ML20116J176
| ML20116J176 | |
| Person / Time | |
|---|---|
| Site: | Fermi  |
| Issue date: | 01/26/1996 |
| From: | VECTRA TECHNOLOGIES, INC. |
| To: | |
| Shared Package | |
| ML20116J132 | List: |
| References | |
| 0102-00065.F02, 0102-00065.F02-004, 102-65.F2, 102-65.F2-4, NUDOCS 9608130081 | |
| Download: ML20116J176 (23) | |
Text
.-
V CALCULATION "5 " : 0102-00065
. , PACKAGE VECTRA PROJECT NO: 0102-00065 CALC.NO: 0102-00065.F02-004 PROJECT NAME: CLIENT:
Pressure Locking / Thermal Binding Evaluation Detroit Edison - Fermi Unit-2 Plant CALCULATION TITLE: h/h Evaluation of Stem Growth Unseating Load for Valve E4150F001 of Fermi Unit-2 Plant l
I l
PROBLEM STATEMENT OR OBJECTIVE OF TIIE CALCULATION:
The purpose of this Calculation is to determine if stem growth is sufficient to preclude this valve from performing its safety related function.
Safety-Re1ated DOCUMENT AFFECTED REVISION PROJECT ENGINEER NAMES ANDINITIALS REVISION PAGES DESCRIPTION APPROVAL /DATE OF PREPARERS AND CHECKERS j 0 Abb Initial Issue
/ /
2 b dd &
fh'. h5 1
PAGE 1 OF 7 9608130081 960807 QPES 3-2.1.1 PDR ADOCK 05000341 REV.0 P PDR
VECTRA:
Naperville, Illinois 1NEORh1ATloliOffly PROJECT pressure Lockine/ Thermal Bindine Evaluation FILE 0102-00065 OWNER Detroit Edison Comoany CLIENT Detroit Edison Comoanv Fermi Unit 2 0102-00065 F02-004 1.0 Purpose / Objective The purpose of this calculation is to reevaluate the maximum allowed unseating load due to stem growth for valve E4150F001. This is due to the temperature changes between the inside and outside of the valve body. The temperature inside the valve has been increased to 561"F and outside the valve body is 65 F. (Ref.1) 2.0 Methodology The computer sonware program MathCad 5.0 will be used for this calculation and will be treated as a hand calculation.
The methodology for calculating the thrust required to open an MOV subject to thermal binding due to stem growth is based upon calculating the increase in seating thmst due to thermal elongation of the stem. This is done by calculating the free thermal growth of the stem, and then '
using the stiffness of the valve / actuator assembly to convert the change in length to a change in seating thrust. The unseating thrust under the~ thermal binding load is then calculated by l multiplying the thermally bound seating thrust by the ratio of the normal unseating thmst to the I normal seating thmst. The calculations are done using the design inputs as follows:
A. Valve / Actuator Assembly Stiffness Under Thmst Loadine The stem is assumed to move at a constant rate of speed with a constant rate ofincrease in thmst during the period between seating and control switch trip during valve testing. The motor speed during this period is assumed to be known. Then, the stem speed can be calculated from:
Stem Speed = Motor Speed x 1 minwe , Lead 60 seconds OAR :
The motor speed is assumed to be given in revolutions per minute.
The rate ofload increase is calculated directly from the measured values of thmst and time.
Load Rate = '^'" ~ #"'"
CSTrim, - Sentrim, REVISION O PREPARED BY/DATE h kff, oF 7 CHECKED BY/DATE // // /g
~
VECTRA llIFORWTION ONLY Naperville, Illinois ;
PROJEDT' Pr' essure Lockinc/ Thermal Bindine Evaluation FILE 0102-00065 OWNER Detroit Edison Comoany CLIENT Detroit Edison Comoanv. Fermi Unit 2 0102-00065 F02-004 2.0 Methodology,(Cont'd)
The stiffness of the valve / actuator assembly under thrust loading is then obtained from:
Stiffness = Stem Speed i
\
l B. Ratio of Unseatinn Force to Seatine Force The ratio of unseating force to seating force is assumed to be the same for the thermally 3
bound condition as it is for normal valve operation. Using values from an opening test )
performed following a closing test at operating conditions, this ratio is simply: l Unseating Ratio =
MAX#*"
MAXcia,,
where: MAX, =
Maximum Opening Thrust, Ibf.
=
MAXao Maximum Closing Thrust, Ibf.
C. _Slem Eloncation Due to Thermal Expansion The amount of stem elongation due to thermal expansion is calculated by the familiar L x a x aT equation. The stem travel is used as L due to the fact that this the only portion of the total shaft length that sees a change in temperature.
Stem Elongation = Travel x DeltaTemp x TempCoef where: Travel = Valve Stem Travel, in. .
l DeltaTemp =
Change in Temperature, F TempCoef =
Modulus of Thermal Expansion, in/in F l
REVISIs O b9h/, PAGE 3 PREPARED BY/DATE oF 2 CHECKED BY/DATE g // g
- l. -
VECTRA l- .
"anetviiie. iiiinois /// FORMAT /0// 0//Ly PRofEC'T FILE 0102-00065 Pressure Lockinc/ Thermal Bindine Evaluation l
OWNER Detroit Edison Comnany i
CLIENT Detroit Edison Comoany. Fermi Unit 2 l
0102-00065.F02-004 l
2.0 Methodology { Cont'd)
D. Total Force Reauised to Overcome Thermal Bindine Due to Stem Growth The total thrust which is holding the valve closed is now calculated as the sum of the thmst due to normal closing plus the additional thrust due to stem thermal growth.
Final Thrust = Max a , + Stem Elongation x Stiffness The final value for unseating thrust isjust the ratio of the normal unseating thrust to the normal closing thmst times the thermally bound closing thrust.
Final Unseating Thrust = Unseating Ratio x Final Thrust The acceptance criteria recommended for use in this calculation is that the available motor operator thmst capability be at least 120% of that thmst required to unseat the MOV under thermal binding conditions. The 20% margin is provided to allow for uncertainty in the measurements used to calculate the stiffness and the unseating ratio as well as other effects such as valve - to - valve and motor actuator - to - motor actuator variations. All of these effects are random in nature.
The available motor thmst is 26,667 lbf. (Ref. 2).
l 3.0 Assumptions A. Stem Motion The valve stem moves at a constant rate of speed with a constant rate ofincrease in thmst during the period between seating and control switch trip during valve testing. l B. Motor Soeed The motor speed during the period between seating and control switch trip during valve testing is assumed to be known in revolutions per minutg (rpm).
REVISION $
PREPARED BY/DATE d Mk oF 7 CHECKED BY/DATE hg //u/4 -
l .
VECTRA llIFORul/TIOliOfILY
. Naperville, Illinois PRoJfCT Pressure Lockine/ Thermal Bindine Evaluation FILE 0102-00065 ,
OWNER Detroit Edison Comoany I CLIENT Detroit Edison Comoany. Fenni Unit 2 0102-00065 F02-004 3.0 Assumptions,(Cont'd)
C. Ratio of Unseatine Force to Seatine Force The ratio of unseating force to seating force is assumed to be the same for the thermally l bound condition as it is for normal operating conditions observed under testing. I D. Uncertainty Marcin j l
A 20% margin is provided to a!!ow for uncertainty in the measurements taken during testing and the unseating ratio, as well as other effects such as: valve-to-valve variations, motor actuator-to-motor actuator variations and running-to-non-mnning stiffness ,
variations. All of these, except for the running-to-non-running stiffness variations, are !
random in nature.
4.0 References
- 1. Form 4 to VECTRA report number 102-065.F10-001 Rev. O.
- 2. Fax from Paul Otal to Susan Korn,"MOV Torque Switch Setting Calculations Input", for PIS No. #4150F001 of Fermi-2, dated 1/26/96. Fermi Calc.No. 768850, Rev. A excerpt.4 E
%Lddu @O ^ d" h ' <
Md l
- 3. Fax from Ed Cavey to John Kelly, dated 1/25/96: JeadanGJd 2-) g 9
ikhh- u?,$
e VOTES Test #3 dated 3/l8/94 for E4150F001 j e VOTES Post Test Evlauation Data Sheet for Test #3 for Valve E4150F001 1
- Page 37 for DC 2712, Revision H
- 4. Carpenter Stainless Steels, Page 94, Thermal Expansion of Type 410 Sta ss Steels.
REVISION O PAGE 5 PREPARED BY/DATE M/fd CHECKED BY/DATE g f/g /gg
VECTRA Naperville, Illinois ((f[hk[g[/gg g PROJECh pressure Lockine/ Thermal Bindine Evaluation FILE 0102-00065 OWNER Detroit Edison Comoany CLIENT Detroit Edison Comoany. Fermi Unit 2 0102-00065 F02-004 5.0 Desian input:
J Stem Travel (in) Travel = 9.375 in Reference 3 x
Change in Temperature (F) DeltaTemp :500 Reference 1 Mod. of Therm. Exp. (in/in F) TempCoef =.0000065 Reference 4 Reference 3 (Stem material: A182 TP 410)
Max. Static Closing Force (Ibf) Max cjo3e = 36910 lbf ,
Reference 3 Typical Thrust Trace Max. Static Unseating Force (Ibf) Max open : 16548 lbf Reference 3 - # Seating Control Switch Trip Thrust (Ibf) CSTthrust 32157 lbf Reference 3 Control Switch Trip Time (sec)
CSTtime :38.764.see Reference 3 Thrust at Seating (Ibf) Seatthmst .: 1192 lbf Reference 3 Time of Seating (sec) Control Switch Trip Reference 3 Seatt *. :38.607 sec Motor Speed (rpm) MotorSpeed =
Reference 3 min Actuator Overall Ratio OAR = 30.50 Reference 3 Maximum Thrust Stem Lead (in) Lead = .50 in Reference 3 REVISION PAGE 6 PREPARED BY/DATE M/f4 OF 1 CHECKED BY/DATE g %g ,
7-
r 1
l - -
VECTRA
. Naperville, Illinois g/P0R h(([g/[ 0/! Y PRoJE'CT' ' pressure Lockinc/ Thermal Bindine Evaluation FILE 0102-00065 OWNER Detroit Edison Comoany CLIENT Detroit Edison Comoanv. Fermi Unit 2 0102-00065 F02-004 6.0 Calculations:-
I'*
Stem W ::MotorSpeed """- Stem 9g =0.519 5 60 sec OAR sec
, CSTtivust - Seatthrust l Staticrate : Static rate " I 97229
- Ibf t see CSTtime - Seattime Stem speed Stiffness .: Stiffness = 0.000002632 in 1 Static rate Ibf UnsentingRatio : P*" UnseatingRatio = 0 448 Maxclos, StemElongation . : Travel DeltaTemp TempCoef Sf:mElongation =0.03 in I "E"U "
Finalthrust : Maxciose i- Finalthrust = 48486 lbf Stiffncss Finalunseating :UnseatingRatio Finaltluust Finalunseating = 21738 lbf F avail = 26667 lbf Reference 2 F ,y, i - Final unseating
-100 Margin = 22.675 %
Final unseatmg 6.0 Conclusion This valve is capable of performing it safety related function based on the results of this calculation.
I REVISION
./ /
PAGE 7 PREPARED BY/DATE 47/ 'd(#74 oF 7 CHECKED BY/DATE h //Q r <
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l itc. . Ote2-Oc85.Foz . ,
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Alle)- 1 i PageiJ7 l l 1
." , i j 4 I Fax Coy l er Sheet IIIFORWTIOli ONLY \
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DETROIT EDISON-FEIG112 l i
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OATE: Ianuary 26,1996 TIME: 2:03 PM TO: $UE KORN PHONE. 708-778 4 244 i YECTRA PAX: 708-778-4444 l 1
FROM: PAUL OTAL PHONE: 313 586 1739 l FAX: 313-586-4911 4
RE: k4150F001 cc: d.SCHERMAN Number of ; ages including cover sheet: 7 Message OPERA '^0R CAPABILITY CALCULATION i
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.3 g.T.iner.f .-.- . ,. Opening 13.417 i t .Strokw.:T.ime 'd[ pass Switch -- Opens seconds 12.620 s. Sten.a. '.e. 5:*.
;f;3- Open, Torque .- !
Calibration Range: 13271 t o -36,8 M 1 :, s . ' 3:. .i t '" +;.Pb.rcesi' C i.. ilbs) Clostng
- c. .* i l -2526 Mar Anning F6ree 3 -1495 .
Ave Thfusit. N nnino.Fcree At Start of Wedging -1192
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secemls Npas:: Time 12.829 secoMs l h,passTime! j 13.433 l
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/Fingsn.........: 0/ B General Cookents: :. i r.<.; t : .#. f.. :. c .
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-05 771 2501 10.5 Maximum Force at Disc Putlout, n.
09 825 16548 19.3 i.'! 2: 839 9320 23.2 Opening Running Condition (Hear Begin'g) it] l
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013 1721 1164 11.0 Opening Running Condition (Hear t~nd) 014 ' - 11812 849 11.0 849 10.5 . - O p e n T o r q u e i< y p a s s S w i t c h Opent. 012 12998 -0 15.9 Open Limit Swatch Opens 016 13S95 -2.7 Motor Start CB . 6988 1059 Inrush Current Peak s7011 1476 -82.3 i on (Hear Middlei I 2 17216 -973 -4.2 Lost Closing Motion Runninij ReitCon <lition (Hear De.i n n' q : 18133 -1633 - 7.1 Closino Running Centti tion t He a r C r..:1 p 4 -6.6 4 C5 28405 -973 Close Turque la y pa s s s w a t e t. O p.e n s 30421 -1083 -6.1 Dise Notion Stops / Start or W ed y a . e* C7 --1192 -6.6 - Gli 30607 --321S7 -42.7 C1ose iornuo Sunt b O pe.: - <.. C :e ) J0764 C14 4S.2
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Max. Thrust Rate: 4 19%;000 42 lbs 4mp catino..: 17.0
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.c ..Humber......: E'4150F001 Sert z.1 W.......: N o .a .
- 50.0
....... ....: GATE Order W........: 373E72-A S t a r *: 5 0.ced. s r.a.u e : .
kun Torque..: ,12. 0! i W...... ....: 19"l
;t4hrust..'.;J!+.2 5631 Ibs Worm Gear Teeth: 34 Hors e : f' owe r. : 1*33 tfom .~. .r. re ' VERTer .
Gear Ratio.....: 30.5 0007-1 Spring Pack N I
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Itse*natertal'. iameter.2.v r. :. 2.125; 9182 TY418- inches -- ; l 0 ,
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N""an .Humber. s 8 J. ;.4' ... . Y.. E4150F991 2;.fTE:: :.\qi .f.. Serial N........: N.......: Nos. i seet ! yJe. . ..& . .:. 4 s. s GATE Order 373272-4 Start toi Run Torgs j
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'arget ThrustJ...: 75631 lbs Gear Ratto.....: 30.5 Horse) Pm !
5pring Pach N 0007-1 '
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