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{{#Wiki_filter:.' | {{#Wiki_filter:.' | ||
Enclosure 2 C ! | Enclosure 2 C ! | ||
MEETING AGENDA , | MEETING AGENDA , | ||
OYSTER CREEK CORE SPRAY SPARGER REPLACEMENT APRIL 15, 1981 , | OYSTER CREEK CORE SPRAY SPARGER REPLACEMENT APRIL 15, 1981 , | ||
\ | \ | ||
I. INTRODUCTION JIM KNUBEL (JCP&L) | I. INTRODUCTION JIM KNUBEL (JCP&L) | ||
A',' HISTORY B'.' MEETING OBJECTIVES II. DESIGN | A',' HISTORY B'.' MEETING OBJECTIVES II. DESIGN | ||
Line 33: | Line 27: | ||
==SUMMARY== | ==SUMMARY== | ||
. JAY ERBES (G.E.) | . JAY ERBES (G.E.) | ||
A. DESIGN CRITERIA B'.' REPLACEMENT DESCRIPTION III. STRUCTURAL DESIGN JIM CHARNLEY (G.E.) | A. DESIGN CRITERIA B'.' REPLACEMENT DESCRIPTION III. STRUCTURAL DESIGN JIM CHARNLEY (G.E.) | ||
A. STATIC ANALYSIS B. DYNAMIC ANALYSIS C. DYNAMIC RESPONSE TESTING IV. REACTOR PERFORMANCE JIM OATES (G.E.) - | A. STATIC ANALYSIS B. DYNAMIC ANALYSIS C. DYNAMIC RESPONSE TESTING IV. REACTOR PERFORMANCE JIM OATES (G.E.) - | ||
~ | ~ | ||
Line 48: | Line 39: | ||
B 2 05 350oo (VI . | B 2 05 350oo (VI . | ||
.~ OYSTER CREEK CORE SPRAY SPARGER REPLACEMENT l l | |||
HISTORY 1978 - | |||
.~ OYSTER CREEK CORE SPRAY SPARGER REPLACEMENT l | |||
1978 - | |||
1 CRACK DISCOVERED BY VISUAL INSPECTION 1980 - | 1 CRACK DISCOVERED BY VISUAL INSPECTION 1980 - | ||
MULTIPLE CRACKS DISCOVERED BY IMPROVED VISUAL TECHNIQUES AND UT, ... | MULTIPLE CRACKS DISCOVERED BY IMPROVED VISUAL TECHNIQUES AND UT, ... | ||
JCP&L SUBMITTAL SUGGESTED SPARGER REPLACEMENT WITHIN 2 REFUELING CYCLES NRC SER REQUIRED REPLACEMENT WITHIN 1 CYCLE OCT 1980 - | |||
JCP&L AND NRC STAFF MEETING MAR 1981 - | |||
JCP&L SUBMITTAL SUGGESTED SPARGER REPLACEMENT WITHIN 2 REFUELING CYCLES | |||
NRC SER REQUIRED REPLACEMENT WITHIN 1 CYCLE OCT 1980 - | |||
JCP&L AND NRC STAFF MEETING | |||
MAR 1981 - | |||
JCP&L SUBMITTAL TO NRC APR 1981 - | JCP&L SUBMITTAL TO NRC APR 1981 - | ||
JCP8L AND NRC MEETING | JCP8L AND NRC MEETING | ||
. JK-1 4/15/81 | . JK-1 4/15/81 | ||
0YSTER CREEK CORE SPRAY SPARGER REPLACEMENT | 0YSTER CREEK CORE SPRAY SPARGER REPLACEMENT | ||
~ | ~ | ||
MEETING OBJECTIVES | MEETING OBJECTIVES | ||
; | ; | ||
: 1. CONCURRENCE WITH DESIGN QUALIFICATION PROGRAM e- APPLICABLE CODES i e ANALYTICAL SUPPORT e TEST PROGRAM ! | : 1. CONCURRENCE WITH DESIGN QUALIFICATION PROGRAM e- APPLICABLE CODES i e ANALYTICAL SUPPORT e TEST PROGRAM ! | ||
i II. ESTABLISH REQUIRED DOCUMENT SUBMITTALS o PRELII:! NARY MODIFICATION REPORT (3/81) e FINAL MODIFICATION REPORT (10/81) i III.- ESTABLISH SCHEDULE OF PRESENTATIONS e CORE SPRAY TESTS RESULTS (9/81) | |||
IV. DISCUSS PRELIMINARY MODIFICATI0ll REPORT Y | |||
i II. ESTABLISH REQUIRED DOCUMENT SUBMITTALS | JK-;l 4/15/81 | ||
o PRELII:! NARY MODIFICATION REPORT (3/81) e FINAL MODIFICATION REPORT (10/81) | |||
i | |||
III.- ESTABLISH SCHEDULE OF PRESENTATIONS e CORE SPRAY TESTS RESULTS (9/81) | |||
IV. DISCUSS PRELIMINARY MODIFICATI0ll REPORT | |||
OYSTER CREEK . | OYSTER CREEK . | ||
\ | \ | ||
f ~0VERHEAD CORE SPRAY SPARGER | f ~0VERHEAD CORE SPRAY SPARGER l | ||
DESIGN CRITERIA I. SYSTEM e 2,45 GPM/ BUNDLE e DUAL SYSTEMS - 100% REDUNDANCY-e i1Ih! MUM IMPACT ON EXISTING IllTERtlALS AND REACTOR OPERATI0tlS e ONE SPRAY N0ZZLE PER 4 BUNDLES II. APPLICABLE CODES s ASME SECTION XI s ASME SECTION III, Sil3SECTI0tl flG AS DESIGN GUIDE e SAFETY ESSENTIAL, 10CFR21 APPLIES III, MECHANICAL - | |||
e WATER SUPPLIED THROUGH EXISTING REACTOR PRESSURE VESSEL t!0ZZLES e REMOVA3LE FOR REFUELING AND INSPECTI0tl e MATERIAL - TYPE 316 (L) OR 304 (L) ' | |||
f.'02% MAX, CARBON JGE - 1 4/15/81 | |||
I. SYSTEM e 2,45 GPM/ BUNDLE | |||
e DUAL SYSTEMS - 100% REDUNDANCY-e i1Ih! MUM IMPACT ON EXISTING IllTERtlALS AND REACTOR OPERATI0tlS e ONE SPRAY N0ZZLE PER 4 BUNDLES | |||
II. APPLICABLE CODES s ASME SECTION XI | |||
s ASME SECTION III, Sil3SECTI0tl flG AS DESIGN GUIDE | |||
e SAFETY ESSENTIAL, 10CFR21 APPLIES III, MECHANICAL - | |||
e WATER SUPPLIED THROUGH EXISTING REACTOR PRESSURE VESSEL t!0ZZLES | |||
e REMOVA3LE FOR REFUELING AND INSPECTI0tl e MATERIAL - TYPE 316 (L) OR 304 (L) ' | |||
f.'02% MAX, CARBON JGE - 1 | |||
4/15/81 | |||
e ', 1 I N ' | e ', 1 I N ' | ||
ww & | ww & | ||
OJ C I N e | OJ C I N e | ||
Line 141: | Line 72: | ||
e ,e .:rN ; | e ,e .:rN ; | ||
>- i. . g | >- i. . g | ||
. g . | . g . | ||
l , CD7 | l , CD7 | ||
Line 150: | Line 80: | ||
* \' ) < | * \' ) < | ||
%W Scv d | %W Scv d | ||
i | i t: | ||
t: | |||
- d | - d | ||
/ . E t m E / f' ,.d: - o | / . E t m E / f' ,.d: - o | ||
: a. w y h- | : a. w y h-a 50 i m .. | ||
e a-cs a5 w "5 s* =e s ae En n | |||
a 50 i m .. | |||
e a-cs a5 | |||
w "5 s* =e s | |||
ae En | |||
n | |||
e , | e , | ||
k a | k a | ||
C N c 25 | C N c 25 E N' 0* | ||
5 % / s Y | 5 % / s Y | ||
- =- | - =- | ||
wA E 5 / 9' , | wA E 5 / 9' , | ||
$E j | $E j | ||
/ | / | ||
E_ _ . | E_ _ . | ||
km # | km # | ||
s . _., | |||
g g g . - | g g g . - | ||
E o | E o | ||
Line 194: | Line 107: | ||
mu | mu | ||
* .. Nq- | * .. Nq- | ||
< x vg- | < x vg- | ||
. W i | . W i | ||
E, g- . | E, g- . | ||
J I | J I | ||
OVERiiEAD CORE SPRAY SYSTEM - PLAN VIEW I l | |||
OVERiiEAD CORE SPRAY | |||
SYSTEM - PLAN VIEW | |||
I l | |||
/ , | / , | ||
/ | / | ||
w-til bl t-ws 1 - | w-til bl t-ws 1 - | ||
's k III' | 's k III' | ||
* 7 llll | * 7 llll | ||
,A _ | ,A _ | ||
Y .- -- . | Y .- -- . | ||
,'f e x_ w i..r. $_ /fi . | ,'f e x_ w i..r. $_ /fi . | ||
x,. . .'. td- ' | x,. . .'. td- ' | ||
ry x r r 7, 4* | ry x r r 7, 4* | ||
6 | 6 | ||
[ b% &' | [ b% &' | ||
, %_1 | , %_1 I'l n | ||
I'l n | |||
+. | +. | ||
f | f | ||
.e -- | .e -- | ||
i y | i y | ||
e e. | e e. | ||
7 | 7 t | ||
t | |||
- v.m L . - . L- .. | - v.m L . - . L- .. | ||
M;J Qg i s OW % A 6i .V Zs . .i D' ~4i _ ___.N(\, | M;J Qg i s OW % A 6i .V Zs . .i D' ~4i _ ___.N(\, | ||
. x Ma - | . x Ma - | ||
- -'hmn_ __,hwA*I51 _ - | - -'hmn_ __,hwA*I51 _ - | ||
g h - V 4 * ~n-- m'~__ _- -Myt f -_ ;n ' ' M } | g h - V 4 * ~n-- m'~__ _- -Myt f -_ ;n ' ' M } | ||
z i . ~ | z i . ~ | ||
_i SJ t . x-> .iWi i v,._ s j . | _i SJ t . x-> .iWi i v,._ s j . | ||
.; _. _ . | .; _. _ . | ||
.~ ;_ __ h_ | .~ ;_ __ h_ | ||
i i In y i- +vymw,, a-., u | i i In y i- +vymw,, a-., u I-wiui | ||
I- | |||
wiui | |||
~ | ~ | ||
i i v v_mg . ,t-m r, | i i v v_mg . ,t-m r, | ||
,w_ ;g~mu O, . 7, d _O i - , | ,w_ ;g~mu O, . 7, d _O i - , | ||
t_*-- | t_*-- | ||
%vi du i | %vi du i | ||
. .,_,.j , | . .,_,.j , | ||
/ S Ul N N_ ! SM en D4 yyu w- | / S Ul N N_ ! SM en D4 yyu w- | ||
Line 276: | Line 152: | ||
a-pn , p 3 e,_ / @ c .; | a-pn , p 3 e,_ / @ c .; | ||
,,v..__.-, | ,,v..__.-, | ||
i =. w m i g | i =. w m i g | ||
i | i | ||
Line 285: | Line 160: | ||
5 - | 5 - | ||
hi - | hi - | ||
DISTRIBUTION PIPES T, CD' Gb \ | DISTRIBUTION PIPES T, CD' Gb \ | ||
g L. WATER INLET vs l | g L. WATER INLET vs l | ||
[ | [ | ||
t | t | ||
\f SPARGER HEADER SUPPORT " TRUSS"- . | \f SPARGER HEADER SUPPORT " TRUSS"- . | ||
SUPPORT RING - SPRAY H0ZZLES | SUPPORT RING - SPRAY H0ZZLES | ||
= | = | ||
3/81 | 3/81 | ||
t .O SPARGER PIPING - ONE SYSTEM a e | |||
t .O | |||
SPARGER PIPING - ONE SYSTEM a e | |||
S f | S f | ||
C e | C e | ||
Line 309: | Line 175: | ||
- .e. | - .e. | ||
p., | p., | ||
.. -- 1 f | |||
.. -- 1 | |||
f | |||
-3 -- -- 1 | -3 -- -- 1 | ||
. y ,, y -- | . y ,, y -- | ||
- ; | - ; | ||
8 l 6- -- -- , | 8 l 6- -- -- , | ||
j | j | ||
== -- | == -- | ||
== | == | ||
i i- -S-unapu ps.- | |||
i i- -S- | |||
unapu ps. | |||
.. ,- yQ -- | .. ,- yQ -- | ||
O. | O. | ||
ta O' 3 r | ta O' 3 r | ||
.- A + y- -T- I | .- A + y- -T- I | ||
- y -- I. | - y -- I. | ||
i Y i 4 | |||
i | |||
Y i 4 | |||
l | l | ||
" O., (A C.- /-a e-v s | " O., (A C.- /-a e-v s y-4 l | ||
y- | |||
4 l | |||
4- .a -- Q J @ = 2 T ' | 4- .a -- Q J @ = 2 T ' | ||
i A Y Y | i A Y Y y | ||
7 w | |||
w | |||
\ | \ | ||
, .cD.\ | , .cD.\ | ||
V i | V i | ||
i | i | ||
* I 6 | |||
* I | JGEe+ | ||
k,.r.) 8., | k,.r.) 8., | ||
1 i | |||
1 | |||
i | |||
SPARGER PIPING - BOTH SYSTEMS | SPARGER PIPING - BOTH SYSTEMS | ||
?. _- ._ | ?. _- ._ | ||
-9 2 | -9 2 | ||
- gl s m | - gl s m | ||
. I, | . I, Ai A w s of"% | ||
Ai | |||
A w s | |||
of"% | |||
y Au% | y Au% | ||
9 __ | 9 __ | ||
_. w __ ,, w. | _. w __ ,, w. | ||
7__ __ __ __ | 7__ __ __ __ | ||
.L __ __ __ | .L __ __ __ | ||
A | A e | ||
e | |||
6 e v | 6 e v | ||
_-_ __ __ __ __ __ w | _-_ __ __ __ __ __ w a cy c a p 4,) ,m, . | ||
a cy c a p 4,) ,m, . | |||
_-_ _y_ | _-_ _y_ | ||
/ __ __ __ __ Q | / __ __ __ __ Q | ||
-+. | -+. | ||
A A | |||
A | |||
A | |||
A - ,~ ,~ Al e e y __ | A - ,~ ,~ Al e e y __ | ||
y, __ | y, __ | ||
Line 465: | Line 226: | ||
s- __ | s- __ | ||
y __ | y __ | ||
y | y y | ||
y | |||
__ __ __ __ _.I_ | __ __ __ __ _.I_ | ||
k I A e y y AN e e e e | |||
k I A e y y AN e e e | |||
e | |||
__ k_ _' | __ k_ _' | ||
e e | |||
e | e | ||
__ . __ _,_ __ y L, - ey Ly = | |||
__ . __ _,_ __ y | |||
L, - ey Ly = | |||
s ay e' - | s ay e' - | ||
__ __ _-_ __ .I __ | __ __ _-_ __ .I __ | ||
Ak c | Ak c | ||
#k y w &% | #k y w &% | ||
y e | |||
y | &k e | ||
e | |||
&k | |||
e | |||
= b __ | = b __ | ||
& __ .g. __ .g. _ | & __ .g. __ .g. _ | ||
Line 515: | Line 244: | ||
e f. | e f. | ||
g __ | g __ | ||
M MN #A W Y C W 7 b' | M MN #A W Y C W 7 b' | ||
$l T i __ __ __ | $l T i __ __ __ | ||
* | * | ||
* T Y A A 1 | * T Y A A 1 r l | ||
_d | _d | ||
, I . | , I . | ||
N | N | ||
- __ A __ I - | - __ A __ I - | ||
c' t::;' A ::: | c' t::;' A ::: | ||
- 4- - | - 4- - | ||
- - 5y g .. | - - 5y g .. | ||
7 _ | 7 _ | ||
3 | 3 | ||
.g. . | .g. . | ||
JGE -5 | JGE -5 | ||
> '8.1 k'/_l.~/ | > '8.1 k'/_l.~/ | ||
~ | ~ | ||
i OVERilEAD CORE SPRAY SPARGER , | |||
OVERilEAD CORE SPRAY SPARGER , | |||
SUPPORT STRUCTURE 1 | SUPPORT STRUCTURE 1 | ||
t | t 1 | ||
1 | |||
SUPPORT BEAMS | SUPPORT BEAMS | ||
) l 3l | |||
) l | |||
3l | |||
/ ' | / ' | ||
p , | p , | ||
d | d g | ||
h. | |||
1 i= | |||
1 | |||
i= | |||
w(p . . | w(p . . | ||
l . | l . | ||
. SUPPORT RING .. | . SUPPORT RING .. | ||
i . | i . | ||
l . | l . | ||
G 8 | |||
W . | |||
N 1 | N 1 | ||
SPARGER SUPPORT STRUCTURE PLAN VIEW | SPARGER SUPPORT STRUCTURE PLAN VIEW | ||
~ | ~ | ||
SHROUD HEAD | SHROUD HEAD | ||
.e # ~g, ATTACHMENT LUGS l ' | .e # ~g, ATTACHMENT LUGS l ' | ||
j i I | j i I | ||
# i i | # i i | ||
'I SUPPORT | 'I SUPPORT 7 1 : i o j j RING i | ||
7 1 : i o j j RING i | |||
'l | 'l | ||
- j i . | - j i . | ||
.. s l :' | .. s l :' | ||
' l ! ALIGNMENT I i PLATES J_ t ! - | ' l ! ALIGNMENT I i PLATES J_ t ! - | ||
, { I | , { I F | ||
i | |||
; | ; | ||
; | ; | ||
i E , | i E , | ||
i i | i i | ||
! i | ! i 1 i l | ||
1 i l | |||
; | ; | ||
! i | ! i i , | ||
i , | |||
i ! | i ! | ||
' f ! | ' f ! | ||
h , _ | h , _ | ||
'k i h l / | 'k i h l / | ||
; | ; | ||
L SUPPORT 1 | |||
L | |||
SUPPORT 1 | |||
! j l i BEAMS W. '' | ! j l i BEAMS W. '' | ||
_ a ' | _ a ' | ||
! i | ! i J | ||
J | |||
1 JGE - 7 f4/15/31 | 1 JGE - 7 f4/15/31 | ||
N0ZZLE ARRANGEMENT . | N0ZZLE ARRANGEMENT . | ||
{ | { | ||
; | ; | ||
I u -_ ,I '~c h. ! | I u -_ ,I '~c h. ! | ||
d s_ 1 s - , ,,g , , | d s_ 1 s - , ,,g , , | ||
Line 691: | Line 321: | ||
/ CRUCIFORM ORIFICE 1 IN. PIPE | / CRUCIFORM ORIFICE 1 IN. PIPE | ||
;\ | ;\ | ||
3h IN. PIPE N0ZZLE 1 | 3h IN. PIPE N0ZZLE 1 | ||
s . | s . | ||
10.5 0 | 10.5 0 | ||
\ - . | \ - . | ||
" TARGET SURF ACE | " TARGET SURF ACE 1 i i | ||
1 i i | |||
JGE - 8 | JGE - 8 | ||
!4/15/81 | !4/15/81 | ||
N SOPPORTRING l l | |||
SHROUD ' | |||
,cHEAD J'94 ^ v ;3 N \\w DISCONNECT x w'[= | |||
N SOPPORTRING l | |||
,cHEAD | |||
J'94 ^ v ;3 N \\w DISCONNECT x w'[= | |||
g | g | ||
.= | .= | ||
M 5 1 | M 5 1 | ||
-W | -W | ||
'R - | 'R - | ||
gre | gre mm TOP GUIDE h:fV 2 N . | ||
mm TOP GUIDE | |||
h:fV 2 | |||
N . | |||
f | f | ||
\ | \ | ||
JGE-9 4/15/81 | JGE-9 4/15/81 | ||
f i | f i | ||
\ | \ | ||
a | a | ||
/) | /) | ||
w | w | ||
<> s V/ " - | <> s V/ " - | ||
- I 5 4 | - I 5 4 | ||
E | E | ||
. THERMAL SLEEYE , I j bl = | . THERMAL SLEEYE , I j bl = | ||
b | b (um h~ | ||
s l l | |||
(um h~ | |||
s | |||
l l | |||
% h | % h | ||
- VESSEL WALL - - | - VESSEL WALL - - | ||
Line 779: | Line 358: | ||
\ | \ | ||
+ | + | ||
l f _ CONNECTOR y$ | |||
l f _ CONNECTOR | 4 F. | ||
? l rs . | |||
y$ | |||
4 | |||
F. | |||
? l | |||
rs . | |||
/ | / | ||
s - | s - | ||
Line 799: | Line 366: | ||
/ | / | ||
/j Saa0un a | /j Saa0un a | ||
} | } | ||
t / | t / | ||
/ | / | ||
"s. 4 Q b,/ | |||
"s. 4 | |||
Q b,/ | |||
V - | V - | ||
y 1 | |||
y | *\'w 7 | ||
e y / ,, | |||
1 | |||
*\'w | |||
y / ,, | |||
7- JGE -10 | 7- JGE -10 | ||
,/ v15/81 | ,/ v15/81 | ||
/ j/ , | / j/ , | ||
DIVERTER . | DIVERTER . | ||
f.' \ | f.' \ | ||
/l - | /l - | ||
~ | ~ | ||
SHROUD FLANGE | SHROUD FLANGE WATEREXII' | ||
WATEREXII' | |||
[-(3- | [-(3- | ||
. ,/ . | . ,/ . | ||
/ !s | / !s s | ||
5 , | |||
N W | N W | ||
SPRING 1 -~ i / | SPRING 1 -~ i / | ||
N | N | ||
, u- - | , u- - | ||
2 s | 2 s | ||
(1 s B-s ev- s y : _,, | |||
(1 s B- | |||
s ev- s y : _,, | |||
N_.Q) i I ; s . | N_.Q) i I ; s . | ||
~ | ~ | ||
."-). : -~T~'; * . | ."-). : -~T~'; * . | ||
Y. /// w | Y. /// w | ||
.- i- ,t_ b ]n_____ _ . _ _ __ _. ,_ A hN\\h | |||
.- i- ,t_ b ]n_____ _ . _ _ __ _. ,_ A | |||
hN\\h | |||
'); | '); | ||
'l f - | 'l f - | ||
s- ' | s- ' | ||
(' p ' | (' p ' | ||
i | i | ||
- DISCONNECT FLANGE | |||
- DISCONNECT | |||
FLANGE | |||
. . i , | . . i , | ||
8 | 8 | ||
/ | / | ||
n | n | ||
~ | ~ | ||
JGE -11 1 | JGE -11 1 4/15/81 i | ||
4/15/81 i | |||
1 | 1 | ||
/'/ .. | /'/ .. | ||
e . | e . | ||
] | ] | ||
TEE BOX HOLE PLUG | TEE BOX HOLE PLUG I | ||
e I | |||
I | |||
- , e | - , e | ||
) SEAL RING | ) SEAL RING | ||
/ | / | ||
e B | e B | ||
S RERIE . | |||
S | |||
RERIE | |||
. | |||
WW8N ..Oe em L | WW8N ..Oe em L | ||
1 - | 1 - | ||
a - | a - | ||
e f . . . == .:I s | |||
f . . . == .:I s | |||
\ % | \ % | ||
3 I | |||
i . | |||
3 | |||
JGE -12. | JGE -12. | ||
l l 4/15/81 | l l 4/15/81 | ||
HOLE PLUG RETAINER PLATE 1 | HOLE PLUG RETAINER PLATE 1 | ||
p e | p e | ||
/ N | / N | ||
/ \ | / \ | ||
/ \ | / \ | ||
/ | / | ||
7 | 7 ase p | ||
ase p | |||
\ | \ | ||
/ . | / . | ||
[ ,.... | [ ,.... | ||
1 | 1 | ||
$ . -w. . | $ . -w. . | ||
v.sa4 / i | |||
\ | \ | ||
,/ | ,/ | ||
/. | /. | ||
\/ s / | \/ s / | ||
\. , | \. , | ||
,/ | ,/ | ||
; | ; | ||
!lf////// /l \/ h l*'ffYf k | !lf////// /l \/ h l*'ffYf k | ||
~ | ~ | ||
b. | b. | ||
JGE - 13 4/15/81 | JGE - 13 4/15/81 | ||
e | e | ||
. 0YSTER CREEK CORE SPRAY SPARGER REPLACEMENT 4 | |||
. 0YSTER CREEK CORE SPRAY SPARGER REPLACEMENT | |||
4 | |||
~ | ~ | ||
. STRUCTlJRAL DESIGN - | . STRUCTlJRAL DESIGN - | ||
CORE SPRAY SPARGER AND CORE SPRAY LINE | CORE SPRAY SPARGER AND CORE SPRAY LINE | ||
. A. STATIC ANALYSIS . | . A. STATIC ANALYSIS . | ||
~ | ~ | ||
B'. DYNAMIC ANALYSIS . | B'. DYNAMIC ANALYSIS . | ||
: C. DYNA!ilC FESPONSE TESTING e g . | : C. DYNA!ilC FESPONSE TESTING e g . | ||
* e | * e s . , | ||
s . , | |||
* e e | * e e | ||
e | e | ||
* e E . | * e E . | ||
e | e | ||
. . Tee -I l 4/IS/BI | . . Tee -I l 4/IS/BI | ||
\ | \ | ||
; | ; | ||
STATIC ANALYSIS SIZING | |||
STATIC ANALYSIS | |||
SIZING | |||
-A. . | -A. . | ||
DRAG COEFFICIENT = 1 | DRAG COEFFICIENT = 1 | ||
. LIFT COEFFICIENT = 1 . | . LIFT COEFFICIENT = 1 . | ||
. DAMPING = 2% | . DAMPING = 2% | ||
EXCITATION FREQUENCY = NATURAL FREQUENCY | EXCITATION FREQUENCY = NATURAL FREQUENCY | ||
' PPLIED A LOAD = 25 TIES HYDRAULIC LOAD ALTERNATING STRESS <10 KSI B'. ' DEAD WEIGHT - - | |||
' PPLIED A LOAD = 25 TIES HYDRAULIC LOAD ALTERNATING STRESS <10 KSI | |||
B'. ' DEAD WEIGHT - | |||
- . C. THERMAL' | - . C. THERMAL' | ||
' ~ | ' ~ | ||
D. SEISMIC 4 | |||
D. SEISMIC | 4 m.; | ||
4 | |||
4 | |||
m.; | |||
4/i5g1 | 4/i5g1 | ||
. SPARGER DYllAMIC Ai1ALYSIS : | . SPARGER DYllAMIC Ai1ALYSIS : | ||
~ A. MATHEllATICAL MODEL . . | ~ A. MATHEllATICAL MODEL . . | ||
. . 1332 DEGREES OF FRF.EDOM . | . . 1332 DEGREES OF FRF.EDOM . | ||
LOWEST NATURAL FREQUEllCY = 42 HZ DAMPIllG = 1.5% ~ | |||
LOWEST NATURAL FREQUEllCY = 42 HZ | |||
DAMPIllG = 1.5% ~ | |||
~ | ~ | ||
-B'.' H'YDRAULIC FORCE FLUCTUATING LIFT COEFFICIENT = .2 CYLINDERS - | |||
-B'.' H'YDRAULIC FORCE | = 1.0 PLATES APPLIED SIPULTAt1E0VS TO ALL NODES IN PHASE | ||
FLUCTUATING LIFT COEFFICIENT = .2 CYLINDERS - | |||
= 1.0 PLATES | |||
APPLIED SIPULTAt1E0VS TO ALL NODES IN PHASE | |||
, PREDICTED VORTEX SHEDDING FREQUENCY | , PREDICTED VORTEX SHEDDING FREQUENCY | ||
=.13HZ(3-1/2." PIPE 5) | =.13HZ(3-1/2." PIPE 5) | ||
= 10 HZ (5" PIPES) | = 10 HZ (5" PIPES) | ||
= 11 HZ (1.5" BEAMS) | = 11 HZ (1.5" BEAMS) | ||
APPLIED FREQUEf1CY = 5, 10, 13, 15, 20, 25, 30, 35, 40 | APPLIED FREQUEf1CY = 5, 10, 13, 15, 20, 25, 30, 35, 40 | ||
. AtlD AT 5 LOWEST NATURAL FREQUENCIES . | . AtlD AT 5 LOWEST NATURAL FREQUENCIES . | ||
.'C. | .'C. | ||
~ | ~ | ||
CRITERIA . | CRITERIA . | ||
ALTERNATIf1G STRESS 4 10 KSI | ALTERNATIf1G STRESS 4 10 KSI | ||
* ' ' JeZ-3 4/Elal | |||
* ' ' JeZ-3 | |||
4/Elal | |||
LINE DYNAMIC ANALYSIS f | |||
LINE DYNAMIC ANALYSIS | |||
A. | A. | ||
IMTHEMATICAL l'0 DEL , | IMTHEMATICAL l'0 DEL , | ||
. 174 DEGREES OF FREEDOM LOWEST NATURAL FREQUENCY = 114 HZ DAMPING = I4 % | |||
. 174 DEGREES OF FREEDOM | |||
LOWEST NATURAL FREQUENCY = 114 HZ DAMPING = I4 % | |||
B. HYDPAULIC FORCE . | B. HYDPAULIC FORCE . | ||
FLUCTUATING LIFT COEFFICIENT = .2 APPLIED SIMULTANEOUSLY TO ALL NODES IN PHASE PREDICTED VORTEX SHEDDING FREQUENCY = 7 Ilf , | |||
APPLIED FREQUENCY = 10, 20, 30, 40, 50, 60, 70, 80 AND AT 5 LOWEST NATURAL FREQUENCIES C. CRITERIA | |||
' ALTERNATIllG STRESS < 10 KSI e | |||
1 Jsc-4 4/6/81 | |||
FLUCTUATING LIFT COEFFICIENT = .2 | |||
APPLIED SIMULTANEOUSLY TO ALL NODES IN PHASE PREDICTED VORTEX SHEDDING FREQUENCY = 7 Ilf , | |||
APPLIED FREQUENCY = 10, 20, 30, 40, 50, 60, 70, 80 | |||
AND AT 5 LOWEST NATURAL FREQUENCIES | |||
C. CRITERIA | |||
' ALTERNATIllG STRESS < 10 KSI | |||
e | |||
1 | |||
Jsc-4 4/6/81 | |||
' ' ~ | ' ' ~ | ||
DYNAMIC RESPONSE TESTING I | |||
DYNAMIC RESPONSE TESTING | |||
I | |||
~ | ~ | ||
A. SPARGER . | A. SPARGER . | ||
SHOP TEST TO VERIFY NATURAL FREQUENCIES - | SHOP TEST TO VERIFY NATURAL FREQUENCIES - | ||
AND l'0DE SHAPES FROM MATHEMATICAL MODEL B'. LINE , | |||
AND l'0DE SHAPES FROM MATHEMATICAL MODEL | |||
B'. LINE , | |||
~ | ~ | ||
. FULL SC LE INTER:!AL FLOW TEST TO VERIFY . | . FULL SC LE INTER:!AL FLOW TEST TO VERIFY . | ||
PERFORMANCE DURING CORE SPRAY' INJECTION e | |||
PERFORMANCE DURING CORE SPRAY' INJECTION | |||
e | |||
w | w | ||
. e | . e | ||
*e | *e JEL-S 4p5/al | ||
JEL-S | |||
4p5/al | |||
, , g - , - ~ - - . .,, | , , g - , - ~ - - . .,, | ||
REACTOR PERFORMAllCE NORMAL OPERATION . | REACTOR PERFORMAllCE NORMAL OPERATION . | ||
o SEPARATOR / DRYER PERFORMANCE N0 PERFORMANCE DEGRADATION DUE TO REDUCED SEPARATOR / DRYER SPACING SPARGER HEADER COULD IMPACT PERFORMANCE OF PERIPHERAL SEPARATORS (18 0F 151 TOTAU ,. | |||
o SEPARATOR / DRYER PERFORMANCE | |||
N0 PERFORMANCE DEGRADATION DUE TO REDUCED SEPARATOR / DRYER SPACING | |||
SPARGER HEADER COULD IMPACT PERFORMANCE OF PERIPHERAL SEPARATORS (18 0F 151 TOTAU ,. | |||
TOTAL BLOCKAGE RESULTS Iti: | TOTAL BLOCKAGE RESULTS Iti: | ||
o 1,7 PSI PRESSURE DROP INCREASE | o 1,7 PSI PRESSURE DROP INCREASE | ||
( o CARRYUllDER WITHIN DESIGN LIMITS o CARRYOVER WITHIN DESIGN LIfilTS | ( o CARRYUllDER WITHIN DESIGN LIMITS o CARRYOVER WITHIN DESIGN LIfilTS N0 IMPACT ON PLAtlT PERFORMANCE o SHROUD LEAKAGE STEAM SKIRT PREVENTS STEAM LEAKAGE TO ANilVLUS CONSERVATIVE ANALYSIS SHOWS SKIRT REMOVAL: | ||
N0 IMPACT ON PLAtlT PERFORMANCE | |||
o SHROUD LEAKAGE | |||
STEAM SKIRT PREVENTS STEAM LEAKAGE TO ANilVLUS | |||
CONSERVATIVE ANALYSIS SHOWS SKIRT REMOVAL: | |||
o <0.03% CARRYUt! DER INCREASE o NO RECIRC SYSTEM PERFORMANCE DEGRADATI0tl o <0.4 BTU /LB CORE INLET EtiTHALPY INCREASE CYCLE SHORTEilED BY ONE-HALF FULL POWER DAY INCONSEQUENTIAL EFFECT ON NORMAL PLANT OPERATION JH0 - 1 4/15/81 l | o <0.03% CARRYUt! DER INCREASE o NO RECIRC SYSTEM PERFORMANCE DEGRADATI0tl o <0.4 BTU /LB CORE INLET EtiTHALPY INCREASE CYCLE SHORTEilED BY ONE-HALF FULL POWER DAY INCONSEQUENTIAL EFFECT ON NORMAL PLANT OPERATION JH0 - 1 4/15/81 l | ||
i REACTOR PERFOR.''.ANCE | |||
i | .- NORMAL OPERATION (CONTINUED) o RECIRCULATION SYSTEM PERFORMANCE SPARGER INCREASES AP <0.8 est SUBSTANTlAL EXCESS FLOW CAPABILITY EXISTS | ||
REACTOR PERFOR.''.ANCE | |||
.- NORMAL OPERATION | |||
(CONTINUED) | |||
o RECIRCULATION SYSTEM PERFORMANCE | |||
SPARGER INCREASES AP <0.8 est | |||
SUBSTANTlAL EXCESS FLOW CAPABILITY EXISTS | |||
- - NO RECIRCULATION SYSTEM PERFORMANCE CONCERN - | - - NO RECIRCULATION SYSTEM PERFORMANCE CONCERN - | ||
EVEN CONSIDERING BLOCKED SEPARATORS | EVEN CONSIDERING BLOCKED SEPARATORS i | ||
t JHO - 2 l 4/15/81 v -w- w- | |||
i | |||
t | |||
JHO - 2 l | |||
4/15/81 | |||
v -w- w- | |||
REACTOR PERFORMANCE . | REACTOR PERFORMANCE . | ||
TRANSIENT / ACCIDENT CONDITIONS . | TRANSIENT / ACCIDENT CONDITIONS . | ||
/ | / | ||
o CORE HYDRAULIC STABILl!Y | o CORE HYDRAULIC STABILl!Y | ||
~ | ~ | ||
CONSERVATIVELY MODELED . | CONSERVATIVELY MODELED . | ||
- DECAY RATIO INCREASES | - DECAY RATIO INCREASES | ||
* 0,04 | * 0,04 | ||
. NO IMPACT BECAUSE DECAY RATIO CONSIDERING OVERHEAD CORE SPRAY SfARGER IS SIGNIFICANTLY LESS THAN 3.0 | . NO IMPACT BECAUSE DECAY RATIO CONSIDERING OVERHEAD CORE SPRAY SfARGER IS SIGNIFICANTLY LESS THAN 3.0 o ANTICIPATED OPERATIONAL TRANSIENTS PEAK VESSEL PRESSURE INCREASES < l est PEAK HEAT FLUX INCREASES < 0.5% FOR PRESSURIZATION EVENTS | ||
o ANTICIPATED OPERATIONAL TRANSIENTS | |||
PEAK VESSEL PRESSURE INCREASES < l est | |||
PEAK HEAT FLUX INCREASES < 0.5% FOR PRESSURIZATION EVENTS | |||
... CHANGES TOO SIALL TO AFFECT RELOAD LICENSE ANALYSIS 4 | ... CHANGES TOO SIALL TO AFFECT RELOAD LICENSE ANALYSIS 4 | ||
._ o INTERNAL PRESSURE DIFFERENCES SHROUD STEADY STATE HYDRAULIC LOADS INCREASE DUE TO HIGHER aP INCONSEQUENTIAL DYNAMIC LOAD INCREASE SUBSTANTIAL MARGIN TO DESIGN LIMITS ACCOMODATES HIGHER AP JHO - 3 4/15/81 I | |||
._ o INTERNAL PRESSURE DIFFERENCES | |||
SHROUD STEADY STATE HYDRAULIC LOADS INCREASE DUE TO HIGHER aP | |||
INCONSEQUENTIAL DYNAMIC LOAD INCREASE SUBSTANTIAL MARGIN TO DESIGN LIMITS ACCOMODATES HIGHER AP JHO - 3 4/15/81 | |||
I | |||
P Q REACTOR PERFORMAilCE . | |||
P Q | |||
REACTOR PERFORMAilCE . | |||
/ TRAllSIErlT/ACCIDEllT C0flDITI0flS ' | / TRAllSIErlT/ACCIDEllT C0flDITI0flS ' | ||
(CONTINUED) | (CONTINUED) | ||
. o LOSS OF COOLA!!T ACCIDEllTS | . o LOSS OF COOLA!!T ACCIDEllTS NO EFFECT ON CURRENT LOCA AtlALYSES WITH REQUIRED CORE SPRAY FLOW / BUNDLE GRID REMOVED DURING REFUELING - | ||
o ZER0 LOCA POTEllTIAL MAINTEllANCE ISSUE: . | |||
NO EFFECT ON CURRENT LOCA AtlALYSES WITH REQUIRED CORE SPRAY FLOW / BUNDLE | |||
GRID REMOVED DURING REFUELING - | |||
o ZER0 LOCA POTEllTIAL | |||
MAINTEllANCE ISSUE: . | |||
o ONE SYSTEM SUFFICIENT TO FLOOD BYPASS. | o ONE SYSTEM SUFFICIENT TO FLOOD BYPASS. | ||
REGION a SPILL OVER INTO CHANNELS o UTILIZE ADMIf1ISTRATIVE PROCEDURES TO PREVEilT lilADVERTENT DRAlillilG NO REDUCTI0ft IN SAFETY MARGIflS JHO - 4 | |||
REGION a SPILL OVER INTO CHANNELS | |||
o UTILIZE ADMIf1ISTRATIVE PROCEDURES TO PREVEilT lilADVERTENT DRAlillilG NO REDUCTI0ft IN SAFETY MARGIflS | |||
JHO - 4 | |||
~4/15/81 | ~4/15/81 | ||
+ | + | ||
r * | r * | ||
: f. ; | : f. ; | ||
5 CORE SPRAY PERFORMANCE AND TESTING Y | 5 CORE SPRAY PERFORMANCE AND TESTING Y | ||
; | ; | ||
o DESIGN REQUIREMENTS o CONCEPTUAL OVERVIEW o FLOW DISTRIBUTION . | |||
o DESIGN REQUIREMENTS | |||
o CONCEPTUAL OVERVIEW | |||
o FLOW DISTRIBUTION | |||
o SPRAY DISTRIBUTION | o SPRAY DISTRIBUTION | ||
* I l . | |||
1 1 | |||
* I | |||
l . | |||
1 | |||
i | i | ||
; | ; | ||
) | ) | ||
JHO - 5 ll/15/81 | JHO - 5 ll/15/81 | ||
,O 'O | ,O 'O CORE SPRAY PERFORMAllCE AtlD TESTING DESIGN REQUIREMEllTS o' ORIGINAL DESIGN BUNDLE FLOW: | ||
CORE SPRAY PERFORMAllCE AtlD TESTING | |||
DESIGN REQUIREMEllTS | |||
o' ORIGINAL DESIGN | |||
BUNDLE FLOW: | |||
2.45 GPM | 2.45 GPM | ||
~ | ~ | ||
SPARGER FLOW: | SPARGER FLOW: | ||
3400 GPM a 125 PSIA VESSEL o OVERHEAD CORE SPRAY SPARGER ORIGINAL DESIG!1 REQUIREMENTS PLUS VESSEL ENVIRONMENTAL RANGE: | |||
3400 GPM a 125 PSIA VESSEL | |||
o OVERHEAD CORE SPRAY SPARGER | |||
ORIGINAL DESIG!1 REQUIREMENTS PLUS VESSEL ENVIRONMENTAL RANGE: | |||
15 PSIA AIR, 15 TO 125 PSIA STEAM t | 15 PSIA AIR, 15 TO 125 PSIA STEAM t | ||
e JHO - 6 , | e JHO - 6 , | ||
4/15/81 | 4/15/81 | ||
~ | ~ | ||
CORE SPRAY PERFORMAi1CE AllD TESTING: : | CORE SPRAY PERFORMAi1CE AllD TESTING: : | ||
CONCEPTUAL OVERVIEW o BUNDLE FLOW AVAILABLE 3400 | |||
CONCEPTUAL OVERVIEW | |||
o BUNDLE FLOW AVAILABLE 3400 | |||
^: 6 GPM/BUilDLE (GROSS) 560 . - | ^: 6 GPM/BUilDLE (GROSS) 560 . - | ||
~ | ~ | ||
a 4.'5 GPM/ BUNDLE (NET) o APPR0X. 2 GPM/ BUNDLE EXCESS o 11AXIMUM MARGIN DESIGN OBJECTIVE DIRECT BUNDLE INJECTION DIRECT SPRAY TO 4 BUNDLES o REDUf1 DANT SYSTEMS > 4 BUNDLE SPRAY JH0 - 7 4/15/81 l | |||
a 4.'5 GPM/ BUNDLE (NET) | |||
o APPR0X. 2 GPM/ BUNDLE EXCESS | |||
o 11AXIMUM MARGIN DESIGN OBJECTIVE | |||
DIRECT BUNDLE INJECTION | |||
DIRECT SPRAY TO 4 BUNDLES o REDUf1 DANT SYSTEMS > 4 BUNDLE SPRAY | |||
JH0 - 7 4/15/81 l | |||
CORE SPRAY PERFORMANCE AtlD TESTING FLOW DISTRIBUTION o PER SPARGER ARM o PER SPRAY N0ZZLE o EASY TO ACHIEVE UNIFORMITY o SPARGER PRESSURE LOSSES ARE IMPORTANT, SYSTEM CAPACITY o OVERHEAD DESIGN STRAIGHTFORWARD. | |||
JHO - 8 1 11/15/81 P00ROR'8lNAL | |||
CORE SPRAY PERFORMANCE AtlD TESTING | |||
FLOW DISTRIBUTION | |||
o PER SPARGER ARM o PER SPRAY N0ZZLE | |||
o EASY TO ACHIEVE UNIFORMITY | |||
o SPARGER PRESSURE LOSSES ARE IMPORTANT, SYSTEM CAPACITY | |||
o OVERHEAD DESIGN STRAIGHTFORWARD | |||
JHO - 8 1 11/15/81 | |||
P00ROR'8lNAL | |||
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, CORE SPRAY PERFORMANCE AND TESTING SPRAY DISTRIBUTION o THE CONCEPT COVER 4 BUNDLES /N0ZZLE WORST ENVIRONMENT , | |||
, CORE SPRAY PERFORMANCE AND TESTING | |||
SPRAY DISTRIBUTION | |||
o THE CONCEPT | |||
COVER 4 BUNDLES /N0ZZLE | |||
WORST ENVIRONMENT , | |||
OVERLAP SPRAYS . | OVERLAP SPRAYS . | ||
MULTIPLE COVERAGE / BUNDLE N0ZZLE LOCATION INSENSITIVITY o THE DESIGN PROCESS | MULTIPLE COVERAGE / BUNDLE N0ZZLE LOCATION INSENSITIVITY o THE DESIGN PROCESS EMPIRICAL EMPHASIS STRAIGHTFORWARD ANALYSIS JHO - 12 f1/15/81 4 | ||
EMPIRICAL EMPHASIS | |||
STRAIGHTFORWARD ANALYSIS | |||
JHO - 12 f1/15/81 | |||
4 | |||
. .o ! | . .o ! | ||
I | I | ||
* spi 2AY cosice p7- | * spi 2AY cosice p7- | ||
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* \ | * \ | ||
A enoET suart:c 6/\//,5X/NE/J71// m | A enoET suart:c 6/\//,5X/NE/J71// m | ||
~ | ~ | ||
Line 2,800: | Line 1,036: | ||
\ | \ | ||
BA A.lS r | BA A.lS r | ||
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F% g' - | |||
"' / ( / . ;p .. | "' / ( / . ;p .. | ||
h :e. | h :e. | ||
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Line 2,819: | Line 1,050: | ||
// | // | ||
N . . | N . . | ||
v'l;.* | v'l;.* | ||
I.'' | I.'' | ||
U /19 /P1 _. | U /19 /P1 _. | ||
o0 8 0 | o0 8 0 l | ||
I CORE SPRAY PERFORP.AllCE AND TESTING , | |||
SPRAY DISTRIBUTION o' N0ZZLE SELECTION SINGLE N0ZZLE - HIGH PRESSURE STEAM SINGLE N0ZZLE - LOW PRESSURE STEAM 4 N0ZZLES - AIR , | |||
o SELECTED N0ZZLE - STEAM TESTS MULTIPLE N0ZZLE INTERACTION SINGLE SYSTEM | |||
CORE SPRAY PERFORP.AllCE AND TESTING , | . DUAL SYSTEMS LOCATION SENSITIVITY FLOW SENSITIVITY | ||
SPRAY DISTRIBUTION o' N0ZZLE SELECTION | |||
SINGLE N0ZZLE - HIGH PRESSURE STEAM | |||
SINGLE N0ZZLE - LOW PRESSURE STEAM | |||
4 N0ZZLES - AIR , | |||
o SELECTED N0ZZLE - STEAM TESTS | |||
MULTIPLE N0ZZLE INTERACTION SINGLE SYSTEM | |||
. DUAL SYSTEMS | |||
LOCATION SENSITIVITY | |||
FLOW SENSITIVITY | |||
] | ] | ||
o- SPRAY MODULE QUALIFICATION | o- SPRAY MODULE QUALIFICATION 4 | ||
JHO - 14 4/15/81 4 | |||
4 | |||
a..o | a..o | ||
= | = | ||
ee | ee CORE SPRAY PERFORMANCE AND TESTING | ||
, SPRAY DISTRIBUTION o FULL CORE SIMULATION IN AIR DIRECT VERIFICATION OF MODULAR AIR TESTS - | |||
VERIFICATION OF FLOW DISTRIBUTION ORIFICING FULL CORE BuilDLE FLOW MEASUREMENT VERIFICATION SPARGER FLOW CHARACTERISTIC | |||
CORE SPRAY PERFORMANCE AND TESTING | |||
, SPRAY DISTRIBUTION | |||
o FULL CORE SIMULATION IN AIR | |||
DIRECT VERIFICATION OF MODULAR AIR TESTS | |||
VERIFICATION OF FLOW DISTRIBUTION ORIFICING | |||
FULL CORE BuilDLE FLOW MEASUREMENT | |||
VERIFICATION SPARGER FLOW CHARACTERISTIC | |||
~ | ~ | ||
o fit!AL SPRAY QUALIFICATION JHO - 15 4/15/81 G | |||
o fit!AL SPRAY QUALIFICATION JHO - 15 4/15/81 | |||
G | |||
. .,__s. .._. | . .,__s. .._. | ||
Line 2,902: | Line 1,075: | ||
, , -- - .g . | , , -- - .g . | ||
: 4. '+ | : 4. '+ | ||
MEETING | MEETING | ||
==SUMMARY== | ==SUMMARY== | ||
DISTRIBUTION Docket NRC PDR , | DISTRIBUTION Docket NRC PDR , | ||
Local PDR ORB RE= ding J. Olshinski | Local PDR ORB RE= ding J. Olshinski | ||
= S . .- Va rga T. Ippolito R. Clark J. Stolz D. Crutchfield W. Paulson J. Lombardo - | = S . .- Va rga T. Ippolito R. Clark J. Stolz D. Crutchfield W. Paulson J. Lombardo - | ||
0 ELD OI&E.(3) | 0 ELD OI&E.(3) | ||
HSmith | HSmith ACRS (10) ~ | ||
NSIC ETERA? mle K. Wichman 3 q H. Shaw s C. Y. Cheng ' | |||
NSIC ETERA? mle K. Wichman 3 q H. Shaw s | |||
C. Y. Cheng ' | |||
L ") | L ") | ||
B R. Frahm G. walton lh}:6 ' ' | B R. Frahm G. walton lh}:6 ' ' | ||
__d 1A M 1 4 196 - | __d 1A M 1 4 196 - | ||
I W i | I W i | ||
h u.s.1gCJsIonk,/ | h u.s.1gCJsIonk,/ | ||
s 'S ' | s 'S ' | ||
l. | l. | ||
4 L | 4 L | ||
-,-}} | -,-}} |
Revision as of 01:53, 31 January 2020
ML19347F023 | |
Person / Time | |
---|---|
Site: | Oyster Creek |
Issue date: | 05/14/1981 |
From: | JERSEY CENTRAL POWER & LIGHT CO. |
To: | |
Shared Package | |
ML19347F021 | List: |
References | |
NUDOCS 8105150100 | |
Download: ML19347F023 (37) | |
Text
{{#Wiki_filter:.' Enclosure 2 C ! MEETING AGENDA , OYSTER CREEK CORE SPRAY SPARGER REPLACEMENT APRIL 15, 1981 ,
\
I. INTRODUCTION JIM KNUBEL (JCP&L) A',' HISTORY B'.' MEETING OBJECTIVES II. DESIGN
SUMMARY
. JAY ERBES (G.E.) A. DESIGN CRITERIA B'.' REPLACEMENT DESCRIPTION III. STRUCTURAL DESIGN JIM CHARNLEY (G.E.) A. STATIC ANALYSIS B. DYNAMIC ANALYSIS C. DYNAMIC RESPONSE TESTING IV. REACTOR PERFORMANCE JIM OATES (G.E.) -
~
A .' NORMALOPERATION B. TRANSIENT AND ACCIDENT V. CORE SPRAY PERFORMAMCE AND TESTING JIM OATES (G.E.) l A. DESIGN REQUIREMENTS B. CONCEPTUAL OVERVIEW
~ - - ~
C'.' FLOW DISTRIBUTION D. SPRAY DISTRIBUTION i
SUMMARY
AND FUTURE SCHEDULE JIM KNUSEL (JCPEL) B 2 05 350oo (VI .
.~ OYSTER CREEK CORE SPRAY SPARGER REPLACEMENT l l
HISTORY 1978 - 1 CRACK DISCOVERED BY VISUAL INSPECTION 1980 - MULTIPLE CRACKS DISCOVERED BY IMPROVED VISUAL TECHNIQUES AND UT, ... JCP&L SUBMITTAL SUGGESTED SPARGER REPLACEMENT WITHIN 2 REFUELING CYCLES NRC SER REQUIRED REPLACEMENT WITHIN 1 CYCLE OCT 1980 - JCP&L AND NRC STAFF MEETING MAR 1981 - JCP&L SUBMITTAL TO NRC APR 1981 - JCP8L AND NRC MEETING
. JK-1 4/15/81
0YSTER CREEK CORE SPRAY SPARGER REPLACEMENT
~
MEETING OBJECTIVES
;
- 1. CONCURRENCE WITH DESIGN QUALIFICATION PROGRAM e- APPLICABLE CODES i e ANALYTICAL SUPPORT e TEST PROGRAM !
i II. ESTABLISH REQUIRED DOCUMENT SUBMITTALS o PRELII:! NARY MODIFICATION REPORT (3/81) e FINAL MODIFICATION REPORT (10/81) i III.- ESTABLISH SCHEDULE OF PRESENTATIONS e CORE SPRAY TESTS RESULTS (9/81) IV. DISCUSS PRELIMINARY MODIFICATI0ll REPORT Y JK-;l 4/15/81
OYSTER CREEK .
\
f ~0VERHEAD CORE SPRAY SPARGER l DESIGN CRITERIA I. SYSTEM e 2,45 GPM/ BUNDLE e DUAL SYSTEMS - 100% REDUNDANCY-e i1Ih! MUM IMPACT ON EXISTING IllTERtlALS AND REACTOR OPERATI0tlS e ONE SPRAY N0ZZLE PER 4 BUNDLES II. APPLICABLE CODES s ASME SECTION XI s ASME SECTION III, Sil3SECTI0tl flG AS DESIGN GUIDE e SAFETY ESSENTIAL, 10CFR21 APPLIES III, MECHANICAL - e WATER SUPPLIED THROUGH EXISTING REACTOR PRESSURE VESSEL t!0ZZLES e REMOVA3LE FOR REFUELING AND INSPECTI0tl e MATERIAL - TYPE 316 (L) OR 304 (L) ' f.'02% MAX, CARBON JGE - 1 4/15/81
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. 0YSTER CREEK CORE SPRAY SPARGER REPLACEMENT 4 ~ . STRUCTlJRAL DESIGN -
CORE SPRAY SPARGER AND CORE SPRAY LINE
. A. STATIC ANALYSIS . ~
B'. DYNAMIC ANALYSIS .
- C. DYNA!ilC FESPONSE TESTING e g .
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STATIC ANALYSIS SIZING
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DRAG COEFFICIENT = 1
. LIFT COEFFICIENT = 1 . . DAMPING = 2%
EXCITATION FREQUENCY = NATURAL FREQUENCY
' PPLIED A LOAD = 25 TIES HYDRAULIC LOAD ALTERNATING STRESS <10 KSI B'. ' DEAD WEIGHT - - - . C. THERMAL' ' ~
D. SEISMIC 4 4 m.; 4/i5g1
. SPARGER DYllAMIC Ai1ALYSIS : ~ A. MATHEllATICAL MODEL . . . . 1332 DEGREES OF FRF.EDOM .
LOWEST NATURAL FREQUEllCY = 42 HZ DAMPIllG = 1.5% ~
~ -B'.' H'YDRAULIC FORCE FLUCTUATING LIFT COEFFICIENT = .2 CYLINDERS - = 1.0 PLATES APPLIED SIPULTAt1E0VS TO ALL NODES IN PHASE , PREDICTED VORTEX SHEDDING FREQUENCY =.13HZ(3-1/2." PIPE 5) = 10 HZ (5" PIPES) = 11 HZ (1.5" BEAMS)
APPLIED FREQUEf1CY = 5, 10, 13, 15, 20, 25, 30, 35, 40
. AtlD AT 5 LOWEST NATURAL FREQUENCIES . .'C. ~
CRITERIA . ALTERNATIf1G STRESS 4 10 KSI
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LINE DYNAMIC ANALYSIS f A. IMTHEMATICAL l'0 DEL ,
. 174 DEGREES OF FREEDOM LOWEST NATURAL FREQUENCY = 114 HZ DAMPING = I4 %
B. HYDPAULIC FORCE . FLUCTUATING LIFT COEFFICIENT = .2 APPLIED SIMULTANEOUSLY TO ALL NODES IN PHASE PREDICTED VORTEX SHEDDING FREQUENCY = 7 Ilf , APPLIED FREQUENCY = 10, 20, 30, 40, 50, 60, 70, 80 AND AT 5 LOWEST NATURAL FREQUENCIES C. CRITERIA
' ALTERNATIllG STRESS < 10 KSI e
1 Jsc-4 4/6/81
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DYNAMIC RESPONSE TESTING I
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A. SPARGER . SHOP TEST TO VERIFY NATURAL FREQUENCIES - AND l'0DE SHAPES FROM MATHEMATICAL MODEL B'. LINE ,
~ . FULL SC LE INTER:!AL FLOW TEST TO VERIFY .
PERFORMANCE DURING CORE SPRAY' INJECTION e w
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REACTOR PERFORMAllCE NORMAL OPERATION . o SEPARATOR / DRYER PERFORMANCE N0 PERFORMANCE DEGRADATION DUE TO REDUCED SEPARATOR / DRYER SPACING SPARGER HEADER COULD IMPACT PERFORMANCE OF PERIPHERAL SEPARATORS (18 0F 151 TOTAU ,. TOTAL BLOCKAGE RESULTS Iti: o 1,7 PSI PRESSURE DROP INCREASE ( o CARRYUllDER WITHIN DESIGN LIMITS o CARRYOVER WITHIN DESIGN LIfilTS N0 IMPACT ON PLAtlT PERFORMANCE o SHROUD LEAKAGE STEAM SKIRT PREVENTS STEAM LEAKAGE TO ANilVLUS CONSERVATIVE ANALYSIS SHOWS SKIRT REMOVAL: o <0.03% CARRYUt! DER INCREASE o NO RECIRC SYSTEM PERFORMANCE DEGRADATI0tl o <0.4 BTU /LB CORE INLET EtiTHALPY INCREASE CYCLE SHORTEilED BY ONE-HALF FULL POWER DAY INCONSEQUENTIAL EFFECT ON NORMAL PLANT OPERATION JH0 - 1 4/15/81 l
i REACTOR PERFOR..ANCE
.- NORMAL OPERATION (CONTINUED) o RECIRCULATION SYSTEM PERFORMANCE SPARGER INCREASES AP <0.8 est SUBSTANTlAL EXCESS FLOW CAPABILITY EXISTS - - NO RECIRCULATION SYSTEM PERFORMANCE CONCERN -
EVEN CONSIDERING BLOCKED SEPARATORS i t JHO - 2 l 4/15/81 v -w- w-
REACTOR PERFORMANCE . TRANSIENT / ACCIDENT CONDITIONS .
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o CORE HYDRAULIC STABILl!Y
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CONSERVATIVELY MODELED .
- DECAY RATIO INCREASES
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. NO IMPACT BECAUSE DECAY RATIO CONSIDERING OVERHEAD CORE SPRAY SfARGER IS SIGNIFICANTLY LESS THAN 3.0 o ANTICIPATED OPERATIONAL TRANSIENTS PEAK VESSEL PRESSURE INCREASES < l est PEAK HEAT FLUX INCREASES < 0.5% FOR PRESSURIZATION EVENTS
... CHANGES TOO SIALL TO AFFECT RELOAD LICENSE ANALYSIS 4 ._ o INTERNAL PRESSURE DIFFERENCES SHROUD STEADY STATE HYDRAULIC LOADS INCREASE DUE TO HIGHER aP INCONSEQUENTIAL DYNAMIC LOAD INCREASE SUBSTANTIAL MARGIN TO DESIGN LIMITS ACCOMODATES HIGHER AP JHO - 3 4/15/81 I
P Q REACTOR PERFORMAilCE .
/ TRAllSIErlT/ACCIDEllT C0flDITI0flS '
(CONTINUED)
. o LOSS OF COOLA!!T ACCIDEllTS NO EFFECT ON CURRENT LOCA AtlALYSES WITH REQUIRED CORE SPRAY FLOW / BUNDLE GRID REMOVED DURING REFUELING -
o ZER0 LOCA POTEllTIAL MAINTEllANCE ISSUE: . o ONE SYSTEM SUFFICIENT TO FLOOD BYPASS. REGION a SPILL OVER INTO CHANNELS o UTILIZE ADMIf1ISTRATIVE PROCEDURES TO PREVEilT lilADVERTENT DRAlillilG NO REDUCTI0ft IN SAFETY MARGIflS JHO - 4
~4/15/81
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5 CORE SPRAY PERFORMANCE AND TESTING Y
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o DESIGN REQUIREMENTS o CONCEPTUAL OVERVIEW o FLOW DISTRIBUTION . o SPRAY DISTRIBUTION
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,O 'O CORE SPRAY PERFORMAllCE AtlD TESTING DESIGN REQUIREMEllTS o' ORIGINAL DESIGN BUNDLE FLOW:
2.45 GPM
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SPARGER FLOW: 3400 GPM a 125 PSIA VESSEL o OVERHEAD CORE SPRAY SPARGER ORIGINAL DESIG!1 REQUIREMENTS PLUS VESSEL ENVIRONMENTAL RANGE: 15 PSIA AIR, 15 TO 125 PSIA STEAM t e JHO - 6 , 4/15/81
~
CORE SPRAY PERFORMAi1CE AllD TESTING: : CONCEPTUAL OVERVIEW o BUNDLE FLOW AVAILABLE 3400
^: 6 GPM/BUilDLE (GROSS) 560 . - ~
a 4.'5 GPM/ BUNDLE (NET) o APPR0X. 2 GPM/ BUNDLE EXCESS o 11AXIMUM MARGIN DESIGN OBJECTIVE DIRECT BUNDLE INJECTION DIRECT SPRAY TO 4 BUNDLES o REDUf1 DANT SYSTEMS > 4 BUNDLE SPRAY JH0 - 7 4/15/81 l
CORE SPRAY PERFORMANCE AtlD TESTING FLOW DISTRIBUTION o PER SPARGER ARM o PER SPRAY N0ZZLE o EASY TO ACHIEVE UNIFORMITY o SPARGER PRESSURE LOSSES ARE IMPORTANT, SYSTEM CAPACITY o OVERHEAD DESIGN STRAIGHTFORWARD. JHO - 8 1 11/15/81 P00ROR'8lNAL
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SUMMARY
DISTRIBUTION Docket NRC PDR , Local PDR ORB RE= ding J. Olshinski
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