ML20215L079

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Rev 1 to Purge Containment Isolation Valve, Operability Analysis & Test Rept
ML20215L079
Person / Time
Site: South Texas STP Nuclear Operating Company icon.png
Issue date: 04/17/1987
From:
VALTEK, INC.
To:
Shared Package
ML20215L035 List:
References
34753-2-48, 34753-2-48-R01, 34753-2-48-R1, NUDOCS 8705120094
Download: ML20215L079 (58)


Text

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Operability Analysis and Test Report 34753/2-48 Purge Con +=b=aett Isolation Valve for Bechtel Energy Corporation Job No. 14926 Purchase Order 14926-4409/8409, Item 38 Revision 1 April 17, 1987 (Replaces Operability Pre-Analysis Report 34753/2-48 Rev 1)

Q& Al&cl%7 A/: pre-ana.48(8) 8705120094 870508 PDR ADOCK 05000498 A PDR s

4 J TABLE OF 00lfrENTS Purpose.............................................................. 4 Procedure............................................................ 4 Torque Requirement.............. .................................... 4 Torque Measurement Procedure......................................... 5 Equipment List for Torque Measurement. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Seat ing Torque . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Dynamic Torque Procedure............................................. 6 Dynamic Torque Tests . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 Discussion of Dynamic Torque Tests . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 Actuator Torque Output . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9 Valve and Actuator Stresses.......................................... 10 Tables Table 1.- Dynamic Torque Si===vy................................ 11 Table 2 - Actuator Torque Output. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12 Table 3 - Stasmary of Stresses and Stress Ratios. . . . . . . . . . . . . . . . . 13 Figures 4 Figure 1 - Sample Torque Measurement............................ 14 Figure 2 - HP 71B Proin e Listing. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 Figure 3 - Dynamic Torque Test T/AP............................. 16 Figure 4 - Dynamic Torque Prediction............................ 17 Figure 5 - Dynamic Torque Test Setup............................ 18 Figure 6 - Actuator Torque Output. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19 Figure 7 - Actuator Torque Output and Required Torque........... 20 Appendix A - Operability Pre-Analysis Report 34753/2-48............... A-1 Appendix B - Valve and Actuator Stresses . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B-1 Appendix C - Operability Demonstration and Qualification.............. C-1 Attachment 1 .................................................... C-5 At h4u=n t 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . C- 8 EI 1

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8 J Recorti cf Revicions Page Description of Changes Rev No.

1 Update to Rev 1 from Rev 0 1 2 Add Attachment 1 and 2, rentanber pages -

1 3 Add Record of Revision 1 4-20 Rentanber page 4-20 1 A22 Remove redundant page 1 C1 lat s attence: add " copies of which are included in this repor?."

C1 Cr==arits 1D: add last sentence about dynamic test 1 C1 Cammarits IES: Completely revised 1 C4 Comments A2: revise orientation 1 C5-C9 Add attachment 1 and 2 to Appendix C 1 l

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Operability Analysis and Test PURPOSE h purpose of the operability analysis is to demonstrate by a combina-tion of analysis and testing that the referenced valve and actuator meet the following requirements.

1. h available actuator torque must be twice that required at all angles of disk opsmimt when considering valve differential pres-sures of 48.4, 24.2, and 0 poi.
2. h actuator torque pMM by the actuator spring alone must be

, twice that required to close and seat the valve with no flow assist.

3. Valve and actuator stresses critical to operability must have a ratio of allowable to actual stress equal to or greater than two.

Stresses will be r=1mfated based on the worst case torques / loads.

PROCEDURE h theoretical torque analysis for requirement neber 2 above and an analysis of valve and actuator stresses for requirement nimber 3 above were perforined in the operability pre-analysis (Appendix A of this report).

Operability tests were perforined to verify the torque requirements of the valve and the torque capability of the actuator.

n e detailed stress analysis and/or static deflection operability test required to qualify the valve and actuator are included in the valve Design Report which will be issued at a later date.

Environmental qualification of the valve seat is by test. A Qualifica-tion Test Report will be issued at a later date.

We operability tests were perforised on valve serial number V34752-048-1.

10RQUE REQUIREMENT

% e torque required to operate the valve consists of three components.

a) Dynamic Torque b) Frictional Torque c) Seating Torque (occurs at 0 degrees open)

- Page 4 of 20 I

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l In the operability g . r lysio the marimam torque required to operate the valve as asstmed to be 7351 in-lbf, which was the estimated seating plus i i frictional torque at the fully closed position. h stress analysis in the operability pre-analysis m port was h==ad on 7351 in-lbf.

Operability tests were performed to verify the dynando, frictional, and seating torque, and to verify that the actuator would produce the torque required to operate the valve, including a 2-to-1 margin.

TOREJE MEASUREMENT PROCEDURE h dynamic, frictional, and seating torque, and actuator torque output were all measured by means of strain gases attached to the valve shaft. Two strain sages were placed diamatrically opposite each other on the valve shaft approximately 1.75 inch down from the top of the actuator yoke.

A data acquisition / control smit was used to read the strain sages and calculate the correspnndinn torque on the valve shaft. Both the excitation and the ir-had voltages were monitored. Each torque measurement consisted of two raading= of excitation and induced voltages. A sample of the data is

shown in Figure 1. h time and date of the measurement are printed for reference. Actuator pressure (P) and disk position (% rot) are both input by the operator and printed for reference only. h y do not affect the torque calculation. He values of shaft diameter (D), Poisson's Ratio, endulus of elasticity (E), and strain sage factor which are used in the torque calcula-tion are printed for reference. Next, the data for each of the two raadings are printed. Excitation voltage is ei, irwhead voltage is eo. h calcu-lated strain, shear stress and shaft torque are printed. h polarity of the calculated strain is such that a positive torque indicates the actuator is tending to open the valve, opposed by friction or dynamic torque as the case say be.

At the start of each test the strain sage bridge was zeroed at a known j operation condition (usually while the valve was streking open with no flow through the valve). Torque measurements were made with the valve stroking open and closed to establish a frictional hysteresis null value. his null value, which is the average of the opening and closing frictional torques, was subtracted from each torque reading. In the case of dynanic torque measurements, the frictional torque and null torque were eliminated by the method used to perforin the calculations.

BEJIPMENT LIST FOR 'ITEQUE MEASUREMENTS Strain Gages - Micro Measurements Div CEA-06-187UV-120 Lot R-A40AD04 Gage factor 2.035 f,0.5%

Data Acquisition / Control Unit - Hewlett Par *mM 3421A calibrated December 2, 1986 Printer - Hewlett Packard 82162A Calculator / Controller - Hewlett Packarti 71B Program listing is shown in Figure 2.

Page 5 of 10 l

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Seating Torque h valve seat was installed in the valve and the valve was installed between flanged fixtures. h valve was opened to 100% open and the strain sage bridge was zeroed. H e null torque reading was established as -515 in-

-lbf.

h valve was allowed'to stroke closed several times while the induced voltage from the stain sages was monitored to verify that the maximum seating

. torque does indeed coeur when the disk av=== to a stop against the seat.

He valve was opened and allowed to close due to the actuator spring torque only. A seat leakage test was performed to ensure that the disk was fully closed: leakage was zero bubble per minutes at 54 psig.

h valve was opened and closed (by spring only) six times. After each closure, the shaft torque was measured. h average of the six tests, corrected for the null torque raarHng, was 4403 in-lbf. His value includes both seating torque and frictional torque.

h required actuator torque to close and seat the valve is therefore 8806 in-lbf, including the 2-to-1 margin.

DYNAMIC '!UGUE PREDICTION

REFERENCE:

Floyd P. Harthtm, ' Effects of Fluid Compressibility on Torque in Butterfly Valves,' ISA Transactions Vol. 8, No. 4, p. 281.

S e valve specification requires thit the valve actuator be able to produce at least twice the torque requin d to operate the valve. Se torque required to operate (stroke), but not seat or unseat the valve, consists of two components: dynamic and frictional.

%e dynamic torque (Te) is caused by fluid reaction forces acting on the valve disk. h e friction torque (T,) is caused by bearing friction.

H e dynamic torque can be determined experimentally from tests conducted with water flowing through the valve. However, the dynamic torque due to compressible flow (r.ir or steam) will not be the same as the dynamic torque predicted by a test using water. The ISA paper referenced above contains a method to predict dynamic torque due to compressible flow once a test has been performed with incompressible flow.

Two equations from the ISA paper are used Ka = To/D8^P (test with incompressible flow) (1)

Ts ' = Ka D8 Pa (Ca C /59.64)8 Sint8 (2)

Page 6 of 20

In equation (1), To and AP are dynamic torque (in-lbf) on the valve disk and pressure drop (psid) through the valve measured during a test with water flowing through the valve. D is the disk diameter (inch). E is the dimensionless torque coefficient which relates torque to pressure drop. E varies with disk position and must be =1 & 1=ted at different disk angles.

In equation (2), To ' is dynamic tortpe (in-lbf) due to compressible flow through the valve when upstream pressure is Pi (psia) and disk angle is 9 (closed = 0, open = 90 degrees). S e factors C and Cs are used in a particular valve flow sizing equation. C is a correction factor for variation in specific heat ratio and for all practical purposes can be assumed to be 1.0. Cs is a correction factor which corrects the flow

. coefficient (Cv) for gaseous flow. Valtek Incorporated uses the valve sizing equation based on ANSI /ISA standarti S75.01, which does not use the factor C .

Werefore values of Ci are not available for the valve. However, typical values of Ci for a similar valve con be found in Fisher Catalogue 10, October 1984, page 1-15. For valves 18-inch and larger, size does not have a large effect on the value C,. S e values for C are listed in Table 1 of this report.

DYNAMIC ltElUE TESTS Tests were performed.to determine the torque coefficient E . He results are shown in Figure 3 and Table 1, where dynamic torque divided by pressure drop, rather than K , is shown, Frictional torque has been elim-insted in the prMnw (see Discussion of Dynamic Torque Tests).

Ts/oP = E Ds (Test with incompressible flow) (3) 1 In all cases, the dynamic torque tends to close the valve.

Equation (2) becomes Ts ' =(L D8 ) (C )8 sin 8 9 Pi (4) i (59.64)8 where & D8 'is given by equation (3)

! Values' of the squared terms are given in Table 1.

S e valve specification requires the actuator to be able to close the valve with a 2-to-1 torque margin at pressure drops of 48.4, 24.2 and 0 paid.

With no pressure drop (0 paid) there will be no flow and no dynamic torque.

Asstating that the downstream pressure in the other 2 cases is 14.7 psia, the dynmaic torque must be predicted at 63.1 and 38.9 psia upstream (P ).

Table 1 lista values of dynamic torque (which tends to close the valve) less frictional torque (which resists closing) for 24.2 and 48.4 pcid pres-sure drop. Se torque values listed for 0 paid are simply zero dynamic Page 7 of lo

.. . = - -_ .=_ . - - , . _ .

l torque less frictional torqua. % ese torque values are also shown in Figure

4. A negative value indicates that the dynrunic torque tending to close the valve is less than the frictional torque which resista closing, so the~

actuator torque must exceed the negative value by a 2-to-1 margin. %e required actuator torque hamad on dynamic and frictional torque is listed in Table 1.

DISCUSSION OF DYNAMIC 'IERQUE TESTS h dynamic torque testa presented two problems. First, the water flow rate available for test was limited, so the pressure drop that could be

, developed across the valve was limited. h dynamic torque exerted on the valve disk was therefore limited. Second, the pressure fluctuations at the pressure tape, due to turbulent flow, were large enough that the small pressure drop through the valve could not be accurately deterimined with a manometer. A thirti problem was that during the test the valve disk position would change slightly because the valve does not have a positioner. %ese problems were solved by using the procedure explained below to calculate the change of dynamic torque due to change of pressure drop.

% e valve was installed as shown in Figure 5. Se valve downstream of the test valve was used to change the pressure drop through the test valve..

h flow meter was used to measure flow rate, which uns later used to calculate pressure drop.

, (Q (gpa))8 j aP = (5)

(Cv)2 Values of Ov were taken from Valtek Engineering Data 2, Rev 8/85 Section 16 Table 1. %e flow meter was calibrated in accortlance with 7altek proce-dures, and the calibration was checked after the torque tests were completed to verify the calibration had not been affected during the tests.

h procedure to take a measurement at a given disk position is as follows. First, with no flow through the valve, the actuator pressure was adjusted until the valve disk moved to the desired position and stopped. %e l disk position was recorded. % e downstream valve ~would then be opened. A

torque and flow measurement would be taken simitaneously and the disk l position would be recortled. h downstream valve would be opened further to l

produce a higher pressure drop through the test valve. A second torque and flow measurement would be taken and the disk position would be recortied.

h e pressure drop at each of the two flow conditions was calculated,

using equation (5). %e torque at each flow condition was taken as the

! average of the two readings taken at the flow condition, without subtracting j the null readings or correcting for friction.

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%e factor T/oP was calculated by dividing the difference in the torque for the two flow conditions by the difference in pressure drop for the two flow conditions.

Page 8 of to

=

T - Tt ._

e T/aP = (T is average of two torque raariings (6) aPa-oP at a flow condition) h calculation eliminated the need to subtract the null torque rearling or frictional torque harmina the difference in torque for the two flow conditions was used, rather than the torque at one condition.

His prnrwhere was repeated approximately even 10 des _ from fully closed to fully opened and then back to fully closed.

As stated before, the disk position would change slightly during a test.

h is was due to the fact that with a constant pressure on the valve actuator the valve would move to a particular position with a residual torque opposing the motion left in the bearing-shaft. When water started to flow, the resulting vibrations would tend to ' jog' the valve shaft slightly further in the same direction as tha original motion. h average of the disk positions for the two flow conditions was used.

h re was considerable scatter in the data due to the small pressure drops and the resulting low torques. h data shown in Table 1 and Figure 3 envelop the lowest values from the tests. In all cases, the dynamic torque tends to close the valve. Because the valve is required to close during an accident, the use of the highest values of dynamic torque would result in smaller required actuator torque to close the valve. h refore, the use of the lowest dynamic torque is conservative in that it requires hisher actuator torque.

h question of highest or lowest dynamic torque is actually a moot point, because as shown in Table 1, the highest actuator torque is required when there is no flow through the valve to assist closing.

ACIUA'IOR 'IORQUE OUTPUT

%e actuator torque output test was perforined on the valve with no seat installed, and no flanges installed. h is was necessary in ortler to be able to lock the disk in position.

%e strain gage bridge was zeroed while the disk una stroking open. he null torque raading was established as -493 in-lbf.

he valve was opened and allowed to close, by the actuator spring only, against a wooden block set between the disk and body stop. A torque reading was taken. h n air pressure was applied to-the actuator, tending to close the valve. A torque raadinn was taken. his procedure was repeated at various disk positions.

The results of the test are shown in Table 2 and Figure 6. he torque values shown are corrected for the null torque reading. % e actuator torque at 70 psi actuator pressure was found by subtracting the torque due to the Page 9 of 20

. o spring from the torque due to spring-plus-air pressure and divided the result by the applied air gessure. H is value of T/ psi was then multiplied by 70 psi. h net torque to open the valve is the difference between the torque due to 70 poi pressure opening the valve and the spring torque closing the valve. h torques p M M with 70 psi actuator pressure are shown for comparison with the theoretical values shown in Appendix A of this report.

VALVE AND ACIUA10R m*=

h e Operability Pre-Analysis Report (Appendix A of this report) explains the =len1= tion of atresses and allowable stresses. N =len1=ted stresses in the Operability Pre-Analysis Report were all based on a maximum torque of 7361 in-lbf (seating), and a ratio of allowable to calculated stress of 2 to 1 or more is shown.

h Operability Tests showed that the maxista torque actually is 4403 in-lbf. h erefore, the analysis in Appendix A is conservative. Stresses and stress ratios which are calculated h==ari on 7351 in-lbf torque should be adjusted to correspond to 4403 in-lbf. h corrected values are shown in Table 3 of this report. Calculations are shown in Appendix B.

Page 10 of 30

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9o 16 0 195 . o7197 -488 338 851 to 10 Notes ~

(i) Fr. m Fisher cat l 3 io , ocisher 1984 ;, p.,e I-is .

(2) Dynam*,c torque wif k comp ressible flaw , less fric.Honel torqu e of 488 in A f measur ed durinj dynemic ' torque test. Values less ,

than zero in dicof f friclionel torque .is ogre

  • Yer than dynamic heque tending to close the volve j so theit aefugier brqu e '

is ieguired 6 order to close tk.e va lve .

h) A+ P , = I 4 7 psic. the prestore drse hra he valve is O prid so there is n o flaw aJ hrefore n. d.gn mic frque.

(+) Require a gefu hr %cque h close the valve. is equal h Iwo

+1mes the fr;< fione l forque (see Disconn .9 0., nom;c Tocqwe

' Tests). The htskost fetef tan mecauer d darin3 tke sertes of +est.s was 516 in.Af . ( see Seccting Torqu c).

(5) Tocque v. luc 3 lis ted 4 0 dgree_ epen do n.F cnclu de disk seating forq u e.

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FIGURE 1. SAMPLE TORQUE MEASUREMENT 10:35:19 86/12/15 P= 80 psi on Top

?. rot.= 63 Des. rot.= 56.7 B= 1.749 in Poison's Ratio = .272 E= 28500000 psi Case Factor = 2.035 ei=+0'.50150E+1 eo=-0.00030E-1 eo/ei=-5.982054E-6 Strain =-2.939575E-6 -

Tau =-65.86313E0 asi Tort =-69.18974E0 in-lbf ei=+0.50151E+1 eo=-0.00031E-1 eo/ei=-6.181332E-6 -

Strain =-3,037500E-6 Tau =-68.05720E0 psi Tors =-71.49463E0 in-lbf A

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.I 450 E5=4*El/(4*E2*F3-2*F'; -

[, /130 IF El=1 T.NE.N...A.=.1.00.

I iF _.

3*El) ' *i " l" 3 . '

- p7 .

. t 460 il=E5*E/(1+N!) ;s ... -V:

I -

.J 4 470 T=il*Pl*B^3/16 'N I.h.140 IF 31=2 TIEN 150 1. IlFUT. .'S.er. ins f.e..rs

~

A=104.7,- ....

M, 400 PRINT - " Strain =*sE3 i:-

,  ; j. e: *sF1 ' '

  • i '
n. . ps' i

, 170Sig

., 100 F=Fl+D s ' ""' -d3' P}y.i M::'.. ".v.-Id 'J 1*

J.'".p _

4M '. *F' INT Ir.' 4*iau=*sTis*Liy iM.

4:

,.500 MINT. " Tort ="1T1'! in

,a.!IIMPRINTTIMES,s%'sNTf4' ,"-lbF 7 ' ! ' 'l A,7 -"

.! .'. Et I.

+' ! '. I 1.:. i i . t ; '"L

. e .-

  • 500 E3= VAL (E38) '

j.k

. .200 PRINT.'.P=*;P.s.".. psi o F.. i' g . .. ..l590E4= , VAL ..(E4,8).. .

i, s '. 2tg IF B1=1 THEN PRINT

  • h . -

610 PRINT *ei=*sE48 ;'.Y.

ll' Tee"ELSEPRINT*0ot.

. r220.l. PRINT *FS="#Fis

  • I

"-'- L. . . :i' 620 PRINT "

. '".*eo=*sE38 !

i C1 630 ENG 6 l' -

} bf* I' ' * ' ' ' ' l '. W ' .' 4 *.

.:..h 640 PRINT *eo/ei=*JE3/E4 '

. j.:!2301: PRINT *Flot=? s? - ., ,.

.Q. 650 E5=4*E3/(4*E4*F3-2*F.

g.P lbf'~' ' l;'Wii' ,* --"

i','f3*E3) ' '7" : ! ' .C

{h

... g. 660 Tl=E5*E/(1+NI)

'. -((  ; PRINT 231'2INPUT rot.="sB2 '?2 .' rot. '*s82.'

235 '

"E '670 init*Pl*Ba3/16 :'

~~

.': 1.J'24'8 PRai;! 'les.' ret =*sl T *.' ~~.' 600 PRINT Strain =*sE5 7-

. ;f2*M/100 : '

N' t' ' f. ... - d .' 690 PRINT." Tau ="siist as

250CALLTORCO,N1,E,F3) -

y' 1 3 el' ". 3.

.1.I #.! ,260 GOTO TS M /*3".4

-" ~.

2 P 270 U S ' { P w .h .h ..

~. " 695 PRINT:?iort=*.;is". in

.;' 'i 200 SUS TORC (3,NI E.F3).

... . -lbf* id @ c..i l

W W J,700 PRINT / V . i h!,'.290.STI i.d.t*t"il.T ':'D. T ''.1,h/ Til PRINT f 9 l'h}r "l% M b,'C'

  • N.(291 OUTPUT.:1.#P KV22,23

' .i . 720 EMB SUS i . ' ., ! d

,1 : ,, ;

  • h ,
  • W: l .'t i ;'.g*_. *

'O'  %

,3

,s l fc!292 ENTER 11 sElt.'."c'?.y.';' .

.;'l293 ENTER ti sE28 ' ' : P f

..'H 294 00TPUT.:1 s*0CV22,23 % p. ., i.

,p .,

,i . . ,

.. g * [ .: I9fM l- p m".! Nie)l MP##-  ;. e o c-

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Page !!i of 20

--,w'yg.w...e-m.w m,'w- i.-,-e-.----.ey--y,-o,.g.Md-e ws _+ pee ==seem-a- wcw w -

_h""""s""4u'"-e"u==f'se'-m*eNww.wier -.__.W-""w-W"es-PW"..'NM*TWD PP'.*9WW"=='-eM'"r'"*V"-

lr FIGURE 3. DYNAMIC TORQUE TEST T/ Delta P 4

500 4........................... r m .....,...................v

....,........,,.........J. .

1, -

1 400 _

1 T  :

l

/ -

300 -

F

~

,- D -

g .

i 1 -

l

~

t 200 I l

f E

1 a -

! P  :  :

\ .

l 100 - _

i -

i 3 -

t -

g ...............s...............................................,,,,,,,,,,,,,,,,,,,,,,-

i j 0 10 20 30 40 50 60 70 80 90 ,

l Degrees Open j Page 16 of 20  :

i i e

FIGURE 4. DYNR

.3000  ;.............r............... ... ...............................................

M I C L E S S F R I C T I O N R L T.........

ORQUE

.i, i 2000 -

r n -

P 1000 -

o

.- 3 u .

1 n

~

d ,

s -

0

/  :

j!  ! x x x x x x x i:

-1000 """"'""""'""""'"""^'""""'""""'au'*"'""""'"""^E O 10 20 30 40 50 60 70 80 90 Degrees Ooen

  • Delta P O # De ta P 24.2 O Delta P 48.4 Page n of 20

(

n, o, l g -

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l FtG UR E E , %ne,A Tokue Test Seid  !

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14s 3 18xl4 l San 21480 , NerSty *  ! IA"  !

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t7 ReJacer /Redwcer g,P=. A F8Peader  ; W I :$ itO _!'. 8 o f F A 'k m.

i i last 8
  • t Velvt I

l F16wmeter!

' j e vertical Pbet!

8" BeeWiig .

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Drain to i j 5"mP i i I

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FIGURE G. RCTURTOR TORQUE OUTPUT 40000 .

.................................................nm..................................

~

i 30000 -

n [ .

n :t N 1,

P 20000 -

o a -

u

" i s

10000 ,._'

,, x A e a S A e a alea a a a a a haa aa a aaaaha aaa a a aam lA a a aaaa aa lA aa a aaaaaha a a a a a aa a a a a a aa a aalm g 0 10 20 30 40 50 60 70 80 . 90 0

M Spi-i ng C1 os i ng

'9"*[*7genpsi Opening O- Net Opening i

i Page 19 of zo P

1 _. - - _ - _ _ - _ _ _ _ _ _ _ _ _

e-FIGURE 7. ACTURTOR TORQUE RND REQUIRED TORQUE 20000 ...................... m n............,.........,.........,.........,.........,.........

18000 -

16000 -

1 .

n 14000 -

  • 12000 -

l l

P 10000 -

o , , ,. -

n 8000 -

d .

s 8000 -

4000 -

2000 - _

M M M x x x x x x  ::

0 ' ' ' - '- ' * -'

n --

~ 1 0 10 20 30 40 50 60 70 80 90 l

  • Degrees Open TORQUE REQUIRED T0,.CLOSE # SPRING TORQUE AVRILRBLE TO CLOSE l Page 2o of 2o l

Apperxlix A to Operability Analysis and Test Report 34753/2-48 Page Al of A 3.1

Operability Pre-Aaslysis Report 34753/2-48 Purge Containment Isolation Yalve for Bechtel Emergy Corporation Job No.14926 Purchase Order 14926-4409/8409, Item 38 Revision 1 October 15, 1986 I

e k e 0

{

Pase A1 1

- , - - - , , . .._ _.-_- _ _ _ - , _ _ , , - - - _ . , _ , - - - _ _ - - _ _ . . . _ , , , - , . _ , . . - . _ . , . - , - . , - . - ,_,-_n- , _ . - - -

. - _ - - . -_ . - _ -, .-. . - - - = - - - _ _ . .

l Operchility Pre-Analysis FURPOSE ,

- N purpose of the operability analysis is to demonstrate by 'a oombination of analysis and testing th~at the referomoed valve and actuator  !

meet the following requirements.

1. h available setuator torque must be twice that required at all angles of disk opening when considering valve differential pressures of 48.4, 24.2, and 0 psi.
2. The actuator torque produced by the satsator spring alone must be i

twies that required to elose and seat the valve with no flow assist.

3. Valve and setuator stresses eritical to operability must have a ratio of allowable to natual stress ogsal to or greater than tso.

Stresses will be calesisted based on the worst case torques / loads.

PROCEDURE N operability pre-analysis will isolsde only the theoretical torgne analysis for requirement number 2 above and sa analysis of valve and metaator stresses for requirements asaber 3 above.

Operability tests which will verify the torque requirements of the valve and the torque capability of the motsator will be isoladed in the final operability smalysis report. See Appendia A for a brief description of the operability tests that will be performed.

The detailed stress analysis and/or statio defloation operability test

~

required to gsalify the valve and actuator will be isolsded in the valve Design Report and/or Qualifloation Test Report but will be referessed in the final operability report. The final operability report will address all operability questions in Requisition 4409/8409 Rev 15 and in the April 18, 1986 meeting.

h operability pre-analysis is based on the design which is detailed in'the valve Assembly Drawing A34753/3-48 Rev 1 and the valve Bill of Material V34753/2-48 Rev 1.-

TORQUE REQUIREMENT I -

ne torque required to close and seat the valve with no flow assist is

{ simply the torque required to overcome bearing sad seat friction. It osa be i

estimated by the following formula, which was.eapirically developed from aumerous tests by Valtok on various sizes of valves.

l T, = 27(Dd I*

i where T, is disk seating torque with no flow assist (f a-1bf)

Dd is disk disaster (la).

Pye A-2 l

l L_. - - - - - - - - - - ~ - - ~

T, = 27(16.5) * = ~ 7351 ia-1bf Note that this torgue oseurs at the fully closed disk position.

m valves will be installed so that flow from 'the oostainment vessel will as.sist the seating.of the disk and will more tham.eospensate for the additional frietion eassed by the pressure drop through the valve. It is assumed that the dynamis torque on the valve disk due to flow through the valve is less than the disk seating torque. This assumptio's will be verified by the operability tests whiek will be eondmoted later (see Appendix A).

m required torque at which the sotuator torgue (spring only) sad stresses' will be analysed is therefore 7351 in-lbf. This value will be verified by test (see Appendix A).

TERORETICAL ACTUATDE M M N theoretical torgue output of the valve setustor with 70 psi pressure applied to the actuator is listed in Table 1. These values were calculated ignoring frietional losses.

m first solana of Table 1 lists the torgue due to 70 psi actuator pressure only.

m second oolana of Table 1 lists the torque due to the actuator spring only. The third solema is the met torgue available to opes the valve. hee three sets of torgue values are plotted la Figures 1-3.

Table 1 shows that the sotsator spring will supply 20443 in-ibf of torque at the closed position, which is greater than twice the required seating torque.

(2)(7351) = 14702 20443 > 14702 -

J,& H Atg ACTUAIDE STRESSES .

The stresses in valve and sotuator composeats which are critical to valve operability we're smalyzed. Other ocoponents which are not critical to valve operability were not analyzed.

m aseeptsase criteria is that the stress must have a ratio of allow-able stress to notaal (calculated) stress ogsal to or greater than two.

Nome of the composeats which were analyzed are classified as pressure retalning and acas of the materials for these components are ASME code-controlled. In addition, all of these components, with the exception of the valve shaft, are external to the pressure boundary and are not subject to the harsh environment (323*F). The valve shaf t is exposed to the harsh

' environment for the short duration of the elevated temperature. The rules for dete,rmining allowable stresses given la ASME Sec III NB-3546.3(a) apply P% e. A- 4

.._= _- . . _ . - - - - . - - . - _ - -_ __ . .- _ . . _.

, specifically to tho volva sh,ft. Be 3ts3 no rules are gives for determining the allowable stresses for the other sosponents, 'the same rules given la NB-3546.3(a) will be used.

m rules in ND-3546J(a) state that the allowable (tensile) stress is the lesser of two-thirds'of the minimum specified yield strength or one-fourth of the minissa specified tessile strength. . N allowable stress in shear will be takes as 58% of the allowable tessile stress in scoordance with the eaziana distortion energy failure theory.

I m a ma Coun m 0NS h valve actsstor is designed so that the actuator limit stops absorb

the portion of' the trust of the pistos/ spring which eseeeds the thrust that is required in order to produce the assessary torque at the valve shaf t.

The valve shaf t and setuator linkage seaposeats are subject only to the forces and torques aseded to prodsee the required torque at the valve shaf t.

' Based on the assumption that the nazimaa torgue oeeses as the valve (isk oloses against the seat (or breaks out of the seat) and based on the fact i

that side loads are greatest at that same position, the valve shaf t and linkage components will be analysed at the seating torque (7351 in-1bf).

h pistos stem and spring stem will be analysed at the worst combination of pistos thrust and side load.

i NA11mm4 0F CtBISTEUCTION AND ALLotAE,5 51EESSES MATERIAL TIELD STREN G TENSILE STRENG1R ALLOWABLE 31125S PSI PSI (TENSILE) PSI c

.A-564 630 145,000 155,000 33,750 E1025 SAE 4140 200,000 215,000 53,750 EEAT TREATED 416 STAIM,ESS 100,000 125,000 31,250

! EEAT TREATED l

l OILITE BEONZE N/A N/A -

2,000 l

I l

hse ks

g VALTEK co UTADON SHEE nue olems. study sr et No. Ae<I sutvect *

%t orStudy No-hy Date 19 kmm a r ., o[ stre sses eind se te b F.c tons Part , Ma terial ,Allwa61e ,CekuleteJ , Stress , Comment Stress. Stress . P atio Vo lve Sha 9 . A -56 + 4,3 o . a.3 475 . lll7 g . 2.'o . hear a t keved sechs't H 102 F (shear) Ishter) 'k actualer connet h Shqft ke ys < A -i64 630 22475 264o 8,5 shene on keys max H fois (sheo r) (shece)

Piston Ste m A -f64 63o 39750 15 099 1.4 uppe threaded ca4 mn H8015 noresI $ tress Spring Ste m A 5(.+ 63o 38750 +l+5 %3 l% ,r eat me.x n=rva.I H 1o15 strest Siem Adopbr SAE 414o 537.Fo 12441 4'. 3 at lichge pin HT Stem I3ushig 0l life Sr.nte 1000 SWo F.3 s prin3 sten ~ cus'n63 Achfor Lints A -564 630 53750 2serio 2,o exl,1 p)wi beog;g H102.5 -

LinL3e Pins 416 st.st. 3115 o 79ol 4.o ske r plus bencling

%lve She f f ' A -56+ Mo 5375o. 486o. 11.l usaI plus ur oln3 Cr.nk HIoas .

Sboli Crank, 0;);ie Braate loco 338- 5". 9 P u thinp Pope A-4.

Rep. 2/se/10M Mountain Sortngs Parkway i Sox 22001 Spnngvme. Utah 84663 2200 USA / Phone 80148486111 Telex 3884L

T;.blo 1.

TIBORETICAL ACTUATOR 7080UE.00TPUT Torque (im-lbf)

Disk Position at 70 psi Spring Only Not (degree open) ,

(to open) (to olose) (to open) ,

0 69239 20443 48796 10 56672 18492 38180 20 51196 18081 33115 30 48723 18425 30298 40 47791 19212 28579 50 47664 20298 27366 60 47843 21514 26329 70 47896 22699 25197 80 47401 23595 23806 90 45928 23922 22006 O

G 9

e #

l Pose A 1 i

9

, ,-._-_.-,._.,.m., , , _ . _,.,,, - , , - . . , , , , _ . _ _ . . . _ . . - _ _ . . _,,,..___.-_,,__.__,_.,...-,_.,_.-_--e_ - _ - _ . , . , , , . , . . . , . _ . - . _ -

rD

~

i 70000  ;.....................F IGURE 1 70 psi TO.OPEN r' . .mmrmmWm mnTmun nrn- mivnmmrn-m1. . .

1 I

i 65000 -

-1 T

O . ~

I R -

O 60000 -

U -

E I. '

, i ~

o o n 55000 -

a .

. > - I -

t. co b - . .

1 -

50000 -

t t

o -

x - -

1 F

i

45000 -

- "a " " " " 2 " " " " a t * " " '" 2n " " * " 8 " " " " 8 " " " " 8 " u " " 2 " " " ' '

! O 10 20' 30 40 50 60 70 80 90

' DISK POSITION (degree)

( . -

-FIGURE 2 - SPRING TO CLOSE 24000 vmnmr nnnurmmmimrrmvim r ~ri.m amrmnymr m aminu mr t

23000 -

d T . d O .

R 22000 -

- 2 O -

U .

E  :

21000 -

o i .

.o n 0 u . .

?

a 20000 -

2 1

b

- 3 ,

19000 - '

2 18000 -----'m'"" "*"~''"""*"""'""=""'"""*"""""'"'"""

O 10 20 30 .

40 50 60 70 80 90 DISK POSITION (degree)

I l

FIGURE 3 - NET TO OPEN 50000 . . . . . . . . . . . . . . . . . .

  • r . . . . . . . . . n . . . . . . . v.-m . . . . . . m r Trrm . . . . . . . <rm v=> m m -

p .

45000 -

1 1 T -

O R 40000 -

5 Q .

U -

E '

35000 -

~

i m .

o n *

'st ~ '

30000 -

5

? I B b -

25000 -

V 20000 -- - -- '- - -

- '-- "' " " " ~ ~ ~ ~1 ~ ~ " 'n " " " 1 n- ' ~ ~ 1' " = ~ ~ " " "> " '

O 10 20 30 40 50 60 70 80 90

~ '-

~ '~~

DISK POSITION (degree) ' ~

g V A LT ROL. m ca ,rcio. r

-. ' TInsief % Sludy I A8e I Sheet No.

s Sueleet Rolost or Study No.

ny Cc.H one. Oef is igL Va lve. Ehen o2d ke,,s Tne va,lve sh<Al Is:ike sis-dsed , proven Va,I+rk. de:ign he s yaioc of 1k;s siae. sed preuure clce ss, tuert the<f dou kle b ep rahre t aa n en involute .splia Are w. red to transeni f the ecfge f>r bepe h the shc#. .The keyed Sha h and kev J wi ll b e or. 9.e d, The sh,9 *aJ keys are 6eth m 4 km A -n4 63o # loAs.

The. She # is f.7h inch diame. ter . The keys are Us inc h s,w.,, by 6 inch l ong . The Aeorines on the she N crea k 6 eg e the rlde 1onJ gener t#J 6 7 the oc fwe for to the valve shg6 is sdjetf 04/

7

. ti hen >aol .s h es e .

The valve she# is suQe t. to the 'interr.1 v lve icwed.ch

.f b-) dr3ce, F, hat the. ..f 6..cd e,J d the sh ft Gil not se t ik.t het .6ecause the dur.fi% of the 323 deecce fempu,+,cc

.Is Very Ah.et..The. inbrnei volve fampeca.kre exceeds n o d.3 m F for- only soo seuoJs. ASM E fac. E . T &le I-7.I r h m.t tk.t the ollewghle a trets Or m ter'el A -564 63 o ( H lt50 ,ll ll90, .se H 1075) is The sen.e e f raam ken.penAre la 1 00 desvor. F. Besed so f*nis infsemtion ik < ell ,a61e rfre.rs far the vulve she is 377s0 p s','

I1en slle) no J 22 W pri in :We , ,

b' =Tc . (7bri in Ad (l.75 in /1) .

61f6 psi J 2 (l.7tinl* -

u From ' S tress, Strain, . d 5trensth,' h y Tuvicell , the 3 frers eincea trafix he .% keyra shaft is I.le i for The heralened sha the st*%. .ead feb.e- stress -e xc ~ l ra k en fec hes *re a pprev6e tely efuelf t E 6976 vl. 6 r ll, llt p r/ s h e<. r TH r. th of c,llw. Ale stress to calculafed rfrefs is n= _22A75 . 2.0 (1,17# Pase kl\

n , , iou u ns.nn.ep y,e noo,s % n.a.ns.ms.moouu,m n.oi ueitit asue

g VAL.I t::K. memaina cowurmon ser rm.a % s 4 '

sw wo.  :. ro s i Sutgect Protect or Study Na_

by Date 19 Tr.e r s. b ew) tw . ihe .s kdt txe ae. didde ci1b

'hn e . on .he . ke f P a. fi f"4 d 45

.h e

. F, =. 3 151  ; o M :.. .?4cl . At ..

LWin /A . _.. ..

Tre s\ ac. ar e 1 .09 ' .he. kc,.s. is. % . ker Aa ta enaltiplied h,ihe A3: (~% in) (4 tg in): 4 5 in" ( N, k er)

T a e. 5 n e<, Stress is

~

te R= _P44 44  : I 86 ~1 ps; 73 4.5' :a * -

l ec tuness, u l ac. J .a he key, fe.dcy b cessh tne ke ,r i .< he -.

u ru e. s k e a. r. Ca < e . The c~ ness;o- ores ;s holf k xe, heigkr nsitiel:sc k

y be ic,,3 tk.

A : i(*4 ia) (6 + 6 , A = 2. >.5 it-

  • le n.<-,1 stress is c ,,_ F, , - 2 4 al M - 3 3 3 4 e s,'

A ,. 2.'ar,r'

%,=[Y+(TAI  :

ISO *tf"[**2s40pl c ,,, ,,, , , ; , v. "4 r A, = ( 3734 /1 ) .t A64o = 77 3  ; - 4ro'l p s,'

nu 5,, , lg ,,. 9 la 415 or 39"lio A (.4 0 4507 nu .__ *5 or 8. la f.he ft kef m ;n u Pase A il

.%nu,n sen :, n r .a.u e 2. ::z s: ,ng. . e u n p:.:. ::x es. any,: .u:am tre ns -

i t!_) VALTEK - ,,,,.oco - r - . or .

v ninor m4 stuoy sneet m 3 bi subsect

% or Study No.

w C6H o te Aua iT to_%

l.Ac4eabeusteEsjldep+<d, an dlfusCas!

. I I I

Il '

i  !  :

1 1  ! l l l I '

. I I i l l l l l f  ! l  !  !

i T' h e. ' o J 4Eb i N e k s ; cin Jl k_dde berI k,Wne' t t!

We I e$lInder- 'Esto.a._

l 6 S ', !I:nkdgei b3 6'm fs M d b I theal.ve Lou M J ,1% !s Ql I

t  !  ! l i l l  ! I I l l4 ! I i l l l  ! l  ! l l l l l l I I  ! l l l I '

I

,'sphn @ 2e '

i ,

I I '

5pr.ing Stem a

s ream.

s

.N

- -^

cua u.ua FineJ 5 h eke 5 top

. _ _ _ . - . . ._ y Lankag e_Ein . __ - _ _ . _ _ _

1.inka3c Foc a _ _ _ _ . .

Sktm_.Unp.tte _.- - .-

,s~ ~, .__

ir - ri

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APPENDIX A tts opemWilb, Pre Anal ysis Report 3+753/P 99 Brief Descripties of Operability Teste m purpose et the operability teste is to verify the valve seating and 4

dressie testes regstremente and te verify the setsator targes estyst. Yelve tergse regstremente and seteater tergse estyst will be mesessed by means of strata sages attached to the valvo shaft.

, Terges Rogstremente '

i Valve seating targes will be mesenrod with me flew thressh the valve.

i Valve toeges will be messered with water flowing thresch the valve. The l prosesse drop and corroepending dressie tartes will be recorded at valve disk positiene free is11 etened to is11 eyes in 10 degree incrosente, with the valve moving from etened to eyes posittener and free eyes to stooed j posittoa. '

l h proceense defined la the ISA paper 'Effect of F1ste Ceapressibility on ,

i Tergse La Betterfly Valves' will be seed to salesiste the valve tergse l' j regstrements with eempressible flew thressh the valve with preesses drepe of' j 0, 24.2, and 43.4 pe t.

i l Aetaster Terges t I

The setsster torque estyst w!!! be mesessed at disk posittees of 0,10, 20 30, 40 and 90 degrees opea. The tergse w!!! be mesessed by leeklag the valve shaf t at a set posities and sales 1 sting the toeges applied en the ,

, , shaf t by the setsator. It will be aseeeeary to perform this test at redseed

) setsster air prosesse to eveld damage to the valve shaf t (se esplataed i

earlier la this report. La sermal operaties the valve shaf t is esbjected .

esty to the toeges regstred to rotate the disk, not the is11 available '

j sensater tergse).

i j l

.Deta Presentaties l

I The reesite of the operability tests will be presented la tabster and graphie

{ feem la the f aael operability report. - -

l .

i i

d P

q-j .

Pa,e n a  ;

4 i

a .

~

. Appendix B to 0perability Analysis and Test Report 34753/2-48 Stress Calculations Based on 4403 in-lbf maxima torque.

h calculations shown in Appendix A are corrected here to show the stress resulting from the maximum seating torque of 4403 in-lbf which was verified by test.

h omiculation procedure is identical to that shown in Appendix A so only the omiculations will be shown here, with a reference to the corresponding page in Appendix A.

IMan 81 of G6

C VALTEK

~

.,,.oco ur 1 -

Tit 4 of Pnt Study Stwet No. b~1 Sobrect Protect or Study No.

/ -

by Date 19

%lve_ S%d4

. Tn,, : TJ= (44o3 ),, /w) (175 : /2) , 4184 psi

_. _3 . _ _

J._ ( l 7GM. ._ .

3 J. . .

tc . 4 f l 4.r. l.G = 6 6.9.4. .ps * . .

n= 2bN4'15 .s e e . pay A-\\

669.4 m.{3.4.f.

T _. . _ . _ . . . _ .

ShJ+ Ken .

. _ . . . s

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F s # 5 a l in - A r L A .~. 3 o 3 1 A s s .. - . ~ .

. - . - - . . .l .15.i n]2.

(' .._._..A5= 4 5 in'.. _ ._. _ _ .

-  %* E1 : S'0 1 Q ls1 . ...III 8 P si ..- . .. . .

A3 4,5 in * .._.. . .

A c. - 2.17 . ia

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r. r F , -sol 2su .

2236pg . .

. A. 5 2 2Sina 3

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' O VALTEK ritte of Proj. Study

. o co Ur 1,. m Sheet No " O ~3 Subpct Project of Study No.

by Date 19 Pis. A Ste n . _ .

F= Psy;,,, .t Fy;a., = .%M ' h t . . ._.

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de 3 B7 Fo ._ _3.'1 (_ _ .. .llows r . Yh ree elf d co d). ._see p4se A 14 122 9 . . . _ . . _ . . . . . . . .. ._ ..

A4 . g r enJ: ... S tr.in3 . Scc.. .i3 3 900.16f .

. Link. g . be . is IF20.Af O' 33.,6 Lint.se F.ne g'd ;, . ._ .

J* + .5,Je Is.d Fs: ID o cos 33.6*= 1266 Af

._ . _ _ . . . . _ . Compentanlad Fc : 3 900 + 0n o) s;,134' B ein F mea .. ._. __. . _ . . . . . . . .. 474l Af r81ill1 $sJil** $ . . .__ __ _ .. .. . . . . . _ . . . . .

l _ . . . . . - . . . . . - . . . . - . - . . . .

i EI3I'm I* rt e . . . . . __ _ . _. . .. . . .

Be n d;3 N e,d .f po',nt . M = (lau Ad(L) = 6330 in 4 f t: 3 12 6(o 164 . 438p>l A 3.99?

  • 6= 3c = (6330 in 46f) (lin) , 95'19 ps; r .us;+

%g e (C15'li /2 ) , 43N

+  :

4770 ps; e- y ,,,to : 9fl9/;t I +7flo = 95 W ,-2I p r,'

nr smaller of 32 477 or 3975b 4 7vo 95'4o n= 4. 'i or 4.l bd at lower <nd n e, L 2-see p.,e A 15 Pase. B-3 No 2/84/10M Mountain Springa Parkway I Don 22001 Springene Utah 8#A3 2200 USA I Phone 80148Hl6111 Tale: 308458

o U VALTEK Titleof Prof. Study

. c-m m E* 4 Sheet No-Subrect Pro;ect or Study No.

p. by Date 19 6Prinoi km . . . . . . _ . . _ . . . _ . . ..

f$ * . I b b . h$ . . _ . J.. . . - . . . . . . - . . - . _ - - . . . . _ , .. . . . . .

. ._.1% 2_(l>66 46d_fhG ) *_. I BM_.in A t__.. .- - . _ . _ _ _ . _ . . _ _ _ _

. _ ._ __ t.i Fs /A = 12 & 6 AL., 4o3 p si..._. . _ . . . . . . _ . ..

__-._ _.._ _. ....( 4 2F/4 ._ _.. ...... _... _ . . . _ . . _ _

.. .. 7m r.ki t99 in-AT) (l;n). .: 2 419 psi .. . . . . __

T

. _ . . . . . . . . . _ _ .(64 }_(1in Y

%y c[AAlR/2)# + 403 .. ". .l3 psi ..

%, . :. .. 3Al L/A.Z . I 2 7 L_=__. 2M3, ~ 65 pso - .-

. n:.. sm.ller d 22415 .r..__384o..__._.

(~ . . _ _ . . .

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3.4 8 3 .. .._ __ _. . . . ..

h= 17 6 o r. / 15. 6 '. See p 4 3 e A -14.

Siem Acha te r Ar 4. % '

F .- 23M M

<r = ) 3 s'86 A< , a.4 = 12441 ps; 4 f5 to n: F3 7to f 4.3 some as p 3e A I6 lA44l l 5 tem BA3%

A: 3.Plin' betria3 pren.<e 116616f. /.1 2 3 3.5 p s,'

N

2. g i ;,,
  • n 1000 , I S. 9 see pqe A - 17

>>5 P43e.3-4 Rep. 2/84110M Mountain $pnngs Parkway I Box 2200 i SonngvtHe. Utah 64663-2200 USA i Phone 80148Se611/ Telex 388458

c F )VALTEK v -. u- - 1 Titleof Prof. Study Sheet No. 13 '$

Submet Propet or Study No.

by Date 19

/ .. . . _ _ _ _ . . . . . . . . .

. . . . _ . _.._._~.__. . . . _ . .

C W4 Jr blah 3 . . . _ . _ _ . _ _ _ _ _ . ... .

. ._ . F. n e .a .4se...I;n ks. is is2a .si _.f> r. 44o3..jir u forg e . _ _ .

.._ Vwe e. .ee, Ital,is. . half._oLI D.o ,.a '16 0 .pbF .- . . .__. ..

. .___N . ?Y. = ' l'16O_.'esN SY. ._$. A3L4 fI_.$.

.. ._?

._ . ...' (L.3]F.. . 8751nlL70,n)... _ .._:......_... . _ .

. . . . _ _ _ _ . . _ . . . _. . .( 31.n...stren ..c.nce,, fra h). __ ..

h * {76 0.M ).( .35.+.. 'l5 in)..*... II40 'io hi

  • I..a _.. 053 ie9 .

.k$2_ . . le 7 _-...... . - . . .

~

_[...'.__ [r[e (Ilkb5Eh[](.5 io)(1,7) . /37/2 psi.

. . - _ . . . - _ . . _ - _ 0 53

(' .

. l _- ._. .. . . ..

G., y p. tr, .3. . A144_ rJ 70. .. _= _l60 7 6 psi n: T 3 150 .r1 3.3 } see pos e A-19 l6616 linkase Pini -

t = _760 Af . D 6 5 psi

.60 u ,,2 76= (76o m) (.3u in)(,875 in 4) = 4319pst

.oass u

%, =/(4n94)* + D65* ' .

= ).56-) psi r,n. ,, , ,, - 4 Ma 1 1547 = 471, -3 41 pr n=tm.ller .P (.sy M g #Mo) e r- II) fo

\ y rn Asn

. D5 l ' 1 O T* i Eff $4)f b*l Rep. 2/84110M Pne 5-5 Mountain Sonngs Parkway I Box 22001 Springville. Utah 84663-220 USA i Phone 80148Se611/ TeWx 368458

ENGINEERING COMPUTATION SHEET Title of Proj. Study S.wtNo. O~6 SuMoct Project or Study No.

,. by Date 19 Vale M Crsat . . . . .

. . ., .Jef. !p%3 C. .. ~1b . . _ . . . _ _ . . _.

, ,. 5

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.. . fg 2' . I be . . . ... _.].310__ .p s; . ._.._ __ . . _ . . . . ...

(2.ris ,y15)r,75)' -

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t =.(hIai)5

. ( 3, M -1..' I SX,7 d 3 C .T.43iAi . _ . . . ..

A = 44o3 in-Af -

22 o3. .in-4 t

_ . 3 . .. _ . . _ . . _ . . . .

. 6 = .() N 5 A+)(I. E 5 [ .I9J1 ps,-

I . v. n ,, + . _ . _

(

(

a+ t w ee.J . .r :. .g + q = 936

  • lan7 = 2 913 psi n= S S'1Co '

1-18 5J '

see pese A-1l 3913

%# Crank Bearings

_f If20 AL F , 203 psi A 1. To e' n: 5000  : *0 $ 9C. page A-2l 2n Pag e. - S - fo Rep. 2/84/10M Mountain Spnngs Parkway / Box 22001 Sonngville, Utah 84663 2200 USA / Pnone 8014894611/ Telex 388458

Appendix C to Operability Analysis and Test Report 34753/2-48 Operability Demonstration and Qualification

%e following infomation is given in response to Attachment I and 2, copies g of which are included in this Appendix.

Operability Qualification of purse and Vent Valves - Attehment 1 1A. Dynamic torque coefficient test results shown in Figure 1 and Table

1. h e test setup is shown in Figure l

1B. Operability Demonstration is by a combinat on of analysis and bench testing. See Demonstration, page C-2 of this report.

1C. Stress analysis of the valve and actuator, to show operability, is shown in Table 3 and Appendix B of this report.

1D. Seismic analysis and testing will be included in the valve Design Report which will be issued at a later date. Note that the environmental qualification test of the valve seat includes a static operability test which, while not intended specifically to riaernstrate operability or the valve, does demonstrate the integrity of the seat- disk seal under seismic loads. A dynamic test was performed to qualify the valve actuator and % trate operability during a seismic event. RI 1E. Refer to assembly drawings A34753-49 and A34752-48 for

1. Flow direction - nomal purge and accident
2. Disk closure direction is clockwise viewed from the actuator end of the valve shaft.
3. Curved side of disk is away from containment
5. he valve was originally intended to be installed with the shaft vertical, actuator up. Operability testing was perfomed with the valve oriented that way. See c e t A2 under Attachment 2. he R1 valves were later installed with the shaft horizontal, spring case up.

4,6. Orientation of pipe and other valves is not considered here per instructions from Bechtel Energy Corporation. ~

1F.  % e torque tests reported in this report demonstrate that the actuator pr~h m sufficient torque to operate the valve. See Figure 7.

2. Specific valve type questions are not applicable, per Bechtel Energy Corporation.
3. he torque coefficients were detemined by test. Piping did not simulate field installation. However, the ratio of actuator torque to required torque is sufficient to overcome twice the dynamic torque even in the event that piping effects cause the dynamic torque to reverse direction.

l PageCt of C9

4. In-situ tests are not applicable.
5. Not applicable per Bechtel Energy Corporation.

Page C7. of C9

\

Guidelines for Demonstration of Operability of purge and Vent Va'lves -

Attachment 2 l

Operability l

%e operability tests showed that the valve actuator torque capability is at l least two times the required torque to overcome valve friction. Se worst case valve torque requirements is with the valve closed. See Discussion of Dynamic Torque Tests page 7.

1. Valve closure rate is asstamed to be linear. However, no credit for pressure buildup to assist valve closure is taken so the closure rate is not important to the operability analysis.
2. In accidental conditions, flow is toward the shaft side of the disk and tends to close the valve. However, no credit is taken for this dynamic torque when calculating the worst case torque requirements.

3,4,5,6. Not applicable per Bechtel Energy Corporation.

7. See <wn-nt 3 to Atteh-nt I above.
8. Not applicable here.

Demonstration Operability has been demonstrated by a combination of analysis and bench testing as reported in this report.

'lhe stress analysis contained in this report shows that the components critical to operability have a stress margin of at least 2 to 1. Seisedc loading has negligible effect on the components analyzed in this report in Appendix B. See also cam-nt ID on page C-1.

Sealing integrity of the valve seat-disk is ensured by the environmental qualification test performed on the valve seat. H is test includes thermal

, aging, mechanical aging, irradiation, and LOCA simulation with chemical spray. %e environmental qualification test is being perforsned on a valve of identical size and construction as the production valves. %e results of this test will be reported later.

Bench Testing A1. All tests reported in this operability repart have been perforined on a production valve or on a valve of identi::ai size and construction as the production valves.

pcge C3 of Cq

w - .

A2. With the exception of the actuator torque output test and seating torque test, all tests were conducted with the valve oriented with shaft vertical, actuator up. h valves were later installed with shaft g horizontal, spring case up. Piping during the testa did not simulate field installation. See comment 3 on page C-1.

A3. he following factors 'have been included in the operability tests and -

analysis.

a) IACA similation (internal components only) b) Seismic l<=dina will be considered in the valve Design Report as stated in Cr== ant ID on page C-1.

c) Temperatum soak d) Radiation exposure (internal components only)

Chemical exposure (as part of the I4CA similation) e)

f) Debris could affect operability in two ways. First, in a gross sense, large objects left in the pipe line could prevent the disk from closing. Obviously, construction tools and materials, etc.,

cannot be left in the pipe line. Second, small debris such as pipe scale or weld slag left in the pipe line could <iamare the disk and/or seat or become lodged between the disk and seat, which would affect the ability of the valve to shut off tightly. Pipe scale did cause a sealing problem during the IDCA simulation of the i

environmental qualification test of the seat (as will be reported in the Qualification Test Report to be issued at a later date).

he pipe scale in the test came from the boiler and ILCA chamber used to perfom the IDCA simulation. During the IDCA simulation the valve outlet consisted of a 1/2-inch pipe. h e velocity of steam through the valve was very low and allowed the pipe scale to e-late in the bottom of the valve. In the field, the valve will be installed in a galvanized pipe system which will prevent the fomation of pipe scale . The pipeline must be properly cleaned before the valve is installed.

In-situ testing is not applicable.

l l-l t

1 f

i Page C4 of C1 l

l l

.... .. t 4 Attachment 1

,. ,, Operability Qualification of .

Purge and Vent Valves Demonstratton of operability of the contalment purge and vent valves and the ability of these valves to close during a design basis accident is necessary to assure containment isolation. This demonstration of operability is required by NURErr 0737, " Clarification of TMI Action Plan Requirements,' II.E.4.2 for containment purge and vent valves which are not sealed closed during operational conditions 1, 2, 2 and 4

1. For each purge and vent valve covered in the scope of this review, the following documentation denonstrating compliance with the

" Guidelines for Demonstration of O Valves" (attached. Attachment #5) is perability of Purge and to be submitted Vent for staff review: ,

i A. Dynamic Torque Coefficient Test Reports (Butterfly valves only) - including a description of the test setup. 2,

8. Operability Demonstration or In-situ Test Reports (when used)

C. Stress Reports D. Seismic Reports for Valve Assembly 1

(valve and operator) and associated parts.

( E. Sketch or description of each valve installation showing the following (Butterfly valves caly):

1. direction of flow -

/

2. disc closure direction
3. curved side of disc, upstream or downstream (asynetric discs) 4 orientation and distance of elbows, tees, bends, etc.

within 20 pipe diameters of valve

5. shaft orientation l

l 6. distance between valves F. Demonstration that the samtmum combined torque developed by the valve is below the actuator rating.  !

4

2. The applicant should respond to the ' specific Valve Type Questions" -

l (attached) which relate to his valve. ,

l

~

  • .. l PAE ? iO? ~C9 -

i

3.

Analysis if used, should be supported by tests which establish torque

. coefficients of the valve at various angles. As torque coefficients closure flow direction and approach flow, these things should accurately represented during tests.

Specifically, piping installation (upstream and downstreans of the valve) during the test should be repre s sentative of actual field installations. For example non synetric approach flow from an elbow upstream of a valve can re,sult in fluid dynamic torques of double the magnitude of those found for a valve with straight piping upstream and downstream. l

4. In-situ tests, when performed

~ performed on a valve of each si a representative valve, should be represent the' worst case load. e/ type which is determined to should be considered. orst' case flow direction, for exar.ple, For two valves in series where the second valve is a butterfly valve, the effect of non.symetric flow from the first valve should be considered if the valves are within 15 pipe diameters of each other.

5.

If tue applicant takes credit for closure time vs. the buildup of contain-ment respect pressure, he must to the actual demonstrate valve closure rate. that the method is conservative with to be determined under both loaded and unloaded conditions and periodic

(. inspection under tech. spec. requirements should be performed to assure closure rate does not increase with time or use. '

O e

PAGE _ 0F "

. . ~

Specific Valve Type Ovestions '

The following questions apply to specific valve types only 'and need to be answered only.where applicable. If not applicable, state so.

N.'

k. Torque Due To Containment sackpressure tffect -

(TC8)

For those air operated valves located inside containment. is the operator design of a type that can be affected by the containnent

  • pressure rise (backpressure effect) 1.e. where the containment

,' pressure acts to reduce the operator torque capability due to

- TCS. Discuss the operator design with respect to the air vent and bleeds. Show how TCS was calculated (if applicable). N B. Where air operated valve assemblies use accumulators as 15[fa11-safe -

feature, describe the accumulator air system configuration itnd its oper-

stfon. Discuss and the basis us, active electrical.cosponents in the accumulator system, ed to determine their qualification for the environmental conditions experienced. Is this system seismically designed? How is the allowable leakage from the accusulators determined and monitored.

. C. For valve main seal)(. describe the air pressurfzation system configuration

,( ' operation including means used to determine that valve closure sh,d seal i

' pressurization have taken place. Discuss active electrical cosponents in

.this system, and the basis used to determine their qualification for the i~.

i environmental condition esperienced. Is this system seismically designed?

D. Where electric actor operators are used to close the valve has the minimum available voltage to the electric operator under both  !

normal or emergency modes been determined and specified to the.,

eperator annufacturer to assure the adequacy of the operator to stroke the valve at accident conditions with these lower limit voltages available? Does this reduced voltage operation result in ary significant change in stroke tfeing? Describe the emergency mode power source used. '

E. Where eiectric motor and air operator unf ts are envfpped with

  • hanetheels, does thifr design provide'for automatic re-engagement eif the motor operator following the banerheel mode of operation?

If not.'what steps are taken to preclude the possibility of the

. valve bef ag left in the banetheel mode following some asintenance.

. test etc. type operatten?

  • F. For electric motor operated valves have the torques deve'1oped  !

durin operation been found to be less than the t,orque Itait ng settings? '

/ 1

, fh3E QF_

fR l -

  • e - -

i,,,.

Attachment 2

  • . ~
  • l l

i e t SU1DELINES FOR DEMONSTRATION

'0F OPERA 81LITY OF PURGE AND  :

VENT VALVES '

i-

, OPERABILITY In order to establish operability it must be shown that the valve' actuator's forces (i.e., fluid dynamic, bearingtorque seating, frictioncapability has sufficient ma when in the stroking time limitfrom the initial open p,osition to full sea)ted (bubble tithat resist specified. )

established in the containment following a design basis LOCA.This shou which,should be addressed in assuring valve design adequacy include: Considerations

'1. Valve closure rate versus time - i.e.

2. Flow direction through valve; AP acros,sconstant valve. rate or other. ,
3. Single valve closure '

4.

or simultaneous closur(e.inside Esta'blish worstcontainment case. or outside containmen Containment back pressure effect on closing torque margins of air operated 5.

valve which vent pilot air inside containment.

' r' Adequacy of accumulator (when used) sizing and initial charg closure requirements.

5. For valve operators usin the devices compatible w th the tortorque Ilmiting devices - are the settingsfof during the design basis condition. ques required to operate the va.ve g/A

! 7. '

~

The effect of the piping system (turns, branches) upstream and downstream *

8. of all valve installations.

i The effect of butterfly valve disc and shaft orientation to the fluid

  • siature egressing from the containment.

t ,

i .

. DEMONSTRATION '

Demonstration'of the~various aspects of operability of purge and went valves may means. be by analysis, bench testing, insitu testing or a combination of these Purge and vent valve structural elements (valve /setuator assembly) must be evaluated to have sufficient stress margins to withstand loads taposed while valve closes during a design basis accident.

i tension and compression loads / stresses should be considered. Seismic loading Torsional shear >

should be addressed. '

- t Once valve closure and structural integrity are assured by analysis, testing, or a suitable closure and 1 combination, a determination of the sealing integrit.y efter Cvaluated. term exposure to the containment environment should be the containment spray chemical solutions on seal material. asis should i '

Other aspects such he considered.as the effect en sealing from outside ambient temperatures and debris PAGE C8 0F G i

- . - - - - . - - --.-----_-._---.__----___-________1____-_.___---__

=

~. y x

. Thefollowingconsiderationsapplywhentestingischosenaiasilans'for demonstrating valve operability:

Bench Testino -- -

A. Bench testing can be used to demonstrate suitability of the in-selvice valve by reason of its traceability in design to a test valve.

factors should be considered when qualifying valves through bench Thefollow testing. ing

1. Whether a valve was qualified by testin ofanideNtichjheassembly
orbyextrapolationofdatafromasimiarlydesign4dvafy .
2. Whether measures were taken to assure that piping upstream'aWd down-stream and valve orientation are simulated.
3. Whether the following load and environmental factors were considered '
a. Simulation of LOCA
b. Seismic loading
c. Temperature soak  !
d. Radiation exposure  !
e. Chemical exposure  !

W. Debris S. Bench testing of installed valves to demonstrate the suitabIlifff' f the specific valve to perform its required function during the posturated design basis accident is acceptable.

1. The factors listed in items A.2 and A.3 should be considered when taking this approach.

In-Situ Testino la-site testing of purge and went valves may be performed to confir e suitability of the valve under actual conditions. When perf tests.

the conditions (loading, environment) to which will' the stijected valve (s) pra l during the test should staulate the design basis accident.

i ..

l 80TE: Posttestvalveexaminationshouldbeperformedtoifiab1Hh'Iductural

lategrity of the key valve / actuator components..
"-

\ .

l i

PAGE C9 0F C9

. - . _ , _ _ _ - - . , . - . _ . _ _ . ._ ._..-_,______..___ _, _ -_,. ..._..~ ,,,_, ._ . _ , , . . _ _ _ . - _ , . . _ - - - , - . . , _ , , , , - _ . - , _ - _ -

. ._ _ _ _ . . . . _ _ _ _. . _____._._.m._ _...._.____.m _. _

I D i e

CisTitieUTION T3: FOR. CEVIE3 INp3

  • MECH ANICAL

' e EAL ANCE OF PLANY e SOILE R/NSSS PLANY UTILef sE S d e PL ANT DESIGN e CONTROL SYSTEMS e ELECTRICAL  !

WIRING CONOutT e MQS e PAINTING & COATINGS

  • CivlL/STRUCTU RA L e NUCLE AM e STRE SS e ARCHITECTURAL eSTARTUP e CONST RUCTION j e NOT REQ'O SV ENGRG e CLIENT IDENTIFYlNG TITLE OF THis OOCURSENT CR -33\ Slo-) CDt1 Ab TEniT M M OLM hAC.Tb4D L 1

HOUSTON OFFICE ISSUED hh mbt INFORMATION ONLY /88d9 STP 14926 L

I I4 M -4409-oozzo Sochtel Log No.

yr

. 14q21 - gyce- oozn- r LMPORTANT au s.wte ovat 4.

r.: .te3 .#...g =ra m Syre'::n.:::t:'.

rars.ne stelegese .

tvEO 4M'37 W ENT STATUS  % -

1 WORK M AY PROCE E D. gg 2 REvaSE AND RESuSMIT 4

i WORK M AY PROCEED SUSJEC T TO INCORPO g"ECHTE L R Af TON OF CH ANCES INosC ATE D. ENERGY j

' 30 aE vise ANo aE Sv.MIT Cone.

WORK M AY NOT PROCE E D 40 aEv'EW NoT atov'aEo WORK M AY PROCEE D D o'STaisuT.OM atO o MOS4012(Mel

t. 1