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=Text=
=Text=
{{#Wiki_filter:.                   .      -
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O ATTACNMENT B TENNESSEE VALLEY AUTHORITY SEQUOYAH NUCLEAR PLANT (SQN)
O ATTACNMENT B TENNESSEE VALLEY AUTHORITY SEQUOYAH NUCLEAR PLANT (SQN)
UNITS 1 AND 2 SUPPLEMENTAL RESPONSE TO GENERIC LETTER (GL) 95 PRESSURE LOCKING AND THERNAL BINDING OF SAFETY-RELATED PONER OPERATED GATE VALVES 3-INCil AND 4-INCli 1500# VELAN VALVE TEST AND CALCULATED PRESSURE LOCKING RESULTS FOR SON VALVES 4
UNITS 1 AND 2 SUPPLEMENTAL RESPONSE TO GENERIC LETTER (GL) 95 PRESSURE LOCKING AND THERNAL BINDING OF SAFETY-RELATED PONER OPERATED GATE VALVES 3-INCil AND 4-INCli 1500# VELAN VALVE TEST AND CALCULATED PRESSURE LOCKING RESULTS FOR SON VALVES 4
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VM R & D Department o
        , ..-        VM                                                     R & D Department Test and Calculated Results RD 466 Pressure Locking FOB INF0By AT10F '00 RD-466 Tennessee Valley Authority Sequoyah Nuclear Plant P.O. Box 2000 - STB-4A Soddy Daisy, TN 37379 Velan P.O. No.: P9-81035-K T.V.A. Order No.: P-96N4E-176161 Velan Dwo. No.:             Size and Flaure No.:
Test and Calculated Results RD 466 Pressure Locking FOB INF0By AT10F '00 RD-466 Tennessee Valley Authority Sequoyah Nuclear Plant P.O. Box 2000 - STB-4A Soddy Daisy, TN 37379 Velan P.O. No.: P9-81035-K T.V.A. Order No.: P-96N4E-176161 Velan Dwo. No.:
88405 2                     3" B10-30548-13MS 88415-2                     3" B10-3054813MS 88521-3                     4" B12-20548-13M 88517-3                     4" B12-3054B-13M
Size and Flaure No.:
                                                                                        *          \
88405 2 3" B10-30548-13MS 88415-2 3" B10-3054813MS 88521-3 4" B12-20548-13M 88517-3 4" B12-3054B-13M
                                                          ?                           a.u. re r t Compiled By:          /        ,
\\
                                                                  /1A/W                 M!i.=.'' '
?
a.u. re r t
/1A/W M!i.=.'' '
Compiled By:
/
! John M. Farrell, Eng.
MC"
MC"
                                                    ! John M. Farrell, Eng.
'Vice,-#residen, Engineering I~::
                                                    'Vice,-#residen , Engineering Reviewed By: ./ I~::                ~
Reviewed By:./
Eemewy         l
~
: k. Isbitsky, Eng, Manager, Stress Dept.                     ,
Eemewy
DATE:                 bY:                       RE V.:             PAGE No:
: k. Isbitsky, Eng, l
!                Auaust 5.1997           J.M. Farroll                   1                     i 1                                                                                                   -
Manager, Stress Dept.
DATE:
bY:
RE V.:
PAGE No:
Auaust 5.1997 J.M. Farroll 1
i 1


kYM                                                             R & D Departm:nt i
kYM R & D Departm:nt i
Test and Calculated Results Pressure Locking                                     RD466 l
Test and Calculated Results RD466 Pressure Locking
                                                                        -nn tungppTTinpf UN'l:V l       CERTIFICATE of COMPLIANCE:
-nn tungppTTinpf UN'l:V l
CERTIFICATE of COMPLIANCE:
We hereby certify that the following data are in compilance with the applicable purchase order:
We hereby certify that the following data are in compilance with the applicable purchase order:
CUSTOMER:           Tennessee Valley Authority CUSTOMER P.O.: P-96N4E-176161 VELAN P.O.:         P9-81035 K DESCRIPTION:         Test and Calculated Results - Pressure Locking Signature.              blYb/AM n                           u nmd       l W/
CUSTOMER:
Tennessee Valley Authority CUSTOMER P.O.: P-96N4E-176161 VELAN P.O.:
P9-81035 K DESCRIPTION:
Test and Calculated Results - Pressure Locking blYb/AM n u nmd l
Signature.
John M. Farrell, Eng.
John M. Farrell, Eng.
                                              ,/
W/
,/
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==Title:==
==Title:==
Vice President, Engineering Date:               Original: July 7th,1997 Revised: August 5th,1997 DATE:                 BYi                             REY.:             PAGE No:
Vice President, Engineering Date:
Auaust S.1997             J.M. Farrell                       1                   il
Original: July 7th,1997 Revised: August 5th,1997 DATE:
BYi REY.:
PAGE No:
Auaust S.1997 J.M. Farrell 1
il


      .. VVfLAN                                                     a a o oepartment Test and Calculated Results Ro46a.
VVfLAN a a o oepartment Test and Calculated Results Ro46a.
Pressure Locking TOliINFliffMXTION UKY 2       PECORD of REVIS1QN1 A
Pressure Locking TOliINFliffMXTION UKY 2
Her       Descriotion:         Dy/Date:                 Cert _ By / Date:
PECORD of REVIS1QN1 A
A      %
Her Descriotion:
0          Initial Release      J.M. Fbr[ ell, Eng.Hsbitsky, /p/ .3Eng. -
Dy/Date:
July 7,1997             July 8,1997
Cert _ By / Date:
                                                  .-                                          ,/
J.M. Fbr[ ell, Eng. /p/.3 -
1         Revised per         J.M. F 5 rell, Eng. /     sis i 5(E6g. t customer             Augtist 5,1997         August 5,1997 comments, n             -
A Hsbitsky, Eng.
e DATE:                 BY:                     REV.:               PAGE No:
0 Initial Release July 7,1997 July 8,1997
Auoust 5.1997           J M Farrell               1                       iii
,/
1 Revised per J.M. F 5 rell, Eng. /
sis i 5(E6g. t customer Augtist 5,1997 August 5,1997
: comments, n
e DATE:
BY:
REV.:
PAGE No:
Auoust 5.1997 J M Farrell 1
iii


VM R & D Departm:nt Test and Calculated Results RD 466 Pressure Locking
VM R & D Departm:nt Test and Calculated Results RD 466 Pressure Locking FOR INF0RMXTI0F0NEY
                                                                ~~                   ~
~~
FOR INF0RMXTI0F0NEY 3     TABLE of CONTENISJ P_aga
~
: 1. Certificate af Compliance                                     il
3 TABLE of CONTENISJ P_aga 1.
: 2. Record of Revision                                           ill
Certificate af Compliance il 2.
: 3. Table of Contents                                             iv
Record of Revision ill 3.
: 4. Summary of Test Pesults & Analysis                           1
Table of Contents iv 4.
: 5. Appendix 'A' - Test Results                                   A1
Summary of Test Pesults & Analysis 1
: 6. Appendix 'B' - Supplementary Data                             B1 t           -
5.
Appendix 'A' - Test Results A1 6.
Appendix 'B' - Supplementary Data B1 t
I I
I I
DATE:                 BY;                   REY.:           PAGE feo:
DATE:
Auaust 5.1997           J.M. Farrell           1                       iv
BY; REY.:
PAGE feo:
Auaust 5.1997 J.M. Farrell 1
iv


    .          VELAN                                                     R & D Departm:nt Test and Calculated Results RD-466 Pressure Locking                                                       l
VELAN R & D Departm:nt Test and Calculated Results RD-466 Pressure Locking l
: 1)     It[TRODUCTl01h                                   FOR INF6RMXTOW Unry Under a purchase order from T.V.A. tests were carried out on a 3" 1500 lb. Velan gate valve in order to determine the amount of pressure locking which occurred due to various cavity pressures and differential pressures. The resuits of the tests were compared with those of an analytical model with the intent of using this analytical model to evaluate the   i potential for pressure socking in similar valves at the T.V.A. Sequoyah plant.
FOR INF6RMXTOW Unry 1)
: 2)     IEST EQUIPMENT:
It[TRODUCTl01h Under a purchase order from T.V.A. tests were carried out on a 3" 1500 lb. Velan gate valve in order to determine the amount of pressure locking which occurred due to various cavity pressures and differential pressures. The resuits of the tests were compared with those of an analytical model with the intent of using this analytical model to evaluate the i
potential for pressure socking in similar valves at the T.V.A. Sequoyah plant.
2)
IEST EQUIPMENT:
The tests were carried out on a Velan 3" 1500 lb. t; ate valve with a configuration corresponding to Velan drawing No. BR415 2 which is the drawing number for one of the valves under !nvestigation at T.V.A. As back-up data he results of a previous test performed on a 10" 1500 lb. Velan gate valve (Dwg. Nc 88802-1) are presented to substantiate the analytical model used. The results from a (Urd test, on a Velan 10" 300 lb. API 600 gate valve are also reviewed.
The tests were carried out on a Velan 3" 1500 lb. t; ate valve with a configuration corresponding to Velan drawing No. BR415 2 which is the drawing number for one of the valves under !nvestigation at T.V.A. As back-up data he results of a previous test performed on a 10" 1500 lb. Velan gate valve (Dwg. Nc 88802-1) are presented to substantiate the analytical model used. The results from a (Urd test, on a Velan 10" 300 lb. API 600 gate valve are also reviewed.
All valves are clamped in a fixture and pressurised by means of a hydraulic pump connected to the bonnet of the valve. Details are given in report RD 459.
All valves are clamped in a fixture and pressurised by means of a hydraulic pump connected to the bonnet of the valve. Details are given in report RD 459.
: 3)     TEST RESULTS:
3)
TEST RESULTS:
The test results for the 3" valve are given in RD-459 (Appendix 'A'). The results of the tests on the 10" 1500 lb. and 10" 300 lb. valves are also included in Appendix 'A'.
The test results for the 3" valve are given in RD-459 (Appendix 'A'). The results of the tests on the 10" 1500 lb. and 10" 300 lb. valves are also included in Appendix 'A'.
: 4)     ANALYSIS of TEST RESULTS Nomenclature:
4)
ANALYSIS of TEST RESULTS Nomenclature:
The following nomenclature is used:
The following nomenclature is used:
T,,    =      Total opening load - Ibf. from tests.
Total opening load - Ibf. from tests.
Tw    =       Static unwedging load - Ibf. from tests, gf    =       Gland friction load - Ibf. from tests.
T,,
=
Static unwedging load - Ibf. from tests, Tw
=
Gland friction load - Ibf. from tests.
gf
=
Stem piston effect Ibf.
Pe
Pe
                    =       Stem piston effect Ibf.
=
Pt    =      Pressure locking load - Ibf.
Pressure locking load - Ibf.
Po    =       Differential pressure load -Ibf.
P
X      =       Difference between test and calculated loads - Ibf.
=
oATE:                     en                       REY.:                 PAGE No:
t Differential pressure load -Ibf.
Atmst 5,1997               J M. Farrell                 1                         1 of 3
Po
=
Difference between test and calculated loads - Ibf.
X
=
oATE:
en REY.:
PAGE No:
Atmst 5,1997 J M. Farrell 1
1 of 3


7VfLAN                                                                   a a o oepartm:nt Test and Calculated Results Pressure Locking RD46
7VfLAN a a o oepartm:nt Test and Calculated Results RD46 Pressure Locking FOR INFORMATION ONEY 4) musis of Test assutrs remem Inillally the intention was to use the analytical method of Com. Ed. given in Nureg/CP-0152 for evaluating the pressure locking load. However, it had been found in the test on the 10" 1500 lb. Velan gate valve that no seat loading due to deflection of tha wedge plates in the axis of the valve bore centerline was detested. (Rnf. Nureg/CP-0146 Velan paper), in the results of the tests on the 3" 1500 gate valve, again no significant effect of wedge plate deflection could be seen.
: 4)     musis of Test assutrs remem                           FOR INFORMATION ONEY Inillally the intention was to use the analytical method of Com. Ed. given in Nureg/CP-0152 for evaluating the pressure locking load. However, it had been found in the test on the 10" 1500 lb. Velan gate valve that no seat loading due to deflection of tha wedge plates in the axis of the valve bore centerline was detested. (Rnf. Nureg/CP-0146 Velan paper), in the results of the tests on the 3" 1500 gate valve, again no significant effect of wedge plate deflection could be seen.
Therefore it was decided that the deflection of the wedge plate would be ignored, and only the downward force component due to the cavity pressure acting on the wedge would be considered. In the equation that is used, an unknown factor X is used which shows the deviation of the calculated from the test results.
Therefore it was decided that the deflection of the wedge plate would be ignored, and only the downward force component due to the cavity pressure acting on the wedge would be considered. In the equation that is used, an unknown factor X is used which shows the deviation of the calculated from the test results.
The equation used is then:
The equation used is then:
T,,    =        Tw & gf - Pc + Pt + Po + X                                               (1)
Tw & gf - Pc + P + Po + X (1)
IIIII Using the following dimensional data:                                                   fliw    '
T,,
g   i d,      =        Valve stem diameter -ins,                     ddb -           +             D D      =       Valve mean seating fall diameter - ins.                 -      -
=
0      =       Valve' seat angle - degrees.                               ,        ,
t IIIII fl i
Y p      =       Valve seating / unseating factor - 0.3 assumed.               ggg p       =       Cavity pressure - psig.                                         p delP    =       Differential pressure across wedge - psi.
Using the following dimensional data:
2 T,,    =        Tw + gf - 0.785 d,2 p + 2 x 0.785 D       pSinD + 0.765pD2 delP + X.~(2)
g iw Valve stem diameter -ins, ddb -
+
D d,
=
Valve mean seating fall diameter - ins.
D
=
Valve' seat angle - degrees.
Y 0
=
Valve seating / unseating factor - 0.3 assumed.
ggg p
=
Cavity pressure - psig.
p p
=
Differential pressure across wedge - psi.
delP
=
2 2
Tw + gf - 0.785 d,2 p + 2 x 0.785 D pSinD + 0.765pD delP + X.~(2)
T,,
=
Using the above equation and the results of the tests on the 3" and 10" 1500 lb. valves the results shown in Table 1 were obtained. it will be seen from Table 1 that the variation between test and calculation is not large, sometimes positive and sometimes negative.
Using the above equation and the results of the tests on the 3" and 10" 1500 lb. valves the results shown in Table 1 were obtained. it will be seen from Table 1 that the variation between test and calculation is not large, sometimes positive and sometimes negative.
This suggests that the method of calculation is reasonable.
This suggests that the method of calculation is reasonable.
A possible cxplanation of this is that, for this particular valve design, the wedge is relatively much less flexible than the body. That is, the assumption that the seats are fixed is overly conservative.
A possible cxplanation of this is that, for this particular valve design, the wedge is relatively much less flexible than the body. That is, the assumption that the seats are fixed is overly conservative.
1 Further discussion of this conclusion if given in Appendix 'B'.                     -
1 Further discussion of this conclusion if given in Appendix 'B'.
DATE:                       SY:                       REV.:                       PAGE No:
DATE:
Atpst 5,1997                 JM Farrell                   1                           2 of 5
SY:
REV.:
PAGE No:
Atpst 5,1997 JM Farrell 1
2 of 5


          ,          VfM                                                                               R & D D:partm:nt Test and Calculated Results RD-466 Pressure Locking FOR INFORM ATION ON1.Y
VfM R & D D:partm:nt Test and Calculated Results RD-466 Pressure Locking FOR INFORM ATION ON1.Y P_REf}1GIl_QR of OPENING LOAD includina PRESSURE LOCKING:
: 5)      P_REf}1GIl_QR                     Q          of OPENING LOAD includina PRESSURE LOCKING:
Q 5)
Using the equation (2), the calculated opening loads for the T.V.A. valves are given in Tabia 2.
Using the equation (2), the calculated opening loads for the T.V.A. valves are given in Tabia 2.
i The pressures are taken from Attachment 1 in Appendix 'B'. The data were supplied by T.V.A It is assumed that the unwedging load includes the packing friction; therefore gf is shown as zero in the table.
The pressures are taken from Attachment 1 in Appendix 'B'. The data were supplied by i
: 6)       CONCLUSlDNS1 For the particular design of valve analysed, Vs'an 3" and 4" 1500 lb. gate valves, the amount of pressure locking which occurs due to cavity pressure is reasonably predictable by assuming that only the downward component of the cavity pressure load on the wedge (reverse piston effect) is effective.
T.V.A It is assumed that the unwedging load includes the packing friction; therefore gf is shown as zero in the table.
In other designs, this assumption may not be valid. In fact the results obtained on a 10" t                    300 lb. Velan gate valve showed considerable effect due to the deflection of the wedge plates. The conclusion is that the relative flexibilities of the wedge and the body must be taken into account and the assumption of fixed seats is valid only in some cases, in most cases a simple analysis of the relative flexibilities would not be very accurate, end finite element methods would be recommended.
6)
i DATE:                                                   BY:                   REV.:             PAGE No:             )
CONCLUSlDNS1 For the particular design of valve analysed, Vs'an 3" and 4" 1500 lb. gate valves, the amount of pressure locking which occurs due to cavity pressure is reasonably predictable by assuming that only the downward component of the cavity pressure load on the wedge (reverse piston effect) is effective.
August 5, 1997                                         J.M Farrell               1                   3 of 5     l
In other designs, this assumption may not be valid. In fact the results obtained on a 10" 300 lb. Velan gate valve showed considerable effect due to the deflection of the wedge t
plates. The conclusion is that the relative flexibilities of the wedge and the body must be taken into account and the assumption of fixed seats is valid only in some cases, in most cases a simple analysis of the relative flexibilities would not be very accurate, end finite element methods would be recommended.
i DATE:
BY:
REV.:
PAGE No:
)
August 5, 1997 J.M Farrell 1
3 of 5 l


PRESSURE LOCKING FORCE ( Ref. RD459)
PRESSURE LOCKING FORCE ( Ref. RD459)
Test Valves                                             Valve No. 88415-2 (3*)                             88802-1 (10")
Test Valves Valve No. 88415-2 (3*)
test no.                                               b1           c1                 b2                 c2 Tr0             1915         2216             2423                 2715   15292 Opening Thrust Unwedging Thrust                 Tw                 994         994             1440                 1440     7634 gf               900           900                 900               900     800 Gland Friction ds           _ 1.125         1.125             1.125               1.125     2.25 Stem Dia.
88802-1 (10")
p                2500         2500               2500                 2500     2000 cavity pressure Mean Seating Dia.                 D               2.735         2.735           2.735                 2.735           7 delP                 O         300                   0               300           0 Differential Press.
test no.
Residual Pressure Locking Force   X
b1 c1 b2 c2 Opening Thrust Tr0 1915 2216 2423 2715 15292 Unwedging Thrust Tw 994 994 1440 1440 7634 Gland Friction gf 900 900 900 900 800 Stem Dia.
                                                                    - 54       -282                   8             - 229     1396
ds
                                                                                                                                        ~TI O
_ 1.125 1.125 1.125 1.125 2.25 cavity pressure p
:Z3 E-T1 O
2500 2500 2500 2500 2000 Mean Seating Dia.
23 EE TABLE 1                                                                       ->.
D 2.735 2.735 2.735 2.735 7
                                                                                                                                          --4 3f 2     g
Differential Press.
* O 2
delP O
A                                                                                                                                      r-
300 0
300 0
Residual Pressure Locking Force X
- 54
-282 8
- 229 1396
~TI O
:Z3 E
-T1 O
23 EE TABLE 1
--43f 2
g O
2 A
r-


1                                                                                                                                           !
1 l
l                                    CALCULATED OPENING FORCE Site Valves                                                                                               -T1'           l 88415-2 p')                     88405-2 (3*)
CALCULATED OPENING FORCE Site Valves
D Drawing No.                                                                                                ~23]
-T1' l
Tag No.                   2-FCV-68-332, -333             1 & 2 -FCV-62-138                               gi
D Drawing No.
                                                                                                                              ~11 Unwedging Thrust   Tw         5228               5228       3300             3300 ,
88415-2 p')
d, Gland Friction      gf            0                    0          0                0                      y Stem Dia.           ds         1.125               1.125       1.125             1.125                     g             I cavity pressure     p           2250               2235           220             120                     p Mean Seating Dia. D         2.735         -
88405-2 (3*)
2.735         2.56             2.56 33 Q---t Differential Press. delP           O                 300         102 C")
~23]
Z Opening Thrust     Tr0         5296               5824       3436             3339                       d, 88521 -3 (4')               88517-3 (4'L         4 Drawing No.                         88405-2 '(3')
Tag No.
Tag No.                    1-FCV-68-332 & 333             1 & 2 --FCV-63-152 & 153     1 & 2 -FCV-63-156 & 157 Tw         5228               5228       5645                             9630 Unwedging Thrust gf             0                   0           0                                 0 Gland Friction ds         1.125               1.125       1.375                             1.375 Stem D!a.
2-FCV-68-332, -333 1 & 2 -FCV-62-138 gi
cavity pressure     p           2250               2235       1520                             2235 Mean Geating Dia. D           2.56                 2.56       3.53                             3.53 Differerdial Press. de!P           O                 300           0                               25 Tr0         5010               5475       5981                             10197 Opening Thrust 5                                                                                                                                   s 2
~11 Gland Friction gf 0
w R                                                 TABLE 2 w
0 0
[ -.  - _ _ - _ .
0 d,
Unwedging Thrust Tw 5228 5228 3300 3300 y
Stem Dia.
ds 1.125 1.125 1.125 1.125 g
I cavity pressure p
2250 2235 220 120 p
Mean Seating Dia.
D 2.735 2.735 2.56 2.56 Q
---t Differential Press.
delP O
300 102 33 C")
Z Opening Thrust Tr0 5296 5824 3436 3339 d,
4 Drawing No.
88405-2 '(3')
88521 -3 (4')
88517-3 (4'L Tag No.
1-FCV-68-332 & 333 1 & 2 --FCV-63-152 & 153 1 & 2 -FCV-63-156 & 157 Unwedging Thrust Tw 5228 5228 5645 9630 Gland Friction gf 0
0 0
0 Stem D!a.
ds 1.125 1.125 1.375 1.375 cavity pressure p
2250 2235 1520 2235 Mean Geating Dia.
D 2.56 2.56 3.53 3.53 Differerdial Press.
de!P O
300 0
25 Opening Thrust Tr0 5010 5475 5981 10197 5
s 2
w R
TABLE 2 w
[ -.


VVfLAN                                                       a a o Departmsnt
VVfLAN a a o Departmsnt
(     '
(
Test and Calculated Results                             RD-466 Pressure Locking                               APP.A
Test and Calculated Results RD-466 Pressure Locking APP.A FOR INF0RM ATl0N '0NEY
                                                                                                                                            ~
~
FOR INF0RM ATl0N '0NEY APPENDIX 'A'                                   ,
APPENDIX 'A' This appendix contcins:
This appendix contcins:
(a)
(a) The test report on the 2" 1500 lb. Velan gate valve.
The test report on the 2" 1500 lb. Velan gate valve.
(b) The test results on the 10" 1500 Velan gate valve.
(b)
(c) The test results on the 10" 300 lb. Velan gate velve.
The test results on the 10" 1500 Velan gate valve.
DATE:                 DY:                       REV.:
(c)
The test results on the 10" 300 lb. Velan gate velve.
DATE:
DY:
REV.:
l PAGE No:
l PAGE No:
Auaust 5.1997           J M. Farrell                 1         i       A1 of A9
Auaust 5.1997 J M. Farrell 1
i A1 of A9


YhN R & D DEPT.
YhN R & D DEPT.
Investigation of Pressure Locking in Gate Valves                                                 RD-459
Investigation of Pressure Locking in Gate Valves RD-459 F0R' it'F0RM ATIOR ~0NCY
                                                                                                                                    ~               ~
~
: 1.       Purcose of Testi                                                     F0R' it'F0RM ATIOR ~0NCY To investigate whether pressure locking would occur in 3" & 4" 1500 gate valves due to locked pressure in the bonnet and if pressure locking occurs, determine the thrust required to overcome this condition.
~
: 2.       Valve Tested:
1.
Purcose of Testi To investigate whether pressure locking would occur in 3" & 4" 1500 gate valves due to locked pressure in the bonnet and if pressure locking occurs, determine the thrust required to overcome this condition.
2.
Valve Tested:
The tests were conducted on a 3" 1500 lb. similar to 88415-2 carbon steel bolted bonnet gate valve. The valve was checked for seat tightness by pressurizing the bonnet to 1500 psi with nitrogen. There was no loss of pressure after 4 hours and soap and water solution test indicated
The tests were conducted on a 3" 1500 lb. similar to 88415-2 carbon steel bolted bonnet gate valve. The valve was checked for seat tightness by pressurizing the bonnet to 1500 psi with nitrogen. There was no loss of pressure after 4 hours and soap and water solution test indicated
                                                  'O' leakage through the seats.
'O' leakage through the seats.
: 3.       Test Conditions:
3.
Test Media:                     Water           Upstream Pressure:                             300 psig Temperature:                     Ambient         Downstream Pressure:                           0 psig Pressure in bonnet:             2500 psig Tests were conducted under extreme pressure conditions. If the pressure locking does not occur under these conditions, it will not occur at lower pressures.
Test Conditions:
: 4.       Signifiennt To t Results and
Test Media:
Water Upstream Pressure:
300 psig Temperature:
Ambient Downstream Pressure:
0 psig Pressure in bonnet:
2500 psig Tests were conducted under extreme pressure conditions. If the pressure locking does not occur under these conditions, it will not occur at lower pressures.
4.
Signifiennt To t Results and


== Conclusions:==
== Conclusions:==
 
4.1 Closing thrust:
4.1       Closing thrust:     7500 - 7600 lbs. Thrust required to pull out the wedge from seats:
7500 - 7600 lbs. Thrust required to pull out the wedge from seats:
a)       With 'O' pressure in bonnet:           -
a)
With 'O' pressure in bonnet:
2075 lbs.
2075 lbs.
b)       With 2500 psi of pressure locked in bonnet:                     1915 lbs.
b)
4.2     Closing thrust:     10,200 - 10,400 lbs. Thrust required to pull out the wedge from seats:
With 2500 psi of pressure locked in bonnet:
a)       With '0' pressure in bonnet:                                     2525 lbs.
1915 lbs.
b)       With 250'' psi of pressure locked in bonnet:                     2423lbs.
4.2 Closing thrust:
10,200 - 10,400 lbs. Thrust required to pull out the wedge from seats:
a)
With '0' pressure in bonnet:
2525 lbs.
b)
With 250'' psi of pressure locked in bonnet:
2423lbs.
The above results indicate that the thrust needed to pull the wedge flom the seat, with or without the locked pressure in the bonnet cavity is nearly the same. This suggests that no stem load due to spreading of the wedge faces occurs in this design of valve.
The above results indicate that the thrust needed to pull the wedge flom the seat, with or without the locked pressure in the bonnet cavity is nearly the same. This suggests that no stem load due to spreading of the wedge faces occurs in this design of valve.
The downward component of the pressure load on the we.dge (reverse piston effect) is almost exactly balanced by the piston effect of the stem.
The downward component of the pressure load on the we.dge (reverse piston effect) is almost exactly balanced by the piston effect of the stem.
DATE:                       BY:                         REV.:                                     PAGE No; Augusc 5, 1997                     M. Abbas                               1                               A2 of A9
DATE:
BY:
REV.:
PAGE No; Augusc 5, 1997 M. Abbas 1
A2 of A9


YEbM                                                                                                           R & D DEPT.               ;(
YEbM R & D DEPT.
Investigation of Pressure Locking in Gate Valvea                                                                     RD-459
;(
                                                                                                                                ~
Investigation of Pressure Locking in Gate Valvea RD-459 FOR INF0'RMXTION MCY
FOR INF0'RMXTION MCY Therefore the actual stem load was almost the same with und without pressure in the valve cavity.
~
: 5.     Test Plan:
Therefore the actual stem load was almost the same with und without pressure in the valve cavity.
5.1     Determiv the packing friction load.
5.
5.2     Close the valve using the following closing torques;
Test Plan:
: a. 75 ft.lb. (8000 lb. thrust)
5.1 Determiv the packing friction load.
: b. 100 ft. Ib. (10,700 lb. thrust) and determine the following:
5.2 Close the valve using the following closing torques; a.
: a. Torque required to unlock the stem thread.
75 ft.lb. (8000 lb. thrust) b.
: b. Torque and thrust required to pull the wedge from the seats under following conditions:
100 ft. Ib. (10,700 lb. thrust) and determine the following:
a.
Torque required to unlock the stem thread.
b.
Torque and thrust required to pull the wedge from the seats under following conditions:
5.1 a With packing loose (i.e. with no packing friction) and 'O' pressure inside the valve.
5.1 a With packing loose (i.e. with no packing friction) and 'O' pressure inside the valve.
5.2b Packing tightened and 'O' pressure in the valve.
5.2b Packing tightened and 'O' pressure in the valve.
5.2c With 2500 psig in the bonnet cavity and 'O'_ differential pressure.
5.2c With 2500 psig in the bonnet cavity and 'O'_ differential pressure.
5.2d 2500 psig in the bonnet cavity and 300 psig differential pressure across the wedge.
5.2d 2500 psig in the bonnet cavity and 300 psig differential pressure across the wedge.
: 6.     Instrumentation:
6.
6.1     Toroue Measurernent:
Instrumentation:
6.1 Toroue Measurernent:
Closing and opening torque shall be measured with the torque wrench.
Closing and opening torque shall be measured with the torque wrench.
BY;                                                           REY.:
lOATE:
lOATE:                                                                                                                      PAGENo:
BY; REY.:
August 5, 1997                             M. Abbas 1                                                                                                                 1                A3 of A9
PAGENo:
,k_ __ ____                       _ _ _ _ - - - _ -              - - - - - - - - - - - - - _ - - - - - - - - - - -                      - --          -- --
1 August 5, 1997 M. Abbas 1
A3 of A9
,k_ __ ____


VELAN                                                                                             R & D DEPT.
VELAN R & D DEPT.
Investigation of Pressure Locking in Gate Valves                                                           RD-459
Investigation of Pressure Locking in Gate Valves RD-459 95NNNENNU 6.
: 6.     imon,meut2iion < cont dn                                                   95NNNENNU 6.2     Stem Thmst Mensurement-Stem thrust shall be calculated from the strain readings of the two (2) strain gages fixed on                                 <
imon,meut2iion < cont dn 6.2 Stem Thmst Mensurement-Stem thrust shall be calculated from the strain readings of the two (2) strain gages fixed on diametrically opposite ends of the stem. Strain due to bending is equal and opposite at the two diametrically opposite locations. Therefore, taking the average of the two strain gage readings eliminates the effect of any bending and gives a fairly accurate estimate of axial strain in the stem, 6.3 Stem thrust is calculated as follows:
diametrically opposite ends of the stem. Strain due to bending is equal and opposite at the two diametrically opposite locations. Therefore, taking the average of the two strain gage readings eliminates the effect of any bending and gives a fairly accurate estimate of axial strain in the stem, 6.3     Stem thrust is calculated as follows:
4 Strain gage reading of gage #1 = q x 10 in.
4 Strain gage reading of gage #1 = q x 10                           in.
Strain gage reading of gage #2 = e2 x 10 in, 4
4 Strain gage reading of gage #2 = e2 x 10                           in, e
e The area of stem at the location of gages = A in.
The area of stem at the location of gages = A in.
The modulus of elasticity (E) for stem = 29.2 x 10'lb./in.2 for stem material 13% Cr. steel at 70 'F.
The modulus of elasticity (E) for stem = 29.2 x 10'lb./in.2 for stem material 13% Cr. steel at 70 'F.
Stem thrust       =                      Axial strain x E x A
Stem thrust Axial strain x E x A
                                                                                                                                  =     ,              29.2 (si A .2Lx A lbs.
=
2 6.4     Calculation of stem torque required to produce the required thrust:
29.2 (si A.2Lx A lbs.
=
2 6.4 Calculation of stem torque required to produce the required thrust:
Required stem torque (ft.lbs.) = Stem Thmst (lbs.) x T.F.
Required stem torque (ft.lbs.) = Stem Thmst (lbs.) x T.F.
T.F., the thread factor is the mechanical advantage ratio for the type and size of stem thread.                               '
T.F., the thread factor is the mechanical advantage ratio for the type and size of stem thread.
: 7.     Valve Datn:
7.
Seat Bore                                                   =  2.63 in.
Valve Datn:
Stem Thread                                                 =  1 1/8 - 5 ACME T.F.                                                         =  .00936 Stem area at the location of gages                           =   n (11/8)2/4 = 0.994 in.:                         .
Seat Bore 2.63 in.
Wedge Angle                                                 =  10' OATE:                       BY:                                         REV.:                                 PAGE Ho:
=
August 5, 1997         ,
Stem Thread 1 1/8 - 5 ACME
M Abbas                                           1                                 A4 of A9
=
T.F.
.00936
=
Stem area at the location of gages
=
n (11/8)2/4 = 0.994 in.:
Wedge Angle 10'
=
OATE:
BY:
REV.:
PAGE Ho:
August 5, 1997 M Abbas 1
A4 of A9


        .                                                                                                  VELAN                                                                                                                                       R & D DEPT.
VELAN R & D DEPT.
Investigation of Pressure Locking in Gate Valves                                                                                                             RD 459
Investigation of Pressure Locking in Gate Valves RD 459 F0n INFliRMXTION ~0EY 8.
: 8.                               Test Results:                                                                           F0n INFliRMXTION ~0EY 8.1                             Test #1:
Test Results:
8.1 Test #1:
Thrust required to pull the wedge from seats with packing loose and '0' (zero) internal pressure:
Thrust required to pull the wedge from seats with packing loose and '0' (zero) internal pressure:
Closing Strain Cage reading                                         closing   Torque to                                 Torque to puli Strain gage reading                 Wedge Torque                               a 10
Closing Strain Cage reading closing Torque to Torque to puli Strain gage reading Wedge Torque a 10
* inch                   Thrust   unlock stem                               out wedge                   a 10''             Pull out ft.lten Qae il Cace f7                                               h Threads.ft.lb.                                     ft. Its               Caan #1   Cace f2     t hru s t 75                         -260             -291             8,040           25                                     10                       0         + 70       1015 100                             -362             -416             11,290           40                                     18                       0         + 120     1752 8.2                             Ten #2:
* inch Thrust unlock stem out wedge a 10''
Packing stud tightened to 25 ft.lbs. packing stress == 4000 psi.
Pull out ft.lten Qae il Cace f7 h Threads.ft.lb.
Wedge pull test:                                               a)   With '0' pressure in the bonnet and 'O' differential pressure across                                             g wedge, b)   With 2500 psi in the bonnet and 'O' differential pressure across wedge, c)   With 2500 psi in the bonnet and 300 psi differential across the wedge.        ,.
ft.
a.1                                 75                             -246             -278             7,604           30                                   20                     +50         + 70       2075 75                             -258             -264             7,575 b.1                                                               -255               -264             7,532           30                                   20                     +68         + 64       1915 75                           -258               -271             7,692 c.1                                                               -258               -269             7,648             35                                   20                     +78         + 82       2219 a.2                               100                             -332               -380             10.333           45                                   25                     +72         + 102     2525 100                             -340               -370             10,304 b.2                                                               -338               -365             10,202           45                                   25                     + 64       + 103     2423 100                             -350               -378             10.565 c.2                                                               -347               -376 .           10,492           45                                     25                     +68         + 118     2715 CATE:                                                                                 B Y;                             REY.:                                                       FAGE Nm Atmust 5,1997                                                                     M Abbas                                                     1                                     A5 of A9       -
Its Caan #1 Cace f2 t hru s t 75
_ _ _ _ _ _ _ _ . _ _ - _ - _ - _ _ _ _ _ . - . - _ _ - - - - - . - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - '- - -                                    - - - - - - - - - - - - ' - ~ ^ ^             " - ^ ^ ^ ^ ~
-260
-291 8,040 25 10 0
+ 70 1015 100
-362
-416 11,290 40 18 0
+ 120 1752 8.2 Ten #2:
Packing stud tightened to 25 ft.lbs. packing stress== 4000 psi.
Wedge pull test:
a)
With '0' pressure in the bonnet and 'O' differential pressure across g
: wedge, b)
With 2500 psi in the bonnet and 'O' differential pressure across
: wedge, c)
With 2500 psi in the bonnet and 300 psi differential across the wedge.
a.1 75
-246
-278 7,604 30 20
+50
+ 70 2075 75
-258
-264 7,575 b.1
-255
-264 7,532 30 20
+68
+ 64 1915 75
-258
-271 7,692 c.1
-258
-269 7,648 35 20
+78
+ 82 2219 a.2 100
-332
-380 10.333 45 25
+72
+ 102 2525 100
-340
-370 10,304 b.2
-338
-365 10,202 45 25
+ 64
+ 103 2423 100
-350
-378 10.565 c.2
-347
-376.
10,492 45 25
+68
+ 118 2715 CATE:
B Y; REY.:
FAGE Nm Atmust 5,1997 M Abbas 1
A5 of A9
- - - - - - - - - - - - ' - ~ ^ ^
" - ^ ^ ^ ^ ~


          .                                                                                VVELAN                                                                                                                                                                 R & D DEPT.
VVELAN R & D DEPT.
Investigation of Pressure Locking in Gate Valves                                                                                                                       RD-459 F0FiiNFURNinTION UffCY
Investigation of Pressure Locking in Gate Valves RD-459 F0FiiNFURNinTION UffCY
)
)
: 8.       Test Results (Cont'd)                                                                                                                                                     '
8.
8.3       Packing Friction Load:
Test Results (Cont'd) 8.3 Packing Friction Load:
Measured Running                                                                                                       Strain gage 104 and             Packing Friction Load (lbs.)   ,
4 Measured Running Strain gage 10 and Packing Friction Load (lbs.)
Iproue (ft. Ibst                                                                                                       Gage #1       G2&cf2             . Average of 3 rendingst Opemng                                                                                                             -16             +42 6-8                                                                                                               + 18             +42                     880
Iproue (ft. Ibst Gage #1 G2&cf2
                                                                                                                                                                                                                        + 20             +46 Closing                                                                                                             -18             -42 6-8                                                                                                                 -19         , -46                       924
. Average of 3 rendingst Opemng
                                                                                                                                                                                                                        -20             -46 l               _
-16
DATf;                                                                                 ) BY                                                       REV.:                     PAGE No; August 5, 1997                                                                     l                                     M Abbas                       __
+42 6-8
1                          A6 of-A9
+ 18
+42 880
+ 20
+46 Closing
-18
-42 6-8
-19
, -46 924
-20
-46 l
DATf;
) BY REV.:
PAGE No; August 5, 1997 l
M Abbas 1
A6 of-A9


RD-459
RD-459 F0FiINFliifNiATI0F MY
                                                                                                                                                      ,p                                       F0FiINFliifNiATI0F MY r                                                                           a T       !
, p r
a T
I STRAIN GAUGET l
I STRAIN GAUGET l
                                                                                                                                                                              ~
~
                                                                                                                                                                                          /
/
t-                                                                                                                                                                                   ~[                 -iPRESSURE GAUGE l l -
t-
                                                                                                                                                                                          --          n
~[
                                                                                                                                                                    -f r ,-  i CAVITY PRESSU9E FROM HYDRO PUMP l                       l i   I I/
-iPRESSURE GAUGE l l
                                                                                                                                                                      %              Ds c"'"
n
I I             1
-f r
i CAVITY PRESSU9E FROM HYDRO PUMP l
l i
I I/
*g Ds c"'"
I I
{
{
aP FROM HYDRO PUMP
1 HYDRO PUMP d
                                                                                  ~
aP FROM
                                                                                                                                                  -            -                d              -        -
~
* i
i
__.7__.
__.7__.
TIE BOLTSI                                               lENO CLAMPS l Page A7 of A9
TIE BOLTSI lENO CLAMPS l Page A7 of A9


VVELAN                                                                                   R & D Departm:nt Test and Calculated Results                                             RD-466 Pressure Locking                                               APP.A
VVELAN R & D Departm:nt Test and Calculated Results RD-466 Pressure Locking APP.A r0g INF0RM ATIOR MCY
                                                                                                                  ~
~
r0g INF0RM ATIOR MCY (b)         Test Results on 10" 1500 lb. Gate - Dwa.' 88802-1 Initial         1 Cavity         Calculated                   Actual           Value                 Closing Press.p       Ooenino Load         Ooenino Load                 of X                 Load 0                                   7634                       -355                 24500 1000           10264                 9909                                             24800 1500           12530                 12234                     -296                 23700 2000           13895                 15292                     +1397                 24800 Using equation 2 the values of the calculated opening lead and the actual opening load are plotted in graph 1. !! appears as if some wedge spreading effect is present at 2000 psig, (c)         10" 300 lb. Gate Valve:     ,                      _
(b)
Cavity         Calculated                       Actual.       Value                 Closing Press. o     Ooenina Load         Ooenino Load                 of X                 Load 0                                   8000                                             14000 500           14460               21000                       +6540                 14000 in this case the calculated figure for opening load is 6540 lbs. too low suggesting wedge plate deflection loading over seat.
Test Results on 10" 1500 lb. Gate - Dwa.' 88802-1 Initial 1
                                                                                    ~
Cavity Calculated Actual Value Closing Press.p Ooenino Load Ooenino Load of X Load 0
DATE:                         gY:                               REV.:                       PAGE No:
7634
Auaust 5.1997               J.M. Fanell                       1                               A8 of A9 l
-355 24500 1000 10264 9909 24800 1500 12530 12234
-296 23700 2000 13895 15292
+1397 24800 Using equation 2 the values of the calculated opening lead and the actual opening load are plotted in graph 1. !! appears as if some wedge spreading effect is present at 2000
: psig, (c) 10" 300 lb. Gate Valve:
Cavity Calculated Actual.
Value Closing Press. o Ooenina Load Ooenino Load of X Load 0
8000 14000 500 14460 21000
+6540 14000 in this case the calculated figure for opening load is 6540 lbs. too low suggesting wedge plate deflection loading over seat.
~
DATE:
gY:
REV.:
PAGE No:
Auaust 5.1997 J.M. Fanell 1
A8 of A9 l


OPENING LOAD / CAVITY PRESSURE                                       .  .
OPENING LOAD / CAVITY PRESSURE 10 in. VALVE - 2.25 dio. STEM 16 r 1 15 p
10 in. VALVE - 2.25 dio. STEM 16 r1 15                                                                               '
14
p 14
[
[       20 E
20 E
                  '                                                                      /
/
l<n                                                   '                 */
l
S8  12                                                                 J'
/
                                                                                    /
<n S8 J'
o8 Zm b$   1;-                                                       ,!
12 o8
              $D                                                         /
/
to 3   10 -                                           Jcf
Zm b$
                                                              /
1;-
5 9-        -                /                      -
$D
                                            /
/
8   ,-
to Jcf 3
7                     _                                    --
10 -
0   0.2       0.4     0.6       0.8       j       j*p               1.8     2
/
@                                                            (Thousands)
5
PRISSURE ffJ VALVE CAVITY-PSI s                                                                                                       5 A                          "                                              FOR INFORMATION ONLY         >m 3                           x    'c*ut". c GC4Dt1 [.
/
9-
/
8 7
0 0.2 0.4 0.6 0.8 j
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(Thousands)
PRISSURE ffJ VALVE CAVITY-PSI s
5!
FOR INFORMATION ONLY A
3
' * ". c
>m x
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VVELAN                                                                                   R & D Departmant Test and Calculated Results                               RD 466
VVELAN R & D Departmant Test and Calculated Results RD 466
                                                                                                                                                                                    ' Pressure Locking                                   APP.B
' Pressure Locking APP.B F0fi INF0RM ATION '0KY
                                                                                                                                                                                                                                ~~                   ~
~~
F0fi INF0RM ATION '0KY APPENDIX 'B' This appendix contains:
~
(a)   Data supplied by T.V.A.
APPENDIX 'B' This appendix contains:
(b)   Calculation of the pressure locking load due to deflection of the wedge plates and assuming fixed seat for the 10" 1500 lb. gate, 3" 1500 lb. gate and 10" 300 lb. gate.
(a)
DATE:                                             DY:                   REv.:                 ' PAGE No:
Data supplied by T.V.A.
Auaust 5.1997             J.M. Farrell                 1                     B,1 of B6           __
(b)
Calculation of the pressure locking load due to deflection of the wedge plates and assuming fixed seat for the 10" 1500 lb. gate, 3" 1500 lb. gate and 10" 300 lb. gate.
DATE:
DY:
REv.:
' PAGE No:
Auaust 5.1997 J.M. Farrell 1
B,1 of B6


                                                                  ~~
J0R INFORMATION 0'NiiY
n                          J0R INFORMATION 0'NiiY                     =                 AL
~~
    /*                                                                   . APP. B ATTACH?ENT 1             -          /
AL n
=
/*
APP. B ATTACH?ENT 1
/
y&
y&
Please determine whether pressure locking would occu:, at the conditions listed below, for the subject Velan motor operated valves. If you deter =ine that pressure locking would occur, provide the thrust required to overcome the pressure locking conditi-on.
Please determine whether pressure locking would occu:, at the conditions listed below, for the subject Velan motor operated valves.
VLV No.         Size       Drawino   Press Uo/In Bonnet /Down         Unwedoinc 1&2-FCV-62-138           3"       88405-2     102         220       0         3300 /
If you deter =ine that pressure locking would occur, provide the thrust required to overcome the pressure locking conditi-on.
1&2-FCV-62-138             3"       88405-2         50       120     17         3300 /
VLV No.
1-FCV-68-332,333           3"       88405-2     300         2235       0         5228 /
Size Drawino Press Uo/In Bonnet /Down Unwedoinc 1&2-FCV-62-138 3"
1-FCV-G8-332,333           3"       88405-2             0   2250       0         5228 v 2-FCV-68-332,)33             3"   . 88415-2     300         2235       0         5:28 s 2-FCV-68-332,333             3"       88415-2             0   2250       0         5228 /
88405-2 102 220 0
1 & 2 --FCV- 63 -15 2 ,15 3 4"       88521-3             0   1520       0         5645 1&2-FCV-63-156,157           4"       88517-3       25       2235       0         9630 Press up = Pressure in the upstream piping Press down = Pressure in the downstream piping Press in Bonnet a Pressure assumed to be trapped in the Bohnet The unwedging loads, shown above, were taken fro:a the most recent diagnostic tests data.
3300 /
The deter =ination of susceptability and the thrust required to overcome pressure         locking will be used to satisfy concerns of NRC Generic Letter 95-07., Any calculated values must be supported by test data.
1&2-FCV-62-138 3"
88405-2 50 120 17 3300 /
1-FCV-68-332,333 3"
88405-2 300 2235 0
5228 /
1-FCV-G8-332,333 3"
88405-2 0
2250 0
5228 v 2-FCV-68-332,)33 3"
88415-2 300 2235 0
5:28 s 2-FCV-68-332,333 3"
88415-2 0
2250 0
5228 /
1 & 2 --FCV-63 -15 2,15 3 4"
88521-3 0
1520 0
5645 1&2-FCV-63-156,157 4"
88517-3 25 2235 0
9630 Press up = Pressure in the upstream piping Press down = Pressure in the downstream piping Press in Bonnet a Pressure assumed to be trapped in the Bohnet The unwedging loads, shown above, were taken fro:a the most recent diagnostic tests data.
The deter =ination of susceptability and the thrust required to overcome pressure locking will be used to satisfy concerns of NRC Generic Letter 95-07.,
Any calculated values must be supported by test data.
Calculation methodologies and associated test dat; must be provided to TVA.
Calculation methodologies and associated test dat; must be provided to TVA.
                                                                                                      .l
.l
                                                                                                      .i g
.i g
Page B2 of B6 g'
Page B2 of B6 g'


    ..            VEM                                                                                                                                                                   R & D Dopartm:nt Test and Calculatect Results                                                                                                                   RD-466                 -
VEM R & D Dopartm:nt Test and Calculatect Results RD-466 Pressure Locking APP.B FOR' INFORM ATION '0NEY
Pressure Locking                                                                                                                       APP.B
, Calculation of oressure Iqpkina load. assumina seats are fixed The following calculations are made to see what the pressure lock ng load would be if the seats were considered fixed.
      , Calculation of oressure Iqpkina load. assumina seats are fixed FOR' INFORM ATION '0NEY The following calculations are made to see what the pressure lock ng load would be if the seats were considered fixed.
The Roark Case No. 2d is used, as shown below, using the Roark nomenclature:
The Roark Case No. 2d is used, as shown below, using the Roark nomenclature:
                                                                                                                                                                      + (9 &
+ (9 &
N*                                                                                                                #y j'   /                 s.
N j'
I$2rJWp(Ng_CQ,C,
/
                                                                                                                                                                    'Jb
s.
                                                                                                      .                                            .                                  . Q.
#y I$2rJWp(Ng_CQ,C,
(a)     10" 1500 Valve:
'Jb
q                                         =                 2000 psi a                                         =                 3.5     ,                                                      _.
. Q.
b                                        =                 1.9 = r, Kas                                       =                0.4 Q,                                       =                qxax0.4 Q4                                      =                 Q, x b     _q. (a2 - b 2) a     2a
(a) 10" 1500 Valve:
                                                                        =                 2000 x 3.5 x 0.4 x 1.9 -                                               2000 (3.5 2 3,9 )
2000 psi q
2 3.5                                                 2 x 3.5
=
                                                                        =                -948 lb.lin.
a
DATE:                                                                   BY:                                                                   REV.:                                                       PAGE No:
=
August 5, 1997                                                               J M Farrell                                                             1                                                     B3 of B6
3.5 b
=
1.9 = r, Kas 0.4
=
Q, qxax0.4
=
2 2
Q Q, x b
_q. (a - b )
=
4 a
2a 2
2
=
2000 x 3.5 x 0.4 x 1.9 -
2000 (3.5 3,9 )
3.5 2 x 3.5
-948 lb.lin.
=
DATE:
BY:
REV.:
PAGE No:
August 5, 1997 J M Farrell 1
B3 of B6


VEM
VEM R & D Department Test hnd Calculated Results PD-466 Pressure Locking APP.B l
        .                                                                                                                                                                                                          R & D Department Test hnd Calculated Results                                                                                                     PD-466 Pressure Locking                                                               APP.B             l FOR'INFORMA~ TION TfNTY (a)     10" 1500 Valve (Cont'd):
FOR'INFORMA~ TION TfNTY (a) 10" 1500 Valve (Cont'd):
Total Seat Load                                                                                                   =                              2 x 2na x Q,
Total Seat Load 2 x 2na x Q,
                                                                                                                                                        =                             2 x 2n x 3.5 x (-948)
=
                                                                                                                                                        =                             -41674 lbs.
2 x 2n x 3.5 x (-948)
Assuming a seat factor of 0.3 Pt                                                                                                                  =                            -41,674 x 0.3
=
                                                                                                                                                          =                           -12,502 lbs.
-41674 lbs.
=
Assuming a seat factor of 0.3
-41,674 x 0.3 P
=
t
-12,502 lbs.
=
This value of pressure locking due to wedge plate deflection is far too large to have been missed in the test.
This value of pressure locking due to wedge plate deflection is far too large to have been missed in the test.
(b)     3" valve; a                                              =                                              1.36 b                                             =                                           0.875 q                                               =                                           2500 Kaa                                            =                                           0.25 Q,                                            =                                            q x a x 0.25 DATE:                                                                                                             BY:                                                     REV.:           PAGE No:
(b) 3" valve; 1.36 a
Anaust 5.1997                                                                                                                                 J . A Farrell                   1                 B4 of B6
=
b
=
0.875 2500 q
=
=
0.25 Kaa q x a x 0.25 Q,
=
DATE:
BY:
REV.:
PAGE No:
Anaust 5.1997 J. A Farrell 1
B4 of B6


VfLAN                                                                                                                                 R & D Departmsnt Test and Calculated Results                                                                                                       RD-466 Pressure Locking                                                                                                           APP.B F0fiINFlijnMTTON tiEY (b)                       3" Valvg_(Cont'd)
VfLAN R & D Departmsnt Test and Calculated Results RD-466 Pressure Locking APP.B F0fiINFlijnMTTON tiEY (b) 3" Valvg_(Cont'd) 2 2
Ox            =      0, x k         .g_ (a2 - b 2) a           2a 2         2
0, x k
                                                                                                                                                              =      2500 x 1.36 x 0.25 x 0.875 - 2500                                                                               (1.36 -0.875 )
.g_ (a - b )
1.36                                                                               2 x 1.36
Ox
                                                                                                                                                              =      546.8 - 996.3                                                                                                                             i
=
                                                                                                                                                              =       -449 lb.lin.
a 2a 2
Total Seat Load      =       2 x 2na x 0 4
2 2500 x 1.36 x 0.25 x 0.875 - 2500 (1.36 -0.875 )
                                                                                                                                                              =
=
2 x 2n x 1.36 x (-449)
1.36 2 x 1.36 546.8 - 996.3 i
                                                                                                                                                              =     -7,678 lb.
=
Using 0.3 seat factor i                                                               _
-449 lb.lin.
Pt              =      0.3 x -7678
=
                                                                                                                                                              =       -2303 Again this load is too large to have been missed in the tests.
2 x 2na x 0 Total Seat Load
DATE:                     BY:                                                                               REV.:                                 PAGE No; Auaust 5.1997               J.M Farrell                                                                                             1                     B5 of 86
=
4 2 x 2n x 1.36 x (-449)
=
-7,678 lb.
=
Using 0.3 seat factor i
0.3 x -7678 P
=
t
-2303
=
Again this load is too large to have been missed in the tests.
DATE:
BY:
REV.:
PAGE No; Auaust 5.1997 J.M Farrell 1
B5 of 86


    ~
VVELAN R & D D partment
VVELAN R & D D partment
                                            . Test and Calculated Results                                                                                                                       RD-466 Pressure Locking                                                                                                                           APP.B
~
                                                                                                                                                                                                            ~
. Test and Calculated Results RD-466 Pressure Locking APP.B F0fiINFliRM ATION ~0NI'Y
F0fiINFliRM ATION ~0NI'Y (c)     10" 300 lb. Valve:
~
q     =                               500 a     =                               5.18 b      =                                3.125 Q,    =                               q x a x 0.25 2                                   2 Q3      =                              0, x b   __q.                   (a - b )
(c) 10" 300 lb. Valve:
a     2a 2
500 q
                                                      =                               500 x 5.18 x 0.28 x 3.125                                                                   -    500             (5.18 -3.1252) 5.18                                                                               2 x 5.18
=
                                                      =                               437 - 823
a
                                                      =                              -385 Total Seat Load             =                              2 x 2n x 5.18 x (-385)
=
                                                      =                               -25,080 Assuming a seat factor of 0.3 Pt    =                                -25080 x 0.3
5.18 3.125 b
                                                        =                               -7524 lbs.
=
q x a x 0.25 Q,
=
2 2
0, x b
__q. (a - b )
Q
=
3 a
2a
=
500 x 5.18 x 0.28 x 3.125 500 (5.18 -3.1252) 2 5.18 2 x 5.18
=
437 - 823
-385
=
Total Seat Load 2 x 2n x 5.18 x (-385)
=
-25,080
=
Assuming a seat factor of 0.3 P
-25080 x 0.3
=
t
-7524 lbs.
=
This is consistent with the test value of 6540 lbs. giver, in Appenaix 'A'.
This is consistent with the test value of 6540 lbs. giver, in Appenaix 'A'.
DATL                           BY;                                                                         REV.:                                                         PAGE No:
DATL BY; REV.:
Auaust 5.1997                           J M Farrell                                                                                                   1   _
PAGE No:
Auaust 5.1997 J M Farrell 1
B6 of B6 l
B6 of B6 l
                                                          .___-___________._____m_..               _ _ _ _ _ _ _ . _ _ _ - _ _ _ _ _ _ _ _ _ _ _ _ _ _ - - . _ _ _ _ _ _ _ _                  _ _ _ _
.___-___________._____m_..


                        .  . _. ~     .    ._    - . - - . _            ..
_. ~
    ,  e'#'
e'#'
e s'
e s'
ENCLOSURE 2 TENNESSEE VALLEY AUTHORITY SEQUOYAH NUCLEAR PLANT (SQN)
ENCLOSURE 2 TENNESSEE VALLEY AUTHORITY SEQUOYAH NUCLEAR PLANT (SQN)
UNITS 1 AND 2 SUPPLEMENTAL RESPONSE TO GENERIC L2TTER (GL) 95 PRESSURE LOCKING AND THERMAL BINDING OF SAFETY-RELATED PONER OPERATED GATE VALVES TVA Commitment 1
UNITS 1 AND 2 SUPPLEMENTAL RESPONSE TO GENERIC L2TTER (GL) 95 PRESSURE LOCKING AND THERMAL BINDING OF SAFETY-RELATED PONER OPERATED GATE VALVES TVA Commitment 1
TVA will implement design changes to eliminate the potential for pressure locking for the following valves:
TVA will implement design changes to eliminate the potential for pressure locking for the following valves:
  '                FCV-63-25 FCV-63-26 FCV-72-2 FCV-72-39 FCV-72-40 FCV-72-41 The design changes will be completed prior to startup from the Cycle 9 refueling outage for both units.
FCV-63-25 FCV-63-26 FCV-72-2 FCV-72-39 FCV-72-40 FCV-72-41 The design changes will be completed prior to startup from the Cycle 9 refueling outage for both units.
5
5
                                                ~}}
,n.
~
- -}}

Latest revision as of 01:50, 8 December 2024

Rev 1 to RD-466, Test & Calculated Results Pressure Locking
ML20203B973
Person / Time
Site: Sequoyah  
Issue date: 08/05/1997
From: Farrell J, Isbitsky S
TENNESSEE VALLEY AUTHORITY
To:
Shared Package
ML20203B931 List:
References
RD-466, RD-466-R01, RD-466-R1, NUDOCS 9712150197
Download: ML20203B973 (26)


Text

.

O ATTACNMENT B TENNESSEE VALLEY AUTHORITY SEQUOYAH NUCLEAR PLANT (SQN)

UNITS 1 AND 2 SUPPLEMENTAL RESPONSE TO GENERIC LETTER (GL) 95 PRESSURE LOCKING AND THERNAL BINDING OF SAFETY-RELATED PONER OPERATED GATE VALVES 3-INCil AND 4-INCli 1500# VELAN VALVE TEST AND CALCULATED PRESSURE LOCKING RESULTS FOR SON VALVES 4

REPORT NUMBER RD-466, DATED AUGUST 5, 1997

.i a

1 4

9712150197 971201 PDR ADOCK O y7 P

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w.

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VM R & D Department o

Test and Calculated Results RD 466 Pressure Locking FOB INF0By AT10F '00 RD-466 Tennessee Valley Authority Sequoyah Nuclear Plant P.O. Box 2000 - STB-4A Soddy Daisy, TN 37379 Velan P.O. No.: P9-81035-K T.V.A. Order No.: P-96N4E-176161 Velan Dwo. No.:

Size and Flaure No.:

88405 2 3" B10-30548-13MS 88415-2 3" B10-3054813MS 88521-3 4" B12-20548-13M 88517-3 4" B12-3054B-13M

\\

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a.u. re r t

/1A/W M!i.=. '

Compiled By:

/

! John M. Farrell, Eng.

MC"

'Vice,-#residen, Engineering I~::

Reviewed By:./

~

Eemewy

k. Isbitsky, Eng, l

Manager, Stress Dept.

DATE:

bY:

RE V.:

PAGE No:

Auaust 5.1997 J.M. Farroll 1

i 1

kYM R & D Departm:nt i

Test and Calculated Results RD466 Pressure Locking

-nn tungppTTinpf UN'l:V l

CERTIFICATE of COMPLIANCE:

We hereby certify that the following data are in compilance with the applicable purchase order:

CUSTOMER:

Tennessee Valley Authority CUSTOMER P.O.: P-96N4E-176161 VELAN P.O.:

P9-81035 K DESCRIPTION:

Test and Calculated Results - Pressure Locking blYb/AM n u nmd l

Signature.

John M. Farrell, Eng.

W/

,/

l tg,3,,,,

N /

~

Title:

Vice President, Engineering Date:

Original: July 7th,1997 Revised: August 5th,1997 DATE:

BYi REY.:

PAGE No:

Auaust S.1997 J.M. Farrell 1

il

VVfLAN a a o oepartment Test and Calculated Results Ro46a.

Pressure Locking TOliINFliffMXTION UKY 2

PECORD of REVIS1QN1 A

Her Descriotion:

Dy/Date:

Cert _ By / Date:

J.M. Fbr[ ell, Eng. /p/.3 -

A Hsbitsky, Eng.

0 Initial Release July 7,1997 July 8,1997

,/

1 Revised per J.M. F 5 rell, Eng. /

sis i 5(E6g. t customer Augtist 5,1997 August 5,1997

comments, n

e DATE:

BY:

REV.:

PAGE No:

Auoust 5.1997 J M Farrell 1

iii

VM R & D Departm:nt Test and Calculated Results RD 466 Pressure Locking FOR INF0RMXTI0F0NEY

~~

~

3 TABLE of CONTENISJ P_aga 1.

Certificate af Compliance il 2.

Record of Revision ill 3.

Table of Contents iv 4.

Summary of Test Pesults & Analysis 1

5.

Appendix 'A' - Test Results A1 6.

Appendix 'B' - Supplementary Data B1 t

I I

DATE:

BY; REY.:

PAGE feo:

Auaust 5.1997 J.M. Farrell 1

iv

VELAN R & D Departm:nt Test and Calculated Results RD-466 Pressure Locking l

FOR INF6RMXTOW Unry 1)

It[TRODUCTl01h Under a purchase order from T.V.A. tests were carried out on a 3" 1500 lb. Velan gate valve in order to determine the amount of pressure locking which occurred due to various cavity pressures and differential pressures. The resuits of the tests were compared with those of an analytical model with the intent of using this analytical model to evaluate the i

potential for pressure socking in similar valves at the T.V.A. Sequoyah plant.

2)

IEST EQUIPMENT:

The tests were carried out on a Velan 3" 1500 lb. t; ate valve with a configuration corresponding to Velan drawing No. BR415 2 which is the drawing number for one of the valves under !nvestigation at T.V.A. As back-up data he results of a previous test performed on a 10" 1500 lb. Velan gate valve (Dwg. Nc 88802-1) are presented to substantiate the analytical model used. The results from a (Urd test, on a Velan 10" 300 lb. API 600 gate valve are also reviewed.

All valves are clamped in a fixture and pressurised by means of a hydraulic pump connected to the bonnet of the valve. Details are given in report RD 459.

3)

TEST RESULTS:

The test results for the 3" valve are given in RD-459 (Appendix 'A'). The results of the tests on the 10" 1500 lb. and 10" 300 lb. valves are also included in Appendix 'A'.

4)

ANALYSIS of TEST RESULTS Nomenclature:

The following nomenclature is used:

Total opening load - Ibf. from tests.

T,,

=

Static unwedging load - Ibf. from tests, Tw

=

Gland friction load - Ibf. from tests.

gf

=

Stem piston effect Ibf.

Pe

=

Pressure locking load - Ibf.

P

=

t Differential pressure load -Ibf.

Po

=

Difference between test and calculated loads - Ibf.

X

=

oATE:

en REY.:

PAGE No:

Atmst 5,1997 J M. Farrell 1

1 of 3

7VfLAN a a o oepartm:nt Test and Calculated Results RD46 Pressure Locking FOR INFORMATION ONEY 4) musis of Test assutrs remem Inillally the intention was to use the analytical method of Com. Ed. given in Nureg/CP-0152 for evaluating the pressure locking load. However, it had been found in the test on the 10" 1500 lb. Velan gate valve that no seat loading due to deflection of tha wedge plates in the axis of the valve bore centerline was detested. (Rnf. Nureg/CP-0146 Velan paper), in the results of the tests on the 3" 1500 gate valve, again no significant effect of wedge plate deflection could be seen.

Therefore it was decided that the deflection of the wedge plate would be ignored, and only the downward force component due to the cavity pressure acting on the wedge would be considered. In the equation that is used, an unknown factor X is used which shows the deviation of the calculated from the test results.

The equation used is then:

Tw & gf - Pc + P + Po + X (1)

T,,

=

t IIIII fl i

Using the following dimensional data:

g iw Valve stem diameter -ins, ddb -

+

D d,

=

Valve mean seating fall diameter - ins.

D

=

Valve' seat angle - degrees.

Y 0

=

Valve seating / unseating factor - 0.3 assumed.

ggg p

=

Cavity pressure - psig.

p p

=

Differential pressure across wedge - psi.

delP

=

2 2

Tw + gf - 0.785 d,2 p + 2 x 0.785 D pSinD + 0.765pD delP + X.~(2)

T,,

=

Using the above equation and the results of the tests on the 3" and 10" 1500 lb. valves the results shown in Table 1 were obtained. it will be seen from Table 1 that the variation between test and calculation is not large, sometimes positive and sometimes negative.

This suggests that the method of calculation is reasonable.

A possible cxplanation of this is that, for this particular valve design, the wedge is relatively much less flexible than the body. That is, the assumption that the seats are fixed is overly conservative.

1 Further discussion of this conclusion if given in Appendix 'B'.

DATE:

SY:

REV.:

PAGE No:

Atpst 5,1997 JM Farrell 1

2 of 5

VfM R & D D:partm:nt Test and Calculated Results RD-466 Pressure Locking FOR INFORM ATION ON1.Y P_REf}1GIl_QR of OPENING LOAD includina PRESSURE LOCKING:

Q 5)

Using the equation (2), the calculated opening loads for the T.V.A. valves are given in Tabia 2.

The pressures are taken from Attachment 1 in Appendix 'B'. The data were supplied by i

T.V.A It is assumed that the unwedging load includes the packing friction; therefore gf is shown as zero in the table.

6)

CONCLUSlDNS1 For the particular design of valve analysed, Vs'an 3" and 4" 1500 lb. gate valves, the amount of pressure locking which occurs due to cavity pressure is reasonably predictable by assuming that only the downward component of the cavity pressure load on the wedge (reverse piston effect) is effective.

In other designs, this assumption may not be valid. In fact the results obtained on a 10" 300 lb. Velan gate valve showed considerable effect due to the deflection of the wedge t

plates. The conclusion is that the relative flexibilities of the wedge and the body must be taken into account and the assumption of fixed seats is valid only in some cases, in most cases a simple analysis of the relative flexibilities would not be very accurate, end finite element methods would be recommended.

i DATE:

BY:

REV.:

PAGE No:

)

August 5, 1997 J.M Farrell 1

3 of 5 l

PRESSURE LOCKING FORCE ( Ref. RD459)

Test Valves Valve No. 88415-2 (3*)

88802-1 (10")

test no.

b1 c1 b2 c2 Opening Thrust Tr0 1915 2216 2423 2715 15292 Unwedging Thrust Tw 994 994 1440 1440 7634 Gland Friction gf 900 900 900 900 800 Stem Dia.

ds

_ 1.125 1.125 1.125 1.125 2.25 cavity pressure p

2500 2500 2500 2500 2000 Mean Seating Dia.

D 2.735 2.735 2.735 2.735 7

Differential Press.

delP O

300 0

300 0

Residual Pressure Locking Force X

- 54

-282 8

- 229 1396

~TI O

Z3 E

-T1 O

23 EE TABLE 1

--43f 2

g O

2 A

r-

1 l

CALCULATED OPENING FORCE Site Valves

-T1' l

D Drawing No.

88415-2 p')

88405-2 (3*)

~23]

Tag No.

2-FCV-68-332, -333 1 & 2 -FCV-62-138 gi

~11 Gland Friction gf 0

0 0

0 d,

Unwedging Thrust Tw 5228 5228 3300 3300 y

Stem Dia.

ds 1.125 1.125 1.125 1.125 g

I cavity pressure p

2250 2235 220 120 p

Mean Seating Dia.

D 2.735 2.735 2.56 2.56 Q

---t Differential Press.

delP O

300 102 33 C")

Z Opening Thrust Tr0 5296 5824 3436 3339 d,

4 Drawing No.

88405-2 '(3')

88521 -3 (4')

88517-3 (4'L Tag No.

1-FCV-68-332 & 333 1 & 2 --FCV-63-152 & 153 1 & 2 -FCV-63-156 & 157 Unwedging Thrust Tw 5228 5228 5645 9630 Gland Friction gf 0

0 0

0 Stem D!a.

ds 1.125 1.125 1.375 1.375 cavity pressure p

2250 2235 1520 2235 Mean Geating Dia.

D 2.56 2.56 3.53 3.53 Differerdial Press.

de!P O

300 0

25 Opening Thrust Tr0 5010 5475 5981 10197 5

s 2

w R

TABLE 2 w

[ -.

VVfLAN a a o Departmsnt

(

Test and Calculated Results RD-466 Pressure Locking APP.A FOR INF0RM ATl0N '0NEY

~

APPENDIX 'A' This appendix contcins:

(a)

The test report on the 2" 1500 lb. Velan gate valve.

(b)

The test results on the 10" 1500 Velan gate valve.

(c)

The test results on the 10" 300 lb. Velan gate velve.

DATE:

DY:

REV.:

l PAGE No:

Auaust 5.1997 J M. Farrell 1

i A1 of A9

YhN R & D DEPT.

Investigation of Pressure Locking in Gate Valves RD-459 F0R' it'F0RM ATIOR ~0NCY

~

~

1.

Purcose of Testi To investigate whether pressure locking would occur in 3" & 4" 1500 gate valves due to locked pressure in the bonnet and if pressure locking occurs, determine the thrust required to overcome this condition.

2.

Valve Tested:

The tests were conducted on a 3" 1500 lb. similar to 88415-2 carbon steel bolted bonnet gate valve. The valve was checked for seat tightness by pressurizing the bonnet to 1500 psi with nitrogen. There was no loss of pressure after 4 hours4.62963e-5 days <br />0.00111 hours <br />6.613757e-6 weeks <br />1.522e-6 months <br /> and soap and water solution test indicated

'O' leakage through the seats.

3.

Test Conditions:

Test Media:

Water Upstream Pressure:

300 psig Temperature:

Ambient Downstream Pressure:

0 psig Pressure in bonnet:

2500 psig Tests were conducted under extreme pressure conditions. If the pressure locking does not occur under these conditions, it will not occur at lower pressures.

4.

Signifiennt To t Results and

Conclusions:

4.1 Closing thrust:

7500 - 7600 lbs. Thrust required to pull out the wedge from seats:

a)

With 'O' pressure in bonnet:

2075 lbs.

b)

With 2500 psi of pressure locked in bonnet:

1915 lbs.

4.2 Closing thrust:

10,200 - 10,400 lbs. Thrust required to pull out the wedge from seats:

a)

With '0' pressure in bonnet:

2525 lbs.

b)

With 250 psi of pressure locked in bonnet:

2423lbs.

The above results indicate that the thrust needed to pull the wedge flom the seat, with or without the locked pressure in the bonnet cavity is nearly the same. This suggests that no stem load due to spreading of the wedge faces occurs in this design of valve.

The downward component of the pressure load on the we.dge (reverse piston effect) is almost exactly balanced by the piston effect of the stem.

DATE:

BY:

REV.:

PAGE No; Augusc 5, 1997 M. Abbas 1

A2 of A9

YEbM R & D DEPT.

(

Investigation of Pressure Locking in Gate Valvea RD-459 FOR INF0'RMXTION MCY

~

Therefore the actual stem load was almost the same with und without pressure in the valve cavity.

5.

Test Plan:

5.1 Determiv the packing friction load.

5.2 Close the valve using the following closing torques; a.

75 ft.lb. (8000 lb. thrust) b.

100 ft. Ib. (10,700 lb. thrust) and determine the following:

a.

Torque required to unlock the stem thread.

b.

Torque and thrust required to pull the wedge from the seats under following conditions:

5.1 a With packing loose (i.e. with no packing friction) and 'O' pressure inside the valve.

5.2b Packing tightened and 'O' pressure in the valve.

5.2c With 2500 psig in the bonnet cavity and 'O'_ differential pressure.

5.2d 2500 psig in the bonnet cavity and 300 psig differential pressure across the wedge.

6.

Instrumentation:

6.1 Toroue Measurernent:

Closing and opening torque shall be measured with the torque wrench.

lOATE:

BY; REY.:

PAGENo:

1 August 5, 1997 M. Abbas 1

A3 of A9

,k_ __ ____

VELAN R & D DEPT.

Investigation of Pressure Locking in Gate Valves RD-459 95NNNENNU 6.

imon,meut2iion < cont dn 6.2 Stem Thmst Mensurement-Stem thrust shall be calculated from the strain readings of the two (2) strain gages fixed on diametrically opposite ends of the stem. Strain due to bending is equal and opposite at the two diametrically opposite locations. Therefore, taking the average of the two strain gage readings eliminates the effect of any bending and gives a fairly accurate estimate of axial strain in the stem, 6.3 Stem thrust is calculated as follows:

4 Strain gage reading of gage #1 = q x 10 in.

Strain gage reading of gage #2 = e2 x 10 in, 4

e The area of stem at the location of gages = A in.

The modulus of elasticity (E) for stem = 29.2 x 10'lb./in.2 for stem material 13% Cr. steel at 70 'F.

Stem thrust Axial strain x E x A

=

29.2 (si A.2Lx A lbs.

=

2 6.4 Calculation of stem torque required to produce the required thrust:

Required stem torque (ft.lbs.) = Stem Thmst (lbs.) x T.F.

T.F., the thread factor is the mechanical advantage ratio for the type and size of stem thread.

7.

Valve Datn:

Seat Bore 2.63 in.

=

Stem Thread 1 1/8 - 5 ACME

=

T.F.

.00936

=

Stem area at the location of gages

=

n (11/8)2/4 = 0.994 in.:

Wedge Angle 10'

=

OATE:

BY:

REV.:

PAGE Ho:

August 5, 1997 M Abbas 1

A4 of A9

VELAN R & D DEPT.

Investigation of Pressure Locking in Gate Valves RD 459 F0n INFliRMXTION ~0EY 8.

Test Results:

8.1 Test #1:

Thrust required to pull the wedge from seats with packing loose and '0' (zero) internal pressure:

Closing Strain Cage reading closing Torque to Torque to puli Strain gage reading Wedge Torque a 10

  • inch Thrust unlock stem out wedge a 10

Pull out ft.lten Qae il Cace f7 h Threads.ft.lb.

ft.

Its Caan #1 Cace f2 t hru s t 75

-260

-291 8,040 25 10 0

+ 70 1015 100

-362

-416 11,290 40 18 0

+ 120 1752 8.2 Ten #2:

Packing stud tightened to 25 ft.lbs. packing stress== 4000 psi.

Wedge pull test:

a)

With '0' pressure in the bonnet and 'O' differential pressure across g

wedge, b)

With 2500 psi in the bonnet and 'O' differential pressure across

wedge, c)

With 2500 psi in the bonnet and 300 psi differential across the wedge.

a.1 75

-246

-278 7,604 30 20

+50

+ 70 2075 75

-258

-264 7,575 b.1

-255

-264 7,532 30 20

+68

+ 64 1915 75

-258

-271 7,692 c.1

-258

-269 7,648 35 20

+78

+ 82 2219 a.2 100

-332

-380 10.333 45 25

+72

+ 102 2525 100

-340

-370 10,304 b.2

-338

-365 10,202 45 25

+ 64

+ 103 2423 100

-350

-378 10.565 c.2

-347

-376.

10,492 45 25

+68

+ 118 2715 CATE:

B Y; REY.:

FAGE Nm Atmust 5,1997 M Abbas 1

A5 of A9

- - - - - - - - - - - - ' - ~ ^ ^

" - ^ ^ ^ ^ ~

VVELAN R & D DEPT.

Investigation of Pressure Locking in Gate Valves RD-459 F0FiiNFURNinTION UffCY

)

8.

Test Results (Cont'd) 8.3 Packing Friction Load:

4 Measured Running Strain gage 10 and Packing Friction Load (lbs.)

Iproue (ft. Ibst Gage #1 G2&cf2

. Average of 3 rendingst Opemng

-16

+42 6-8

+ 18

+42 880

+ 20

+46 Closing

-18

-42 6-8

-19

, -46 924

-20

-46 l

DATf;

) BY REV.:

PAGE No; August 5, 1997 l

M Abbas 1

A6 of-A9

RD-459 F0FiINFliifNiATI0F MY

, p r

a T

I STRAIN GAUGET l

~

/

t-

~[

-iPRESSURE GAUGE l l

n

-f r

i CAVITY PRESSU9E FROM HYDRO PUMP l

l i

I I/

  • g Ds c"'"

I I

{

1 HYDRO PUMP d

aP FROM

~

i

__.7__.

TIE BOLTSI lENO CLAMPS l Page A7 of A9

VVELAN R & D Departm:nt Test and Calculated Results RD-466 Pressure Locking APP.A r0g INF0RM ATIOR MCY

~

(b)

Test Results on 10" 1500 lb. Gate - Dwa.' 88802-1 Initial 1

Cavity Calculated Actual Value Closing Press.p Ooenino Load Ooenino Load of X Load 0

7634

-355 24500 1000 10264 9909 24800 1500 12530 12234

-296 23700 2000 13895 15292

+1397 24800 Using equation 2 the values of the calculated opening lead and the actual opening load are plotted in graph 1. !! appears as if some wedge spreading effect is present at 2000

psig, (c) 10" 300 lb. Gate Valve:

Cavity Calculated Actual.

Value Closing Press. o Ooenina Load Ooenino Load of X Load 0

8000 14000 500 14460 21000

+6540 14000 in this case the calculated figure for opening load is 6540 lbs. too low suggesting wedge plate deflection loading over seat.

~

DATE:

gY:

REV.:

PAGE No:

Auaust 5.1997 J.M. Fanell 1

A8 of A9 l

OPENING LOAD / CAVITY PRESSURE 10 in. VALVE - 2.25 dio. STEM 16 r 1 15 p

14

[

20 E

/

l

/

<n S8 J'

12 o8

/

Zm b$

1;-

$D

/

to Jcf 3

10 -

/

5

/

9-

/

8 7

0 0.2 0.4 0.6 0.8 j

j*p 1.8 2

(Thousands)

PRISSURE ffJ VALVE CAVITY-PSI s

5!

FOR INFORMATION ONLY A

3

' * ". c

>m x

c ut GC4Dt1 [.

VVELAN R & D Departmant Test and Calculated Results RD 466

' Pressure Locking APP.B F0fi INF0RM ATION '0KY

~~

~

APPENDIX 'B' This appendix contains:

(a)

Data supplied by T.V.A.

(b)

Calculation of the pressure locking load due to deflection of the wedge plates and assuming fixed seat for the 10" 1500 lb. gate, 3" 1500 lb. gate and 10" 300 lb. gate.

DATE:

DY:

REv.:

' PAGE No:

Auaust 5.1997 J.M. Farrell 1

B,1 of B6

J0R INFORMATION 0'NiiY

~~

AL n

=

/*

APP. B ATTACH?ENT 1

/

y&

Please determine whether pressure locking would occu:, at the conditions listed below, for the subject Velan motor operated valves.

If you deter =ine that pressure locking would occur, provide the thrust required to overcome the pressure locking conditi-on.

VLV No.

Size Drawino Press Uo/In Bonnet /Down Unwedoinc 1&2-FCV-62-138 3"

88405-2 102 220 0

3300 /

1&2-FCV-62-138 3"

88405-2 50 120 17 3300 /

1-FCV-68-332,333 3"

88405-2 300 2235 0

5228 /

1-FCV-G8-332,333 3"

88405-2 0

2250 0

5228 v 2-FCV-68-332,)33 3"

88415-2 300 2235 0

5:28 s 2-FCV-68-332,333 3"

88415-2 0

2250 0

5228 /

1 & 2 --FCV-63 -15 2,15 3 4"

88521-3 0

1520 0

5645 1&2-FCV-63-156,157 4"

88517-3 25 2235 0

9630 Press up = Pressure in the upstream piping Press down = Pressure in the downstream piping Press in Bonnet a Pressure assumed to be trapped in the Bohnet The unwedging loads, shown above, were taken fro:a the most recent diagnostic tests data.

The deter =ination of susceptability and the thrust required to overcome pressure locking will be used to satisfy concerns of NRC Generic Letter 95-07.,

Any calculated values must be supported by test data.

Calculation methodologies and associated test dat; must be provided to TVA.

.l

.i g

Page B2 of B6 g'

VEM R & D Dopartm:nt Test and Calculatect Results RD-466 Pressure Locking APP.B FOR' INFORM ATION '0NEY

, Calculation of oressure Iqpkina load. assumina seats are fixed The following calculations are made to see what the pressure lock ng load would be if the seats were considered fixed.

The Roark Case No. 2d is used, as shown below, using the Roark nomenclature:

+ (9 &

N j'

/

s.

  1. y I$2rJWp(Ng_CQ,C,

'Jb

. Q.

(a) 10" 1500 Valve:

2000 psi q

=

a

=

3.5 b

=

1.9 = r, Kas 0.4

=

Q, qxax0.4

=

2 2

Q Q, x b

_q. (a - b )

=

4 a

2a 2

2

=

2000 x 3.5 x 0.4 x 1.9 -

2000 (3.5 3,9 )

3.5 2 x 3.5

-948 lb.lin.

=

DATE:

BY:

REV.:

PAGE No:

August 5, 1997 J M Farrell 1

B3 of B6

VEM R & D Department Test hnd Calculated Results PD-466 Pressure Locking APP.B l

FOR'INFORMA~ TION TfNTY (a) 10" 1500 Valve (Cont'd):

Total Seat Load 2 x 2na x Q,

=

2 x 2n x 3.5 x (-948)

=

-41674 lbs.

=

Assuming a seat factor of 0.3

-41,674 x 0.3 P

=

t

-12,502 lbs.

=

This value of pressure locking due to wedge plate deflection is far too large to have been missed in the test.

(b) 3" valve; 1.36 a

=

b

=

0.875 2500 q

=

=

0.25 Kaa q x a x 0.25 Q,

=

DATE:

BY:

REV.:

PAGE No:

Anaust 5.1997 J. A Farrell 1

B4 of B6

VfLAN R & D Departmsnt Test and Calculated Results RD-466 Pressure Locking APP.B F0fiINFlijnMTTON tiEY (b) 3" Valvg_(Cont'd) 2 2

0, x k

.g_ (a - b )

Ox

=

a 2a 2

2 2500 x 1.36 x 0.25 x 0.875 - 2500 (1.36 -0.875 )

=

1.36 2 x 1.36 546.8 - 996.3 i

=

-449 lb.lin.

=

2 x 2na x 0 Total Seat Load

=

4 2 x 2n x 1.36 x (-449)

=

-7,678 lb.

=

Using 0.3 seat factor i

0.3 x -7678 P

=

t

-2303

=

Again this load is too large to have been missed in the tests.

DATE:

BY:

REV.:

PAGE No; Auaust 5.1997 J.M Farrell 1

B5 of 86

VVELAN R & D D partment

~

. Test and Calculated Results RD-466 Pressure Locking APP.B F0fiINFliRM ATION ~0NI'Y

~

(c) 10" 300 lb. Valve:

500 q

=

a

=

5.18 3.125 b

=

q x a x 0.25 Q,

=

2 2

0, x b

__q. (a - b )

Q

=

3 a

2a

=

500 x 5.18 x 0.28 x 3.125 500 (5.18 -3.1252) 2 5.18 2 x 5.18

=

437 - 823

-385

=

Total Seat Load 2 x 2n x 5.18 x (-385)

=

-25,080

=

Assuming a seat factor of 0.3 P

-25080 x 0.3

=

t

-7524 lbs.

=

This is consistent with the test value of 6540 lbs. giver, in Appenaix 'A'.

DATL BY; REV.:

PAGE No:

Auaust 5.1997 J M Farrell 1

B6 of B6 l

.___-___________._____m_..

_. ~

e'#'

e s'

ENCLOSURE 2 TENNESSEE VALLEY AUTHORITY SEQUOYAH NUCLEAR PLANT (SQN)

UNITS 1 AND 2 SUPPLEMENTAL RESPONSE TO GENERIC L2TTER (GL) 95 PRESSURE LOCKING AND THERMAL BINDING OF SAFETY-RELATED PONER OPERATED GATE VALVES TVA Commitment 1

TVA will implement design changes to eliminate the potential for pressure locking for the following valves:

FCV-63-25 FCV-63-26 FCV-72-2 FCV-72-39 FCV-72-40 FCV-72-41 The design changes will be completed prior to startup from the Cycle 9 refueling outage for both units.

5

,n.

~

- -