 of 2 6M721-2017-2 Diagram - Off Gas Process System, Activity Reduction Chain, Sheet 2 of 2 6M721-2023 Diagram - Feedwater System 6M721-2027 Piping Diagram - Reactor Building Closed Cooling Water and Emergency Equipment Cooling Water Systems 6M721-2034 Diagram - Core Spray (C.S.S.)
6M721-2035 Diagram High Pressure Coolant Injection System - Reactor Building Unit 2 6M721-2043 Diagram - High Pressure Coolant Injection System - Barometric Condenser (HPCI) - Reactor Bldg. Unit 2 6M721-2044 Diagram - Reactor Core Isolation Cooling System 6M721-2045 Diagram - Reactor Core Isolation Cooling Barometric () 6M721-2046 Condenser (RCIC) Diagram - Reactor Water Clean-up, Reactor Bldg. (RWCU) 6M721-2047 Diagram - Reactor Water Clean-up, Filter /Demin., (RCiC) 6M721-2081 Diagram - Control Rod Drive System (CRD) 6M721-2082 Standby Liquid Control System 6M721-2083 Diagram - Residual Heat Removal (R.H.R. ) Division I 6M721-2084 Diagram - Residual Heat Removal (R.H.R.) Division II 6M721-2087 P&ID - Combustible Gas Control System 6M721-2088 Diagram - Reactor Water Clean-up Phase Separators 6M721-2089 Diagram - Nuclear Boiler System 6M721-2090 Diagram - Nuclear Boiler System 6M721-2833 Diagram - Reactor Recirculation System - Nuclear Boiler System 6M721-2985 , Diagram - Drips and Drains from
- team Lines and Mair Turbine 6M721-3445 Diagram - Nitrogen Inerting Diagram 6M721N-2046 P&ID Diesel Generator System - Division I-R.H.R. Complex 6M721N-2047 P&ID Diesel Generator System - Division II-R.H.R. Complex 6M721N-2048 P&ID Diesel Fuel Oil System and Lube Oil System '
Division I - R.H.R. Complex 6M721N-2049 P&ID Diesel Fuel Oil System and Lube Oil System I Division II - R.H.R. Complex O 3071-525A.11 1 -.
Specificcticn 3071-525 Rov. A: 3-21-80 P;g2 6
- 6. APPLICABLE DOCUMENTS (cont'd) h
- 2. (cont'd) 6M721N-2054 P&ID Service Water, Make-up, Decant and Overflow Systems - R.H.R. Complex 6M721N-2056 P&ID Diesel Cenerator Ventilation - R.H.R. Complex-Division 1 6M721N-2057 P&ID Diesel Generator Ventilation - R.H.R. Complex-Division 1 6M721N-2058 P&ID Diesel Generator Ventilation - R.H.R. Complex-Division II 6M721N-2059 P&ID Diesel Generator Ventilation - R.H.R. Complex-Division II 6M721-2028 Process Diagram - Radwaste System 6M721-2031 Sump Pump Diagram Sheet 1 - Radwaste System 6M721-2032 Sump Pump Diagram Sheet 2 - Radwaste System 6M721-2215 Chemical Waste System Diagram - Radwaste System 6M721-2263 Evaporator Feed Diagram - Radwaste System 7M721-2709 Diagram - Standby Gas Treatment and Primary Containment Purge System - Reactor Building SM721-3435 Diagram - Evaporator Drains hetering System to Drum Disposal Radwaste Building 6M721-4127 Reactor Drywell Cooling System Flow Diagram (P&ID) 6M721-4325 Control Center Air Condition System - Water Side 61721-2400-1 6I721-2400-2 Plant Sampling Data Plant Sampling Data R.W.B. g 61721-2400-3 Plant Sampling Data T.B.
61721-2400-4 Plant Sampling Data R.B. 61721-2649-1 Standby Gas Treatment System Diagram 61721-2181-1 Process Radiation System Diagram 61121-2181-2 Process Radiacion System Diagram 61721-2181-3 Process Radiation System Diagram
- 3. Other reference documents as listed under Article 14.
- 7. DESIGN 7.1 System Design Life The system shall be designed for an effective design life of 40 l years, accounting for corrosion, erosion, and fatigue. The corrosion l allowance to be used is: 1 0.120" for steam in carbon steel piping 0.080" for water in carbon steel piping 0.0024" for stainless steel piping 0.000 for gas filled lines 3071-525A.12 O
- Specificctien 3071-525 Rsv. At 3-21-80 Pego 7
- 7. DESIGN (cont'd) 7.2 Normal and Upset Environmental Conditions The small Piping Systems, situated in the primary containment will be exposed to the following condition during the life of the plant:
External Pressure = 0.0 to 2.0 psig External Temperature = +105 to 150 F (Range) Relative Humidity = 40 to 90% Atmosphere = 97% N2 , 3% 02 External Radiation - Gamma 50 Rads / Hour Neutron 140,000 N/Cm2 _ see, 7.3 Faulted Environmental Conditions in Drywell (one time only) External Pressure - -2 to 56 psig for 1 minute at 340 F.
-2 to 35 psig for 3 hours at 340 F.
-2 to 35 psig for 6 hours at 320 F.
O to 25 psig for 1 day at 250 F. O to 20 psig for 100 days at 200 F. O a 1 tive n" taitF - iooz Radiation = 2.6 x 107 RADS (gamma) 7.4 System Fluid Those piping systems within the scope of this specification will l contain the following fluids. , l Media: demineralized water, steam, air, and nitrogen I Radioactivity: 0.07 micro curie /mL at zero decay time ph 0 25 C: 6.0 to 8.5 ) Suspended Solids: <10 ppb Dissolved Oxygen: <200 ppb Halogens: <1.0 ppm O 3071-525A.13
Specifiestien 3071-525 Rev. A: 3-21-80 P g2 8
- 7. DESIGN (cont'd) 7.5 Environmental Conditions of Secondary Containment g Those piping systems within the scope of this specification situated in the secondary containment will be subjected to the following conditions:
External Pressurc = atmospheric External Temperature = winter minimum of 40 F faulted maximum of 148 F (for 8 hours) average operating of 70 F Relative Humidity = 50 to 90% Radiation = 7.9 x 103 RADS (gamma), (includes faulted dose)
- 8. SYSTEM DES 1CN BASIS 8.1 Deformation Limits
- a. Piping Components Cold working, cold forming, or bending of the Class 2 and 3 piping components within the juristiction of this specification is permitted.
- b. Pipe Suspension Components Pipe suspension components may be cold formed during fabrica-tion. Subsequent heat treatment is not required.
8.2 Cold springing is not permitted in the design of the piping. In esses where mismatches due to fabrication tolerances exist during the installation the size of the closure piece shall be field adjusted to provide the required fit. 8.3 Dimensional Limits Piping components shall be fabricated in accordance with the Fabrication Specification 3071-30 and the fabrication tolerances shall be per P.F.1. Standard ES-3. Dimensional standards for fittings shall be per ANS1 B16.9 for butt welding fittings and B16.11 for socket-welding fittings, unles: otherwise specified on the Piping Isometric Drawings. 3071-525A.14
Specificati n 3071-525 R2v. A: 3-21-80 Pcgs 9
- 8. SYSTEM DESIGN BASIS (cont'd) 8.4 Temperature Limits The metal and fluid temperature for cleaning, flushing, and decontaminating shall be above +60 F, but not exceeding 200 F for small piping systems.
- 9. COMPONENT DESIGN BASIS 9.1 Equipment Nozzle Interface Loads 9.1.1 In the case where piping designed in accordance with this specification is connected to process connections (nozzles on pumps, heat exchangers, etc. ) consideration as to the maximum loading imposed upon the equipment is required. The maximum loadings for piping designed in accordance with this specification are given in Table I. The system Design Specification (Reference 1) for the system in question must be consulted and a determination made that the maximum loads from the piping do not exceed the allowable nozzle loads specified for the piece of equipment under consideration.
9.1.2 In case of non process line small piping connections to equipment (i.e. instrument taps, bearing cooling water connections, etc.) the maximum loads imposed on the equipment are negligible, and need not be considered. 9.2 Major Piping Connection Interface Loads In those cases where piping designed in the field, in accordance with this specification, connects to main process piping, the maximum probable loads imposed by the small piping will be considered in the design of the main process piping, and no further consideration of these effects is required. 9.3 Equipment Nozzle and Primary Containment Penetration Thermal Deflection Process equipment nozzles which connect to piping designed under this specification are considered as anchor points and are not subject to significant thermal deflection. Unless provided elsewhere, design thermal and pressure displacements for smali pipe penetrations on the drywell shall be assumed to be 1.92-in. vertical and 1.11-in. radial. Des?.gn thermal displacements for small pipe penetrations on the sunpression chamber (torus) shall be assumed to be 0.43-in. vertical and 1.30 in. radial. 307b 525A.15
Specificati:n 3071-525 R v. A: 3-21-80 P:ga 10
- 9. COMPONENT DESIGN BASIS (cont'd)
O TABLE I MAXIMUM PIPING TERMINAL LOADS Pipe Size Schedule Moment Load (ft-lb) Shear Force (lb) 1/2 40 85 72 80 100 78 160 110 99 3/4 40 147 103 80 178 128 160 209 145 1 40 277 170 80 335 207 160 396 246 1-1/4 40 489 270 80 607 329 160 713 383 1-1/ 2 40 679 342 80 160 858 1060 427 529 lll 2 40 1170 536 80 1520 683 160 2040 912 2-1/2 40 2220 903 80 2790 1120 160 3410 1360 3 40 3590 1360 80 4630 1680 160 5990 2200 4 40 6690 2250 80 8890 2920 160 12300 3950 1 1 3071-525A.16 l l
Specificction 3071-525 Rev. A 3-21-80 Page 11
- 9. COMPONENT DESIGN BASIS (cont'd)
C) ' 9. 4 Thermal and Seismic Deflection of Major Process Piping Connections 9.4.1 Thermal Deflections of Major Process Piping Connections Small pipe connection points on major process piping linea are subject to the thermal deflections of the major process pipe . The design of the small pipe must incorporate suffi-cient flexibility to accommodate these thermal deflections. This flexibility will be provided by incorporating of f-set legs in the small pipe, oriented in a direction perpendicular to the direction of movement of the process pipe. The meth-ods of designing and sizing the thermal of fset legs in the small pipe shall be as given in Appendix D of Reference 2. Thermal deflections of the major piping systems are available in the computerized piping stress analysis, and will normally be supplied by Edison's Project Design Organization. In lieu of using the above information, the thermal deflection of the major process pipe connection may be calculated using the below listed formulae: (1) For carbon steel process pipe: AXT = 8.68 x 10~$ X AT AYT = 8. 68 x 10-5 Y AT Aa7 = 8. 68 x 10-5 I AT Where AX = the thermal movement of the process pipe in the east-wes t direction. AY = the thermal movement of the process pipe in the vertical direction. X = the distance g feet along an east-west line between the small pipe connection on the process pipe and the first anchor on the process pipe. i' = the dif ference in elevation in feet between the small pipe connection on the process pipe and the fits t anchor on the process pipe. 3 = the distance, in feet, along a north-south line, between the small pipe connection on the process pipe and the first anchor on the ,3 process pipe. b 3071-525A.17
Specificcticn 3071-525 Rav. A: 3-21-80 Pcgg 12
- 9. COMPONENT DESIGN BASIS (cont'd) 9.4 fcont'd) 9.4.1 (cont'd)
AT = the operating temperature of the major piping system minus -70 F. (2) For stainless steel process pipe: AXT = 1.18 x 10-4 ~X AT AYT = 1.18 x 10-4 Y AT AET = 1.18 x 10-4 5 AT Where all terms are as previously defined. In those cases where the connection point on the major process line is between two anchors, the distances to the farther anchor shall be used in the equations above. 9.4.2 Seismic Deflections of Major Process Piping The seismic deflections of major piping systems are available in the computerized piping erress analysis, and will normally be supplied by Edison's Project Design Organization. In the absence of the above information, the maximum probable seismic deflections of main process piping at points of intersection with field-designed small pipe withing the scope of this specification is 1/4 inch in each of three mutually perpendicular directions. These deflections shall be added to the thermal deflections calculated in paragraph 9.4. I and used as the basis for design of the offset legs, as described in Appendix "D" of Reference 2. 9.5 Seismic Deflection of Process Equipment The equipment attached to those Category I Piping systems within the scope of this specification, shall be considered as a rigid anchor, subjected to the seismic displacements of the supporting floor slab or other building structural component. The maximum probable seismic dispincements for the various major structural elements in the Reactor / Auxiliary Building and the RHR Complex are given in Tables 2 and 3 respectively. 3071-525A.18
i Specificcticn 3071-525 l Rsv. A: 3-21-80 l Page 13
- 9. COMPONENT DESIGN BASIS (cont'd)
[) TABLE 2 SEISMIC DISPLACEMENTS OF j RECTOR / AUXILIARY BUILDING STRUCTURAL COMPONENTS I Component Seismic Displacements (2*0.B.E.) East-West North-South Up-Down l 1st Floor Slab 0.024 in. 0.024 in. 0.0032 in. 2nd Floor Slab 0.056 in. 0.06 in. 0.0064 in. 3rd Floor Slab 0.08 in. 0.08 in. 0.0084 in. I 4th Floor Slab 0.096 in. 0.095 in. 0.0094 in. j i Sth Floor Slab 0.107 in. 0.102 in. 0.014 in. Biological Shield Wall 0.108 in. 0.104 in. Negligible Reactor Pedestal 0.21 in. 0.02 in. Negligible O TABLE 3 SEISMIC DISPLACEMENTS OF THE RHR COMPLEX STRUCTURAL COMPONENTS Component Seismic Displacements (2*0.B.E.) East-West North-South Up-Down Grade Floor Slab 0.012 in. 0.042 in. Negligible Upper Floor Slab 0.028 in. 0.056 in. Negligible Roof Slab 0.045 in. 0.059 in. Negligible f ( 3071-525A.19 l
Sp;cificatien 3071-525 R3v. A: 3-21-80 Pcgs 14
- 9. COMPONENT DESIGN BASIS (cont'd) 9.6 PIPE SUPPORTS O
9.6.1 Design Stress Limits or Load Ratings Supports shall be designed to resist the loads and permit the calculated piping movements determined by field calculations made in accordance with Reference 2, Appendices B thru D. Design stress limits and/or components standard support load ratings shall be determined in accordance with American National Standards Institute, Standard ANSI B.31.1.0 Paragraphs 120 and 121. 9.6.2 Column Design Structural members such as columns and struts may be long in proportion to their diameter or lateral dimensions. The slenderness ratio, K1/r, of compression members used in the design and fabrication of guides, sway braces, snubbers, seismic restraints and supplementary structural attachments shall not exceed 120. 9.6.3 Anchor Design Anchors, limit stops and rigid ties shall be provided for directing expansion away from equipment, control of line g behavior during temperature changes and for protection of elements in the system against excessive expansion travel. Provision must be made to assure that the anchor, limit stop or rigid tie is designed and proportioned to resist the absolute sum of the forces and/or bending moments in the pipe at either side of the anchorage location. 9.6.4 Structural Attachment 9.6.4.1 Wherever possible component support beam attachments shall be welded to major structural l steel or embedded steel plates as detailed on Detroit Edison Standard Drawing SP732 (see 9.7.8 for welding requirements). l l i l 3071-525A.20 i
Specificcticn 3071-525 Rsv. A: 3-21-80 Page 15 () 9. COMPONENT DESIGN BASIS (cont'd) 9.6 PIPE SUPPORTS (cont'd) 9.6.4.2 Continuous Inserts (cont'd) Continuous steel " Gateway" inserts are provided for situations where the pipe is to be supported from concrete slabs and/or walls. A design load limit of 3000 lb, within any l'-0" section of the insert has been established. Point loading within the first 6" of the ends of any insert is to be avoided. 9.6.4.3 Self-Drilling Concrete Anchors Where it is not possible to erect supports per 9.6.4.1 or 9.6.4.2, steel plates may be attached to concrete structures by use of concrete expansion anchors. Acceptable anchor types and allowable load ratings are provided in Specification 3071-226. Threading of hanger rods directly to anchors that have been installed overhead is not permitted. A
positive method of providing a moment-free connec-tion must be used for attachment of hanger rods to the structure.
9.6.4.4 Floor Attachment All base plates of solid or spring stanchion sup-ports must be leveled and anchored to the struc-ture. 9.6.4.5 Support of Valve Motor Operators and By-Pass Piping All motor operators attached to valve stems must be supported independently of the pipe line supports. By pass or warmup piping around valves shall be supported from the main process pipe with appropriate supplemental supports. Consideration shall be given to insure that vibration of the by pass piping-relative to the main process can not occur. s-3071-525A.21
Specificcticn 3071-525 Rev. At 3-21-80 Prg2 16
- 9. COMPONENT DESIGN BASIS (cont'd)
- 9. 6 PIPE SUPPORTS (cont'd) 9.6.4.6 Seismic Supports Piping classified as ASME III, Class 3 (Group C),
Seismic II does not require seismic supports. Other piping within the scope of this specification requires restraint against uplift and sway during earthquake conditions. Computions of pipe line supports requiring seismic considerations must ensure that valve accelerations will be limited to 5.0 g horizontal and 3.0 g vertical (simultaneously) during the Safe Shut-down Earthquake (SSE) event. 9.6.4.7 Assembly of Supports Where possible, support and hanger assemblies shall be assembled using standard and production parts, completely prefabricated in the conventional designs of good engineering practices specified in the Ibnufacturers Standardization Society Guides SP-58 and SP-69. 9.6.5 Variable Spring and Mechanical Snubber Design O Variabie springs or mechanical snubbers shall be used at support or snubber locations where the calculated movement is in excess of .125" except where indicated below:
- 1) Variable springs or snubbers should be added to the first support or restraint located near equipment where the calculated movement in the direction of the load is in excess of .02 inches.
- 2) Variable springs or snubbers should be added to the first support or restraint located near pipe changes in direction where the calculated movement in the direction of the load is in excess of .06 inches.
O 3071-525A.22
Sp;cificatien 3071-525 Rav. A: 3-21-80 Peg 2 17
- 9. COMPONENT DESIGN BASIS (cont'd) 9.6 Pipe Supports (cont'd) 9.6.5 Variable Spring and Mechanical Snubber Design (cont'd)
Variable springs should have a spring variability factor equal to or less than the values shown in the table below: Spring Variability Selection Chart
~
System Pipe Runs At Nozzle Conn. QA Level 1, Class B & C 25% 25% All other systems 25% 25% Spring = Pipe travel (IN) x spring rate (lbs/in) Variability Operating (Hot) Load (lbs) 9.6.6 Pipe Supports
- a. Design Load:
The design load shall be taken as the algebraic sum of the dead weight, anchor deflection and seismic loads, combined in a manner consistant with the loading conditions specified in Article 11.0.
- b. Materials The selection of construction materials used in the design and fabrication of supports will be based on the conventional theory which gives a linear distribution of stress and strain in the elastic range up to the proportional limit.
9.7 System Line Valves All system line valves used in piping systems within scope of this specification shall be designed in accordance with the requirements of Edison Valve Specification 3071-12, or Edison Control Valve Specification 3071-26, and Design Specification 3071-501. f l 3071-525A.23 l l l I
.1- i
Specificati n 3071-525 Rsv. A: 3-21-80 Pcg2 18
- 9. COMPONENT DESIGN BASIS (cont'd)
O 9.8 Seismic Analysis of Piping Thermal Insulation Piping systems within the scope of this specification will be either uninsulated or will be insulated with approximately one inch of fiberglass insulation having an average density of 3 lb/f t 3, It shall be assumed for purposes of design that all pipes are insulated in order to conservatively maximize calculated piping system stress and support loading. 9.9 Seismic Analysis of Piping Piping designed to the requirements of this specification shall be seismically analyzed using a simple beam as the analytical model. The assumed seismic excitation shall be based upon the most energetic seismic response spectra for the building in which the piping is to be installed. Seismic restraints shall be designed and seismic spans determined such that the maximum fiber stress, in bending, does not exceed 7000 psi for the Operating Basis Earthquake (OBE) and 14,000 psi for the Safe Shutdown Earthquake (SSE). Additionally, the seismic restraints shall limit the deflection of the pipe to two inches during the SSE event, independent of stress level. Piping classified as ASME III, Class 3 (Group C), Seismic 11 does not O require seismic analysis, however, the applicable portions of paragraphs 9.10 and 9.11 will still apply. 9'.10 Consideration of Piping Flexibility Requirements The piping system shall be designed to limit the sum of the stress range variations due to thermal expansion and dif ferential terminal movement to 15,000 psi. Thermal expansion analysis shall be based upon the operating temperature of the piping system (process piping) and/or the operating temperature of the source connection (1&C tubing). For piping and tubing with an operating temperature of 150 F and below, no detailed thermal expansion analysis is required. 9.11 Dead Weight Analysis of Piping Dead weight analyses shall be conducted for all piping which is to be field designed to the taquirements of this specification. In conducting the dead weight analysis, the analytical model assumed shall be a simply-supported beam, subjected to a uniformly distributed load. 3071-525A.24 O t l
Specificatien 3071-525 Rev. A 3-21-80 Page 19 () 9. COMPONENT DESIGN BASIS (Cont'd) 9.11 Dead Weight Analysis of Piping (Cont'd) The analysis shall consider the weight of the pipe and its contents. All piping shall be assumed to be insulated, as specified in paragraph 9.8. Consideration shall be given to the inclusion of concentrated loads , such as valves , flanges, flow sections, etc. , to the piping spans between supports. Pipe support spacing shall be determined by analysis, so as to limit the maximum weight-induced bending stress to 3000 psi. The maximum allowable span between gravity supports on vertical pipe runs shall be three (3) times the values shown in Table B-1 of Sargent and Lundy Report SL-3159. On Seismic Class 11 Piping Systems a guide should be added between supports whose span is greater than two times the normal spans in Table B-1.
- 10. COHPONENT CHARACTERISTICS 10.1 Process Piping Characteristics
- a. Design Pressure: 1750 psig (maximum assumed for purpose of design).
l (~~) s_ b. Design Temperature: per the system Isometric Drawings
- c. Materials : Process piping materials and weights are listed in Appendix "A", Tables 1 and 2, as a function of ANSI pressure classification and material type. Pipe sizes may be determined from the System Process and Instrumentation Diagrams (Paragraph 6.2). ANSI pressure ratings and material !
types are determined by reference to the pipng fabrication (-1) drawing for the connected main process piping. 10.2 Instrumentation and Control Tubing and Piping
- a. Design Pressure: 1750 PSIG (maximum assumed for purpose of design)
- b. Design Temperature: per the system Isometric Drawings
- c. Material:
- 1. Class 2: (inside containment only)
Pipe - 3/4" SCH 80S Scamless - ASME SA 312, T316L A O 3071-525A.25 1
Specificcti:n 3071-525 R;v. A: 3-21-80 Pcg2 20
- 10. COMPONENT CHARACTERISTICS (cont'd) 10.2 Instrumentation and Control Tubing and Piping (Cont'd) O
- c. 1. Class 2: (inside containment only) (Cont'd)
Fittings: Socket welded 3000# ASME SA 182, Grade 316L Pipe - 1" SCH 160S - Seamless - ASME SA 312, T316L Fittings - Socket Welded, 6000# ASME SA 182, Grade 316L
- 2. Class 2 & 3: (outside primary containment)
Tubing - 5/8" x 0.083 Wall Seamless ASME SA 213, Type 304, 316 or 321 Tubing - 3/8" x 0.049 Wall Seanless ASME SA 213, Type 304, 316 or 321 Fittings - Socket Welded, 3000# ASME SA 182, T316 (shall be used with 5/8" tubing). Fittings - Compression, ASME SA 403, T316 Swagelok, Parker Hannifin or equivalent (shall be used with 3/8" tubing).
- d. Unique Characteristics:
To determine the size and class of instrument piping required refer to the Master Instrument List.
- 11. CLASSIFICATION OF CONDITIONS 11.1 Operating Conditons The operating conditions for the piping systems within the scope of this specification vary, and asy be determined from the applicable System Design Specification (Ref. 1). In no case do the operating conditions exceed the design conditons specified in Paragraph 10.1.
11.2 Earthquake Loadings For analysis of all Class 2 and 3 components the SSE shall be considered to occur concurrently with all other normal and transient loads, and the combination shall be considered as an emergency condition. One SSE shall be assumed to occur during the life of the plant. 3071-525A.26 O i i
Specificatien 3071-525 Rav. A 3-21-80 Pega 21
- 11. CLASSIFICATION OF CONDITIONS (cont'd)
O 11.2 Earthquake Loadings (cont'd) For the analysis of Class 2 and 3 components, the OBE shall be considered to occur concurrently with all normal and transient loads and the combination shall be considered as an upset condition. Two OBE's shall be assumed to occur during the life of the plant. All liquid-retaining piping is considered to be flooded at all times. Gas (air, steam) retaining piping shall be considered unflooded during all operating conditions. 11.3 Pipe Whip and Missile Impact Design criteria of the above nature is not part of this document or the stress analysis required by the ASME Code. The conditions are evaluated in a separate report. 11.4 Jet Impingement Loadings Piping within the scope of this specification does not require analysis for jet impingement loadings. 11.5 Pipe Break Criteria Analytical consideration of pipe breaks between the inner and outer ; isolation valves of Class 2 piping systems is not within the scope of this specification. The requirements for this analysis are given in the applicable system design specifications (Reference 1).
- 12. HYDROSTATIC AND LEAK TESTS 12.1 Process Piping and Connecting Instrumentation and Control Piping and Tubing Process piping and connecting Instrumentation and Control piping and tubing, up to, but not including connecting instruments, which carry steam or water during normal operating shall be hydro-statically tested prior to being placed in service.
Hydronatic testing shall meet the requirements of ASME III Subsection NC-6200. Valve bodies shall be in accordance with ANSI B16.5 or MSS SP-66 for Class 2 and 3 valves. The test pressures and temperatures shall be determined from the applicable system Design Specification (Reference 1). Prior to hydrostatic test, all system valves with leak off connections shall have the connections open-ended. Exercisable O 3071-525A.27 l
Specificcticn 3071-525 Ra y. A 3-21-80 Pcg2 22
- 12. HYDROSTATIC AND LEAK TESTS (cont'd) 12.1 Process Piping and Connecting Instrumentation and Control Piping and Tubing (cont'd) check valves shall be held open with the disc exercisor prior to and during the hydrostatic test. Those check valves which are not exercisable shall have the test pressure applied to the upstream side. System line valves er. cept those providing isolation between different pressure classes shall be open, but not backseated to provide full differential pressure against the stem packings.
During hydrostatic test, examination for leakage shall be made. There shall be absolutely no visible leakage on any of the pressure retaining components, including valve stem packings, relief valve seats and check valve exercising devices. The test medium shall be demineralized water. 12.2 Instrumentation and Control Piping and Tubing Not Connected to_a Process Barrier Process Piping and Instrumentation and Control Tubing which normally carries a gas, other than steam, shall be pneumatically tested prior to being put in service. Pneumatic testing shall be conducted in accordance with the g requirements of ASME III, Subsection NC-6300. W ' The test pressure shall be 150 psig. The test temperature shall be 60 F minimum, 100 F maximum. During the pneumatic test, all valves shall be open, but not backseated to insure that full test pressure is applied across the l stem packings. j During the pneumatic test, all piping and tubing joints and valve stem packings shall be coated with a soapy water solution. There shall be no evidence of bubble formation with the lines at full tes' pressure. The test medium shall be clean dry compressed air or nitrogen.
- 13. IN-SERVICE INSPFCTION The piping systems within the scope of this specification will not be subject to in-service inspection.
3071-525A.28
~
Specificati:n 3071-525 Rev. At 3-21-80 Page 23
- 14. REFERENCES
- 1. The Detroit Edison Company Sys tem Design Specifications, 3071-500 series.
3071-501 Nuclear Valves 3071-502 Core Spray System 3071-503 Residual Heat Removal System 3 071-504 HPCI System 3071-505 RCIC System 3071-506 Control Rod Drive System 3071-507 Standby Liquid Control System 3071-508 Reactor Water Cleanup System 3071-509 Fuel Pool Cooling System 3071-510 Feedwater System 3071-511 Steam Drain Sys tem 3071-512 Emergency Equipment Cooling Water Sys tem 3071-513 Of f-Gas Sys tem 3071-514 Reactor Refueling Bellows and Drywell Seal Bellows 3071-515 Reactor Primary Containment Electrical Penetrations 3071-516 Primary Containment Penetration Assemblies 3071-517 RHR Complex
- 3071-518 Essential Accumulators for Nuclear Class I Air Operated Valves 3071-519 Primary Containment and Reactor Building Equipment and Floor Drainage Sump Disposal Systems O- 3071-520 Station and Control Air Sys tem 3071-521 Liquid Radwaste Sys tem 3071-522 Reactor Drywell Cooling coils 3071-523 Reactor and Auxiliary Building Emergency Equipment Cooling Coils 3071-525 Field Designed Nuclear Class 2 and 3 Small Piping and Instrument and Control Piping and Tubing 3071-526 Hydrogen Recombiner Piping System 3071-527 Condenser Coils for Control Center Air Conditioning Sys tem Chillers ,
3071-528 Mechanical Seismic Shock Suppressors 1 3071-529 Miscellaneous Containment Interface Piping
- 2. "Small Pipe Design Standard" - Enrico Fermi Power Plant - Unit No. 2, l Satgent and Lundy Report No. SL-3159.
- 3. The Enrico Fermi Power Plant - Unit No. 2, Master Valve List.
- 4. BWR Equipment Enviro'imental Requirements General Electric Specification 22A3019,
- 5. The Edison Pipe Erection Specification 3071-31.
- 6. The ASME Boiler and Pressure Vessel Code, Section III,1971 issue.
O
\/
3071-525A.29
Specificsticn 3071-525 Ray. A: 3-21-80 Pego 24
- 14. REFERENCES (cont'd)
O
- 7. The Edison Pipe Fabrication Specification, 3071-30.
- 8. The ASME Boiler and Pressure Vessel Code, Section XI, 1974 issue.
- 9. The Edison Welding Specifications 311, 3071-98.
- 10. Edison Design Calculation No. 526, Enrico Fermi Power Plant - Unit No. 2.
- 11. The Edison Concrete Expansion Anchor Specification 3071-226
- 12. Edison Drawing SC721-2002.
- 13. Letter EF2-48,349 dated March 31, 1980.
O 3071-525A.3C
O I APPENDIX A ANSI Primary Pressure Rating, Materials and Dimensions for Nuclear Piping O O 3071-525A.31
l
. Al i TABLE I
() CARBON STEEL PIPING SYSTEMS ANSI ASTM ITEM PRESSURE RATING SIZE RATING TYPE SPECIFICATION Pipe 900 lbs 3" and Smaller Schedule 160 Seamless A106 Gr B 4" Schedule 120 Seamless A106 Cr B 600 lbs 3" and Smaller Schedule 160 Seamless A106 Cr B 4" Schedule 80 Seamless A106 Gr B 300 lbs 2" and Smaller Schedule 80 Seamless A106 Gr B 2-1/2" - 4" Schedule 40 Seamless A106 Cr B 150 lbs 2" and Smaller Schedule 80 Seamless A106 Gr B 2-1/2" - 4" Schedule 40 Seamless A106 Gr B Fittings 900 lbs 2" and Smaller 6000 lbs S.W. A234 Gr WPB - 2-1/2" - 4" Match Pipe Wall B.W. A234 Gr WPB ( }) 600 lbs 2" and Smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 3" Schedule 160 B.W. A234 Gr WPB 4" Schedule 80 B.W. A234 Gr WPB 300 lbs 2" and smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 4" Schedule 40 B.W. A234 Gr WPB 150 lbs 2" and Smaller 3000 lbs S.W. A234 Gr WPB 2-1/2" - 4" Schedule 40 B.W. A234 Gr WPB Valves 900 lbs 2" and Smaller 1500 lbs S.W. A105 2-1/2" - 4" 900 lbs B.W. A216 Gr B 600 lbs 2" and Smaller 600 lbs S.W. A105 600 lbs B.W. A216 Gr B 300 lbs 2" and Smaller 600 lbs S.W. A105 2-1/2" - 4" 300 lbs B.W. A216 Gr B 150 lbs 2" and smaller 600 lbs S.W. A105 2-1/2" - 4" 150 lbs B.W. A216 Gr B
- continued -
3071-525A.32 l 1
A2 TABLE I CARBON STEEL PIPING SYSTEMS (cont'd) h ANSI ASTM ITEM PRESSURE RATING SIZE RATING TYPE SPECIFICATION Flanges 900 lbs 2" and smaller 1500 lbs SW, RF A105 2-1/2" - 4" 900 lbs WN, RF A105 600 lbs 2" and Smaller 600 lbs SW, RF A105 2-1/4" - 4" 600 lbs WN, RF A105 300 lbs 2" and Smaller 300 lbs SW, RF A105 2-1/2" - 4" 300 lbs WN, RF A105 150 lbs 2" and Smaller 150 lbs SW, RF A105 2-1/2" - 4" 150 lbs WN, RF A105 Bolts All Bolt Studs A193 Gr B7 Hex A194 Gr 2H O Nuts All Caskets All Flexitallic Style CG 3071-525A.33 9
A3 TABLE 2 STAINLESS STEEL PIPING SYSTEMS
~
ANSI ASTM ITEM PRESSURE RATING SIZE RATING TYPE SPECIFICATION Pipe 900 lbs 3/4" Schedule 80S Seamless A312TP304 or 316L 1" - 2" Schedule 160S Seamless A312TP304 or 316L 2-1/2" & 3" Schedule 160S Seamless A376TP304 or or Seamweld A358TP304 600 lbs 2" and Smaller Schedule 80S Seamless A312TP304 2-1/2" - 4" Schedule 80S Seamless A376TP304 or or Seamweld A358TP304 300 lbs 2" and Smaller Schedule 40S Seamless A312TP304 2-1/2" - 4" Schedule 40S Seamless A376TP304 or or Seamweld A358TP304 150 lbs 2" and Smaller Schedule 40S Seamless A31?TP304 or or O 2-1/2" - 4" Schedule 10S Seamweld A358TP304 Fittings 900 lbs 2" and Smaller 3000 lbs S.W. A182 Gr F304 or 316L 2-1/2" & 3" Schedule 160S B.W. A403 Gr WP304 4" Schedule 120S B.W. A403 Gr WP304 600 lbs 2" and Smaller 3000 lbs S.W. A182 Gr F304 2-1/2" - 4" Schedule 80S B.W. A403 Gr WP304 300 lbs 2" and Smaller 2000 lbs S.W. R2 Gr F304 2-1/2" - 4" Schedule 40S B.W. 3 Gr WP304 150 lbs 2" and Smaller 2000 lbs S.W. A182 Gr F304 2-1/2" - 4" Schedule 10S B.W. A403 Gr WP304 2-1/2" - 4" Schedule 40 B.W. A234 Gr WPB Valves 900 lbs 2 and Smaller 1500 lbs S.W. A182 Gr F304 or 316L 2-1/2" - 4" 900 lbs B.W, A351 Gr CF8M 600 lbs 2" and Smaller 600 lbs S.W. A182 Gr F316 2-1/2" - 4" 600 lbs B.W. A351 Gr CF8M I 300 lbs 2" and Smaller 300 lbs S.W. A182 Gr F316 gx 2-1/2" - 4" 300 lbs B.W. A351 Gr CF8M
\- 150 lbs 2" and Smaller 150 lbs S.W. A182 Gr F316 2-1/2" - 4" 150 lbs B.W. A351 Gr CF8M 3071-525A.34 - continued -
, _ _ 1
A4 TABLE 2 STAINLESS STEEL PIPING SYSTEMS (cont'd) h ANSI ASTM ITEM PRESSURE RATING SIZE RATING TYPE SPECIFICATION Flanges 900 lbs 2" and smaller 1500 lbs SW, RF A182 Gr F304 or 316L 2-1/2" - 4" 900 lbs WN, RRF A182 Gr F304 600 lbs 2" and Smaller 600 lbs SW, RF A182 Gr F316 2-1/4" - 4" 600 lbs WN, RF A182 Gr F316 300 lbs 2" and Smaller 300 lbs SW, RF A182 Gr F316 2-1/2" - 4" 300 lbs WN, RF 182 Gr F316 150 lbs 2" and Smaller 150 lbs SW, RF A182 Gr F316 2-1/2" - 4" 150 lbs WN, RF A182 Gr F316 Bolts All Bol t St ud s Bolt Studs A193 Gr B7 Hex A194 Gr 2H O Nuts All Gaskets All Flexitallic Style CG 3071-525A.35 i 4 III
. = - . _. ,_ _. . - . . - _ _ . _ _ _ _ _ _ _ - _ _ _
m -m-o-o m-si-w3 . Title DERGENCY EQUIPMDIT COOLING WATER (EEI;W) SYSTEM ENRICO FERMI POWER PT ANT; MTT 2 Project Design Specification O Deholt Edison 3071-512 Including Addendum A Number DECDGER 1972 DECEMBER 1974 Date
Specifiestion 3071-512 DETROIT EDISON Prripared By SPECIFICATION Enrico Fermi II ADDENDUM "A" 3*" "*9 " " Organization O' DESIGN SPECIFICATION nue : 11-15-74 FOR EMERGENCY EQUIPMENT COOLING WATER SYSTEM Enrico Fermi Atomic Power Plant Unit #2 i APPROVAL SHEET DATE ^ j
/[-[$ -[h
~
WRITTEN BY: ( . M 4 7U.O D. LEHNERT CHECKED BY:
. (v / 2 ' / { ! 7 8-/
h F.El GREGOR -P.E. APPROVED: d' PROJ. ENG'G. ,P j 4 .. f, p GROUP SUPERVISOR ,; 6 '
,, LA-g EcJ / /2-G 74-v M. S IGET ICt+'
I APPROVED:
-[./ /
ASSIST. PROJECT , ENGINEER, SYSTEMS f g //r /;.%f W.F. COLBERT-P.E. / / APPROVED: EN R 2 , u /s/,2/7/ E.G.(gIPER-P.E. O
Specification 3071-512 Prepared By Enrico Fermi II Project Management Organization O Issued: 11-15-74 Addendum "A" P44 0-000 sA,002/ DETROIT EDISON DESIGN SPECIFICATION FOR ENRICO FERMI ATOMIC POWER PLANT UNIT NO. 2 ADDENDUM "A" 0F DESIGN SPECIFICATION FOR EMERGENCY EQU1PMENT COOLING WATER SYSTEM DESIGN SPECIFICATION NO. 3071-512 o .
~
Specification 3071-512 Issurd: 11-15-74 O oeTao'T co'So" DESIGN SPECIFICATION ADDENDUM "A" EMERGENCY EQUIPMENT COOLING WATER SYSTEM
- 1. On Page 2, delete Article 3. (h),
- 2. On Page 2, Article 4.3, revise to read:
The Installer of the System shall be designated by The Detroit Edison Company ,
- 3. On Page 3, Article 4.8, revise 2nd sentence to read:
The Stress Report for the piping components will be provided by the Owner's engineering organization or designated agent.
- 4. On Page 4, Article 5, revise coolant demands to read:
(1) Reactor Recirculating Pump (2) Residual Heat Removal Pumps (2) Core Spray Pumps O
;
(4) - (5) - sPece cooiers: (i) aesideei seet aemevei (1) Core Spray and Reactor Core Isolation Cooling (1) Emergency Equipment Cooling Water Room (1) Hydrogen Control System or (1) High Pressure Cooling Injection (1) Core Spray (1) Residual Heat Removal (1) Emergency Equipment Cooling Water Room (1) Hydrogen Control System (1) Air Conditioning Equipment Unit for the Control Room (2) Switch Gear Room Space Coolers (1) Standby Control Air System (1) Standby Gas Treatment Room Space Cooler (7) Drywell Coolers. O
. Specification 3071-512 Issurd: 11-15-74 Addendum "A" Page 2 O 5- o# e 9 4. ^rtic' 5 r vis 4th P r ar P8 t= < d:
The EECW system, supplying the above equipment, maintains a condensate de-sign temperature of 95 F by heat rejection loop heat exchangers, which are cooled by Emergency Equipment Service Water (see Design Specification 3071-517).
- 6. On Page 5, Article 5, revise the ist and 2nd paragraphs to read:
During normal plant operation, it is essential to test the operation of the EECW system to confirm that the pumps, heat exchangers, make-up tanks and isolation valves will operate as specified wl.an required. Each divi-sion of the System will be individually tested by isolating the division from the RBCCW system by use of the motor operated valves. A complete flow diagram is shown on the Process and Instrumentation Dia-gram Number 6M721 -2027.
- 7. On Page 7, Article 8.2, revise 2nd paragraph to read:
Dimensional standards for fittings shall be per ANSI Bl6.9, unless other-wise specified on the Piping Isometric Drawings.
- 8. On Page 7, Article 9.1, revise ist sentence to read:
The penetration assemblies shall be designed, manufactured, tested and
- Inspected in accordance with Design Instruction DI-2 and Edison Design ! Speci ficat ion 3071-516.
- 9. Page 7, Article 9.1, revise seismic displacements to read:
The horizontal displacement in X or Z direction for GBr. = 1 .012 inches and for the DBE = 1 .0172 inches. The vertleal displacement for the OBE = .00156 inches and for the DBE = t .0024 inches.
- 10. On Page 8, revise Article 9.3 to read:
Piping of above category, which connects to EECW System piping inside the primary containment up to and including the first source valva is classi-fled as Class 2. Piping beyond the source valve up to and including the ter-minal or instrument is classified as Class 3. This piping shall be design and stress analyzed in accordance with Edison Design Specification 3071- 525 O
. Sp;cification 3071-512 Issurd: 11-15-74 Addendum "A" Page 3 O II. On Page 8, revise Article 9.4 to read:
The pumps, heat exchangers and make-up tanks are classified as Class 3 components. Piping connections to these components shall be designed to limit reactions to the following limits: (a ) . For the pump, the allowable nozzle loads shall be governed by the following expression: FI + Mi / 1 Fo Mo Where: F; = the largest of the three actual external orthogonal forces (Fx, F y, and Fz) that may be imposed by the pipe. 1 M; = the largest of the three actual external orthogonal moments. (Mx. M y , and M 2 ) permitted from the pipe , l when they are combinep + simul conditlon. M2+ taneous gz2 ) ) y for any (Mt = { Mx y l Fo = the allowable of F; when all moments are zero. No = the allowable value of M; when all forces are zero. 5 The values of Fo and No are given below: l OBE DBE Fo Ho Fo Mo Lbs. Ft-Lbs. Lbs Ft-Lbs Combined Resultant i168 2340 1500 3000 Suction Nozzle 875 , 1250 1125 , 1575 Discharse Nozzle 1000 l 2000 l 1275 1 2550 (b) For the heat exchanger, the allowabie nozzle loads are given in the
'ollowing tables:
NORMAL & UPSET CONDITION (OBE) Service Water Service Water EECW EECW Inlet Outlet Inlet Outlet Div. I Div. II Div. I Div. II Div. I Div. II Div. I Div. II Fx 680 260 1600 1500 700 700 680 500 hrz 3800 2200 2400 600 175 770 1100 1300 1600 700 1000 400 550 200 400 200 Mx 3950 3400 2500 5500 3200 1300 700 500 My 2100 600 1100 6900 1000 800 1750 1000 Hz 2200 200 3850 7300 3500 3200 1500 400
Sp;cification 3071-512 Issu:d: 11-15-74 Addendum "A" Page 4
) EMERGENCY C0!4DITION (DBE)
Service Water Service Water EECW EECW Inlet Outlet Inlet Outlet Div. I Div. II Div. I Div. II Div. I Div. II Div. I Div. II i
' 1100 1100 800 Fx 1250 400 j 2600 3000 1000 ,
Fy 7300 4500 300 2100 2500 1700 . 600 600 Fz 4200 1200 1300 2500 1300 600 l 400 300 l Mx 7800 6600 l 3600 l 10,300 1 6200 2500 1100 900 My 3600 1000 2000 14,000 1500 1200 i 2600 1600 Hz 3800 300 6300 2100 5000 1700 2400 700 l a Force in Ibs Moment in ft-lbs (c) For the make-up tanks, the allowable nozzle loads are given in Figures 3 thru 5. O Seismic displacements for the DBE are given in global coordinate form where x is east, z is south and y is vertical. The three displacement components 9 of the three mutually perpendicular directions of excitations are expressed . In inches and represent the square root of the stan of the squares of the I displacements of the vibratory modes. The pump, heat exchanger and make-up i tank nozzle connections shall be rigid anchor points for pip'ng. This equip- l ment is subject to sesimic displacements of the supporting floor slab. The anchor movements are as follows: Horizontal Displacement, OBE = .0302 in. DBE = .0442 in. Vertical Displacement, OBE = .00312 in. DBE = .00468 in. End thermal movements of the heat exchanger and make-up tank will be con-sidered as zero because of the negligible temper ature change.
- 12. Oa Page 11, Article 9.7, revised first sentence to read:
Class 2 and 3 piping 5 inch NPS and larger shall be analyzed by use of a 1 multi-degree of freedom dynamic modal response method.
- 13. On Page 12, Article 9.7, 3rd paragraph, revise 1st sentence to read:
p The multiplier for the DBE shall be taken as 1.875 (minimum). O
1 , Sp;ci ficat ion 3071-512 Issued: 11-15-74 Addandum "A" Page 5
- 14. On Page 12, Article 9.7, revise 4th paragraph to read:
Class 2 and Class 3 piping 4" NPS and smaller shall be analyzed per Edison Speci ficat ion 3071- 525. ;
- 15. On Page 13, Article 9.8, revise the seis.nic displacements to read:
Horizontal Displacement, OBE = .0218 in. DBE = .0397 in. Vertical Displacement, OBE = .00312 in. DBE = .0D468 In.
- 16. On Page 13, Article 9.9, revise the seismic displacements to read:
For the Core Spray System and Residual Heat Removal System Pumps; the Core Spray and Reactor Core Isolation Coolant, Residual Heat Removal and High Pressure Cooling Injection Space Coolers, (sub-bas ement ) : Horizontal Displacement, OBE = .0128 in. DBE = .023 in. Vertical Displacement OBE = .00156 in. DBE = .0024 in. For the Standby Control Compressor, (First Floor), O Horizontal Displacement, OBE = .012 in. DBE = .0172 in. Vertical Displacement, OBE = .00156 In. DBE = .0024 in. For the EECW and Switch Gear Room Space Coolers (Third Floor), Horizontal Displacement, OBE = .0416 In. DBE = .0596 in. Vertical Displacement, OBE = .0042 in. DBE = .00624 in.
- 17. On Page 14, Article 9.9, revise the seismic displacements to read:
For the Switch Gear Space Coolers and the Hydrogen Control System Space ! Coolers, (Fourth Floor), l Horizontal Displacement, OBE = .0 475 in. DBE = .0 676 in. Vertical Displacement, OBE = .00467 in. DBE = .00684 in. O I l i
.' l t' Spscificaticn 0071-512 Issurd: 11-15-74 l Addendum "A"
. Page 6 O 17. On Page 14, Article 9.9, revise the seismic displacements to read: (con t inued)
For the Control Room Air Conditioning Equipment and the Standby Gas Treatment Space Cooler, (Fif th Floor), Horizontal Displacement, OBE = .0552 in. DBE = .0762 in. Vertical Displacement, OBE = .00528 in. DBE = .00768 in. l
- 18. On Page 14, Article 10.0, delete reference to 350 F for design temperature of Class 2 piping.
i
- 19. On Page 16, Article 11.1, Cooling Water Supply Line Temperature shall be 850F. j
- 20. On Page 17, Article 13 (1), revise to read: l Seismic Analysis of the Enrico Fermi #2 Reactor Buildirg, Sargent and Lundy Report #5L-2682.
- 21. On Page 17, Article 13, add the following:
s (14) Stress Report, RGFA-NABC-72-190, Emergency Equipment Cooling s Water Make-Up Tank Seismic and Nozzle Loads, for National e Annealing Box Company. (15) Seismic Stress Analysis. Emergency Equipment Cooling Water Heat Echanger, Yuba Reference 72-N-001. 4 (16) Certified Seismic Analysis Report of Crane Deming Horizontal Split Case Pump, Figure 5063 for Emergency Equipment Cooling Water Pump. O V
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e 9 4 9 THE DETR0li EDISON COMPANY :PecaicAfiO= 3071-512 sec,...- .. ::::::= ,, PROJtcT WAmAGEutu? ORG ANIZ Afl04 SYSTEM DESIGN SPECIFICATION Issued: 9-6-72 FOR EMERGENCY EQUIPMENT (X)0 LING WATER SYSTEM Enrico Femi Atomic Power Plant Unit #2 APPROVAL SHEET l l DATE l
/Ib,162//7i/ J t ~b WRITTEN BY: ('N Di LEHNERT ,
CHECKED BY: 'tf W
) .E. GREGOR hO#
l' ( h-7 APPROVED: PROJ. ENG'G Ih - GROUP SUPERVISOR /'/M/hf.Y P.E. M ~ N' b S.H1 NOIG!CZ V APPROVED: PROJECT SYSTEM ENGINEER
, g - ? '"/[ /C -80 ,"f W.'F. COLBERT P.E.
REVIEWED: QUALITY ASSURANCE , h3nr h , ,, c ]y DIRECTOR bh I ' if a JLll \ k QM - N
- l- b /"
A. ALEXIOU APPROVED: PROJECT ENGINEER h)h. 1 b ' 'y l 2 ~ h R.A. VAhCW.E . l .
; , ,- _
;; _ . _ . _ _ _ _ _ _ . .
- Specification No. 3071-512 ,
Iccued: 9-6-72 ) l O i P44-00C0CO&oo$ THE DETROIT EDISON COMPANY r SPECIFICATION i SYSTEM DESIGN SPECIFICATION FOR
- EMERGENCY EQUIPMENT COOLING WATER SYSTEM l o- ENRICO FERMI ATOMIC POWER PIANT UNIT #2 I
i i O
-\
W .
THE DETROIT EDISON COMPANY settineAfion 3071-512 spaCIPICATION " fCo E isi si P90 JECT MANAGEMENT SYSTEM DESIGN SPECIFICATION '",*7' 7 *,'y'" 9-6 -72 FOR EMERGENCY EQUIPMENT COOLING WATER SYSTEM ENRICO FERMI ATOMIC POWER PIANT UNIT #2 INDEX Article Code Article Page
- 1. SC0PE.......................... NA-3250................ 1 2 CERTIFIO4 TION.................. NA-3250................ 1
- 3. C1 ASS IF ICATION . . . . . . . . . . . . . . . . . NA-2000................ 1 4 DOCUMENTATION . . . . . . . . . . . . . . . . . . NA-3256................ 2
- 5. GENERAL SYSTEM DESCRIPTION..... NA-3252 (a)........... 4
- 6. APPLICABLE DOCUMENTS . . . . . . . . .. . NA-3254................ 5
- 7. DESIGN......................... NA-3252 (b)........... 5
- 8. SYSTEM DESIGN BASIS...................................... 7
- 9. COMPONENT DESIGN BASIS................................... 7 Os 1.0 COMPONENT CHARACTERISTICS................................ 14
- 11. CIASSIFICATION OF CONDITIONS . . . . . NA-2140. . . . . . . . . . . . . . . . 16 12 HYDROSTATIC AND LEAK TESTS . . . . . . . NC-6000. . . . . . . . . . . . . . . . 16
- 13. REFERENCES............................................... 17 ATTACHMENTS:
Process Diagram 6M721-2027 Systems Isometric (See References) Boundaries of Code Jur'sdiction Figure #1 4 Local Coordinate System and Convention Figurc #2 Appendix A - ANSI Primary Pressure Rating, Materials and Dimensions i for Nuclear Piping. l i l h O* I l t
^
Sptcification: 3071-512 Issued: 9-6-72 t o THE DETROIT EDISON COMPANY d DESIGN SPECIFICATION SYSTEM DESIGN SPECIFICATION FOR EMERGENCY EQUIPMENT COOLING WATER SYSTEM
- 1. SCOPE This document constitutes the Design Specification required by Article NA-3250 of the ASME Boiler and Pressure Vessel Code Section III, 1971 Issue " Nuclear Power Plant Components" for the Emergency Equipment Cooling Water Piping System to be installed as part of the Nuclear Steam Supply System of the Enrico Fermi Atomic Power Plant, Unit #2.
- 2. CERTIFICATION The undersigned registered Professional Engineer competent in the field of design of piping and related nuclear energy system requirements, certifies that this design specification together with the referenced documents complies with the requirements of Article NA-3250 of the ASME-Code Section III and is correct and complete with respect to functions and operating conditions as required to provide a complete basis for design, construction and certified inspection in accordance
() ' with the Code. 7- 3i- n DATE
//tb n SIGNAIURE Michigan - 18860 BRANCH REGISTRATION, STATE and NUMBER or SIAMP
- 3. CIASSIFICATION (
REFERENCE:
FIGURE #1) The Emergency Equipment Cooling Water (E.E.C.W.) System is divided into two classes. That portion of the E.E.C.W. System supply and return piping which is between the outboard containment isolation valve and the equipment inside the primary containment that requires cooling water shall be classified as a Class 2 system and shall be designed and constructed in accordance with the rules of Subsection NC of the ASME Code Section III,1971 Issue. .O-
Speelfication: 3071-512 Icsued: 9-6-72 Page Two b_qk. 3. CIASSIFICATION (
REFERENCE:
FIGURE #1) (Continued) The remaining portion of the system shall be classified as a Class 3 system and shall be designed and constructed in accordance with the rules of Sub-section ND of the ASME Code Section III, 1971 Issue. The purchase order dates for the components are as follows: (a) Line Valves : July 19, 1971, The Wm. Powell Company (b) Piping and Fittings : March 29, 1972, Dravo Company (c) Penetration Assembly : Spet. 15, 1970, Tube Turns Company (d) Hangers and Supports : Aug. 24, 1971, Power Piping Company (e) Pumps : June 14 , 1972, Crane Deming Pumps (f) Heat Exchangers : Oct. 30, 1972, Yuba Heat Transfer Corp. (g) Make-up Tanks : July 31, 1972, National Annealing Box Co. (h) Inservice Inspection : , W10, Southwest Research Inst.
- 4. DOCUMENTATION
- 1. The Owner and User of the System will be:
THE DETROIT EDISON COMPANY 2000 Second Avenue Detroit, Michigan 48226
- 2. The System will be installed in the:
ENRICO FERMI ATOMIC POWER PIANT, UNIT #2 6400 Dixie Highway Stony Creek, Monroe County, Michigan 48166 (P. O. Newport, Michigan)
- 3. The Installer of the System will be:
THE RALPH M. PARSONS COMPANY of MICHICAP Post Office Box 300 Monroe, Michigan 48161
~ , . l Specificatien; 3071-512 l Iscu:d: 9-6-72 l Page Three
{ (f 4. DOCUMENTATION (Continued) 1
- 4. The Enforcement Authority having jurisdiction at the location of the System is:
THE STATE OF MICHIGAN DEPARIMENT of IABOR ; BUREAU of SAFETY and REGUIATION DEPARTMENT of IABOR BUI1 DING 300 E. Michigan Avenue Lansing, Michigan 48913
- 5. Consnunications between the installer or manufacturer and the enforcement authority will be through the Owner unless specifically !
required by the Code to be otherwise. In the latter case, prior l approval must be obtained and advance copies of the correspondence j directed to the Owner's documentation office and the certifying l Professional Engineer (s) of this document. 1
- 6. The Owner will comply with Article NA-3256 in filing a copy of this Design Specification with the enforcement authority before the system is placed in service.
- 7. The manufacturer and/or installer shall identify the authorized In-spection Agency to the Owner on or before the contreet date and
{}. shall provide the Inspection Agency with all required documentation, including the Quality Assurance Manual and this Design Specification.
- 8. The Stress Report shall be submitted to the Owner, before filing with the required authorities for review by those responsible for the Design Specification as required per NA-3260. The Stress Report for the piping components will be provided by the Owner's engineering organization or designated agent and submitted to the manufacturer. The Owner will certify that the required review has been conducted and will make available a suitable insert page for inclusion into the Stress Report before it is filed with the enforce ment authority by the manufacturer.
- 9. Each manufacturer and/or installer shall furnish the Owner with a copy of the appropriate Certificate of Authorization not later than the date of contract, (Article NA-3330).
- 10. Upon completion of the contract each manufacturer and/or installer shall complete the appropriate certificate of Compliance and submit a copy of the Certificate to the Owner for inclusion in the Owner's Data Report Form N-3, (Article NA-3270).
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Specification: 3071-512 Issu:d: 9-6-72 Page Four ()[ 5. GENERAL SYSTEM DESCRIPTION (This is a functional description and not a design requirement). The E.E.C.W. System consists of two redundant supply and return cooling loops, Division I and Division II. Each loop will consist of one e condensate circulating water pump of sufficient capacity to circulate water thru the system and return the cooling water to a full capacity t heat exchanger. The E.E.C.W. System will be automatically operable upon a loss of A-C off-site power or may be manually initiated on system failure of the Reactor Building Closed Cooling Water System. The E.E.C.W. System will at all times meet the requirements to provide sufficient water at the proper pressure and maximum temperature. In the case of a failure of a single component of one of the Divisions, the other Division will be capable of supplying coolant to the following equipment. (1) - Reactor Recirculating Pump (2) - Residual Heat Removal Pumps (2) - Core Spray Pumps (2) - (3) - Space Coolers: (1) - Residual Heat Removal O (1) - Core Spray and Reactor Core Isolation Cooling (' or (I) - High Pressure Cooling Injection (1) - Core Spray (1) - Residual Heat Removal (1) - Air Conditioning Equipment Unit for the Control Room (2) - Switch Gear Room Space Coolers (1) - Standby Control Air Systen (I) - Post Loss of Coolant Accident, Hydrogen Control System (1) - Standby Gas Treatment Roort Space Cooler I (2) - Drywell Coolers The E.E.C.W. System, supplying the above equioment, maintains a condensate temperature of 95 F by heat rejection loop hea exchangers, which are cooled by Emergency Equipment Service Water (see Design Specification 3071-517) The E.E.C.W. System make-up tank is used as the source of system water make-up. Condensate is supplied from the condensate storage tanks. The make-up tank will be nitrogen capped to prevent leakage of oxygen into the system and to maintain a positive suction head on the closed loop
- l. system.
l h V s
Specificction: 3071-512 Issurd: 9-6-72 Page Five [ 5. GENERAL SYSTEM DESCRIPTION (Continued) During normal plant operation the E.E.C.W. System will be tested once a month. Each division of the System will be Individually tested by isolating the division from the R.B.C.C.W. System by use of the motor operated valves. The test will be perfortred to assure that the division pumps, heat exchangers, make-up tanks and Isolation valves w*ll operate as specified when required. A complete flow diagram is attached in the Appendix, see Process and In-strumentation Diagram Number 6M721-2027
- 6. APPLICABLE DOCUMENTS The design, material, fabrication, Installation, inspection and testing of the system and the system components shall be in accordance with the
- following
1 This Specification with the attachments.
- 2. The Process and Instrumentation Diagram 6M721-2027.
- 3. The Piping Stress Analysis Isometric (See References).
Oi
- 7. DESIGN 7.1 System Design Life The system shall be designed for an effective design life of 40 years, accounting for corrosion, erosion and fatigue. The corrosion allow-ance to be used Is:
0.120" for steam 0.080" for water 0.0024" for stainless steel 7.2 Normal and Upset Environmental Conditions The Class 2 portion of the system, situated in the primary containment will be exposed to the following condition during the life of the plant: External Pressure = 0.0 to 2.0 PSIG External Temperature = + 105 to 1500F (Range) O. Reiative tiemiditv = 40 to sex Atmosphere = 97% N , 3% 0 2 2 External Radiation = Gamma 50 Rads / Hour 2 Neutron 140,000 N/CM - Sec.
t . Specifiestion: 3071-512 Issu;d: 9-6-72 Page Six h 7 DESIGN (Continued) 7.2 (Continued) All Class 2 components are insulated with an all metal reflective type insulation having a heat loss coefficient of approximately 0.15 BTU /HR/Sq. Ft/0 F/ Inch thickness. For the purpose of thermal analysis, this Insulation shall be assumed to be pe-fect (no heat loss). 7.3 Faul ted Environmental Conditions in Drywell (or.e time only) External Pressure =
-2 to 56 PSIG for i minute at 340 F
-2 to 35 PSIG for 3 r.ours at 3400F ,
-2 to 35 PSIG for 6 hours at 3200F 0 to 25 PSIG for i day at 250 F j 0 to 20 PSIG for 100 days at 2000F Relative Humidity = 107/o Radiation = 2.6 x 107 RADS (gamma) 7.4 System Fluid The system will contain the following fluid:
( Medlum: Demineralized Water pH at 25 C: 6.5 to 7.5 Radioactivity: 0.7 Micro Curle/ml @ zero decay time Specific conductivity, mho/cm @ 250c <0.1 Chloride as Cl- <2 ppb Total metallic impurity <10 ppb Silicia as S102 <5 ppb ! l 7.5 Environmental Conditions of Secondary Containment The Class 3 portion of the system, situated in the secondary contain-ment will be subjected to the following conditions: External Pressure = Atmospheric External Temperature = Winter Minimum of 400F Accidental Maximum of 1480F (for 8 hours) Average Operating of 70 F Relative Humidity = 50 to 9&4 Radia t Ion = 7 9 x 10 5RADS (gama - includes faulted dose)
Specification: 3071-512 Issued: 9-6-72 P:;ge Ssven f 8. SYSTEM DESIGN BASIS t i V 8.1 Cold Springing Cold springing is not permitted in the design of the piping. In cases where mismatches due to fabrication tolerances exist during the instal!ation, the procedures for measuring and closing the gap giver in the syste:r. erection specification will be followed. 8.2 Dimensional Limits Piping components shall be fabricated in accordance with the Fabri-cation Specification 3071-30 and the fabrication tolerances shall be per P.F.I. Standard ES-3. Dimensional standards for fittings shall be per ANSI B16.9. 8.3 Temperature Limits The metal and fluid temperature for cleaning, flushing and decon-taminating shall be above + 600F, but not exceeding 2120F for the entire system (Class 2 and Class 3).
- 9. COMPONENT DESIGN BASIS 9.1 E.E.C.W. Penet ration Assembl ies (X-23, x-24 and x-34 A,B)
! The penetration assemblies shall be designed, manufactured, tested and inspected in accordance with Design Instruction DI-2 The stress analysis shall employ a finite element analysis method for the flued head as defined in Appendix A of DI-2 The flued head constitutes a rigid anchor for the attached piping and allows only for normal thermal expansion of the flued head.
The anchor movements are as follows: Seismic Displacement: The horizontal displacement in X cr Z direction for the OBE = i .012 inches and for the DBE - I .022 inches. The vertical displacement for the OBE = ? .0084 inches and for the DBE = t .016 inches. Thermal Movements: In the normal condition the movements of the penetration assembly will be due to vertical and horizontal expansion from 70 0F to 150 F and pressure expansion from 0 to 2 psig of the primary containment. Y Horizontal Displacement =
.327 in j (O
Vertical Displacement =
.045 in
Specification: 3071-512 Issu;d: 9-6-72 Page Eight 9. ( }{ COMPONENT DESIGN BASIS (Continued) 9.1 (Continued) In the accident condition the movement of the penetration assembly will be due to vertical and horizontal expansion from 700F to 3400F and pressure expansion from 0 to 56 psig of the primary containment. The movements shall be as follows: Horizontal Displacement =
.539 in Vertical Displacement =
.170 in Piping reactions acting on either side of the flued head shall be calculated for the local coordinate data points located at the con-nection weld and reported as part of the Piping Stress Report.
The flued head anchor is subject to seismic displacements of the containment shield. 9.2 Class 2 System Line Valves and Isolation Valves All valves shall be designed, manufactured, tested and inspected in accordance with Edison's Valve Specification 3071-501 and 3071-12. 9.3 Piping of 3/4" NPS and Smaller and Instrument Piping Piping of above category, which connects to E.E.C.W. System piping Inside the primary containment up to and including the first source valve is classified as Class 2 and shall be designed in accordance with A.S.M.E. Section III,1971 Edition. Piping beyond the source valve up to and including the ter-inal or instrument is classified as Class 3 and shall be designed in accordance with ANSI B31.1 " Power Piping", Paragraph 122.3, includ-Ing the application of ANSI B31 Code Case 78. Only seamless stainless steel or carbon steel tubine full stress relieved may be used for source connections. Cold forming, tending flaring etc. is not permitted. 9.4 E.E.C.W. System Pumps, Heat Exchanger and Make-up Tanks The pumps, heat exchangers and make up tanks are classified as Class 3 components. Piping connections to these components shall be designed to limit reactions to the following limits: Based on the moment of inertia and the moment arm of reactions, the pump casing and the shell of the heat exchanger and the make-up tank are assuned to accept and transfer their respective loads to their anchor bolts, which present the weakest link. React ions are therefore limited based on the strength of the bolts.
Specification: 3071-512 Issu:d: 9-6-72 Page Nine i OJ' V '
- 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont'd)
The stress report shall verify the following formulae: (a). For the Pump, (1). Maximum Bending Moment l 6(Fyj + FY2) - 10.5(FZ1 + FZ2} + "X1 - "X2l ( (Later) and l10.5(F X1 -F X2) - 1.5 Fyj + 25.5Fy2 + MZ1+"Z2l$(Later) (2). Maximum Shear Moment l19(F X2 -F ~M
) - 14FZ1 + 13FZ2 Y1 ~MY d ( %d Where, Fj and M yare the forces and moments imposed on the suction nozzle of the pump and, F and M are the 2 2 forces and moments imposed on the discharge nozzle of the pump.
(- (b). For the Heat Exchanger, (1). Maximum Bending Moment l46(FX2 + FX3) + 12(7(Fyj -F Y2) + 5(Fyg - Fy3))+ MZ1 + "Z2
+M73 + M74l ( (Later) 1 and l13.5(-F;+FY2 y + Fy3 -F yg) + 46(FZ2 + FZ3 ~ X1 - X2
~ "X3 - X4 (Later)
(2). Maximum Shear Moment l-219(FZ1 + Z2)- 195(FZ3 + FZ4) + "Y1 ~ "Y2
-My3 + Myql((Later) i l
l
Specification: 3071-512 Issusd: 9-6-72 Page Ten
- 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont'd)
(2). Maximum Shear Moment (Cont'd) Where, Fj and Mj are the forces and moments imposed on the tube side inlet nozzle of the heat exchanger, F 2 and M2 are the forces and moments imposed on the tube side outlet nozzle of the heat exchanger, F and M 3 3 are.the forces and moments imposed on the shell side Inlet nozzle of the heat exchanger, and F gand Mg are the forces and moments imposed on the shell side out-let nozzle of the heat exchanger. (c). For the Make-up Tanks (1). Maximum Bending Moment l14.5F X1 - 25.25 Fyj -MZ1 + 69.5 FX2 + 43.25 FY2
+M Z2l 1.42 x 106 In.-lbs.
and ;
;. l21.5(FY2 -Fyj) + 14.5FZ1 ~ "X1 + 69.5 FZ2 ~
X2 (1.27x106 in.-lbs. (2). Maximum Shear Moment l- Myj + MY2 - 18 FZ2l 8.32 x 105 in.-Ibs. Where, Fj and H jare the forces and moments imposed on the tank supply nozzle and, F2 and M2 are the forces and moments impos d on the condensate supply I nozzle to the tank. In all of the above formulaa the subscripts X,Y and Z are three mutually perpendicular directions referenced to one common axis. The forces and moments F and M are to be taken as the sum of the l forces and moments generated by the computerized stress analysis l due to dead weight and seismic DBE of the piping system,, with due ' consideration of their directions. The direction of the DBE shall be selected to result in the worst combination with dead weight loads. Pr-m
SpIcification: 3071-512 Issurd: 9-6-72 Page Eleven h 9. COMPONENT DESIGN BASIS (Continued) 9.4 (Cont 'd ) Seismic displacements for the DBE are given in the gobal coordinate form where X is east, Z is south and Y is vertical . The three dis-placements components of the three mutually perpendicular directions of excitations are expressed in inches and represent the square root of the sum of the squares of the displacements of the vibratory modes. The displacements for the OBE are defined by multiplying the DBE displacements by 1/1.875. The pump, heat exchanger and make-up tank nozzle connections shall be rigid anchor points for piping. This equipment is subject to seismic displacements of the supporting floor slab. The anchor movements are as follows: Horizontal Displacement, OBE = . 042 in. , OBE = . 079 in. ; Vertical Displacement, OBE = .0096 in. DBE = . 018 !n. End thermal movements of the heat exchanger and make-up tank will l be considered as zero because of the low temperature change. , Q 9.5 Supporting Structures l 1 All support structures for the E.E.C.W. System Class 2 and Class 3 1 components shall be designed for a Class I seismic criteria. Hangers and supports shall be located and spaced in a manner, to limit seismic accelerations for the line valves to 5.0g under DBE condi-tions. Seismic displacement of piping shall be limited to the clearance dimensions of piping where it passes through sleeves in walls and slabs to avoid impact. Anchor movements shall be de-termined from the applicable floor response spectra of the build-ing. 9.6 Insulation I All Class 3 components are insulated with insulation of approximately 1" thickness and a specific density of 15#/cu. f t. 9.7 Seismic Analysis of Pipino l Class 2 and Class 3 piping 8 Inch NPS and larger shall be analyzed j by use of a multi-degree of freedom dynamic modal response method. I i The piping under seismic analysis shall be excited in each of three mutually perpendicular directions, two horizontal and one vertical . T* m. l u
Specification: 3071-512 Issu;d: 9-6-72 Page Twelve V[ I~' 9. COMPONENT DESIGN BASIS (Continued) 9.7 Seismic Analysis of Piping (Cont 'd) The differential seismic movements at interface points between the piping and structures or components as specified in Article 9.0 shall be considered. The effect of seismic reactions from branch piping at piping inter-sections shall be considered if the ratio of the moments of inertia of the piping cross sections, I run/I branch, j{ 7.0. The worst horizontal excitation resulis shall be directly combined with the vertical excitation resul ts for the Operating Basis Earthquake (OBE) and the Design Basis Earthquake (DB E) . The multiplier for the DDE shall be taken as 1.875. The percent of critical damping used in the dynamic analysis shall be 0.5. Class 2 and Class 3 piping 6" NPS and smaller may be subjected to a simplified dynamic analysis employing the independent simply supported beam method. A set of seismic design curves showing period versus span, deflection versus span and seismic load versus span for the first mode seismic deflection of a simply supported beam, employing the respective floor response spectra as input acceleration, shall be used. The method of oad combinations and the allowable stresses shall be as requi red per ASME Code, Section 1 (~} \-- III, 1971 Issue. I ( ! 9.8 Piping Class 2, E.E.C.W. System Equipment Interfaces The movements of the connection weld between the E.E.C.W. System , piping and the Reactor Recirculation Pump nozzles will be due to i the resulting thermal movements (from the hot to the cold position) of the Reactor Recirculation Pump in the Reactor Recirculation ' Piping System. The pump movement i s as fol l ows : 1.43 inches Down 0.265 inches East 1.06 inches South The connection weld between the E.E.C.W. System piping and the Drywell Cooler nozzles shall constitute a rigid anchor. This equipment is subject to seismic displacement of the supporting drywell steel. The anchor movements are as follows:
Specification: 3071-512 Issued: 9-6-72 Paga Thirtsen [{ ~
- 9. COMPONENT DESIGN BASIS (Continued) 9.8 Piping Class 2. E.E.C.W. System Equipnent (Cont'd)
L Horizontal Displacement OBE = . Oil in. DBE = .0206 In. Vertical Displacement OBE = .0034 in. DBE = . 016 in. 9.9 Piping Class 3. E.E.C.W. System Equipment Interfaces The connection weld between the E.E.C.W. System piping out side the primary containment and the equipment (as listed in Section 5) nozzles shall constitute a rigid anchor. This equipment is sub-ject to seismic displacement of the supporting floor slab. The anchor movements are as follows: For the Core Spray System and Residual Heat f.emovat System Pump Motors; the Core Spray and Reactor Core Isolation Coolant and High Pressure Cooling Injection Space Coolers, (sub-ba s ement ) , Horizontal Displacement OBE = .0128 in. DBE = . 024 in. Vertical Displacement OBE = .0084 in. () t DBE = . 016 in. For the Residual Heat Removal Space Cooler and the Standby Control
- Air Compressor, (First floor),
Horizontal Displacement OBE = . 016 in. DBE = . 031'In. Vertical Displacement OBE = .0096 in. DBE = . 018 In. For the Switch Gear Room Space Coolers (Second floor), Horizontal Displacement OBE = . 042 in. DBE = . 079 in. Vertical Displacement ODE = .0096 in. DBE = . 018 in. Or uA. ' t.
. Specification: 3071-512 Issurd: 9-6-72 Paga Fourteen
- 9. COMPONENT DESIGN BASIS (Continued) 9.9 Piping Class 3. E.E.C.W. System Equipment Interfaces (Cont 'd )
For the Switch Gear Room Space Coolers and the Hydrogen Control System (Third floor), Horizontal Displacement OBE = . 056 in. DBE = .106 in. Vertical Displacement OBE = .0096 in. DBE = . 018 in. For the Control Room Air Conditioning Equipment and the Standby Gas Treatment Space Cooler (Fi f th floor), Horizontal Displacement OBE = . 072 in. DBE = .136 in. Vertical Displacement OBE = .0096 in. DBE = . 018 in.
- 10. COMPONENT CHARACTERISTICS 10.1 Class 2 and Class 3 E.E.C.W. System Piping (Weights are given on the referenced piping Isometric drawings),
s Des ign Pressure 150 PSIG Design Temperature 2000F (3500F for Class 2 piping) Material See Appendix "A", Table 7 Dimensions i", li", 2", 2}", 3", 4", 6", 8' & 10" Sch . LO 10.2 Valves As per Valve Specification, Valve List and Valve Design Specif1-cation 3071-501 & 3071-12. 10.3 Pumps Specific pump data is given in Detroit Edison Specification 3071-85 Specific Design Data is as follows: Cl l e-
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4
+
f
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\ IMAGE EVALUATION %
TEST TARGET (MT-3)
;
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l Specification: 3071-512 Issusd: 9-6-72 Paga Fifteen I 10 COMPONENT CHARACTERISTICS (Continued) [' 10.3 Pumps (Cont'd) Design Pressure 120 PSIG Design Temperature 120 F Pump Casing Material A216 WCB Cast Steel Discharge Capacity 1450 GPM Discharge Head 158 Ft. @ 51 Ft. NPSH @ 95 F 10.4 Heat Exchangers Specific heat exchanger data is given in Detroit Edison Specifi-
, cation 3071-88. - Specific Design Data is as follows:
Shell Side Tube Side Design Pressure 120 PSIG 175 PSIG Dest gn Temperature 1200F 1200F Mate rial A-515 Grade 70 Admiralty SB-lli Fluid Condensate RHR Service Water I Quantity 1600 GPM 1450 GPM Temp-In ll00F (890) Temp-Out 950F 102.60F 10.5 Make-up Tanks Specific make-up tank data is given in Detroit Edison Bill of Material S20-17M. Specific Design Data is as follows: Design Pressure 100 PSIG Design Temperature 120 F Material for Shall and Head A-515 Grade 70 Capaci ty 600 Gallons 10.6 Overpressure Protection The E.E.C.W. heat exchangers and make-up tanks are equipped with relief valves.
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Specificat ion: 3071-512 Issurd: 9-6-72 Page Sixteen ( )( 10. COMPONENT CHARACTERISTICS (Cont inued) 10.6 Overpressure Protection (Cont 'd) The set points for the heat exchanger are as follows: Tube Side: 125 PSIG Shell Side: 100 PSIG The set point for the make-up tank is 75 PSIG. II. CLASSIFICATION OF CONDITIONS 11.1 Operating Condition During normal plant operating conditions the E.E.C.W. System will be operating as part of the Reactor Building Closed Cooling Water System. The E.E.C.W. pumps, heat exchangers and make-up tanks j will be in-operative and isolated from the cooling system. This I condition is defined below: Class 2 and Class 3 System Components: l Cooling Water Supply Lines, Pressure 95 PSIA 1 O Temperature 95 F i Flow 8000 GPM j Cooling Water Return Lines, Pressure 95 PSIA l Temperature 1100F I Flow 8000 GPM 11.2 Earthquake Loadings ! A total nunber of one Des ign Basis - Earthquake (DBE) and two Operating Basis Earthquakes (DBE) shall be considered to occur during the 40-year design life. Ve'tical and horizontal seismic excitations will occur simul taneous! ; . The maximum stress re-sulting from horizontal x or z directional excitations shall be added to the stress resultir.g from the vertical excitatien. All pressure retaining componrts are fully flooded at all times.
- 12. HYDROSTATIC AND LEAK TESTS Hydrostatic testing shall meet the requirements of NC-6200, except that the valve bodies shall be tested by the manufacturer in accordance
{ with ANSI Bl6.5 or MSS SP-66 for Class 2 and Class 3 valves.
Specifiestion: 3071-512 Issurd: 9-6-72 Page Seventeen 12 HYDROSTATIC AND LEAK TESTS (Continued) Prior to the hydrostatic test, all valve stem leak-off connections shall be open ended. All line valves, sMil be in the open position, but not bachseated, to provide full differential pressure across the stem pack-Ings. During hydrostatic test, examination for leakage shall be made. There shall be absolutely no visible leakage ,on any of the pressure retaining components, including valve stem packings and check valve exercising devices. The test medium shall be demineralized water. The hydrostatic test pressure for the system shall be 188 PSIG @ 70 0F.
- 13. REFERENCES
( I). Seismic Analysis of the Enrico Fermi #2 Reactor Building, Sargent
& Lundy Report #SI-2682 dated September 2, 1971.
( 2). General Electric BWR Plant requirements Specification 22A1300BC. ( 3). Enrico Fermi Atomic Power Plant Unit #2 PSAR. ( 4). BWR Equ' ment Environmental requirements General Electric g Speci'.c tion 22A3019 ( 5). The ASME Boller and Pressure Vessel Code, Section III,1971 Issue. ( f.) . Edison Pipe Fabrication Specification 3071-30. ( 7). Edison Pipe Erection Specification 3071-31 ( 8). Edison Welding Specifications 311, 512 and 513. ( 9). Edison Valve Specification 3071-12 & 501 (10) . The pr";sure integrity of piping and equipment pressure parts, per FSAR, Appendix A. (II). Edison Specification 3071-85, ti.c E.E.C .W. System Pumps . i (12). Edison Specification 3071-88, the E.E.C.sf. Heat F;. changers. (13) . Emergency Equipment Cooling Water System Isometric Drawings: 6M721-3672 6M721-3368 3351 3337 rs 3347 3336 Q' 3679 3666
Specification: 3071-512 Issutd: 9-6-72 Page Eighteen (( 13. REFERENCES (Cont inued) (13). Emergency Equipment Cooling Vater System Isometric Drawings: (Con 6 *d) 6H721 -3657 6H721-3348 3340 3346 3656 3345 3362 3667 3189 3368 3672 3084 1-O g ([)F-
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O 4 APPENDIX A ANSI Primary pressure rating, materials and dimensions for Nuclear Piping. O . J l l t 1 O l l l l
. t 1ABLE 1 900 LBS ANSI PRESSURE RATING CARBON STEEL PIPING SYSTEMS O
ASIM Trem Size Ratine Tvoc~ Socciffeation Pipe 3" and Smaller Sch 160 Seamless - A106 Gr.
- 4" thru 10" SCH 120 Seamless A106 Gr. B
- 12" thru 14" Sch 100 Seamless or A106 Gr. B
- 16" and Larger Sch 80 Seam Welded A155 Gr. KCF*
Valves 2" and Smaller 1500 lbs. SW' A105
- all 2 1/2" thru 24" 900 lbs. BW A216 Gr. WCB*
Types Fittings 2" and. Smaller 6000 lbs. SW A234 Gr. WPB* 2 1/2" and 10" Match pipe wall BW A234 Gr. WPB* 12"' thru 14" Sch 100 BW A234 Gr. WPB*
,16" and Larger Sch 80 BW A234 C;r. WPB*
() - F1&nge 2" and Smaller 2 1/2" and Larger 1500 Lbs. 900 Lbs. SW, RF WN, RF A105* A105* ( Bolts Bolt Studs A193 Gr. B7* Nuts Hex A194 Gr. 2H3 Class Gaskets Flexitallic Style CG
- For ASME Code Class I the materials must be impact tested per NB-2300 at a temperature of +10 F O
e
TABLE 2 900 LBS' ANSI PRESSURE RATING STAINIESS STEEL PIPING SYSTEMS ASTM Item Size Ratine Tvoe Soecification PIPE 2" and Smaller Sch 160 S Seamless A312 TP304 2 1/2" and 3" Sch 160 S Seamless A376 TP304 4" and thru 6 " Sch 120 S or Seamweld A358 TP304 8" thru 24" Sch 100 S Valves 2" and Smaller 1500 lbs. SW A182 Gr. F304 , all 2 1/2" and Larger 900 Lbs. BW A351 Gr. CF8M Types Fittings 2" and. Smaller 3000 Lbs. SW A182 Gr. F304 2 1/2" and 3" Sch 160 S BW A403 Gr. WP304 4" thru 6" Sch 120 S BW A403 Gr. WP304 ' 8" thru 24" Sch 100 S BW A403 Gr. WP304
~
(:)- l g Flanges 2" and Smaller 1500 lbs. SW, R.F. A182 Gr. F304 )
~
2 1/2" and Larger 903 Lbs. WN, R.F. A182 Gr. F304 1 Bolts Bolt Studs A193 GR. B7 l
, l l
Nuts Hex A194 Gr. 2H. l Gaskets Flexitallic Style CG O d
I TABLE 3 ) l l 600 LBS ANSI PPISSURE RATING CARBON STEEL SYSTDIS )
. ASTM Item Size Ratine Type Soecification
~~
,.. .. \
Pipe 3" and Smaller Sch 160- Seamless A106 Gr. B 4" and Larger l Sch 80 Seamless A106 Gr. B Valves 2" and Smaller 600 lbs. SW A105 all 2 1/2" and larger 600 lbs. BW A216 Gr. WCB Fittings 2" and Smaller 3000 Lbs SW A234 Gr. B l
. 2 1/2"*thru 3"
- Sch 160 BW A234 Gr. B 4" and larger Sch 80 BW A234 Gr. B Flanges 2" and Smaller 600 Lbs SW, R.F. A105 -
21/2" and larger 600 Lbs BW, R.F. A105 Bolting , Bolt Studs A193 Gr. B7 Nuts Hex A194 Gr. 2H,' Gaskets Flexitallic Style CG 4 9
.O-
- 6 l
l -
- l
TABLE 4 rQ . 600 LBS ANSI PRESSURE RATING STAINLESS STEEL PIPING SYSTEMS ASIM Iten Size Ratine Tvoe Sneciffeation Pipe 2" and Smaller Sch 80 S Seamless A312 TP304 2 1/2" thru 12" Sch 80 S Seamless or A376 TP304 or 14" and larger Sch 60 S Seamweld A358 TP304 Valves 2" and Smaller 600 lbs. SW A182 Gr. F316 all 21/2" and larger 600 Lbs. BW A351 Gr. .CF8;; Sizes
. Fittings 2" and Smaller 3000 Lbs. SW A182 Gr. F304 2 1/2"'thru 12" Sch 80 S BW A403 Gr. WP304 14" and larger Sch 60 S BW A403 Gr. WP304 0 - .
( Flanges 2" and Smaller 600 lbs. SW, R.F. A182 Gr. F316 21/2" au1 Iarger 600 Lbs. WN, R.F. A182 Gr. F316 Bolting Bolt Studs A193 Gr. B7 Nuts Rex A194, Gr. 2H, Gaskets Flexitallic Style CG e O.
IABLE 5 300 LBS ANSI PRESSUPI RATING CARBON STEEL PIPING SYSTDIS Item ASIM Size Ratine Tvoo Snecification Pipe 2" and Smaller Sch 80 Seamless A106 Gr. B 2 1/2" and Large r Sch 40 Seamless A10s Gr. B Valves 2" and Smaller 600 Lbs. SW A105 all 2 1/2" and Larger 300 lbs. BW A216 Gr. WCB
, Types Fittings 2" and smaller 3000 lbs SW A234 Gr. B 2 1/2" and Larger Sch 40 BW A234 Gr. B
) Flanges 2" and Smaller 300 Lbs. Sw, R.F. A105 2 1/2" ar.4 Larger 300 lbs. WN, R. F. A105 Bolting Bolt Studs A193 Gr. B7 Nuts Hex A194 Gr. 2H Gaskets Flexitallic**
Style CG
** For non-nuclear piping systems (Group 't") use 1/16" cranite rings (ANSI B31.I).
9 e
i 1 TABLE 6 l
;
O - - l
~
300 LBS ANSI PRESSURE RATING STAINLESS STEEL PIPING SYSID1S
- s. ASIM Item Size Ratine Tvoo ,
Specification Pipe 2" and Smaller Sch 40S Seamless A312 Gr. TP304 2 1/2" thru 10" Seamless or A376 Gr. TP304 c Sch 40S 12" and Larger Std 3/8" Wall Seamwelded A358 Gr. TP304 Valves 2" and Smaller 300 Lbs SW' A182 Gr. F316 all 2 1/2" and larger 300 Lbs BW A351 Gr. CF8M Types Fittings 2" and Smaller
- 2000 Lbs SW A182 Gr. F304
)
2 1/2"'thru.10" Sch 40S BW A403 Gr. WP304 12" and Iarger Std 3/8" Wall BW A403 Gr. WP304
~ ~~
O Flanges 2" and Smaller 300 Lbs. SW, R.F. A182 Gr. F316 ( , 21/2" and larger 300 Lbs. WN, R.F. A182 Gr. F316 Bolting Bolt Studs A193 Gr. B7 Nuts Hex A194Gr.2N' Gaskets Flexitallic Style CG . O. I
l 1 1 TABLE 7 O - 150 LBS ANSI PRESSURE RATING CARBON STEEL PIPING SYSTEMS ASDi Item Size Ratine Tvoe Soecification Pipe 2" and Smaller Sch 80 Seamless A106 Gr. B 2 1/2" thru 10" Sch 40 Seamless A106 Gr. B 12" thru 24" Std 3/8" Wall Seamless A106 Gr. B 26" and larger Std 3/8" Wall Welded A155 Gr. KCF 70
- Valves 2" and Smaller 600 Lbs. SW A105 all 2 1/2" and Larger 150 Lbs. BW A216 Gr. WCB Types Fittings 2" and' Smaller 3000 Lbs SW A234 Gr. B 2 1/2" thru 10" Sch 40 BW A234 Gr. B !
12" and Larger Std 3/8" Wall BW A234 Gr. B 1 l
. . , . i O "
Flanges 2" and Smaller 150 Lb. SW,I.F. . A105 1 ( , 2 1/2" and Larger 150 Lb. WN, R.F. A105 Bolts , Bolt Studs A193 Gr. B7 Nuts Hex A194 2H Gaskets FlexItal1 Ic ** Style CG
- Butterfly valves 4" and larger also used within this pressure range.
** For non-nuclear piping systems (Group "D) use 1/16" cranite rings (ANSI B31.1).
O. - I
TABI2 8
. 150 LBS ANSI PRESSURE - RATING STAINLESS STEEL PIPING SYSEMS AS'Di .
Item Size Ratine Tvoe Soecificotfor Pipe 2" and Smaller Sch 40S Seamless A312 TP304 2 1/2" thru 12" Sch 10S Seamless or 4376 TP304 or 14" and larger Sch 10S Seamwelded A358 TP304 Valves 2" and Smaller 150 lbs. SW. A351 Gr. CF8M all 2 1/2" and Larger 150 Lbs. BW A351 Gr. CF8M Types Fittings 2" and Smaller 2000 Lbs SW A182 Gr. F304
. 2 1/2" and Larger Sch.10S BW A403 Gr. WP 304 O Flanges 2" and Smaller 150 Lbs SW, R.F. A182 Gr'. F316 l
( 21/2" and larger 150 lbs WN, R. F. A182 Gr. F316 i Bolting Bolt Studs A193 Gr. B7 e . Nuts Hex A194 Gr. '2H Gaskets Flexitallic Style CG , 1 O. 4 e
. TABII 9 900 LBS ANSI PRESSURE RATING, CARSON STEEL PIPING SYSTEMS (BRITILE FRACTURE CONTROL)
"SIM A -
Item Size Ratine Tvoe Soccificatior Pipe- 3" and Smaller Sch 160 Seamlers A333 Gt . 6 4" thru 10" Sch 120 Seamless A333 Gr. 6* ! 12" thru 14" Sch 100 A333 Gr. 6* 1 16" and larger Sch 80 ** - A333 Gr. 6* l
. L_
Vilves 2" and Smaller 1500 Lbs SW A350 Gr. LF2 ' s.nd 2 1/2" and larger 900 Lbs BW A352 Gr. LCB Types - or A216 Gr. WCC Fittings 2" and Smaller 6000 Lbs SW A420 Gr. WPL 2 1/2" thru.10" March pipe wall BW A420 Gr. WPI 12" thru 14" Sch 100 3W A420 Gr. WPI 16" and Larger Sch 80** BW A420 Gr. WP1 Flanges 2" and Smaller 1500 Lbs SW, R.F. A350 Gr. LF2 I 2 1/2" and larger 900 Lbs. WN, R.F. A350 Gr. LF2 Bolts 1" Dia and Smaller Bolt Studs A193 Gr. B7 1 1/8" and larger Bolt Studs A320 Gr. L7* Nuta 2" and Smaller Hex A194 Gr. 2H Gaskets Flexitallic Style CG
- Materials must be impact tested per ASME Code Section III, Article NB-2300 at a temperature of (-) 200F.
I
** 20" Feedwater system piping to be schedule 100 ,
-'- ' - ~ ~ ~ ~
. l '-
~ ~
TABLE 10 O f 1500 LBS ANSI PRESSURE RATING STAIN 1ESS SIEEL PIPING SYSTEMS ASIM Item Size Ratin? Tvee Soecification Pipe 2" and Smaller Sch 160 Seamless A312 TP304 2 1/2" and 3" Sch 160 Seamless or A376 TP304 Valves 2" and Smaller 1500 Lbs SW A182 Gr. 3N 2 1/2" and 3" 1500 lbs BW A351 Gr. CFI Fittings 2" and Smaller 3000 Lbs SW A182 Gr.304 2 1/2" and 3" Sch 160 LW A403 Gr. WP 304
..3 k ,
Flanges 2" and Smaller 1500 lbs SW, R.F. A182 Gr.304 2 1/2" and 3" 1500 lbs BW, R.F. A182 Gr. 304 1 Bolts . Bolts, Studs A193 Gr. B7 l 1 1 Nuts Hex -A194 Gr. 2H i Gaskets Flexital.lic Style CG l e D -
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NUCLEAR SAFETY RELATED O SMALL PIPING DESIGN STANDARD ENRICO FliRMI ATOMIC POWER PLANT - UNIT 2 REPORT PREPARED FOR DETROIT EDISON COMPANY O REPORT SL-3150 REVISION 1, JULY 29,19T, SA" GENT &LUNDY O ~~~~~~~ - - a
O TABLE OF CONTENTS Rev.1, 7-29-77 PAGE I INTRODUCTION 1 A. Description B. Relationship to ASME Code Requirements C. Scope II DESIGN PRINCIPLES 2 i A. General I B. Weight Analysis O C. Dermal Analysis D. Seismic Analysis III ASME CODE REQUIREMENTS l 7 i A. Sustained Losds i 1 B. Occasional Loads C. Dermal Expansion IV CONCLUSION 11 A. Stresses B. Nozzle Loads O 11 SL-3159
Rev.1, 7-29-77 V REFERENCES 14 APPENDICES Appendix A - Calculations and Equation Derivations Appendix B - Weight Support System Design Appendix C - Seismic Support System Design i Appendix D - Flexibility Support System Design Appendix E - Small Piping Design Worksheet t O l 1 s O 111 SL-3159 l TL
. -..~ __ _. . - _ _ . _ . . . . _ . . _ - - - - - - -
SARGENT & LUNDY ENGINEERS cmcac Rev.1, 7-29-77 O SMAU_ MPING DESIGN STANDARD ENRICO FERMI ATOMIC POWER PLANT - UNIT 2 DETROIT EDISON COMPANY I INTRODUCTION A. Description The Small-Piping Design Standard presents genc al guidelines and specific rules which are to be applied to the design of piping subsystems to locate weight i supports and seismic restraints and to guarantee adequate flexibility for 1 accommodation of thermal expansion and anchor movements. De recommenda- ! tions of the standard are based on weight, thermal expansion and seismic analysis i of simple beams, which represent elements of the piping subsystem. The assumptions used in the analyses insure conservative results: the estimates of stresses and loads for a given design environment exceed the values which could exist in the actual system. O B. Relationship to ASME Code Requirements Adherence to the recommendations of this standard guarantees satisfaction of the applicable requirements of the ASME Code.
- Specifically, stresses due to pressure, weight, thermal expansion, and seismic excitation are combined and checked against the allowables according to the provisions of NC-3650. Also, the method of analysis requirements of NC-3673.1 arc satisfied since use of the standard amounts to design by comparison with analyzed systems. Satisfaction of ASME Code requirements is shown in detail in Sections il and Ill of this report.
C. Scope his standard may be applied to ASME Code Clar 2 and 3 piping of four inches or smaller nominal diameter. It may not be applied to systems whose maximum operating temperature exceeds 300*F or whose maximum operating pressure exceeds 1750 psi. The pipe material is assumed to have a minimum S *b I 15000 psi for Class 2 and 3. c h Q 0ASME Boiler and Pressure Vessel Code, Section 111 PROJECT 5285-16 SL-3159 _ ___ _ M
SARGENT a LUNDY ENGINEER $ occaco Rev.1, 7-29-77 O 11 DESIGN PRINCIPLES A. General A piping system design represents a compromise t'etween two competing design' requirements: 1) the system must be adequately restrained to prevent overstress due to weight and seismic loads and; 2) it must be flexible enough to accommodate thermal expansion and nozzle movements. Unnecessary or poorly located restraints restrict thermal expansion and nozzle movements and so should be avoided, but enough restraints must be used to limit seismic and weight stresses to allowable values. Recommended spans for seismic and weight supports are given in the Tables of Appendices B and C. To increase the flexibility of a system in a given direction, pipe must be added perpendicular to that direction. The length of perpendicular pipe which is required to accommodate thermal expansion and nozzle movements under various conditions is given in the Tables of Appendix D. B. Weight Analysis
'Ihe standard procedure for designing a weight support system .n colves the use of recommended span lengths to limit the weight-induced bending stress. The requirements of ASME Code may be satisfied by this approach even though the governing equations do not directly indicate an allowable weight stress level.
It is only necessary to determine what fraction of the allowable combined stress the weight load should contribute. Recommenaed spans baseJ on this allowable stress can then be calculated by elementary bending theory (See Appendix A). The span recommendations are listed in Tabic ". I cf Appah il for fluid filled and empty pipes. The effect of the weight of standard insulation for 300"F has also been considered. The recommended span length is given by span (ft) = d 2000Z _y l l O
-i SL-3159
{ a
SARGENT e LUNDY EN GIN E E RS CHICAGO Rev.1, 7-29-77 n =
?) ' where Z is the section modulus (in.3) and W is the I!near weight density (Ib/ft).
The allowable weight stress is 3000 psi. His formula is based on the assumption that the pipe element may be '. , - represented as a simply supported beam. The maximum bending moment for a continuous beam or for a beam with other end conditions cannot exceed the maximum for the chosen model. Therefore, although the analytical model may not always accurately represent the actual piping, it does establish an upper limit for bending stress. To accommodate concentrated weiglits, the spans must be shortened to insure that the allowable bending stress is not exceeded. Rules which are to be used to determine span lengths for spans with concentrated weights are listed in Appendix B. C. Thermal Analysis De object of the thermal expansion ar.alysis is to guarantee adequate flexibility so that nozzle movements and pipe expansion do not cause stresses in excess of the allowable. The design rules of Appendix D limit this stress to 15000 psi. As previously stated, flexibility in one direction is dependent upon the amount of pipe which is perpendicular to that direction. For instance, c component of nozzle movement in the X-direelion can be accommodated if the nozzle is separated from the first X-direction restraint by enough piping in the Y- and Z-directions (See Figure 1). It is the bending stress in the perpenaicular legs, B and D, that must be examined. These may be conservatively modeled as a beam with guided ends subjected to a displacement, 6 ,(Sec Figure 2). The model is conservative since it ignores the flexibility of the elbows and imposes more rigid end conditions than the actual supports. SL-3159
- L l
SARGENT c LUNDY ENGINEERS cmcaco REV.1. 7-29-77 A E ~ g s '/ C 1,
/B D jt
/
c URE1 S=S, + 5 s H I
- s. K H I- H l- l I
c- x l l l ;
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r I
;
I I I l FIGURE 2 i y/: m O itthe etio edie stressis isooo psi the2easta or erneaaieuiereine n re9uiredto accommodate the component of nozzle movement is 1 1 = 1245 r. r. = outside radius -
'Ihe recommended lengths for various values of 6 and r. are listed in Table D-1
;
of Appendix D. Also, a graph or r. vs. 6 is included for various values of1 (See Figure 3 on following Page.). Note that it is necessary to check for nozzle movements in three orthogonal directions. The problem of pipe expansion can be handied in a simite- manner except thut the movement, 6 , is imposed by thc cxpc. c ' a see La. ,f pipe (Sec Figure 4). 1 See Appendix A for derivations of the equations in this section. D* O -
]D *]D
- e au - 'u" 2" - {' h =
SL-3159 1
SARGENT c LUNDY ENGINEER 5 cmcaco REV. 1, 7-29-77 2 25 (,
1 11 t
2 05 7 6 1 85 5 ( 58 1.65 . 4 n
-4 1.45 l O I 1.25 . .
3 t 0 'l s 1.05 . 19 I . 18 0.85
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.5 2!3 s4 '; A 7 0.0 0.5 10 1.5 2.0 25 DEFLECTION FIGURE 3 O. OFFSET REQUIRED TO ACCOMMODATE NOZZLE MOVEMENTS SL-3159 w
SARGENT a LUNDY EN[NEERs REV 1, 7-29-77 4 p*----...,,__ 9_uide i f l FIGURE 4 r7777 The length of pipe required to accommodate the expansion of the length t' , is 1 = 1.475 Y t r. Values for various lengths and radii are listed in Table D-2 of Appendix D. If nozzle movement and pipe expansion occur simultaneously, the total length of perpendicular pipe required is the sum of the lengths required for l each. ' D. Seismic Analysis An adequate number of properly located restraints must be provided to limit the stress and deflection due to seismic excitation to allowable values. Location of supports requires determination of the maximum span (distance between parallel restraints) in each direction, for which the system response is acceptable. To assure satisfaction of ASME Code requiremen's a response shall be considered 2 acceptable if the total stress ( x2y22)l due to bending and torsional moments does not exceed 7000 psi for OBE an,d 14,000 psi for SSE, and the total deflection ( x +y +z) does not exceed two inches.
;
To estimate a system's seismic response it is assumed thrit each section of pipe l 3 between two parallel restraints acts as a simple beam. For the deflection - estimate the beam is assumed to be simply supported and for the natural frequency estimate it is assumed to have one fixed and one simply supported end. - This assures a conservative estimate of the respor.se. O SL-3159 I l'
SARGENT & LUNDY ENGINEERS Rev.1, 7-29-77 O Using the assumed model, seismic deflection versus span length curves are generated. These are based on appropriatt response acceleration spectra. Superimposed on each deflection ( x, y, z) versus span curve is a curve which indicates the deflection at which the stress for each span is 4000 psi. The intersection of these curves indicates the longest span for which the anticipated deflection does not exceed the allowed deflection (See Figures 5 and 6). Note that the deflection is limited to two inches regardless of the stress. The span values taken from these curves are summarized in the span versus pipe size Table C-1 of Appendix C.
'Ihe seismic stresses are determined by using the computer program SIPDA (Sargent & Lundy Document No. 09-5-047-2.0). This program was developed by Mr. E. B. Branch and Mr. M. Nopola of Sargent & Lundy to:
- 1) Enable selection of maximum spans so that the stresses due to each seismic excitation (i.e., N-S, Ver., E-W) are 4000 psi or less for OBE, 8000 psi or less for SSE.
- 2) Provide seismic restraint design loads. I
- 3) Assure that seismic deflections do not exceed two inches. '
III ASME CODE REQUIREMENTS 1 l Class 2 and 3 Systems
)
In the following subsections it is shown that the stress limits which are established by the design rules of this standard satisfy the ASME Code requirements for Class 2 and l 3 piping. A. Sustained Loads
'Ihe effects of sustained mechanical loads must satisfy equation (8) of NC-3652.1:
P, Do+ .751 M, 3 4t n Z t, = wall thickness ( M, = weight induced bending moment Sh = all wable stress in the hot condition. SL-3159 l
SARGENT & LUNDY ENGINEERS REV. 1, 7-29-77 CHICACO SAMPLE SESIMIC DESIGN CURVE SPAN vs DEFLECTION RIGID _ 33 SIR ___ FLEXI3LE _ MAX AL'E.Va_E DEFLECTICN j j l O 2- / s. M ' g1 U ta MAX MID-SRAN CEFLECTION 10 20 ..- v 00
; . .- a i . , r :3 FIGURE 5
! SEISMIC DESIGN CURVES 1 IMPLY SUPPORTED PIPE O SL-3159 l a
SARGENT a LUNDY
'"[ "5 REV. 1, 7-29-77 SAMPLE O 13 .
SEISMIC DESIGN CURVE-SPAN vs REACTION p RIGID 72.3"? - FLEXIE13 _ 11 < 10 . 2 64 6 4 7
- u. .
b O 6 4 3 2 i i f 1- :
._y ,
8 10 15 20 30 e so LETETH IN FEET FIGURE 6 SEISMIC DESIGN CURVES SIMPLY SUPPORTED PIPE O SL-3159
~
s SARGENT C 1. UNDY E >lCIN E E R S c>ucAco Rev.1, 7-29-77 O For pipes of 4 inches nominal diameter or less and subject to pressure not exceeding 1750 psi (or the recommended value from Sargent & Lundy Mechanical Engineering Specifications if that value is lower), the first term has a maximum
~
value of less than 5000 psi. For systems within the scope of this standard, the stress intensification factor 1, in the second term, attains its greatest value of 1.532 for a 4-inch schedule 40 socket welding branch connection (weldolet). The weight iduced bending stress is a maximum of 3000 psi. The hot allowable stress for materials and temperatures which is covered by this standard is no less than 15000 psi. Thus, 5000 + .75 (1.532) (3000) = 8447115000 = Sh ; therefore, equation (8) is satisfied. B. Occasional Loads The effects of sust 7ed and occasional loads must satisfy equation (9) of NC-3652.2. , P max D gMR o +.75 -1S 41" h O Since the weight and maximum pressure were considered for evaluation of equation (8) the only additional term is the seismic stress, M /Z = 7000 psi for . R OBE, and 14000 for SSE. Thus: 5000 + .75 (1.532)(3000 + 7000) = 16490118000 = 1.2Sh 5000 + .75 (1.532)(3000 + 14000) = 24533127000 = 1.8S h So equation (9) is satisfied for upset and energency co.sitions. C. Thermal Expansion l l '!he ASME Code requirements for thermal expan. 'on are satisfied if equation (10) I or equation (11) from NC-3652.3 is satisfied. IM [ 1 S, (10) l l M,/Z is the bending stress due to thermal expansion and anchor movements, so ' O 1.532 (15000) = 22980 psi SL-3159
- 1
SARGENT a LUNDY ENGINEERS CHICACO Rev.1, 7-29-77 O But S, = (1.25S, + .25Sh) = (1.25 15000 + .25 15000) = 22500 psi. So equation (10) is not satisfied and equation (11) must be checked. PD M M 4tn + .751 Y +1 j 1 Sh+8a IIII 5000 + .75 (1.532) (3000) + 1.532 (15000) = 31427 psi 137500 psi So equation (11) is satisfied. i IV CONCLUSION For systems within the scope of this standard, application of iis design rules assures satisfaction of the requirements of NC-3650 of the ASME Code. I* These systems must have the fo!!owing characteristics: - Pipe class: 2 and 3 Nominal pipe size: 4 inches and smaller Maxinium operating pressure: 1750 psi Maximum operating temperature: 300*F Allowable stress: Sh > 15000 psi S, 2.15000 psi A. Stresses
'Ihe stresses in a system designed accordin;- to t" - ytendard arc limited to the following values:
Moment loading Max stress (psi) seismic OBE 7000 weight 3000 thermal expansion plus nozzle movements 15000 0 SL-3159 rt
SARGENT a LUNDY ENGINEERS CHICACO Rev.1, 7-29-77 O TABLE 1 NOZZLE ALLOWABLES CR AMCHoA RE%TIO M Pipe Size Schedule Moment Load ( ft-lb) Shear Force (Ib) 1/2 40 85 72 80 100 78 160 110 99 3/4 40 147 103 80 178 128 160 209 145 1 40 277 170 80 335 207 160 396 246 1-1/4 40 489 270 . 80 607 329 160 713 383 : 1-1/2 40 679 342 80 858 O 160 1060 427 529 j 2 40 1170 536 80s 1520 683 160 2040 912 t 2-1/2 40 2220 903 80 2790 1120 160 3410 1360 3 40 3590 1360 80 4630 1680 - 160 5990 2200 3-1/2 40 6690 2250 80 6540 2240 XXS 10300 3490 4 40 6600 2250 80 8890 2920 160 12300 3950 0 SL-3159
~
b l SARGENT e LUNDY - E NCIN E E RS Rev.1, 7-29-77 B. Nozzle Loads
'Ihe loads imposed on nozzles by piping which is designed according to this standard do not exceed the values listed in Table 1.
Sargent & Lundy Prepared by: e. - , .?ev. 1, 7-29-77 P. Ivy, g Project Engineer, Engineering Mechanics Division Reviewed by: b Rev.1, 7-29-77
. . . Hart, F ineering Analyst, Engineering Mechanics Division O ME. B. Branen, aev 1. 7-29-77 Head, Engineering Mechanics Division
( sw_ = Approved by: Rev.1, 7-29-77 R. F.' Scheibel, Project Director O SL-3159
5ARCENT A LUNDY l E N GIN E E R S Rev.1, 7-29-77 [O V REFERENCES l ASME Boiler and Pressure Vessel Code, Section III,1974 ed. New York: American Society of Mechanical Engineers,1974. 3 Kellogg, M.W. and Company. Design of Piping Systems. Revised 2nd ed. New York: John Wiley and Sons, Inc.1965. Oak Ridge National Laborataries and Teledyne Materials Research. Nuclear Piping
]
d D Ae, ORNL-TM-3645. Oak Ridge: Oak Ridge National Laboratory, Feb.1572. Roark, Raymond J., Formulas for Stress and Strain. 4th ed. New York: McGraw- l 11111 Book Company,1965. 1 L Timoshewko, S. and D.11. Young, Elements of Strength of Materiah. 5th ed. Princeton: 1968. [ l - 1 0 SL-3159
h.4 z._a 2 m. , e ., 4 2 w - -' - - - -- - - APPENDICES O . l l l l l
, I l
i l o
;
9 4 i 1 O 1 m - .- _
Cf ROENT O LUNDY ENGINEEDS APPENDIX A CHICAGO sL-3159 l R E V. 1, 7-29--77 i O 'cAucut ions ^~o EauxTion oERiv4Tions A-1 Weight The recommended weight support spans are based on the following analysis: l The pipe elements between two weight supports may be j l conservatively represented by a simply supported, uniformly loaded beam (fig. lA.). f 1 IY1J 1 V 1 1 i fl 1 1 1 A A g ' x :I fig.1 A 2 fig.1B From symmetry and squilibrium considerations the bending moment at' a cross section X t' nits from A is: O M: Xdx : @ (x I-X' ) R,- p , a : 1incar weight dersity X-f"xo 1 This is a maximum at X = f/2 y - m max- 2 '.!*_ [4,- 62 _ sfe
- The stress due to this moment is 5: *= ^l , 2: se ction m o du'us If S a is the allowable stress sa : a l*/BZ ,so l= fB y '
1 is the maximum span for which the allowable stress is not ! exceeded. j O l A-1 l w-_ - -- -- -
'l
CARGENT Q LUNDY ENOiNEEDS APPENDIX A CM 8C AGO SL-3159 REV.1. 7 29-77 O Ar1 Weight (continued) For an allowable stress of 3000 psi J _F 4x coo; ' For 2 given in (inches) ,3 / in feet, and ee- in lb/ft j = 20032' w g,; ) to allow a construction tolerance of one foot without exceeding the allowable stress, the recommended span is one foot less than indicated by equation (A-1). y: 20,. W -1 m.2) l The maximum support load is calculated assuming that l:fs +1 is used as the span length. Thus LOAD = feu (A-3) This is not the reaction, R,a of fig. 1D. It is the total weight of a full span and represeits the load which would be imposed on an intermediate support of a continuous multi-support system. () l l A-2 l l
3 CARGENT& LUNDY E N C. I N E E N s
> ' " ' " " APPENDIX A SL-3159
- o REV.1, 7-29-77 A-1 Weight (continued)
Span Reduction for Concentrated Weights The maximum total bending moment for a span of length f,,
)
subject to distributed weight, s , and centrally located concentrated weight, W, e is Mmax= + * ,' For a given pipe the allowable maximum moment is where 8 is the recommended span length without the concentrated load. Therefore w8 S. + $ g M S' 4 6 If one half of the recommended span length is used the safe value for We can be obtained. M it?) .y we tit o) S MA'
- 8 4 8
%} g 3 nr f
- 3 32 We 6 3/4 s2 or 75*/. of w l Similarly, if f,:.SR 81ef* 4 _WeL9f) g y .f
- We 6 ,10 t y ) es o .f,og ,)
( l A-3
8 l CARGENTQ LUNDY EN08NEED9 APPENDIX A g cmcaco SL-3159 r RE V. 1, 7-2 9-7 4 ['O A-1 Weight (continued) Span Reduction for Concentrated Weights So, for a concentrated weight of less than 10% of the normal span weight a 10% reduction in span would keep the weight stress below 3000 psi. For a very short span (say 10% of the normal span) a similar analysis shows that a concentrated weight of 2.5 times the normal span support load can be accommodated. Since such concentrated weights are usually very rigid compared to the piping, the length of the concentrated () weight may be ignored in the span length estimate: the 10% span is the pipe length exclusive of the length of the concentrated weight element. A-2 Expansion and Nozzle Movements The recommended offset lengths are based on the following analysis: All segments of pipe in the offset direction are assumed to act as a single guided cantilever, the Flexibility of intermediate elbows and pipes is ignored (see Fig. 2) (2) - A-4
{ CARGENT O LUNDY ENoNEERS C M 6C# GO APPENDIX A SL-3159
~
REV.1, 7-29--77 t' A-2 Expansion and Nozzle Movements (continued) 9 The recommendedc offset lengths are based on the following I analysis: i All segments of pipe in the offset direction are assumed to act as a single guided cantilever. The flexibility of i intermediate elbows and pipes is ignored (see Fig. 2) b-s l "i 's i i , bl #2. - - S
- 5 F I G. 2 Suppose a deflection,d,is caused by a load, W. .
W
- n. ;r
' ~ - - - aa-u W
M Rs U A B IF: j O Q R:W IM:ox 0 > Wf-M a-Mb=O but Ma Mb 50 f-( I Mb ds aW ' M(n) 2 x M*)WY -Wf/ 2 :W( x - f / 2.' v 8: d x' EI M = F.E--( I x -1/ 2 ) dx , A =EI3-.('Y F + c ' dx A :osoc=o 2 2 1 0 W IX* fmai p, Q Y EII'G 4 [+ , y:O at x: O s o C': 0 A-5
CARGENTO LUNDY E N GIN E E AS
"" APPENDIX A SL-3159 o REV. 1, 7-29-77 J
A-2 Expansion and Nozzle Movements ! (cont'nued) . Thus -W y :EI i G M\4 j is the deflection at a distance X from the anchored end. 1 Since Y = -f at X = f - 6.Ef_ i E1 4 _A.',i 4 l W l' , g _12EI - or w:_12SE1 J*
]
The stress due to the defeletion, d , is , r 5 :r.M/t : Wfr- 12 f cI r. JQ 21 29'I
- 9d r. E_ , r. : c u te r radio, f*
If this deflection is the resultant of three equal orthoganal deflections, E' , S: 65 r. E 8:h(S'*) f R' t
= _G66 r.E g GTT 4'r,.r /t 5 5 For an allowable stress of 15000 psi the offset length must be ll _ [ GT3 3 010* r,f
Y2 .
- l 15000 -44(I' 2. ' or ' 2 h , ! r e t '
! I tor r, and E in inches L. 1 i s O ) A-6
i CARGENT O LUNDY ENGINEERS ! C"'C"' APPENDIX A I SL- 3159 m RE V. 1, 7-29-77 U i
.A-2 Expansion and Nozzle Movements (continued)
The def?ection due to pipe expansion is handled in a similar manner except that the imposed deflection is i
=
one-directional. Thus J
- r. E f: :9.129k,[
l
;
- l For' expansion of a length A' l 0 l 2
j = f' A A T : ( .0261 in/f t )f' for austenitic stee: 70* to 3 O O
- F O e f:9.129 @
a R> 1 29.1291r, (.0 2 51 ) f"
' i 77F - !
f :1. 4751 r. J' ~' for / and [in fee t , r. in inches O l Note that the flexibility of the leng th j and the elbow i I is ignored. 1 6 ! Free Ends: The bending moment cannot_ c::cced thi t for a l 3 cantilever. l
.w 4
u bbbbb[ 1 hbbbb , a v M: ex d x:
- ]** -
=
i s i A-7
~
CARGENTOLUNDY E"fj,",EE"5
. APPENDIX A SL-3159 REV 1, 7-29-77 ]o A-2 Expansion and Nozzle Movements (continued) whichis4timesthe[ofasimplysupportedbeam.
Thus,
. the span should not exceed 50% of the value from table I.
If it does, or if a concentrated weight is on the span, an end support should be provided.
]
T
]
TO [ [ r ; l l I o A-8 e
CAGOENT O LUNDY E"fle",E"#8
,o APPENDIX A SL-3159 R E V. 1, 7-29-77
[O A-3 Nozzle Loads [ The maximum bending stress is that due to simultaneous { action of weight, thermal, and seismic loading. That value is 3000 + 15000 + 7000 = 25000 psi. The [ , bending moment corresponding to this stress is Z 25000 psi l M= = 2083 Z ft.lb. I 12 in/ft , [ where 2 = section modulus (in ) 3 The shear force due to weight is one half the maximum ' lJ weight support load from table B-1, Appendix B. 7 The shear force due to seismic loading may be estimated ; by assuming that it is in the same proportion to the ii
)
weight shear force as the seismic stress is to the weight ', i stress. seismic shear = 7000 weight shear 3000 seismic shear = 2.33 weight shear . The shear due to bending moments is estimated by assuming that it is equal to the force required to cause a 15000 psi bending stress with a moment arm equal to the minimum allowed offset from table D-2. l l O A-9
] SARGENT Q LUNDY ENGINFLH%
i .m a . .. . APPENDIX A SL 3159 REV.1, 7 29 77 (m Derivation of Seismic Analyses Equations
]%
A-4 S_e_i_smic, Des _ign Curves A-4.1 I_ntre duc tion
} To arrive at the equations used to predict the actual deficctions, allowable deflections and restraint reactions, the elements of piping betwccr. rcstraints are modeled } as a simply supported beam as shown in Figure A-4.2a. With the exception that the natural frequencies used are those ] that correspond to a beam aith t.he same dimensions which } has one end fixed and one end simply supported. This assures a conservative estimate of the response. ]tOV All design curves, of which typical examples are shown in ] Figures 3f5.la__and 2,. Lib were calculated using the equa-
. tions shown here and enveloped seismic response spectra covering all elevations in the Reactor, Turbine, and RHR Complex Buildings. For each of the Buildings, separate responses were calculated for the East-West, North-South, and Vertical Direction Excita.. . . .
- a. .f at exci tation in any one building the allowabic deficction of the pipe
. segment modeled and analyzed was based on a 4030 psi bending ~
stress. This criteria limits the maximum bending stress due (] to excitation in all three directions simultaneously to A-10
-a, e
CARGENTQLUNDY EN NEERS c,co APPENDIX A SL-3159 RE V.1, 7-29-77
]O 4000 h psi using the square root of the sum of the squares to combine the responses in accordance with NRC Regulatory Guide 1.92.
A-4.2 Derivation of Equations Figure A-4.2a Models and Nomenclature
] o i
3 e f = o =X g g
.. om ex x, umir """'
Cons &t EX, D, or ]o Model Used for Deflection Functions ] ] % 4= 1 = 3
, Consfant EI,D3m-Model Used for Natural Frcqucncy Det.crminations I
. 11 3
_. . . _ -- a
( CARGENTO LUNDY EN N RS APPENDIX A SL-3159 RE V. 1, 7-2 E-77 lo A-4.2 Nomenclature 60' = weight per unit length of beam a E = Youngs modulus k = I Area Moment of Inertia of Pipe Cross-section D = Outside Diameter of pipe - 1 = Length of span ehg = radian natural frequency of nth mode gg = period of nth mode Ys(t)= absolute support acceleration (a function of time 't') hI(ty= Response spectra acceleration (a function of T*t o r t.d ,t ) O gn (t) = generalized displacement of mode n
, T}g = Modal Participation Factor of mode n y(t) = Beam deflection relative to supports M (x, t) = Moment at beam cross sections V (x, t)= She;.r at beam cross sections ee
][ = Absolute acceleration A-4.2-1 Solution The equation of motion, using Euler Bernoulli Beam Theory and neglecting Shear Effects on curvature and Rotary Inertia can be written as follows for a beam segment
(]) between two supports. A-12 4
q CARGENTQ LUNDY J
""L',c"[,,E"5 APPENDlX A SL-3159 '] A-4.2-1 RE V. 1, 7-29-77 I+- '"
l l = 0 .] The absolute acceleration of any point on the beam can be rewritten as: J y = @) + y;a) (2) T j where f h*@ g = the acceleration of any point on the beam relative to the supports. The equation of motion may then be rewritten as: Y =~ 5 b) (3) [O { It can easily be verified by substitution into the homogeneous form of Eq. 3 that the mode shape for the nth mode of a simply supported beam is (sin "[ ) . The solution to Equation 3 can then be written as: I oo d) [ hn 44at) 3.D (4 )
- 93) .
Substitution of this into the uuation of motion yields: (5) aI *- N) O multiply each side of the equation by (sin ( " [ ) A-13
a l CARGENTO LUNDY E N G1N EE Rs c mc ac, APPENDIX A SL-3159 RE V. 1, 7-29-77 and sum over the m index J ll9? +'DWYy}~q-; =-%>f-~y
- )
Integrate both sides on x between o and f. ij -- t i j t 1 O (7)
.. ee k C-3(f) [ k 2. d,X
,=31 Integration:
-] I O m #m 44.nt> %1YX (a) A M rnTfx A Q=) \ ], O f T""
\
Sum the left hand side over the m index. It becomes
+ ( gw and the index on the right side can be changed to n. The equation can then be rewritte n as:
i 9 ., This will be satisfied if, for all n, Y b h [ / 5 A-14
CARGENTO LUNDY EN INE RS g,,, APPENDIX A SL-3159 A-4.2-1
- }
A. REV. 1, 7-29-77 i
)
Define
]= mwrrXA A
= Modal Participation l
} , Factor I Then the equation of motion for each mode is: ; ] !
} [+ k(* g= -
k(OM
, Using the standard spectral analysis technique bb l VCT4 h (d x2 n. (12) where Y ( Ts ) is the response spectra acceleration.
Therefore:.
-e 1
w o v-~ <x) = 2r .. ) M=/ v13 y _,m (' ) l ** .. 4
=. t Z T 4. Y (T ,d p wwx i
4:s 4 TT'2 y
) 2/ (14)
O ' % Mn 71 = I )=ydu = f, 4 o I, g 9 %. M Substitute:
=f{M M W3 (TN d 9t.#"X (15) n=1, 3, 5...
L I Calculation of Moment Distribution:
- O M cx) = E19. EI y b ,. = ! we n. % 74 gg,), ,,x,y (16) l e 1, 3, S' * =
- A-15 w- .I
CARGENTC LUNDY
} * * $j "do'" APPENDlX A SI..-3159 FE V. 1, 7-2 9--77 Calculation of Shear Distribution ]
3 v_=*El p=tavcu = *nx n = 1, 3, 5...
} The maximum shear occurs at x = 0 and x = 1 Vmax 2 1- q2T{y(Tw) (18) n=1, 3, 5...
} The maximum moment is calculated considering the first mode only.
M max 1 TI (T8} OI 7 # (19) T EL g max _ M o _ EDTF V(td g (19a) ) The maximum deflection is also calculated considering the first mode only. ymM ' d T# ~ g (20) 7T3 Considering Equations 19 and 20 ' 3 ~ frE E D Aas = 2 12 Y""# 7O A-16 l
CARGENT O LUNDY
' " $ c"."c,o* " " APPENDIX A SL-3159
.O i A-4.2-1 RE V, 1, 7-29-77
- ]
or 1 I 1 J Y allowable = 2(OM'Ejg (21) Using E = 30 X 10 6p3;
] G max = 4 X 10 3psi Y allowable =(2.70 X IOS (( D jL (22)
This is the equation of the 4000 psi cavelope.
]
The actual deflection is given by
"" p~N y3 (Td (23)
The maximum shear is calculated as follows. For accelerations ( Tg) on the left side of the response spectra peak as shown balcw.
] h left
=
/
s scle f O e Y m s \
)
t O r
=
.e A-17
CARGENTOLUNDY O E N GIN E E R S CMtC&t O APPENDIX A SL 3159 REV.1, 7 29 77 A-4.2-1 Equation 18 may be conaervatively rewritten as: l EI . . (24) J by = 7g Yed) E x^re n=1, 3, 5... This equation is used to calculate the Restraint Reaction Curves. The natural frequencies of the fixed - simple beam shown in figure A-4.2a are accurately approximated by: (25) a)x : (x+%t)*TT* fy ay JL n = 1, 2, 3... l Therefore,
.1 i 2.n 2 WA
- 1 7* ~
A ~ N + r4)*rr EIg (26) l
'! 1 In summury the following equations are used to form i
the design curves. (21) fE Y allowable = 2.(h E TT,a v for the allowable en.relope a (23) Y actual = T'1 Y(Ti) for the actual dis-O placement "3 A .o P
] CARGENT Q LUNDY
, E N GIN F E R S APPENDIX A SL-3159 REV. !, 7-29-77 (24) Vmax = CD) MT for the restraint loads due to 1 span n = 1, 3, 5...
These values should be doubled to calculate restraint loads because there are generally two adjacent spans being restrained by any one restraint. (25) ! for the natural Tx = Ot+%d Tf V E l } periods.
]O I
l' O I
- o b
LO . s A-19 f ~ Final
._ .._. _ _ _ . - ___.__.u- - _. u - - - -
----------.n_----
CARGENTO LUNDY ENG1NEERS C HIC AGO APPENDIX B SL-3159 RE V. 1, 7-29-77 weiowTsueeoaTs
}O B-1 Procedure for Weight Support System Design Starting from a convenient point (nozzle, structural anchor, header connection, etc.) the piping is traversed in steps, called half-spans, of length equal to one half the recommended span from Table B-1 (normal l ] span). The steps may be shortened to accommodate 1
l special piping components and must be supported on one or both sides according to the rules given below. Only l l 3 one ste;p is made at a time and each is assigned a unique ; integer label which is marked on an isometric of system. The isometric is included in the system design
] documentation along with the weight support system design
)
} work sheets (see sample problems). These worksheets list alJ steps nuvarico11y and include a description of the
] elements in each step, the length and recommended supports
, for each step,and the rules which govern the design l decisions. The worksheet. is t. sci as an ..id to system design and as documentation to show that the requirements l '
- of the standard have been met. Enough information should !
be presented to show that the designer has considered ! " i all relevant system characteristi ;. ) ! ' i t B-1
~ _ . _ . - . - . -_-_ .-__ - . __ _ -____ _
CARGENTG LUNDY E N G I N E E *t 9
*" " APPENDIX B SL-3159 RE V. 1, 7- 29-- 77 B-1 Procedure for Weicht Support System Design (continued)
The steps are made in a consistent direction and branch lines are traversed only after an end point of the main run is reached. Each step has two ends, A and B, where A to B is the direction of traversing. The support system is completely defined by specifying the length m of each step and the ends which require support. Note ) that end A of one step is end B of the preceeding step, but each support is listed only once on the worksheet. That is, if a given step must be supported on end A, it _Qb ]- is not necessary to indicate that end B of the previous step is supported. Similarly, if a support at end B is ; required, it is not necessary to indicate tl.at a support l is required at end A of the following step. The [ ! worksheet only indicates additional supports which i - l are required due to the characteristics of cach successive step. I-This procedure for establishing weight support locations l [ is summarized below. .
- 1. Pick a starting point I
r 2. Follow the line for a distance of one half the normal tO eieht suggort seen (one ster). r k B-2 - 6
- . . . . ~ . _ . CARGENT eLUNDY ENGINEERS APPENDIX B - SL 3159 REV.1, 7 29 77 .O B-1 Procedure for Weight Support System Design (continued)
- 3. Examine the components within this step and determine which ends of the section require support and whether or not a shortening of the span is required by the weight support system design rules.
- 4. Mark the end point of the step on the isometric and number the step. (Number steps with consecutive integers.)
Indicate the type and location of supports on the isometric.
~
- 5. Enter all pertinent information on the worksheet.
- 6. Starting from the end point of this step, go to 2 above and continue this procedure until all lines and branches have been covered.
. O 4
r e I 3 l l i i c l
*I
. CARGENTQ LUNDY GNO1NEEao APPENDlX B CHICAGO
RE V. 1, 7-29-77
-() B-2 Rules for Locating Weight Supports '3
- 1. A half-span of plain pipe must have a vertical support J at one end.
- 2. A half-span which includes an elbow must have a vertical
- ]
J support at both e,nds.
.] 3. The length of a half-span which includes a J concentrated weight of less than 10% of the normal span load (Table B-1) should not exceed 40% of the '] normal span length. It must have a vertical support J on one side. - ] 4. A half-span which includes a concentrated weight of from 10% to 40% of the normal span loa'd must have a vertical support on both sides.
- 5. The length of a half-span which includen a concentrated weight of more than 40% but less than 250% of the
]() nonnal span 1 cad should not exceed 10% of the normal span length and should have a vertical support on both sides. Tbis lenoth does not include the actual
{ length of the concentrated weight.
}
- 6. A concentrated weight which exceeds 250s of the ncrmal
]
span load should be supported directly rather tha:. by the piping to which it is attached.
} 7. The length of a half-span with one free end should not exceed 50% of the normal span length.
I
- 8. A halt-span with a concentrated w,ight should not have a free end.
- 9. Supports not required by taese rules should not be used.
M m l L (~) - 7 r i h B-4 l l t - a
l g CARGENTO LUNDY E N G 1 N E E R *' C H K At*U APPENDIX B l SL 3159 REV.1. 7 - 29 77 _ Tabic B-1 RECOMMENDEO se SPA!!3 FOlt DEAD W1:IGi!T SUPI'OltTS NOM. S'"O
- WATER-FILLED GAS-FILLED ROD DIAM, j
_SCH. S PA_!!* LO-\D (LB) SPAN
- LOAD [LB) DIAM.
3/8 0.049 wall 5'-11" 2 5'-6" 2 1/4
] 1/2 40 80 160 6'-5" 6'-6" 12 12 6'-10" 6'-10" 10 12 3/8 l
6'-6" 14 6'-7" 14 5/8 0.083 wall 6*-10" 5 7'-5" 5 1/4 (tubc)
] 3/4 40 80 7'-7" 7'-11" 16 20 8'-4" 8'-4" 16 18 3/8 3/8 i
I 160 7'-10" 22 8'-1" 22 1 40 9'-0" 26 9'-10" 24 80 9'-2" 32 9'-10" 20 ) 160 3/8 l 38 9'-2" 9'-6" 38 ! l-1/4 40 10'-5" 42 11'-7" 38 80 10'-9" 50 46 160 11*-6" 3/8 10'-10" 58 11'-5" 56 1-1/2 40 11'-4" 57 12*-1C" 48 80 11'-9* 64 12*-30" 58 160 3/8 , a 11'-10" 60 12'-6" 76 2 40 12'-9" 82 14'-9"
~
7: 80 13'-2" 102
, 160 14'-9" 94 3/8 13'-6"s . 136 14'-4" 128 2-1/2 40 14'-6" 138 16'-9" 120 80 15'-0" 168 152 160 16'-7' 1/2 15'-1" 202 16'-2" 190 1
3 40 15'-6" 210 la'-)" 199 80 16'-2" 248 18'-1" 232 160 1/2 16'-7" 326 17'-10" 306 j 3-1/2 40 16'-7" 272 19'-9" 232 80 17'-5" 340 19'-9" 302 XXS 5/8 17'-11" 520 18 ' - 11 496 i 4 4 40 17'-7" 346 21'-2" 290 80 18*-7" 436 21'-3" 394
~
160 5/8 19'-2" 584 20'-6" 542 The actual span should not exceed the recommended value by more than 1 foot. I B-5 a c) _ _
f CARGENTO LUNDY E N G1N E E RS B-3 Sample Problem emeno APPENDIX B SL-3159 RE V. 1, 7-29-77 o _ _f /A' . D'
;
"f'.'-f.
@~ @
.b
) !
l
]
Fig. B-1. O I Pipe Size I/" Sch. 40 2 uu 22'O' O uu
] ,
\
1 0
]o / "". _
e*e , e . o g r. e e y 20th 1 H 51b ! l Figure B-1 is an isometric of sampic probl'em one. It includes labels for all steps, marks to indicate the end-points of steps, and symbols ( ) to indicate su.pport locations. The worksheet for this system is attached a44d should be -1 tua. tea with the following discussion. 1 H Step one is a hal::-span of plain pipe nupported at end A by the header. By rule one a support is required at one end. Since the i L ' } support at end A is provided by the header no actual hanger is 1 L q needed, so the worksheet indicates no required supports. The l ]: U y step length is'one half the normal span. The span load may be B-6 'O e
CAR 2ENT O LUNDY ENGINEERS APPENDIX B
**'*^
Sample Problem SL-3159
.} B-3 (continued) REV. 1, 7-29-77 11 ted on the worx deet, but is oa1r 1 gorteat for comgerieoa ]O with concentrated weights. Rule 9 is always used implicitly:
it is not indicated on the worksheet. Step two is also a plain half-span, but it is not supported at end A. Therefore, it must be supported at end B as is indicated
) on the worksheet. Si:.ce a support at end A is unnecessary it is not recommended.
Step three contains an elbow and so must be supported on both sides (Rule 2). The step length is measured along the tangent
] lines of the elbow, 1
lo Step four is plain pipe and is supported at end A (step three end B) so no additional support is required. Step five must be supported at one end. End B is choseri e,ince support at end A would put an unnecessary support on step four at end B.
]
Step six is also plain pipe and the support 2.t end B of section five satisfies the support requirexr.u. Step seven includes an elbow so it must be supported at both ends.
] Notice that this puts a support at end B of step six so that
, step six is a half-span of plain pipe supported at both ends. The B suggert is unnecessary for steg six dut neceesery for steg seven, o]
1
CARGENT O LUNDY E N G1N E E A5 C"'C " APPENDIX D SL-3159 RE V. 1, 7-29-77 A V B-3 Sample Problem (continued) so rule 9 is not violated. I Step B through 12 are plain pipe supported according to rule one as shown on the worksheet. Step 13 contains a valve whose weight is greater than 10% but less than 40% of the normal span load. Rule four requires that it be supported at both ends. This again causes a half-span of plain pipe (step 12) to be supported at both ends.
] Steps 14 and 15 are plain pipe subject to Rule 1.
Step 16 is less than 50% of the normal span but includes a branch which may be treated as a concentrated weight. Therefore, a support at end B is required by rule 8.
]
-]
]
- ) '
]
0 1 ] n-8
9 CARGENTO LUNDY E N GIN E EDS APPENDIX B I C"'C^' SL-3159 REV.1. 7-29-77 i WEIGHT SUPPORT SYSTEM DESIGN WORKSHEET
]
Line Identification Information WEIGHT SAMPLE #1 STEP SPAN PIPING ELEMENT S U PPOR'l STEP DESIGN SO. l NORMAL SPAN l LOADDESCRIPTION A 13 LENGTH RULES . I 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 2 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 3 11' - 4" 52 lb. Elbow X X 5' - 8" 2 4 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 5 11' - 4" 52 lb. Plain Pipe X 5' - 8" 1 6 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 7 11' - 4" 52 lb. Elbow X X S' - 8" 2 8 11' - 4" 52 lb. Plain Pipe 5' - 8" 1 9 11' - 4" 52 lb. Plain Pipe X S' - 8"
- 1 10 11' - 4" 52 lb. Plain Pipe 5' - 8" 1
_ 11 11' - 4" 52 lb. Plain Pipe X 5' - 8" 1
] 12 11' - 4" 52 lb.
Plain Pipe 5' - 8" I n 13 11' - 4" 52 lb. 20 lb. Vnive '
\ \ 5' - 8" 4 g 1 14 11' - 4" 52 lb. Plain Pipe 5' - 8" I h 15 11' - 4" 52 lb. Plain Pipe X 5' - 8" I c
16 11' - 4" 52 lb. Free end Cone. wt X 5' - 8" 8 [O , I B ') b Final e. t
CARGENT Q LUNDY E N GIN E Eno APPENDIX C SL-3159 REV.1. 7-29-77 13 SEISMIC SUPPORTS SYSTEM DESIGN The nature of seismic loading is similar to that of weight loading: a distributed force acts upon each element of a piping system in proportion to its mass. However, the seismic loading is horizontal as well as vertical. Therefore, a procedure similar to that which is used for locating weight supports may be used to locate seismic support.< if provision is made for including horizontal restraints at these locations. Regarding vertical seismie loading, one set of restrainte enn serse as both weight supports and vertical scismic restraints. Choose the shorter of the weight span and , vertical seismic span for_the building in which the, system is locate.d. Once the system is adequately restrained to resist vertical seismic loading, the system must be restrained for the two horizontal scismic loadings. For vertical pipe
] runs, two orthogonallateral supports are required at each r_estraint location (choose the shor'.er of the E-W and N-S spans). For horbntal runs, one horizontal restraint is l
required at each location. The following procedure is recommended for location of : O LJ these horizontal scismic restraints. C-1 Procedure for Seismic Support System Des ,7 Starting from a convenient point (nozzle, st ntural anchor her der connection, etc.) the piping is traversed in steps, called balf-spans, of len, th equal to one half the recommended span from Tatle C-1 (normal seismic ! >an). Th" steps l 3 may be shortened to accommodate special piping componen s and must be
,J supported on one or both sides according to the rules given be civ. Only one l
step is made at a time and each ir asched a ' nig te in'.cger abel which 13
,,, marked on an isometric of the system. The isomety is included in the system design documentation along with the se's'nic support -" stem design orks'ieets (see sample problems). These worksheets lis* all steps numeric: illy and include a description of the elements in each step, the length and rceommended supports for each step, and the rules which govern the design decisions. The worksheet is used as an aid to system design and as documentation to show that the requirements of the standard have been met. Enough information should be
!= presented to show that the designer has considered all relevant system O enaiacteristics. 1 < c-1 b
CARGENTO LUNDY
, ENGINEER 9
***^*
APPENDlX C SL-3159 REV.1. 7-29--77
'Ihe steps are made in a consistent direction, and branch lines are traversed only after an end point of the main run is rehehed. Each step has two ends, A and F, where A to B is the direction of traversing. The support system is completely defined by specifying the length of each step, the ends which require support, and the support types. Note that end A of one step is end B of the preceding step, btit each support is listed only once on the worksheet. That is, if a given I step mi.st be supported on end A, it is not necessary to indicate that a support is J
required at end A of the following step. The worksheet only indicates additional supports, which are required due to the characteristics of each successive ste[. A summary of this procedure follows.
- 1. Pick a starting point.
- 2. Follow the line for a distance of one half the normal seismic support span
] (one step).
- 3. Examine the components within this step and determine which ends of the Q section require support and whether or not a shortening of the span is required by the seismic support system design rules.
- 4. Mark the end point of the step on the isometric and number the step.
(Number steps with consecutive integers.) Indicate t'.e type and location of supports on the isometric.
- 5. Enter all pertinent information on the worksheet.
~
- 6. Starting from the end point of this step, go to 2 above ano continue ti.rs l procedure until all lines and branebes h9"e been covered.
]
l l C-2 Rules for Locating Seismic Supports
] 1. A horizontal half-span must have a horizontal, lateral restraint at one end.
] 2. A ~ vertical half-span must have two orthogonal, horizontal restraints at one end.
- 3. A ha f-span which includes a bend and lies in a vertical plane must be
! g suppcrted at both ends--a horizontal, lateral support at the horizontal end
. and two orthogonal, lateral supports on the vertical end (see rule 14). i e
1 c-2 . 1
- - m ,-- ----
CARGENT O LUNDY ENGlNEER5 CMsCAGO APPENDIX C SL-3159 RE V. 1, 7 77 o 4. A straight, horizontal section of pipe which is less than 4/10 of the normal span in length requires no horizontal restraints. It is treated as a concentrated weight in its axial direction.
- 5. A horizontal section of pipe whose length exceeds 4/10 of the normal span must be restrained along its axis.
- 6. A half-span which contains a concentrated weight of less than 10% of the normal seismic-span weight should not exceed 40% of the normal-span length. It should be supported on one side with horizontal restraints.
- 7. A half-span which includes a concentrated weight of from 10% to 75% of the normal seismic-span weight must be supported on both ends with
] 8.
horizontal restraints. The length of a half-span which includes a concentrated weight of more tnan 75% but less than 250% of the normal seismic-span weight should not exceed 10% of the normal span (exclusive of the actual length of the
~ j concentrated weight). This half-span should be supported on both ends by
]O horizoatel suggerts.
)
] 9. A concentrated weight which exceeds 250% of the normal scismic-span weight should be supported directly, rather than by the piping to which it is attached. Horizontal support i.; required at the center of gravity.
] 10. In general, motor operators fo valves should be restrained in three
] orthogonal directions. For vertically mounted operators, only horizontal, .
lateral support is required. i 2
- 11. A half-span with a concentrated weight shou ~ not have a free end: hori- i 3 zontal, lateral support should be provided.
- 12. Supports not required by these rules alc Ed not be asca.
- 13. If the distance, between adjacent rigid is ngcts exceed- the normal seismic support span, vertical supports shoulc~ be added between these rigid
. hangers.
14.' 'As an alternative to rule 3, a half-span which includes an elbow may end at the elbow and be supported at a tangent point. O 1 l E I 1 ? 1
'1 w CARGENTQ LUNDY E N G 1 N E E C7 8 c .cac.o APPENDIX C SL-3159 REV.1, 7-29-77
'30 i.
TABLE C-1 REACTOR BUILDING RECOMMENDED SPANS FOR SEISMIC SUPPORTS 1 N O Al . N ORTH-SO U TH EAST-W EST \ ERTIC A L DI A M . Scil. SPAN LOAD SPAN LOAD SPAN LOAD 3/8
- 0. 9 q_ 7 1.25 7 1.25 4 1.0 1/2 160 10 16.75 9 9.50 6 15.5
- 5. og8a" s, e 3.0 e 4.25 e 4.50 3
3/4 160 11 14.25 11 22.0 7 24.0 Q 1 160 13 33.0 12 23.0 8 38.5 ' il 160 15 51.5 14 40.0 l 10 63.25 il 160 16 58.0 47.75 _15 10 79.25 ] 2 160 18 91.0 17 81.75 12 141.25 24 160 20 133.0 19 126.75 13 205.0 l 3 160 - 22 178.0 21 185.5 14 271.25 34 80XS 24 265.5 23 26i.0 15 317.75 4 120 26 441 24 299.5 16 423.25 UNITS: NOMINAL DIAMETER - IN. SPANS - FT. LOADS - LBS. I
- o .
C-4
f, CARGENTQLUNDY ENGINEERS APPENDIX C a ** ' ! SL-3159 REV.1. 7-29-77 1 b' TABLE C-2 TURBINE BL'ILDit!G RECOMMENDED SPANS FOR SEISMIC SUPPORTS r NOM. NORTH-SOUTH E AST-W EST DIAM . SCll. VERTICAL SPAN LOAD SPAN LOAD SPAN LOA { 0 9 3/8 5 0.75 6 1.75 4 1.0 1 1/2 160 7 8.25 8 15.75 5 8.0 5/8
- 0. 83 L 6 2.50 8 6.25 4 2.0 3/4 160 8 14.25 10 34.75 0 1 160 9 22.25 11 54.25 5 11.0 6 26.0 Il 160 10 33.25 13 84.75 7 41.5 11 160 11 46.75 14 114.0 8 59.0 2 160 13 77.0 15 105.0 9 98.75 21 160 14 117.75 17 214.75 10 146.5 3 160 16 187.08 19 357.0 11 243.75 34 80XS 17 195.0 20 321.5 12 244.0 4 120 18 289.0 ?2 6P" " 12 371.0 l
) i l i [ UNITS: NOMIN AL DIAMETER - IN. SPANS - FT. h LOADS - LHS. l r u e LO I . 1 i
- n. C-5 l J !
t T*' CARGENTQ LUNDY cuosuceno APPENDIX C SL-3159 REV.1. 7-29-77 h [] TABLE C-3 RHR COMPLEX RECOMMENDED SPANS FOR
, SEISMIC SUPPORTS r
NOM. N ORTH-SOUTH EAST-WEST DIAM. VERTICAL SCH. SPAN LOAD SPAN LOAD SPAN LOAD 3/8 0 49 L 5 0.75 6 1.50 6 1.00 1/2 160 7 8.25 8 18.0 7 9.50 0.083 5/8 7 2.50 8 5.25 8 3.25 3/4 160 8 14.0 9 26.5 9 16.5 1 160 10 22.0 11 46.75 10 25.75 14 160 11 34.75 12 ti8. 75 12 40.75 li 160 12 46.75 13 91.75 13 55.0 2 160 13 75.5 15 158.0 14 89.0 21 160 15 115.5 17 239.50 16 135.75 1 3 160 17 183.5 18 223.25 18 216.0 3i 80XS 18 191.5 20 394.0 19 225.0 4 - 120 19 294.5 21 582.0 , 20 333.5 i i UNITS: NOMINAL DIAMETER - IN. SPANS - FT.
] LOADS - LBS.
t o , C-6 l u e
._,. car 2 GENT O LUNDY E N GIN E E Rs APPENDIX C c .cao SL - 3159 REV.1. 7- 29 77 C-3 Sample Problem Following is an isometric of a system for which horizontal seismic restraint locations have been chosen according to the seismic support system design rules. The isometric is marked as required by the procedure and the worksheet is completed. Certain characteristics of the support system cannot be defined g without consideration of thermal expansion and anchor movements. These J include locations where snubbers rather than rigid restraints are to be used and preferred locations for axial restraints. ] The support description includes the end which is supported, the number of restraints and the restraint orientation. "B-2-liOR-LAT" means two horizontal, lateral supports are required at end B.
s Jo 3
] ] ]
} . J 1 1 } LO8 > C-7 l l
-- yg- ---- wm r n 1 M W &~ O' Y W & W % O O O fY W
,,. ;-=. N' =
! le e s?
/
l] :.8; 2s a
- s. .
es h ft fe,
'r ' F 4 a. z' , / ,,.
g'. /r l
/ 1 & M ny y
? ~@ OS *
@ r ~
9*2 2 --
'A ? A_ F,,
.. : cc\ ir =.
c F s ,, 160 lb. 2 ' ler.g g 3 0 f i (< P1 Y x* L_3 ,
, , FIPf SIZF: 2" M.F . 160 dP WT./FT.:
NORPAL SEl9tlL Str. 20 it. (Horizontal), g, t.0 Ft. (Verrfeal) NORMAL SPAN W ICPT: '90 l b.
- mm>
Qc==a ISOMETRIC FOR SAMPLE SEISMIC PROBLEM .mm Y -. G 2
=9 p o b 7 d
~;
f CARGENT' O LUNDY j ENGINEERS APPENDIX C , c mu.c." SL- 3159 REV.1. 7-29-77 p
'd SEISMIC SUPPORT SYSTEM -DESIGN WORKSHEET I
s l 5.P NORMAL SP/ N SUPPOR'l% S i l l' IHNii s N jN O. SPAN W EPdlT PlPING El,LMEN r 1)ESt:RIPflON A 18 1.ENilTil ItUI.IN t 'OM M I N IN Fixed at End A g i 20' 190 10. Vert. with 281b. valve B-2-l!OR-LAT 10' T- , 2 , Bend in Vertical Plane B-1-ilO R-L A I 3 f l 3 Plain Pipe ; i l l 4 ; Plain Pipe Il- 1 -llO R-i- A I I l l 5 Plain Pipe I l l 14 190 R-l. 41' l l j b Plain Pipe Ending at Elbow li- % \ l l 5 l j 3 ' 7 Plain hoc I LAT. Suppori at 7A Acts al Plain ISpc Endung ut Elbow ll- t -ilO R- LA I I,5 Axistly Plain Pipe Elbow in
, 9 Horizontal Plane I lbl-HOR-L AT g
10 j Plain Pipe Ends at Elbow 11- A Al 14,5 l l11 l Plain Pipe (vertical) l 2 l I /-~jl2 l f Section Ends at Tee l B-t-liOR-LA I 5' l 2 l l IJ Plain Pipe H-2-HOH-L A r 10' i ! i { g 14 Plain Pipe witti Lit >ow Il- 1 -ilOR-L A I 3 15 Plain Pipe 1 in Plain Pipe it-i-HOR-L AT I I; Pinin Pape I lia \ l les l'inin Pym l.'nel, nl 1.ltam li ? !!Oli 84 I 3. 5 u f 19 Plam ISpc l l l I h I 20 Pemt in Vertical Pirene it-I flor-l.? ! I n' 14 l l f 21 Plain Pipe 1 7' l 1 l l
- e. .iuiH. A i
' , Suppict Motor 22 l~ 160 lp. valve iH - HO R-L A T 4' ! 8,10
, Opere tor 2J '
f Plain Pipe Fixed at End 11 '- f 1
' 24 Plain Pipe Supported at End A '
l l l 10' I f
- l-llO;1-L A I ' '
25 l Plain Pipe (Ending at elbowl I- A X I 5' 5,14 l L
, %ertical Plain Pipe 26 Fased at End H
, 10' g,1 V(
h
~
C-9 Final j
CARGENTQLUNDY EN GIN E E R s APPENDIX D c nc^" SL-3159 FLEXIBILITY SUPPORT SYSTEM DESIGN REV. f, 7-29-77 D-1 Procedure O Starting at a convenient point (e.g., equipment nozzle, r structural anchor, header connection) traverse the entire .1 system once for each orthogonal direction of thermal move-ment, following the steps below for each successive pair of adjacent parallel (i.e., acting in the same direction) restraints. 1 i On the thermal worksheet, identify the restraint pair 1. , and direction, l
- 2. Determine the total expanding length of pipe in the restraint direction between the pair and enter it on the worksheet. If one of the restraints is a header or equipment nozzle with thermal movement in the restraint direction, enter this movement on the work-sheet.
I
- 3. From Table D-2, obtain the required offset based on I expanding length determined in step 2 and pipe size, and enter it on the thermal worksheet.. If one of the restraints is a header or equipment nozzle, .from Table i D-1 obtain the offset required based on thermal move-ment and nipe size, and enter it on the worksheet.
-O k 4. Determine the actual existing offset - total length of D-1
]
g gg g g g M M M M M h h h M M h M U \ O O O ; TABLE D-1 MINIMUM OFFSET NEAR NOZ ES WITH EXPANSION MOVEMEPE (*
!!ominal DEFLECTION, I NCH. lZ -
Diawster i Q'O In:h _1/4 y1 3/4 1 _1,- 11 1-1/2 1-3/4 2 2-1/4 2-1/2 . 3/8 (tube) 3ft 61n 4ft llin 6ft lin 7ft Oin 7ft loin Hft 71n 9ft 31n 9ft loin 10ft 61n lift Oin 1/2 3ft 111n 5ft 6in 6ft 91n 7ft 91n 8ft 9in 9ft 6in' 10ft 3in 11ft Oin llft 8in 12f t . 4in 5/6 (tuba) 4ft 2in 5ft 10'i r; 7ft 2in Oft 31n 9ft 3in 10ft lin 10ft llin lift 53in 12ft Sin 13ft lin 0 3/4 4ft 41n 7ft 61n 6ft 2i r: 8fs 91n 9ft 9in 10ft 8in 11ft 6in 12ft 41n 13ft Oin 13ft 91n 1 4ft loin 6ft lii: Bft 5in 9ft 91n 10ft 111n 11ft 111n 12ft 111n 13ft 91n 14ft 7in 15ft Sin $ 1-1/4 Sft 6in 7ft 9ir m3 9ft 61n 30ft 11in 12ft 32n 13ft Sin 14ft 61n 15ft 6in 16ft Sin 17ft 41n 2 O y 1-1/2 Sft loin Bft no m 3i-10ft 2in Ilft 91n 13ft !in 14ft 4in 15ft 61n 16ft '* in 17ft 6in l'Jf t 61D - 2 6ft 61n 9ft 3i 11tt 4in 13ft lin 14ft */ i n 16ft 'in 17ft 41n 18ft sin 19ft 7in 20ft Bin 2-1/2 7ft 2in 10ft 2. a r-12ft 6in 34ft 41n 16ft Iin 17ft 3in 19ft Oin 20ft lin 21ft 71n 22ft 91n *Cz 3 7ft 111, 11ft 3i- O 13ft 91n 15ft loin 17ft 9fn 19ft 5in 21ft Oin 22ft iin 23ft loin 25ft lin "< 3-1/2 Hft 6in 12f t Oi 14 sin 17ft Oin 19ft Oin 20ft 91n 22ft 61n 24ft 'in 25ft 61n 26ft loin 4 9ft nin 12ft 9i .Sft 7in left Oin 20ft ;in 22ft Oin 23ft loin 25ft ein 27ft Oin 28ft 61n (a)This is the minimum lenti th ni piae which is installed perpendicular to the Sirection of no zie move nent between the nozzle and the firsi. r. considered. traint wht-5 acts in that direction. Movements in three orthw onal directions are'
- D (/) >
M f~ T bk2 y eO i X
~
O T 0
mm-N W tomt N O M $ W W E U E E
)
O - O TABLE D-2 MINIMUM OFFSET REQUIRED TO ACCOMMODATE THERMAL EXPANSION OF PIPING, FEET EXPANDING LENGTH OF PIPE., FEET N)minal ,, Diam?ter, i; Inch f
! 10 15 20 25 30 b 35 40 45 50 I 3/8(tubs) 1*-11" 2'-9" 3*-4" 3'-1C" 4'-3" 4'-8" 5'-1" I 5'-5" 5'-9" 6'-1" 1/2 U 2'-2" 3'-0" 3'-8" 4*-3" 4'-9" 5'-3" 5'-8" 6'-1" 6*-5" 6'-9" M ;
5/8(tube) 2 ' - I 3'-3" 3'-11" 4'-6" 5'-1" 5'-7" 6'-0" > 6'-5" 6'-10" 7'-2" j ,3 'l 3/4 2'-5' 3 '-5 ' 4'-2" 4'-9" 1 2 0 m e 5'-4* 5'-10" 6'-4" 6*-9" 7*-2" '7'-7" s no Z u 1 2'-t' 3'-9" 4'-8" 5'-4" 6*-;" 6*-7" 7'-1" 7'-7" z_d 5 i 3'-C" 8'-5" g ,zg, ' 1-1/4 3'-;" 4'-3" 5'-2" 6'-O" 6'-3" 7'-4" 7'-11" On 8'-6" 9'-0" 9'-6" ah 1-1/2 3 -3* 4'-7' 5'-7" 6'-5" 7'-2" 7'-11" 8'-6" 9'-1" 9'-9"
*Z 10'-2" D =2 3'-7" 5'-1" 6*-3" 7*-2" 8'-5" 8'-10" '
9'-S" 10*-2" 10'-9" 11'-4" 2-1/2 3'-11" 5'-7" 6'-10" 7'-11" a*-10" 9'-9" 10'-5" 11'-2" 11*-10" 12'-6"
~
3 4*-4" 6'-2" 7'-7" 8'-9" 9'-9" 10*-8" 11'-7" 12'-4" 13'-1" 13'-10" 3-1/2 4'-8" 6 * - 7 8*-1" 9 '-4 " 1C'-5" 11'-5" 12'-4" 13'-2" 14*-0" 14'-9" 4 4'-11" 7'-0" 8'-7" 9'-11" 11'-1" 12'-1" 13'-1" 14'-0" 14'-10" 15'-8"
% (A > ,
m r" T
<lT l w rfl
. ~n 2 y=2 1 X ro T
u M
k CARGENTOLUNDY ENG1NEERS APPENDIX D c.ucaso SL-3159 1 pipe in the two directions perpendicular to the REV 1, 7-29-77 O ,I restraint direction between the restraint pair.
- 5. Check whether the actual offset exceeds the required offset. For restraint pairs with both expanding 1ength and header or equipment nozzle thermal movement, the actual offset must exceed the sum of the associated t required offsets. If the actual offset exceeds the
~I required offset, move onto the next restraint pair.
If the actual offset is less than the required offset, one of the rigid restraints must be changed to a snubber
~
and/or a variable hanger, or an expansion loop must be O erovided. cenere11 1 . cheneine the reetreine eve is preferred.
, 1 D-2 Sample Problem
~
I Replace w. snubber and S>rino l .
~
10' _ __ g JT .75 2 ' MA
, ,3. .
~
10 C_,L 15' anch >rF l /as 3. S' / D 2p EC i O~ .
. C .N change to snubber '
D-4
l. CARGENTC LUNDY APPENDIX D E N GIN E E R 5 CHICAGO SL-3159 REV. 1, 7-29-77 The above system will be checked for thermal flexibility; pertinent data will be entered on the thermal worksheet. The global X-direction will be considered first. Starting at the header, the first X-direction restraint pair is identified as A-C. The X-direction expanding length is the 10' from A to B; from Table D-2, the offset required for 10' is 5'1". The X-direction header movement of 0.25" must also be considered for restraint pair A-C - the offset required from Table D-1 is 6'6,". The amount of actual offset available (total length of pipe perpendicular to the X-direction) is the 10 f t. from B to C Since 10 f t. is less than the total 11'7" offset required, the C rigid i strut is changed to a snubber.
, i f Since the restraint at C is now a snubber, X-direction I restraint pair A-E is considered. The 25' (10' frcm A to B plus 15' from C1 to E) expanding length requires an 53'0" offset. The 0.25" header mcvement requitec 6'6". The }I total actual offset, 15 ', (i . e . , 10' from B to C plus 5' from C to C1) exceeds the total 14'6"~ required, thus accom-modating the X-direction thermal movement.
Considering thermal movement in the Y-direction, restraint pair A-B is examined first. Since there is no Y-direction i piping between A and B, no accommodation for piping expansion a l D-5
CARGENTQLUNDY E N G I N ER ERS APPENDIX D SL-3159 REV.1, 7-29 77
.O I is required. The Y-direction header movement at A, 0.75",
requires 11'4" of offset. The actual offset available is the 10' from A to B. Since 10' is less than the required 11'4", the rigid strut at B.- hich provided both weight support and seismic restraint - is replaced with a variable
' hanger at B and a Y-direction snubber in the immediate vicinity of B or C. Next, restraint pair A-D is checked.
'I The expanding 10 ' from B to C requires 5 '1" offset. The 0.75" Y-direction header movement requires 11'4". The existing
. offset, 17' (i.e., 10' from A to B plus 5' from C to Cl plus
.10 2' from Cl to D) exceeds the total offset required, 16'5", and is therefore adequate. Regarding restraint pair D-E, no l l d Y-direction anchor movement or piping e xpansion exists. Ig Regarding Z-direction movement, restraint pair A-D is l -3 i considered. The 1.5" header movement requires a 16'0" offset. The 5' run from C to Cl requires a 3'7" offset. The 22' ] actual offset exceeds the total rcquit re ef fect and is there- [ fore adequate. Regarding the D-E restraint pair, no Z-direc-tion movement or piping expansion exists. J o a k n-6
CARGENTO LUNDY NEERS APPENDIX D E N Gj,g SL-3159 RE V. 1, 7-29-77 THERMAL EXPANSION WORKSHEET Restraint Expanding Nozzle Required Actual Pair Dir. Length,ft. Movement,in. Offset, ft. Offset,ft. Recommendation A-C X 10 25 5'1" 6'6" 10 Change to snubber A-E X 25 .25 8'0" 6'6" 15 ok A-B Y 0 .75 0 11'4" 10 Replace w, snubber and spring A-D Y 10 .75 5'1" 11'4" 17 ok D-E Y 0 0 0 0 13 I A-D Z 5 1.5 3'7" 16'0" 22 ok ok D-E Z 0 0 0 0 13 ok 10 J-I
~I J
l 1 No 1
. D-7 Final E .
CARGENT O LUNDY ENGlNEE20 CHICAGO APPENDIX E SL-3159 N f (o REV.1, 7 77 SMALL PIPING DESIGN WORK SHEETS sI WEIGHT SUPPORT SYSTEM DESIGN WORKSHEET 'l I Sm NO SPAN ee-LOAD e1P1- E-DESCRIPTION e-A b eTEe LENGTH Deem. RULED i I LI ,1 i l
- 10 I
I 1 , j , me -M-- wg _ ; I o Il m\ p E-1
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*"'*** APPENDIX E SL-3159 REV.1. 7-29-77 THERMAL EXPANSION WORKSHEET I Restraint Pair Dir.
Expanding Length, ft . Nozzle Movement, in. Required Offset, ft. Actual Offset , ft . Recommendation 1 1 1 1 _le
- I o
E-3 l- Final
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l EF- 2-FS AR TABLE 3.7-8 REACTOR / AUXILIARY BUILDING PROBABLE MAXIMUM DISPLACEMENTS Horizontal Displacements, " ft OBE SSE Mass X-Excit. Y-Excit. X-Excit. Y-Excit. No. X-Disp 1.,ft_ Y-Disp 1.,ft X-Disp 1.,ft Y-Disp 1.,ft 1 0.00110 0.00095 0.00157 0.00136 2 0.00257 0.00245 0.00366 0.00349 3 0.00376 0.00260 0.00535 0.00469 4 0.00430 0.00376 0.00611 0.00534 5 0.00483 0.00340 0.00686 0.00594 6 0.03502 0.03240 0.05082 0.04623 7 0.00149 0.00117 0.00209 0.00164 8 0.00330 0.00143 0.00465 0.00201 9 0.00491 0.00500 0.00692 0.00705 10 0.03500 0.02780 0.05080 0.04040 11 0.00490 0.00310 0.00689 0.00465 12 0.00070 0.00040 0.00094 0.00060 13 0.00110 0.00070 0.00157 0.00102 14 0.00250 0.00160 0.00357 0.00252 15 0.00310 0.00210 0.00436 0.00322 16 0.00380 0.00270 0.00536 0.00419 17 0.00430 0.00320 0.00610 0.00485 18 0.00480 0.00390 0.00689 0.00600 19 0.00090 0.00060 0.00126 0.00086 20 0.00150 0.00100 0.00208 0.00152
' 21 0.00220 0.00160 0.00314 0.00238 22 0.00260 0.00190 0.00371 0.00284 23 0.00310 0.00220 0.00441 0.00341 24 0.00380 0.00270 0.00536 0.00419 25 0.00420 0.00300 0.00602 0.00466 26 0.00440 0.00320 0.00625 0.00483 27 0.00490 0.00350 0.00698 0.00539 28 0.00100 0.00060 0.00140 0.00097 29 0.00140 0.00090 0.00212 0.00164 30 0.00180 0.00120 0.00263 0.00200 31 0.00290 0.00190 0.00409 0.00306 32 0.00380. 0.00270 0.00540 0.00415 Floor Vertical Displacement (a)
Elevation OBE SSE Elev. 583 ft, 6 in. 0.00013 0.00020 (1st Floor) Elev. 613 ft, 6 in. 0.00026 0.00039 (2nd Floor) Elev. 641 ft, 6 in 0.00035 0.00052 (3rd Floor) Elev. 659 ft, 6 in 0.00039 0.00057 (4th Floor) Elev. 684 ft, 6 in. 0.00044 0.00064 (5th Floor) O (a, Displacements are relative to the base of the structure. l 3.7-75 I .
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. FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-84 l
._ . VERTICAL RESPONSE SPECTRA OPERATING BASIS EARTHOUAKE RE ACTOR O,
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UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-57 HORIZONTAL FLOOR RESPONSE SPECTRA SAFE SHUTDOWN EARTHOUAKE ELEVATION - 583*-6" O- (SLAB NO.1) KEACTOR/ AUXILIARY BUILDING EAST - WEST COMPONENT SARGENT & LUNDY REPORT NO. SL-2682
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, UNIT 2 FINAL SAFETY ANALYSIS REPORT FIGURE 3.7-56
.. HORIZONTAL FLOOR RESPONSE SPECTRA SAFE SHUTDOWN EARTHQUAKE ELEVATION - 583'-6
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l ENRICO FERMI ATOMIC POWER PLANT UNIT 2 l \ FINAL RAcf.TY ANALYSIS REPORT FIGURE 3.7-85 l
-- - VERTICAL RESPONSE SPECTRA OPERATING BASIS EARTHOUAKE REACTOR BUILDING l l O'- SLAB EL. 641'- 6", 659'- 6" & 684*-6" !
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