ML20059B632
| ML20059B632 | |
| Person / Time | |
|---|---|
| Site: | Big Rock Point File:Consumers Energy icon.png |
| Issue date: | 08/22/1990 |
| From: | Eddy J CONSUMERS ENERGY CO. (FORMERLY CONSUMERS POWER CO.) |
| To: | NRC OFFICE OF INFORMATION RESOURCES MANAGEMENT (IRM) |
| References | |
| GL-88-01, GL-88-1, NUDOCS 9008290199 | |
| Download: ML20059B632 (40) | |
Text
w !~ m x
+
s e.
.h5' ;-M '
00nSumCIS F
Power POWEMNE
. RUUNGAN'S Nt0GRE55 -
[:
. oeneral Officos 1946 West Pernett Road, Jackson, MI 49201 * (517) 788-0550
' Atigus t ' 22,:1990 F
'l Nuclear Regulatory Commission
. Document Control Desk c
Washington, DC 20555-DOCKET 50-155 - LICENSE DPR BIG ROCK POINT PLANT -
SUPPLEMENTAL INFORMATION REGARDING TECHNICAL SPECIFICATION CHANGE REQUEST --
REACTOR TEMPERATURE LIMTS By' letter dated January 10, 1990, Consumers Power Company subEitted a. request
'for change to the Big-Rock Point Plant Technical Specifications regarding reactor pressure-temperature limits.
Specifically,.the change was requested i
to insure that the specifications for the Big Rock Point Reactor Vescel
.f continue to satisfy the Fracture Toughness requirements of Sect' ion V'of 10CFR j
- Part 50, Appendix G.
Subsequent to submittal of'the change request, NRC
. review produced comments regarding the use of methodology contained in
~ Revision 2 to Regulatory Guide-l.99. This letter submits a revised version 1
of the Technical Analysis which accompanied the Technical Specification j
change request. While NRC comment resolution involved revising the Technical Analysis, no change is required to the original change request or associated l
pressure-temperature curves. This is due to the fact that-resolution on the j
axis of the curves precludes revision due to the small numerical changes h
offered by the revision to the Technical Analysis. The revised Technical l
Analysis is being submitted in response to a verbal request by the NRC
{
reviewer. This subject has been discussed with the Big Rock Point Project Manager. Please contact us if there are any further questions.
[ *'
Q J Daniel Eddy-Plant Licensing Engineer g
.CC~ Administrator, Region III, USNRC NRC Resident Inspector - Big Rock Point 9008290199 900G22 PDR ADOCK 05000155 P
PDC 00 OC0890-0398-NLO2 N
A CAf5 ENt?7?GYCOMPANY
.]
, y %m,.,,m _ m,.e% 4.,, --m_
_e
_d x
- mA pm+,
m x.
x, w w*
--..m wo f.
- /.,,
4 m
ynt-
< /... pi g.
- a.. m e w
-e.,
o w
s.,-
m
,e d 4;e
.m 1
%3
,.. ; c. c w -; g
.w a. :.
g,r s
Wt, m. ~
.m$.q.
s.
s
+,
,.3 q r - AqvM' x_3- -.m v o:7 3..; m4
%( ; m..#
"p h 1 -
3 g
,s
%~-
n-
-- e ra %
.n a.m--
s
?... ~ n. 43. p'N M; t.4 >M, := t --
t 3
Y 4
lQQ.;r c%m % J W "L 4... ! ? r.i W yu 7
1 m
i P s
3 g
7,.
a 3
d\\
--./m N
a;.,.
c 4_-
s a
mm-MNEl m r
m -
- f. ?i N.,
nj*'.
y,' ]
?
i'
~i k
+.
f
' J 'l,,-
f tl.
i
-i,-
- ~
y n _.
p, L c.,-'
3 v.n C'
v
.re
- r..
e:
y-9, v
- p p ',
q pa% W ; c:--@'.m,. y,q~ g.,
m,,,..
v p
-+f; b.\\.. ;
.t.,w'_,
7 1 i
t hy
,,4 r
,,n
. i j t.;
wt q
f i
g, 1
m 4
4 19 4
%=>.,
m..
< s
-s 3
r g
g.,,..
c )
r pg ' t
- me u, g.
- '{s...'
- 3 b ;'t 4
a.
m'y,7 2,
. cyt2
/j
..F x
E
[
, m
?
' Y h #_
".'f h,
p k
- 7
- l I
f p+ g.,p-r a~
+w m
s
,1 g.
. sw n m em:s. '
,'1
+
+
w n
-M M'::
'i v, i. M.,,,
. - w, x.. w E
- 3 :.w
.%9 -=
i a
,r t g -
4
'5 "
s,1 g #9
, r-u g
j m e.'q,s,
nw! <.
,c s-
.mn u, e.
, w v.y 4,; 7,-
w..
m,
.y
- t..
(y 4, yi9%
i t
yo W'bi={'..S-
?,
a 7 y
-D',,,
+
t 4 L.-
- '.t': <
L
[
.J.
e /,3 mi, 1
m.
.n
.c p
e p
'y 1
s?. [.
u ':
y:
. -1 ~b. i -
nat L 1 J
f %.L c...
.,.. r<
-; y v1
(.
g ps 7
1 y I _},.%y.
't
.y:,
>g y?
i >
i a
10
,, n
~,s s.
, t:
-',1.
3 m-m,m,~2..
a k-t e
r
)
n a f..
r y
e i
o 1'
m.d 4
1i
!W
- 6i., ;,Xy
)._
N,l
- j pi 1
oo fm : - o
/ ATTACHMENT!
4 m,
f:
+
g.
wa o
1 v, w w
Wi Q & $ '
! Consumers Power Company; V
.m
%P g ? -
Big. Rock Point Plant: '
N
.-,,y.
iDocket'50-155-
--lW
.e~,
m.
,.;o 1
m, fD
,,(
i
.ji.j fc.
-o,. 4, 3
-, )
m t
,ii,.
- 3
- -i 3
r n
Ms' i
3,,
k
- .,l
,4 4..
I 4
1 _
V i
6 g
I Q
T v
, 4 J'_-
g r
s
?
I'-j!
i de im.
+ r1 4
O i
u,
. v w' v >
~
t
~
=u -
s >
-u s
4.'"n i
w n.w; y
,f.,.
s n.
4 p(
JD - i h_ -
J,g I
e's m 4: a w
.it
>g, (.
s,
- g y e
1 4
. EVALUATION 0F GENERIC LETTER-88-11 W
W Nk_2.
, - w-F F,' ",
M.4 N
m
<ON< BIG ROCK: POINT TEMPERATURE. PRESSURE LIMITATIONS!
- REVISION 1.
W 1
4 m
N ll f
O H'
i y
@1 7%
T&1 1Augustt22, 1990..
Ji a-x o
a%-W,
s
- a g
a m+
%,m
(
,1 s
iyy m.
- n
.8
..n l;9 C Q./
P f;$-Q
- 4l A @; "
5
,g W
l y.'
n _
~
d, e>
n c 4+
" \\ @%*,
~o
.2 l'
r.
L (5
,<Sii T g cd g< % ' 1
' v.,.;
s 3
1 i3 Y
y :p
'i
.* "g, e s
w,, j, : t s
-sm iy e 5
s:l}
% (c
., i-
~
L; ~
s 5
t ai
..r 4.
D-11.'s
- f
{s* $ 'l?
y
?
Y
,p
. a n:#s 3
t M:lit'; ^
3 )
t -
+ -
.~,.,
g y, -
y~.
4
,.1 2
?j ?,j '; g,._
a 64 V' w'w:>
+c;s:
-:ps
]
s.n m.
n,.
H q'g f
u q +;.y.. i 5
.c..
K' t
fr
'~_
i e k
-r a.-
g a,
38 Pages s
s =:
. m v
.WW4
- OC0890-0398-NLO2.
,. y; q%ww a%.. s, py yo n
w.
- h i,c h.
y q
- d w
1 s u:m 3 s 2h
,1. s yuw
< = -
+r.,'
g y?q,,p >
f 9 f
3 l-4
_h3'[d[-N s
b
/Q i
j
'[ if g
BIG ROCK POINT NUCLEAR PLANT ca NL 88-59-01 asas 4mM ENGINEERING ANALYSIS WORK SHEET sheet 1 of 36 EVALUATION OF GENERIC LETTER 88-11 ON BIG ROCK POINT TEMPERAWRE Tih PRESSURE LIMITATIONS.
s P
L INITIATION AND REVIEW'
/
Initiated Rev Method Check (d Technically Rev'd Alt Det Qual Descriptiori By Date Calc Rvw Test By Date l
[
O Original issue
<ATE
%14n
/
Itsh A I - Taglie
/
AAbearco afAc. deua a"Mr
/ kM-fnMr.
/
44 A l'- - itilie l
j 7 f
E l
l I
l l
l l
l l
~RENERENCES lj _ eg.oric'Let.tr)8.-11 I
' d__ R. egiGu.; dek,39,j_Re' _2 v
Nay;lU 8 l-
'3)_WCAt-9p._Sep:paber19.80.a_Lj
.L_
i
+
i i
i i
e t
4 i
i j
1
)..)iTEB.5.2_
J.
4 5)._100FR50.6k ;
l
_.L.]i L _. _
i i
_r.6). Coabustion( Engineeringlhts. led 20 :.794 8 l
! l _L._ _.
l l
._.l 7)..Nemo{,_Jenk.41-77...._2
- 7 l
L _:
4 t
j i
i i
i
..........[_
.. 8).. Standard _ Review Plan.5.3.2-
--._4..
_ a.. ai._.I_..h, h._L-l...' _
_ _.. -.. _.._9).. ASME.S ct III.. Appendix G e
i i
i
_ 10)- ASME. Sect [III,. Appendices,.. Table I-2.1' I
...- 11).. Strength.of Materials II S.-.Timoshenko, 3rd Edition.
1 I
.... -.D r VanNostrand Company,_Inc., 1968
.L--.i
=-.
l i
..t t
- 0BJECTIVEt To assess the -impact of Generic Letter-88-11 requirements on--..
r:
- the pressure-temperature -limitatio'ns 'of Big Rock' Point i
4 s._._, __......
m..
i
--ASSUMPTIONS:- 1.)- Fluence at-18 EFPY-is derived-by simple -ratio of-data---+-
i l
contained in Ref. 3 above.-~ --- ---
'-~
---r---
~'
2)- Temperature T is vessel metal temperature taken froa~-- -
thermocouples on reactor O.D.-
- - - - - - - - - -- -~ ~ ; ---
MI l 0 8 8- 0 5 31 A-BT01 ' ~ ~ ---~ ~ ~~ - -- ~--*- '~~ "- - ~ ---
~~~"-'-",T-
-~
I I
l k
l l
- q. ?"*
l BRP090 02/01/88 l
l m.---
m
...m.._
___m-_
..__m a>
~
- D EA WL-88-59-01'-
j i A '-
- Pags..21 of - 36
.j Rey 1
CALCULATIONS 3:
Per equation (1) of Ceneric Letter 88-11, the Adjusted Reference Temperature (ART) is the sum of the initial reference temperature RTNDT, the change in reference temperature at any given time
[
ARTWDT, and the statistical margin to accomodate scatter in experimental data. - This is then expressed as i.
(EQ.1) i ART = INITIAL RTNDT.+ ARTNDT + Margin i
EQ.1 must be evaluated for both veld metal and base metal (plate) of the reactor vessel. Initial RTNDT for weld and base metals are given N
I below.
p.
1; Weldt-Initial RTNDT = -56'F (Ref. 5)
Base Plates Initial-RTHDT = +30'F (Ref. 4)
Flanget Initial RTNDT = +40'F
.)
The margin (M) for both the initial and change of RTHDT are ierived by the followinF formula i
(EQ.2)'
Margin = M = 2VoI + 04:
8 mil 088-0531A-BT01 1
6' EA NL-88-59-01 L Paga -.3 of 36~
j-i.-
Rdif
- 1 Wherel og '= standard' deviation for inicisl RTNDT ""
o.= standard deviation for the. change in RTNDT-(ARTNDT The values for o and o are given below g
g Weldt o = 17'F g
o = 28'F (Ref. 2, Sect. 1.1) g o = 14'F (Ref. 2, Sect. -2.1)
Base Plate: 0 = 17'F-7 o = 17'F (Ref. 2. Sect.1.1) g o = 8.S* F (Ref. ' 2, Sect. 2.1)
- (
NDT Where CF = Chemistry Factor-(Ref 2) f = fluence (1019 n/ce*, E>1NeV)
- g. (.28
.10 los fl = fluence factor (Ref. 2)
CF is taken from Table 1 for veld metal and Table 2 for base metal.
Both tables are in Reference 2.
M11088-0531A-BT01
+.:;
LEA NL-88-59-01 f,4h s.:.-
Page 4 - of 36 Rev. k l
n 1
Fluence f.is' calculated.at the 1/4 and 3/4 thickness locations of the reactor-vessel well.
,}
The attenuation of f through the vessel wall is derived.by:
w (EQ.4) fx " fourface [e" 4"]
(Ref. 2)
Where.x-is the. depth in inches from the wetted surface (Vessel ID) to the 1/4t & 3/4t locations.
f The' data from Big ~ Rock Point to support the above equations is as follows.
(Calculations for certain data appear later in this i
L analysis.-
t D_ATA.
a Initial RTypT = e56*F (Weld) t.
. Initial RTNDT = +?0'F (Base Plate)
~
. Flange RTNDT = +40'F (Closure Flange)
Weld % Cu =.27 (Ref. 3)
]
Weld % Ni =.10 (Ref. 3)
Base > Plate % Cu =.10 (Ref. 3)
Base Plate % Mi =.18- (Ref. 3)
I-
. HIl088-0531A-bT01 c,.
(
e.
-4 EA NL-88-59-01
.m._.
Page 5 et 36; Rev 1
.h 42.
Weld.CF = 127'F (kef.; 2 interpolation. Table 1.)
Weld CF = 114.8'F (Ref. 2 Sect. 2.1)
Base Metal CF'= 56.3'F (Ref. 2 Interpolation. Table 1.)
Base Metal CF = 80.7'F (Ref. 2 Sect. 2.1)
, eld Margin = 2 V17' + 28' = 66'F (Ref. 2, Sect. 1.1)
W Weld Margin =-2 417 + 148 = - 44* F (Ref. 2, Sect. 2.1) 8 4 ' :,.
- Base Plate Margin = 2417 + 17' = 48'F (Ref. 2. Sect. 1.1) 8 Base Plate Margin = 2417 + 8.5' =. 38'F (Ref. 2, Sect. 2.1) 8
'EFPY to 2/79 = 8.625 19 8
f,,, 'to 2/79 ' = 2.27 (10 n/cm, E>1Mev, Ref. 3) 19 8
n/cm /EFPY f,,p/EFPY = 2.27/8.625 =.263 x 10 19 18 = 4.737 x 1019 n/cm8 cap /AT 18 EFPY =.263 x 10 f
Beltline Wall Thickness = t = 5.40625 inches 1/4t = ~ 25-(5.40625) = 1.3516 inches 3/4t =.75 (5.40625) = 4.0547 inches Operating Pressure = 1335 peig Pressure Measurement Error = 115 psi sw Temperature Measurement Error = 15'F C
mil 088-0531A-BT01 4
EA'NL-88-59-01
~
Page 6 of 36 Ti Rev
)
'~
FLUENCE CALCULATIONS
'From Equation 4 I* " 4 I f, = Fs rf ft/4 = 4.737 [e 24 (1.3516))
fl/4 = 4.737 [e
.3244) ft/4 =.4.737 [.723) 19.n/cm E>1Mev) 8 f1/4 = 3.425-(x 10 f3/4. 4,737 [e
.24(4.0547))
f3/4 = 4.737 [e.9731) f3/4 = 4.737 [.3779) j f3/4 = 1.790 (x 1019 n/ca*, E>lMev)
-l l
m HIl088-0531A-BT01
'r,
~
,N,;
hJiY f y
EA NL-88-59-01 e
Page.7 of 36.
'l 3-;'
Rev.
l'
.l j
.1
-Section 1.1, Reference'2 Analysis'
+
'WeldiART r a Equation 3 NDT i
(.28.10 log fgj )]-
g
NDT 4
-7
(.28.10 los 3.425) a
= 127 [3.425
)-
"l
= 127 [3.425 +2265) l0 127 [1.322]
=
= 167.85 N 168'F j..
L:
(.28
.10 log f,jg) j ART or 3/4t weld = CFy gg (fsjk
)
NDT i
1
(.28.10 los 1.790) 127 [1.790
)
1'
=
l 127 [1'.790 +255)
=
1 127.[1.160)
=
147.3 % 147'F
=
)
(.28
.10 log itjg )
I ART r 1/4t base plate = CF NDT-BASE 1/4
(.28
.10.los 3.425)
= $6.3 [3.425.
]
= 56.3 [3.425 *2265)
= 56.3 [1.316]
= 74.4*F % 75'F-
+
1 mil 088-0531A-BT01 10..
0,L 1
EA WL-88-59-01,
',.~,,, _, -_
Page.=0 of 36
~
Bev 1:
ART r /4t base plateLa CFBASE_l sjk>
NDT-(.28
.10 log.1'.79):
=_56.3 (1.79 l
= 56.3 [1.79 256)
= 56.3 (1.159)
= 65.3'F 4 66'F 4
Weld Margin = 2 40 8+0 8 3
3 2/178 + 288
=
2 RU7T
=
2 '(32.76)
=
65.5 N 66'F
=
8
' Base Plate Margin = 24178+ 17
=2M
=2 (24) 48'F
=
f mil 088-0531A-BT01 I
i t
- - =.,
.N C<.-
FA N1, 88-59-01 o,.
pg 9 og y 4
'Rev 1
19 n/cm E>1Hev 8
RT FOR 18 EFPY & f = _4.737 x 10 NDT NDT + A NDT +
- 8 "
'I
! I "'
= -56'F + 168'F + 66'F-
= 178'F RT f r 3/4t veld = - 56'F + 147'F + 66*F NDT
= 157'F RT r 1/4t base plate = 30*F + 75'F + 48'F NDT
= 153'F RT f r 3/4t base plata = 30*F + 66'F + 48'F NDT
= 144'F 5
mil 088-0531A-BT01 l
EA WL*-88-59-01.
Page 10 cr 36 '
Rev "i I
Section 2.1, Reference 2 Analysist V
.in Data from Ref S
)
t CF = E [ ARTNDT x ( I ) + ARTNDTy ('f ) + ARTNDTs ( s} +
x y
l E [ff a + gg a + gg:. +,,,)
x y
s e
v t
L Weld Datat d
Capsule f
ff _
A 30 ft/lb ff(A30 ft/lb) ffa 1
/
119'
.15
.5028 55 27.654
.2528 I
.71
.9039 135 122.0265
.8170 L
125 2.27 1.2218 135 164.943 1.4927 l-I 122 2.3-1.2251 130 159.263 1.5008 l
l' 124 10.7 1.5214 170 258.638 2.3146 E - 732.5245-E = 6.3779 CF Weld = 732.5245 + 6.3779 = 114.854-l..
t-l' '
mil 088-0531A-BT01
WQ.,
FA NL-88-59-01 y
. -. c. o -
Page 11 of - 36 Rev 1
t Base Plate Datas-4
-Li Capsule _.
f-'
ff A 30 ft/lb' f f'(A30 f t/lb) ff' 119
.15
.5028
- 0 0
.2528 127'
.71
.9039 60
.54.234
.8170 125
- 2.27 1.2218 120_
146.616.-
1.4927-122
'2.3 1.2251 70 85.757 1.5008 124 10 7 1.5214 150 228.210 2.3146 l
I = $14.817 I = 6.3779
~
CF Base Plate = 514.817 + 6.3779 = 80.72 '
=
CF weld = 114.854 CF Base Plate = 80.72-9
-ART r 1/4t weld = C.FWELD I 1/
4 NDT
(.28
'10 log,3,425)
= 114.854 (3.425
)
[
= 114'.854 (3.425.2265)
- 114.854-(1.322]
= 151.79'F N 152'F
=
Y C
mil 088-0531 A-BT01 k
6
o 4<
' u NL-88-59-01
.- =. -.
o p,,,.12 of 36 Rev.
Li g
(.28
.10 log ig g) j I
ART r 3/4t weld ='C.F g '[f1jg NDT
(.28
.10 log 1.790) 114.854 [1.790 l~
=
114.854 (1.790.2547)
=
= 114.854 (1.160).
133.21*F N 134'F
=
ART for 1/4t. Base Plate = C.F yp7 PLATE I/4
(~.28
.10 los 3.425)
= 80.72 [3.425 1
= 80.72 (3.425.2265)
= 80.72 (1.322).
= 106.71'F % -107'F ART r 3/4e Base : Plate = C.FPLATE I 3/ 4 ET
(.28.10 los 1.79)
=.80.72 {1.79 1
= 80. 72 '- (1.79.2 547 )
= 80.72 {1.160)
= 93.64'F N 94*F RT f r 1/4t Weld Initial RTE T + ARTg + Margin NDT
= 56'F + 152'F + 44*F
= 140'F at 18 EFPY HIl088-0531A-BT01
- ,,n
- i FA yt.88-59-01 i-. :.
.oe.
Page 13 of 36 Rev 1.
~-
-?
RTNDT ' #-
+
+
= 122'F at 18 EFPY NDT: f r 1/4t Base Plate = 30'F + 107'T + '38'F RT
= 175'F at 18 EFPY
?
RTHDTfor /t ase ate = 0'F + 94'F + 38'F
= 162'F at 18 EPPY RTNDT Sununary Table 18 EPPY 18 EFPY Sec 1.1 Sec 2.1 Sec 1.1 Sec 2.1 Sec 1.1 Sec 2.1
. Material H
g
^
1/4t Weld 66 44 127 114.8 178'F 140'F 3/4t: Weld 66 44 127 114.8 157'F 122'F 1/4t Base Plate 48 38 56.3 80.7 153*F 175'F l
3/4t Base' Plate 48 38' 56.3 80.7 144'F 162'F s
s e
HIl088-0531A-BT01
\\
3 j' '.
f '..,.
4 EA WL-88-59-01
..s
...c.-
Paga 34.of 3g.
Rev 1
HEAT-UP/COOLDOWW/ HYDRO TEST EQUATIONS =
t av 8
In
' Per Reference 8, Section~ 3.C, the expression for heat-up and cooldown i
pressure-temperature.11mits [s as follows:
w (EQ.5) 1y Kg = 2K -(pressure) + KI (thermal) < K g I
I J-or y"
KIR >;2KI (pressure) + KI (thermal)
From Reference 9, kit is also expressed as KIR=26.78+1.233exp(.0145(T-RTNDT+1600 o
Since the reactor vessel ~expertene.es membrane hoop stress that is pressure induced and thermal stress from through wall temperature gradients, the stress intensity factors for those parameters are given ast' KI (pressure a KIM and KI (temperature).= KIT Therefore,
"}
(EQ.6)
KIR > 2Kry + KIT 5
7 mil 088-0531A-BT01 a
7
~..
Y Ii A
NL-88-59-01
/ !
N:y
.-.a.:.'.
15 36 1
e
.From Reference 9,.
4
- Kgg = Mg (Membrane Stress) and
' KIT " He (AT
) where ATy is the magnitude of the through wall j
i
' temperature gradient.
Therefore, t
u l
Kgg>2Mg (Membrane Stress) + Mt (AT,)
.i The' temper ture gradient profile (data) for BRP is in Table 1.
a
^..
From Reference 9, Figure 6-2214-2, i
N =.268 g
To determine N, the ratio of o/o must be determined, g
y i
i :.
(EQ.7)~
8 y
gg,
) (Ref. 11)
Since o = a P 8 8 b -a i
Where. P = Internal Pressure = 1335 pois 7
a =.r
= Inside Vessel Radius = 53.0625 inches
~
g b=r = outside Vessel Radius = 58.46875 inches 0
r = rgjg = Radius at 1/4t = 54.414 inches HIl088-0531A-BT01
(
t,-
t
+.,
.i*:*
Page 16 or, 36 Rev 1
. m.
and G
r3fgg = Radius at 3/4t = 57.117 inches -
therefore 8
4 875 ogjgt = (53.0625)8 P
(g,5
)
7 8
(58.46875' - 53.0625 )-
= 2815.629 P (g-,3418.5947 )
602.966' 7 2960.8834
= 4.6696 P7 (1 + 1.1546)
=.4.6696 P7 (2.1546)'
= 10.061 P7 8~
(g,58.46875 )
03jgt =:(53.0625)8 P 7 7
(58.46875" - 53.0623 )
- 2815.629 P (g.,3418.590 )
7 602.966 3262.3517 m
= 4.6696 P7 (1 + 1.0479) j
= 9.5628 P 7
for SA-302 3 NOD at 585'P is taken from Ref. 10 as e
,43.8 + [44.5 - 43.8).15 = 43.905 N 43.9 KSI
=
N.306
'Now c/cy 5
mil 088-0531A-BT01
~
l
-eem
,,g.s
'f v,.
EA WL-88-59-01,'_
!:. - c. ;.
0 4
Page 17 - of 36 Rev+
1
.i i
Therefore from Ref.
9,=
k.
Hg = 2.22' i
e Rewriting' Equations 6 & 7 Kgg > 2 KIN + KIT g
or i
KIR > 2 ON MN + ATmax NT
. f_
Therefore'at 1/4T -
1 i
Kgg'.) 2(10.061) P Mg + Atmas NT I
and at 3/478 1
2(9.563) P Hg + Atman NT Kgg )
I 1
' !: }
Solving for Pt.
j 1
For 1/478 P 5'_Kgg - M 67 T
2(10.061) Mg
)
For 3/478
- P$Kgg-MATeam 1
T 2(9.563) Mg si' k
i HIl088-0531A-BT01
.P
EA. NL-88-59-01
.:- = +..
Pag 2 18 of 36 ~
8 Rev 1
Substituting the' values of Mg & MT and multipling by 1000 (ksi to psi), the' equation becomes:
At 1/4T8 1'
f P 5 [ K g - ATeam (.268) ) (1000) 5 22.386 KIR - 6.0 ATmax I
(20.122) (2.22) i At 3/4T:
P.5 ( KIR - ATems (.268) ) (1000) 5 23.552 K a - 6.312 ATm.
I (19.126) (2.22) i since the tolerance on pressure is i 15 pois the heat up/cooldown equation'is written as follows:
L P 5 22.386 K g - 6.0 ATmax - 15 7
At 1/4T:
I P 5 23.552 K g - 6.312 Atmas - 15 At 3/4T:
I i
4 e
'B.
IN-SERVICE HYDROSTATIC TESTING - CRITICALITY TEMPSRATURE Since'the hydro is performed with the core not critical,.heatup rates are low and thermal' gradients 'through the wall are negligible. Therefore, the isothermal heatup condition will be employed for. the test pressure limits.
Only heatup rates need to be considered for the hydro and, according to Reference 8, the equations for K a during the hydro I
are KIR = 26.78 + 1.233 exp [0.0145 (T - RTNDT + 160))
mil 088-0531A-BT01 1
i v
.; n r '
FA NL-88-59-01
' i o
r
~ O! '
Page 19 cf..36
,, m n ~ -, '
'Rev 1
5 1
c.
. s
'(EQ.8).
a -:
- \\ -
- l l
K a > 1.5 Hg og-l
.,1 P
6
?
Therefore, using Equations 7 and 8 4
in
-I
-m ;,.
? <il, '
At 1/478.P 5 29.848 KIR -1$ for O'F/HR heat'up-
]
- 'u
- sic.
,t "
'At 3/4T P 5 31.403 KIR -15 3.
. u-
)
i?h,,.
l!(1j(
t f
f
],'
- h i
i
- gi!
1 kt 1
- l, i
- q.i
- \\.
. t
,'y '
inf s
b k
l.
i i
1' l'
ti
)
l l
l-mil 088-0531A-BT01 l
I l
1
2 1
- L
. %p'.
. u.a EA NL-88-59-01
.. - y
.Page:20 of 36-4
- Rey,
- j
+
TABLE 1-HEAT UP/ COOL DOWN TEMPERATURE CRADIENTS q
d 3fg ATsjg. af,,,
Temperature Change Rate AT
'F/HR
'F
'F
'F.
ri i;. -; !
0 0
0 0
l 20 2.71 4.92 5.19 40-5.42 9.84-10.39' 1
60 8.12 14.76 15.58 l
a 80 10.83 19.68
^^ 77 l
100 13.54 24.60
?5.96 Absolute.value of temperature difference between inside of AT3jg = reactor vessel wall and a point one-quarter of the way I
through the vessel wall.
ATs/g = Absolute value of-temperature difference between inside of.
reactor vessel wall and a point three-quarters of the way 4l through the vessel-wall..
i
~ Absolute value ofLtemperature difference.between.inside of 1
AT.
=
reactor vessel wall and a point on the vessel outer diameter.
t k
.i*__
4 mil 088-0531A-BT01 i
.b FA wt.sg.59-01 PSE' 21 of 36 Rev 1
PORVI'IA
SUMMARY
Notest
- 1) The AT,, tern has been deleted since the 1/4t section is in compression upon heat-up.
- 2) 7, is the temperature at the reactor vessel OD thermocouple (s).
- 3) AT,, -6Tx is the tern which adjusts the temperature to the flaw location.
Weld Metal: Section 1.1 Analysis
-178 +160 -5 + (AT,, - ATg jg)))
Heat up f 1/4tt KIR = 26.78 + 1.233 UP [.0145 (Tg P = 22.386 K, -15 3
Heat up 6 3/4t KIR = 26.78 + 1.233 EXP [.0145 (Ty -157 +160 -5 + (AT,,, - ATsjg)))
P = 23.552 K
-6.312 AT,,, -15 IR Cooldown 6 1/4t: K
= 26.78 + 1.233 EXP [.0145 (Ty -178 +160 (AT,, - ATg g)))
gg j
P = 22.386 K
-6.0 AT,,, -15 IR Cooldown f 3/4t K
= 26.78 + 1.233 n P [.0H5 (Tg -157 +160 (AT,,, - AT3jgD)
IR P = 22.552 KIR -6.312 AT,,,-15
-178 H60 -5))
Hydro-Test 0 1/4t Kgg = 26.78 + 1.233 EXP [.0145 (Tg (O'P/HR)
P = 29.848 K
-15 gg A M M 60 -5))
Hydro-Test 9 3/4tt Kgg = 26.78 + 1.233 2XP [.0145 (Tg (O'F/HR)
P = 31.403 K
-15 gg Base Plate: Section 1.1 Analysis 6.78 + 1.233 HP [.0H5 O -153 H60 -5 + (AT,,, - ATg j )))
Heat up 9 1/4tt K
=
g g
IR P = 22.386 K
-15 IR Heat up 9 3/4tt K, = 26.78 + 1.233 nP [.0145 (Tg -144 4160 -5 + ( AT,,, - AT3 g)))
3 f
IR AT,,, - M P = 23.552 K Cooldown 9 1/4t K3g = 26.78 + 1.233 EXP [.0145 (Ty -153 +160 (AT,, - ATg jg)))
P = 22.386 K
-6.0 AT,,, -15 IR M11088-0531A-BT01 1
\\ *.
PA WL-88-59-01 Pago 22 er 36 Rev 1
Base Platet Section 1.1 Analysis (cont'd) 26.78 + 1.2M EU [.0145 0,- m H 60 (67,,, - 673,)))
Cooldown f 3/4tt K a
7 gg P = 2 3.552 K
-6.312 AT,,, -15 gg Hydro-Test f 1/4tt Kgg = 26.78 + 1.233 En [.0W U -U3 m0 -M) y (O'P/HR)
P = 29.848 K
-15 gg Hydro-Test t 3/4tt E
= 26.78 + 1.233 En[.M U -W G0-M) gg g
(O'P/HR)
P = 31.403 K, ~15 g
~
Weld Metalt Section 2.1 Analysis EU (. W U - W M 60 -5 + (AT,,, - AT jg W Heat up $ 1/4tt'K
= 26.78 + 1.233 y
gg P = 22.386 K
-15 gg Heat up 9 3/4t: K
= 26.78 + 1.233 E U (. W U -122 6 -5 + (AT,,, - AT3fg)))
gg g
P = 23.552 K
-6.312 AT,,, -15 gg Cooldown f 1/4t K, = 26.78 + 1.233 EXP (.0145 (Ty -140 +160 (AT,,, - ATg jg)))
3 P = 22.386 K, -6.0 ' AT,,j -15 3
cooldown f 3/4tt K
= 26.78 + 1.233 m (.0145 (T -122 +160 (6T,,, - AT3jg)))
gg y
P = 23.552 K
-6.312 AT,,, -15 gg Hydro-Test 91/4tt K, = 26.78 + 1.233 EU [.M45 U -M C60 -M) g y
(O'F/HR)-
P c 29.848 K;g -15 Hydro-Test 9 3/4t K
= 26.78 + 1.233 EU (.0145 (T -122 M 60 -5))
gg y
(O'P/HR)
P = 31.403 E
-15 gg Base Platet Section 2.1 Analysis H 75 +160 -5 + (AT,,, - ATgj )))
Heat up t 1/4tt Kgg = 26.78 + 1.233 EU (.0145 (T g
y P = 22.386 K
-15 gg Heat up 9 3/4tt K
= 26.78 + 1.233 EU (.0145 (T -161 +160 -5 + (67,,, - AT3fg)))
gg y
P = 23.552 K
-6.312 AT,,, -15 yg nil 088-0531A-BT01
i yA W1,-88-59-01 i
Page 23 cf' 35 Rev 1
l l
Base Plater Section 2.1 Analysis (cont'd) j I
^
Cooldown f 1/4tt K
= 26.78 + 1.233 EXP [.0145 (T -175 +160 (AT,,, - afg j )))
g IR y
P = 22.386 K
-6.0 AT,,, -15
]
IR CooldoE+3/4ttK'=26.78+1.233EXP[.0145(T -162 +160 (AT,,, - AT3j )))
g g
N P = 23.552 K
-6.312 A,,,-15 T
IR Hydro-Test i 1/4tt K
= 26.78 + 1.233 E U [.0 W U - W +160 -5))
yg y
(O'F/NR)
P = 29.848 K
-15 IR Hydro-Test t 3/4tt Y
= 26.78 + 1.233 ED [.0145 (T -162 +160 -5))
j gg y
(O'F/HR)
P = 31.403 K
-15 gg NOTEt s'F is added to temperature ters to accomodate the temperature
~
measurement tolerance.
+
t l.
mil 088-0531A-BT01 L
l
s e
FA,NL-88-59-01 l
Page 24 et 3I
)
TABLE 2 - HEAT UF SEC.1.1 ANALYSIS WELD METAL - 1/4t LOCATION i
Pressure (psig) at Metal Temperature ('F)
Temperature i
Change Rate
'F/Hr 60*F.
100'F 150'F 200'F 250'F 275'F-0 631 668 758 943 1326 1650 (28.9)
(30.5)
(34.6)
(42.8)
(59.9)
(74.4) f i
20 633 671 764 957 1353 1689 i
(28.9)
(30.7)
(34.8)
(43.4)
(61.1)
(76.1) i 40 635 675 771 970 1381 1730-j (29.0)
(30.8)
(3!.l)
(44.0)
(62.4)
(77.9) 60 637 678 778 984 1411 1777 (29.1)
(30.9)
(35.4)
(44.7)
(63.7)
(79.8) 80 639 681 785 999 1441 1816 (29.2)
(31.1)
(35.7)
(45.3)
(65.0)
(81.7) 100 641 685 792 1014 1472 1861 (29.3)
(31.2)
(36.0)
(46.0)
(66.4)
(83.8)
TABLE 3 - HEAT UF SEC. 2.1 ANALYSIS WELD METAL - 1/4t LOCATION Pressure (psig) at Metal Temperature ('F) l Temperature Change Rate
'F/Hr 60*F_
100'F 150*F 200*F 250'F 275'F 0
666 730 886 1208 1871 2434 (30.4)
(33.3)
(40.2)
(54.6)
(84.2)
(109.4) 20 669 736 897 1230 1919 2502 (30.5)
(33.5)
(40.7)
(55.6)
(86.3)
(112.4) 40 672 741 909 1254 1968 2572 (30.7)
(33.8)
(41.2)
(56.7)
(88.5)
(115.5) 60 675 747 920 1279 2018 2645 I
(30.8)
(34.0)
(41.8)
(57.8)
(90.8)
(118.8) 80 679 753 933 1304 2071 2721 (31.0)
(34.3)
(42.3)
(58.9)
(93.2)
(122.2) 100 682 759 946 1331 2125 2799 (31,.1)
(34.6)
(42.9)
(60,1)
(95.6)
(125.7) l mil 088-0531A-BT01 l
I * "o '
'F.4 WL-88-59-01 Pye 25 or 36' o
TABLE 4 - HEAT UP SECTION 1.1 ANALYSIS _
WELD METAL f 3/4t LOCATION Pressure (psi 8) at Metal Temperature ('F)
Temperature Change Rate
_ 'F/Hr 60'F_
100*F 150*F 200'F 250'F 0
683 735 864 1128 1674 (29.6)
(31.8)
(37.3)
(48.5).
(71.7) 20 650 703 832 1097 1645 (29.6)
(31.9)
(37.3)
(48.6)
(71.9) 40 618 671 800 1066 1617 (29.6)
(31.9)
(37.4)
(48.7)
(72.0) 60 585
'639 768 1036 1588 (29.6)
(31.9)
(37.4)
(48.8)
(72.2) 80 553 606 736 1005 1550 (29.6)
(31.9)
(37.4)
(48.8)
(72.4) 100 520 574 705 974 1531 (29.6)
(31.9)
( 37..t)
(48.9)
(72.6)
TABLE 5 - HEAT UP SECTION 2.1 AHALYS_I_S,S WELD METAL f 3/4t LOCATION Pressure (psig) at Metal Temperature ('F)
Temperature Change Rate
'F/Hf 60'F_
100'F 150*F 200*F 250*F 0
727 815 1028 1467 2374 (31.5)
(35.2)
(44.2)
(62.9)
(101.4) 20 695 783 997 1437
.2348 (31.5)
(35.2)
(44.3)
(63.0)
(101.7) 40 662 751 965 1408 2322 (31.5)
(35.3)
(44.4)
(63.2)
(102.0)60-630 719 934 1379 2296 (31.5)
(35.3)
(44.5)
(63.3)
(102.3) 80 598 687 903 1349 2271 (31.6)
(35.3)
(44.5)
(63.5)
(102.6) 100 565 655 872 1320 2245 (31.6)
(35.4)
(44.6)
(63.66 (102.9)
M11088-0531A-BT01
. FA WL-88-59-01
' 7 ' *-
+
D Pag 2 26 of 36 Rev 1
TABLE 6 - HEAT lit SECTION 1.1 ANALYSIS, BASE PLATE - 1/4t LOCATION Pressure (peig) at Metal Temperature ('F)
Temperature hHr
_6'f F _
100'F 150'F 200'F 250'F 0
652 705 834 1100 1650 (29.8)
(32.1)
(37.9)
(49*8)
(70'4) 20 654 710 843 1119 1689 (29.9)
(32.3)
(38.3)
(50.6)
(76.1) 40 657 714 853 1139 1730 (30.0)
(32.5)
(38.7)
(51.5)
(77.9) 60 '
660 719 863 1159 1772 (30.1)
(32.8)
(39.2)
($2.4)
-(79.8) 80 662 724 873 1180 1816 (30.2)
(33.0)
(39.6)
(53.4)
(81.7) 100 665 729 883 1202 1861 (30.4)
(33.2)
(40.1)
(54.4)
(83.8)
TABLE 7 - HEAT 11F: SECTION 2.1 ANALYSIS BASE PLATE - 1/4e LOCATION Pressure (psig) at Metal Temperature (*F)
Temperature Change Rate
'F/Hr
,60'F 100'F 150'F 200'F 250'F 0
633 672 766 959 1359 (28.9)
(30.7)
(34.9)
(43.5)
(61.4) 20 635 675 772 973 1387 (29.0)
(30.8)
(35.1)
(44,1)
(62.6) 40 637 679 779 9f>7 1417 (29.1)
(31.0)
(35.5)
(t4.8)
(63.9) 60 639 682 787 1002 1448 (29.2)
(31.1)
(35.8)
(45.4)
(65.3) 80 641 686 794 1018 1479 (29.3)
(31.3)
(36.1)
(46.1)
(66.7) 100 643 689 802 1033 1512 (29.4)
(31.4)
(36.5)
(46.8)
(68.2)
M11088-0531A-BT01
+
.u
.'E EA WL-88-59-01 l
Tage 21 ct 31 Rev 1
TABLE 8 - HEAT _UP: SECTION 1.1 ANALYSIS l
BASE PLATE - 3/4t LOCATION Pressure (psig) at Metal Temperature (*F)
?emperature Change Rate
'F/Hr 60'F 100'F 150'T 200'F 250'F 0
697 760 915 1234 1893 '
(30.2)
(32.9)
(39.5)
(53.0)
(81.0) t 20 664 728 883 1204 1866 i
(30.2)
(32.9)
(39.5)
(53.1)
(81.2) 40 632 696 852 1174 1838 l
(30.2)
(32.9)
(39.6)
(53.2)
(81.4)
I 60 599-664 820 1143 1810 l
(30.2)
(33.0)
(39.6)
(53.3)
(81.6) 80 567 632 789 1113 1783 i
(30.2)
(33.0)
(39.7)
(53.4)
(81.9) 100 334 599 757 1083 1755 (30.3)
(33.0)
(39.7)
(53.5)
(82.1)
TABLE 9 - HEAT UP: SECTION 2.1 ANALYSIS BASE Pl. ATE - 3/4t LOCATION Pressure (psig) at Metal Temperature ('F)
Temperature change Rate
'F/Hr 60'F 100*F 150'F 200'F 250'F l
0 678 727 846 1092 1600 (29.4)
(31.5)
(36.5)
(47.0)
(68.5) 20 645 695 814 1061 1571 (29.4)
(31.5)
(36.6)
(47.1)
(68.7) 1.42 40 613 662 782 1030 (29.4)
(31.5)
(36.6)
(47.1)
(68.9)
+
60 580 630 751 999 1513 (29.4)
(31.5)
(36.7)
(47.2)
(69.0) 80 548
(?O 719 969 1484 (29.4)
(31.6)
(36.7)
(47.3)
(69.2) 100 515 565 687 938 1455 (29.4)
(31.6)
(36.7)
(47.4)
(69.4) mil 088-0531A-BT01 l
FA NL-88-59-01 r
Page 28 et 36 Rev 1
I TABLE 10 COOL DWN SECTION 1.1 ANALYSIS i
WELD META 1,,- 1/4t LOCATION Fressure (psig) at Metal Temperature ('F) j Temperature Change Rate
- F/Hr 60'F _
100'F 150*F 200*F 250'F 275'F
{
0 631 668 758 943 1326 1650 t
(28.8)
(30.5)
(34.5)
(42.8)
(59.9)
(74.4) 20 598 634 721 900 1269 1581 (28.8)
(30.4)
(34.2)
(42.2) (58.7)
(72.7) 40 566 600 684 856' 1212 1514 l
(28.7)
(30.2)
(34.0)
(41.7)
(57.6)
(71.0) 60
$33 566 647 813
!!$6 1447 r
l (28.6)
(30.1)
(33.7)
(41.1)
(56.5)
(69.5) 80 500
$32 610 771 1102 1382 (28.6)
(30.0)
(33.5)
(40.6)
(55.4)
(68.0) 100 468 499 574 728 1048 1319 (28.5)
(29.9)
(33.2)
(40.1)
(54.4)
(66.5)
TABLE 11 COOL DOWN SECTION 2.1 ANALYSIS WELD METAL - 1/4t LOCATION Fressure (psig) at Metal Temperature ('F)
Temperature Change Rate
'F/Hr 60'F 100'F 150'F 200'F 240'F 275'?
4 0
666 730 886 1208 1871 2434 I
(30.4)
(33.3)
(40.2)
(54.6)
(84.2)
(109.4) 20 632 694 844 1154 1795 2337 l_
(30.3)
(33.0)
(39.7)
(53.6) (82.2)
(106.4) 40 598 658 803 1102 1720 2243 (30.1)
(32.8)
(39.3)
(52.6)
(80.2)
(103.6) 60 564 622 762 1050 1646 2151 (30.0)
(32.6)
(38.8)
(51.7)
(78.?]
(100.9) 80 550 586 721 999 1574 2061 (29.9)
(32.4)
(38.4)
(50.8)
(76.5)
(98.3) 100 497 550 680 949 1503 1973 (29.8)
(32.2)
(38.0)
(50-0)
(74.8)
(95.7) mil 088-0531A-BT01
~
.~-
i FA NL-88-59-01 Pago 29 cf 3 Rev I'
, TABLE 12 - COOL DOWN: $ECTION 1.1 ANALYSIS l
WELD METAL - 3/4t LOCATION-
]
Pressure (psig) at Metal Temperature ('F)
Temperature Change Rate
'F/Hr 60'F
,_100'F 150'?
20C'F 250'F 0
683 735 864 1128 1674 (29.6)
(31.8) ' (37.3)
(48.5)
(71.7) 20 650 702 830 1093 1637 (29.6)
(31.8)
(37.2)
(48.4)
(71.5) 40 616 669 796 1058 1600 (29.6)
(31.8)
(37.2)
(48.3)
(71.3)
636 762 1024 1563 i
(29.6)
(31.8)
(37.1)
(48.2)
(71.1) 80 550 602 729 989 1526 (29.5)
(31.8)
(37.1)
(48.2)
(71.0)
' i i
100 517 569 695 954 1489 (29.5)
(31.7)
(37.1)
(48.1)
(70.8)
)
TABLE 13 - COOL DOWNt SECTION 2.1 ANALYSIS WELD METAL - 3/4t LOCATION Pressure (psig) at Metal Temperature ('F)
)
Temperature Change Rate
'F/Hr 60'F 100'F 150'F 200'F 250'F 0
727 815 1028 1467 2374 (31.5)
(35.2)
(44.2)
(62.9)
(101.4) 20 694 781 993 1431 1334 (31.5)
(35.2)
(44.2)
(62.7)
(101.1)
]
1.
40 661 748 959 1395 2294 (31.4)
(35.1)
(44.1)
(62.6)
(100.8)
]
60 627 714 924 1358 2255
)
(31.4)
(35.1)
(44.0)
(62.5)
(100.5) 80 594 681 890 1322 2215 (31.4)
(35.1)
(44.0)
(62.3)
(100.2) 100 561 647 856 1268 2175 (31.4)
(35.0)
(43.9)
(62.2)
(99.9) mil 088-0531A-BT01
. - - -. ~
w-vn ne~
r-=
' ~* " '
gA WL-88-59-01
' ' ' * " /
Pag) 30 of 36 Rev 1
L TABLE 14 - COOL DOWNt SECTION 1.1 ANALYSIS
. BASE PLATE - 1/4t LOCATION Pressure (psig) at Metal Temperature (*F)
Temperature Change Rate
'F/Hr 60'F 100'F 150*F 200'F 250'F 275'F 0
657 705 834 1100 1650
'(29.8)
(32.1)
(37.9)
(49.8)
(74.4) 20 618 670 794 1051 1581 (29.7)
(31.9)
(37.5)
(49.0)
(72.7) 40 585 634 754 1002 1514 1947 (29.5)
(31.8)
(37.1)
(48.2)
(71.0)
(90.46) 60 551 599 715 954 1447 1866' (29.4)
(31.6)
(36.8)
(47.4)
(69.5)
(88.2) 80 518 564 676 906 1382 1786 (29.4)
(31.4)
(36.4)
(46.7)
(68.0)
(86.0) 100 485 529 637 860 1319 1708 (29.3)
(31.2)
(36.1)
(46.0)
(66.5)
(83.9)
TABLE 15 - COOL DOWNt SECTION 2.1 ANALYSIS BASE PLATE - 1/4t LOCATION Pressure (ps18) at Metal Temperature ('F)
Temperature Change Rate
'F/Hr 60'F 100'F 150'F 200'F 250'F 275'F 0
633 672 766 959
'1359 1698 (28.9)
(30.7)
(34.9)
(43.5)
(61.4)
(76.5) 20 600 638 728 915 1301 1627 (28.9)
(30.5)
(34.6)
(42.9)
(60.1)
(74.7) 40 568 604 691 871 1243 1558 (28.8)
(30.4)
(34.3)
(42.3)
(58.9)
(73.0) 60 535 570 654 827 1186 1490 (28.7)
(30.3)
(34.0)
(41.8)
(57.8)
(71.4) 80 502 536 617 784 1130 _
1424 (28.6)
(30.1)
(33.8)
(41.2)
(56.7)
(69.8) 100 469 502 580 742 1076 1358 (28.6)
(30.0)
(33.5)
(40.78)
(55.6)
(68.3) nil 088-0531A-BT01
,u yA NL-88-59-01
.;4'.-
Pass 31 of 36 TABLE 16 - COOL DOWNt SECTION 1.1 ANALYSIS BASE PLATE - 3/4t LOCATIDM Pressure (psig) at Metal Temperature ('F)
Temperature Change Rate
'F/Hr 60*F 100'F 150'F 200'F 250'F 0_
697 760 915 1234 1893 (30.2)
(32.9)
(39.5)
(53.0)
(81.0) 20 663 727 881 1199 1856 (30.2)
'(32.9)
(39.4)
(52.9)
(80.8) 40 630 694 847 1164 1818 (30.2)
(32.8)
(39.4)
(52.8)
(80.6) 60 597 660 813 1129 1780 (30.1)
(32.8)
(39.3)
(52.7)
(80.4) 80 564 627 779 1093 1742 (30.1)
(32.8)
(39.3)
(52.6)
(80.1) 100 531 594 745 1058 1705 (30.1)
(32.8)
(39.2)
(55.2)
(79.9)
TABLE 17 - COOL DOWN SECTION 2.1 ANALYSIS BASE PLATE - 3/4t LOCATION Pressure' (psig) at Metal Temperature ('F)
Temperature Changa Rate 60*F
_100*F 150'F 200'F 250'F
'F/Hr ___
0 678 727 846 1092 1531 (29.4)
(31.5)
(36.5)
(47.0)
(68.5) 20 645 694 813 1057 1963 (29.4)
(31.5)
(36.5)
(46.9)
I,68.4) 40 612 661 779 1023 1526 (29.4)
(31.4)
(36.5)
(46.8)
(68.2) 60 579 627 745 988 1490 (29.4)
(31.4)
(16.4)
(46.7)
(68.0) 80 546 594 711 953 1543 (29.3)
(31.4)
(36.4)
(46.7)
(67.9) 100 513 561 678 919 1417 (29.3)
(31.4)
(36.3)
(46.6)
(67.7) mil 088-0531A-BT01
yA NL*.88-59 01
. : i at *.,
Page 32 of 36 Rev 1
TABLE 18 - HYDRO TEST: SECTICN 1.1 ANALYSIS WELD META 1: - 1/4t LOCATION Pressure (psig) at Metal Temperature ('F)
Temperature c
Change Rate
'F/Hr 60'F 100'F
_150'F.
200'F 250'F 0
847 996 1016 1263 1773 (28.8)
(30.$)
(34.5)
(42.8)
(59.9)
WELD METAL - 3/4t LOCATION Pressure (psig) at Metal Temperature (*F)
Temperature Change Rate-
'F/Hr
_60'F_
100'F 150'F 200*F 250'F 0
915 986 1157
' 1~509 2237 (29.6)
(31.8)
(37.3)
(48.5)
(71.7) t
)
mil 088-0531A-BT01 l
l
--n FA WL-88-59-01 Fase 33 of 5I Rev 1
TABLE 19 - HYDRO TEST: SECTION 2.1 ANALYSIS WELD HETAL - 1/4t LOCATION Fressure (psig) at Metal Temperature ('F)
Temperature Change Rate
- F/Hr 60'F 100'F 150'F 200'F 250'F o
893 979 1186 1615 2500 (30.4)
(33.31 (40.27)
(54.6)
(84.2)
WELD METAL - 3/4e LOCATION Fressure (psig) at Metal Tenperature ('F)
Temperature Change Rate
'F/Br 60'F 100'F 150'F 200'F 0
975 1092 1375 1961 (31.5)
(35.2)
(44.2)
(62.9) e 4
mil 088-0531A-BT01
,7, ), ',
FA Ntr88-59-01 Faga 34 et 36 Rev 1
I YABLE 20 - HYDRO TEST: SECTION 2.1 ANALYSIS l
BASE PLATE METAL - t/4C LOCATION Pressure (psig) at Metal Temperature (*F)
Temperature Change Rate
(
'F/Hr 60'F_
100
- F_
150*F 200*F 250'F 0
856 901 1026 1284.
1817 (28.9)
(30.7)
(34.9)
(43.5)
(61.4)
)
WELD METAL - 3/4e LOCATION 1
Fressure (psig) at Netal Temperature (*F)
Temperature Change Rate
'F/Hr 60*F 100'F 150'F 200'F 250'F i
0 909 975 1133 1461 2138 (29.4)
(31. 5)
(36.5)
(47.0)
(68.5) l mil 088-0531A-BT01
-.=.
F.4 ' NL-88-59-01 i
Page 35 er 36 j
Rev 1
.i
- Tall,E 21 - HYDRO TEST SECTION 1.1 ANALYSIS l
a BASE PLATE METAL - 1/4t LOCATION Pressure (psig) at Metal Temperature (*F) l Temperature Change Rate
'F/Hr 60'F_
100'F 150'F 200'F 250'F j
0 874 945 1117 1362 2205 (29.8)
(32.1)
(37.9)
(46.1)
(74.4)
I l
WELD METAL - 3/4t LOCATION l
Pressure (psis) at Metal Temperature ('F)
Temperature j
Change Rate
'F/Hr 60'F_
100*F 150'F 200*F 250'F j
0 934 1019 1225 1651 2530 (30.2)
(32.9)
(39.5)
(53.0)
(81.0) i 9
1 1
i 1
mil 088-0531A-BT01 l
. - ~
o i...
ya ML-88-59-01
.'. y e.
e Page 36 cf 3I j
R;v 1
i TABLE 22'- LIMITING HEAT UP - ALL RATES Pressure (psig) at Metal Temperature (*F)
'F 60'F 100*F 150'F 200'F 250'F l
psig 515 565 687 938 1325 3/4.BP 2.1*
3/4,BP.2.1*
3/4,BP.2.1,*'
3/4,BP.2.1*
1/4,W,1,1*
LIMITING COOL DOWN - ALL RATES Pressure (psig) at Metal Temperature ('F)
'F 60'F 100'F 150'F 200'F 250'F 275'F-psig 468 499 574 728 1048 1319 1/4,W,1.1*
1/4,W,1.1*
1/4 W,1.1*
1/4,W,1.1*
1/4 W,1.1*
1/4,W,1,18-l
- Location, Material Analysis Notest 1
1/4 = 1/4t Location 3/4 = 3/4t Location W
= Weld Metal B,P. - Base Plate 1.1 - Section 1.1 Analysis 2.1 = Section 2.1 Analysis
]
M11088-0531A-BT01 I
FigureL,1($)
1Ld o l' k
BIG ROCK PolNT NUCLEAR PLANT:
PRES 5URE TEMPT.tATURE LIMITS EFFECTIVE TO tt EFFECTIVE g
FULL POWER YEARS FLANGE RTNot e 40*F NEATMP CONDITl0N 5000 UNES ARE NON CRITICAL CONDm0N DASHED UNES ARE CRITICAL CONDITION i
i
/
1600 -
i I
,,00 -
l I
I 1400 -
I
/
II" "
NON. CRITICAL t
l' UMITING HEATUP g
/
ALL RATE 5
/
/
1200 -
/
/
/
1100 -
/
1 b
i 1000 -
/
/
/
900 -
/
CORE CRITICAL l
/
UMITING HEATUP
/
ALL RATES 800--
l I
l 700 -
l 4
600 -
1 425
d 400 -
100 -
l :
LOWER UMIT OF CRITICAUTY 1
-t
..)
0 l
i i
i I
60 100 150 200 250 300 350 400 REACTOR VE55EL METAL TEMPERATURE,*F Proposed
r;
}
L,*'**[
Figure t.1(b)
[
- g.. # $
l' e g
866 ROCK PolNT NUCLEAR PLANT:
PRESSURE TEMPERATURE LIMITS EFFECTIVE TO18 EFFECTWE j
FULL POWER YEARS-l PLANGE ATest = 40'F C00LDOWN CONDm0N l
5000 UNE5 ARE NON4RmCAL CONOm0N OASHED UNE5 ARE CRmCAL CONDm0N i
1500 -
t 1400 -
i I
1300 -
p I
i i
1300 -
l
\\
l 5
NON CRmCAL i
1100 -
UMmNG COOLDOWN g i
.r ALL RATES '
//
j 1000 =
/
/
900 -
l
/
/
e00 -
l l
/ % CORE CRITICAL UMmNG COOLDOWN
/
700 -
,/
ALL gAygg i
i 600 -
1
.g _
s 100 -
I LOWER UMit OF CRmCAUTY I
i' 0
i 60 100 150 200 250 300 350 400 L
j REACTOR VE35Ei METAL TEMPERATURE,'F Proposed I
9