ML20099L442

Submits Addl Info Re Operability of Containment Vent & Purge Valves Under DBA Conditions in Response to 841009 Request.Structural Integrity of Actuator Mounting Hardware Verified

ML20099L442
Person / Time
Site:	FitzPatrick
Issue date:	11/26/1984
From:	Corbin McNeil POWER AUTHORITY OF THE STATE OF NEW YORK (NEW YORK
To:	Vassallo D Office of Nuclear Reactor Regulation
References
JPN-84-74, NUDOCS 8412010130
Download: ML20099L442 (26)

Text

~ _ -.

123 Main Street o

V&te Plauw, N w bk 10001

-D D14 681.6200

1. > NewYorkPbwer 4# Authority November 26, 1984 JPN-84-74 Director of Nuclear Reactor Regulation U.S. Nuclear Regulatory Commission Washington, D.C.

20555 Attention:

Mr. Domenic B. Vassallo, Chief Operating Reactors Branch No. 2 Division of Licensing

Subject:

James A. FitzPatrick Nuclear Power Plant Docket No. 50-333 Containment Vent and Purge Valves Operability

References:

1.

NRC letter, D.

B. Vassallo to J. P. Bayne, dated January 13, 1984, " Containment Vent Valve Operability."

l 2.

NYPA letter, J. ?.

Bayne to D.

B. Vassallo (NRC), dated February 24, 19 84 (JPN-84-14 ),

{

" Containment Vent and Purge Valve Operability."

l 3.

NYPA letter, J. P. BR.yne to D.

B. Vassallo (NRC), dated June 14, 1984 (JPN-84-35),

" Containment Vent and Furge Valve Operability."

4.

NRC letter, D. G. Eisenhut to J. P. Bayne, dated October 9, 1984, " Containment Purge / Vent Valve Operability."

Dear Sir:

l In response to your letter dated January 13, 1984 (Reference 1), the Authority provided information regarding the operability of containment vent and purge valves under design basis accident (DBA) conditions via References 2 and 3.

By letter dated October 9, 1984 (Reference 4), the NRC requested additional information to complete its review for the FitzPatrick vent and purge valves.

DR 3

o

In response to Reference 4, the Authority has performed detailed calculations which der.onstrates i: hat these valves and actuators are operable under DBA conditioras, taking into account the effect of increas<sd dynamic loads resulting from upstream elbows or other fittings.

Structural integrity of the actuator mounting hardware has been verified.

As shown in the curve in Attachment I the increase in dynamic torque due to elbows or other fittings has been offset by reductions in maximum opening angle of the valve, and reduced, recalculated differential pressure loads due to a DBA.

Therefore, the loads to which the mounting hardware is subjected to are no larger than the original design loads of the hardware.

From the tables and graphs shown in Attachment I, it can be seen that with the maximum angle of opening for three 24" valves (27 AOV-111, 27 A0V-112 and 27 A0V-113) restricted to 40* instead of the present limit of 50',

the valve and the actuator would be capable of performing its design function and maintaining its structural integrity under DBA conditions.

For the 24" valve (27 A0V-114) and the 20" valves (27 AoV-115 and 27 AOV-ll6), with the maximum opening angle maintained at the present limit of 50*, the valve and the actuator would be capable of performing its design function and maintaining its structural integrity under DBA conditions.

These results are based on calculations taking into account the increase in the dynamic torque coefficient by a factor of three for the three 24" valves (27 A0V-111, 27 AOV-ll2 and 27 AOV-113) and the two 20" valves (27 A0V-ll5 and 27 AOV-ll6), due to an upstream fitting 90' out of plane with the shaft of the valve.

For the 24" valve (27 AOV-Il4) a factor of 1.5 has been used for the dynamic torque coefficient sinct, the fitting upstream of this valve is in-plane with the valve shaft.

Valves 27 AOV-117 and 27 A0V-ll8 are located 11.5 and 13 diameters (respectively) downstream of a fitting and their operability is not affected by the fitting's presence.

The explanation for tne constants used in the Fisher equations are as shown in Attachment I.

The seismic qualification requirements for these valves are contained in Purchase Specification APO-70 which was provided to Fisher Control Company.

The Aulnority is reviewing the available information on these valves for documentation that assures that the valves were manufactured in accordance with APO-70.

4

• If you h' ave any questions please, please contact' Mr. J. A. Gray, Jr. of my staff.

Very truly yours,

/

N C. A. McNeill, Jr.

Senior Vice President Nuclear Generation

~

State of New York County of Westchester Subscribed and Sworn to before me this 36 day of,0cteneer 1984.

JFAllNF l A LUNA ICT4.CY F:14LIC, STATE OF NEW YORK NC. 604614305 CUAL!FIED IN WESTCHESTERf00NTY hl gg 7 na !#1RES MARCH 30th 19K4....

Notary'Public cc:

Office of the' Resident Inspector U.S. Nuclear Regulatory Commission P.O. Box 136 Lycoming, New York 13093 Enclosure iD

n t,

i r

7

~ ATTACHMENT I JPN-84-74

' CONTAINMENT VENT AND, PURGE VALVE OPERABILITY t

+

3 -

r NEW YORK POWER AUTHORITY I' -

+..

.. JAMES A.

FITZPATRICK NUCLEAR POWER

• PLANT E

' DOCKET NO.;50-333 I.

t i

[

' TABLE #1 i

Loadin capacity for 24 inch valves tag number 27 AOV-111, g

.27'AOV-112 and 27 AOV-113, shaft laying 90 out of plane, dynamic torque multiplication factor = 3.

e s

- c(

• O

-10 20 30 40 0

0 0

Spring torque actuator :

25700'

-18420 14500' 12260 10990 in - ib p

Shaft torque ruinahility -

14159 17688 14026 9370 5005 in - lb t

W developed by DER /ECA 3534 6344 9353 7489 1531 in - lb i

4 Shaft AP mpability (PSI) 145 101 46 27 9.20 Shaft AP deplewwi by Din d (PSI) 32.45 30.41 26.76 19.23 1.n

'E

6 y '

)

(

-, TABLE #2' l

Loading capacity for 24 inch valve tag number 27 AOV-114,

--i shaft laying'in;the' plane'.of the upstream elbow, dynamic itorque multiplication factor = 1.5 0

g*

0 (0 -

10 l

20 30 -

40 50

+

12260 10990 10370 Spring torque 25700 18420-14500 actuator.

tin - lb Shaft torque capability 14159-17688-14026 9370 5005 4232 in

.lb Torque developed by D3A/IOCA 3534-4869-6454 5754 4583 2734 in - lb.

Shaft A P capability (PSI) 145 128.80 72.65 45.44 19.92 8.50

' Shaft AP developed by 32.45 30.66 28.39-24.30 17.45'

-1.99 DaT/IDCA --(PSI).

a t

4 l

l V

l

.o.

~

., =.

TABLE #3 Loading capacity-for 20 inch valve tag number 27 A0V-ll5-and 27 AOV-ll6 shaft laying 60 out of the pla: e of the upstream elbow, dynamic torque multiplication actor = 3.

.j N

0.

10 20 30 40 50 Spring torque 10060 9187 8313 8149 8166 874'O actuator in - lb 8

[*

8401 10419 8941 5928 3165 3381 in - lb D*

P*d 1078 1929 2799 2104 1084 455 by naA/ Inca in - lb 147 103 52.16 30.80 11.22 4.84 capabi ity (PSI)

Shaft a P oped by 13.05 11.50 8.63 5.94 2.55 0.15 naVIOCA (PSI) 7

(,

t-L__

D b

wu v4t.,ie Tu e 2 7 u+ ni, '7 ed %97 ^^-"3 l t

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se

@,),- l n.is) g qrpw. 70go.uc (MuTd l

@) 5pFrPEGE cerP6'IdT[

no*-

@Twaux wstoyer> bpeas in 3*oso o

k b

hh

~~ N

@) 6ttu:r LP peystcPep?>\\)PBA bcA

.138-.

8 8"#-

12s.

24<vt.

,' 18 0.

12000 i

/JQ..

DR f

Sa. / Boat gg.

Il;000 I

7o..

1403r i.

tro..

ILU0s..

o so..

I4000 d o..

8***

Jo.,

(.,000 10__

4,00*..

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O 0

. g Oo 2 0 30 40

&L m g Le.

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1 T M4 F'ct J " T' g, o Id y?

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EVM FIGURE # A 1

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A TDPs A Ev E tJT FIGURE # 2

'fois v At,v c T g A 2 7 Aov'-li9 Mb 17 A W -li I ~ ~

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FIGURE ft 3

N d

C 915 HANDBOOg CFG 408-10 p*

pigg' PAGEI v'ANUARY 1973 CONTINENTAL DIVISION 1

i GFV TORQUE DETERMINATION I

~

Objective it should be noted at this point that the sum of a number of torqugeompo.

1 _

before valve torque is determined, the nents. To avoid confusion, a humber I

l i

h-determining factor in accu.

user shou!d consult CFG 200-20 to of these have be,en combined and a rately selecting the most economical ensure that the pressure drop mi-number of calculations have been i

._ actuator for a butterfly valve is the tations are not exceeded for the specific -performed in ' advance. Thus, each

^

' torque required to open and close the valve construction in consideration.

valve type can be represented with the valve.- The following is a quick and same simple, practical formula shown easy method of determining actuator below. The various torque components torque required in both the open and Introduction and the process of simplification are the closed position of a butterfly explained fully in the appendix (See Butterfly valve torque is actua!!y Page 23).

valve. _

whichever )

where: A, B, C = Tabulated coef ficients I

/r JPacto 3p

,e. = Actual pressure drop lj ac TOTAL TORQUE (IN-LBS) = A (aPacto ) + B + C or is at angle a* '

APerfo* smaller )

AP rro' = Ef fective pressure drop i

e at angle u*

Procedure

4. Select values for A,8 and C again, Refer to CFG 40F.20 for Fisher this time according to the character-cctuator selection.

I

1. From the above table, determir.e istics of the value at the desired maxi-

[

the effective pressure drop, JPett o *,

mum open angle fo"). Write the at the desired maximum angte of equate,n shce.n us:nq the nt.y values T ht-eMer.t we p ev.ec if trip term.

opening.

and perform the simple calcul.4tsors

,. p,,t o '. "505 'I b* ta the Hr.w con j

requaed. This determines the requirtvl 1.t uri, rt.ar the disc it 6 o ralco:..ted

2. Turn to the tatHe for the valve actuator torque (valve torque requirer 1' value and vwill usually vary f rom the'4-type, class and disc type in consider-at the desired ang!e of openin9 actuJI p ressure drop. It may tJe ation.

rtr",crite":d as the pre.ssare drop secn by

5. An actuator may now t,e selcc:cri the o.sc in the region of flow which

3. From the table, choose values for with either:

affects only the "C" multipher in the A, B and C according to the chwacter-inr,:u.? formula. Note that, due to its l:

al nt tmue output grue.:

noture, that (.f f t:ctive pressure drop is 2

istics of the valve in the closed posi-than the larger of the toret+s g,

}

ion (O'). Write the equation shown i

using the selected values and perfrarm tennM in 3 and j

,,,,,,, g,n,@,,,m,,,,,,

the simple calculation required. Th.s bl A var ying torque reutput w% t, eg e., tne..._ty;s u p m ye; jtem determenes 1 he required octuator equah r,r enet ris both of tht fe're

._,P,,,,,,

a torque to move the valvt: disc dway

• iintti

• ne rpits,et tLeer r e sg u e. t n

~

U f rom its seat.

v elvi. gjut trn u n h

54 EFFECTIVE l'N MURE DROP k-t Nu t t' e,

umt.m n giee v.

e

. t

• e o.r e + ce+ f e 'd ol *r*9 r' 8 TABLET T,pe of Type of

_Arve of D.w Wenum 80~90" Osse F luid O*

l 10*

20 30" do" 50" 60*-

l 70' Conventionat Liqu 1 JPact O' O$70P, 0 7 tDPi 0 So0P, O NPOP,

OSAOP, n 4 SOP s's3' & i 0350P i

os C t' set Gas JP,c, g" JPac t 10" 0Wi 02SOPi

0250P, O200P,

02QOP, 0140P 0.14DP, 0.450P 0 500Pi 0 700P, 0 700P 0 670P, 0 600Pi L,qu,,3 JP,, n'-

0 700P o 700Pi i

i 0180P 0ttuP 0 090>,

6 JPact O '

O2GuPg 0350Pg 0 350P, 0 3 SOP O250Pi s

J

>..v-

~

CFG 40B-10 PAGE-23 APPENDIX JANUARY 1973 i.

There are actually five torque components which add to ficient of friction (friction torque factor), the shaft size produce the total torque in a butterfly valve. These are:

(shaft d:ameter ratio based on Type 7600 Class 2 shaft) friction torque (on shaf t), packing torque (on shaf t),

and the actual pressure drop. Dynamic torqueis a function unbalance torque (on offset discs), seating torque (on tight of the valve size and disc opening (dynamic torque factor) shutoff discs) and dynamic torque (on all discs).

and the actual or effective pressure drop whichever is,

smaller. From these factors the following equations are Derivation of Formulas derie:d:

The general formula for butterfly valve torque is:

~

T = Tg + Tp + Tu + Ts + Td t

Tg = (FTF) (SDR) (oP,cio*) -

where:

whichever)

[AP,cro e Tg = Total torque Td = (DTF) or as Tg = Friction torque (AP,rgo*

smaller )

Tp = Packing torque Tu = Unbalance torque where:

Ts - Seating torque Td = Dynamic torque FTF = Friction Torque Factor SDR = Shaft Diameter Ratio AP, ego * = Actual Pressure Drop at Angle a*

Both friction torque and dynamic torque must be calcu-DTF = Dynamic Torque Factor lated. Friction torque is a function of the bashing coef-

• AP,,,o' = Effective Pressure Drop at Angte a' The general equation can now be written:

[dP,ero* whichever)

T= (FTF)(SDR)(aP,cio ) + T + T + Ts + (DTF) or is t

p u

( AP,,, o*

smaller )

)

where:

(FTF) (SDR) = A DTF = C and for Types 7500. 7600*. 7700 and 7800 Types 9100 and 9500 Tp = B; Tu = Ts = 0

+ Ts = B; Tu*O Tj pes 8200 and 8300 Type 9200 Tp + Tu = B; Ts = 0 Tp+Tu + Ts = B l

thus, in each case f AP,c,o whicheveri c

TOTAL TORQUE (IN LBS) = A (aP, cia l + B

• C or is a

AP,,, o*

smaller

• NOTE - The elastomer i;ned Type 7600 is ignored at this point since it is a special case and is treated as such in the tables.

Werait to be included here. it would be simpt:fM in the same manner as the Type 9100 and 9500 since,1 has a seating torque component at closed angies.

Additior'al Comments Note that the tables give values for "B" at both O* and A value of zero is given for "C" fo all'aise tG ' at O v

open angles when seating torque is present. This is due to since dynamic torque is present only at angies of 10' or the fact that seating torque applies only when the disc is more.

near the seat.

.4.-Q

' ;') t 9200 & 9280 BUTTERFLY VALVE TORQUE DETERMINATZON

==

Introduction:==

Use the following procedure and tables to determine actuator torque required for 4-inch through 72-inch 9200 and 9280 series valves.

Warning: This procedure does not consider mechanically adjustable, non-l l-inflatable Type _9200 with TFE. seat 0*, see Table 33.

Q l

s 3m-Butterfly valve torque is actually the sum of a number of torque _

components.

To avoid confusion, a number of these have been com-t l'

bined and a number of calculations have been performed in _ advance.

Thus, the following formulas are used in torque determination.

The various torque components and the process of simplification are explained fully in the appendix.

Neccesary Equations:

[g Torque @ 0* (in-lbs) = AaPshutoff + B + B1 + B, a?shutoft Where A, B, B, B ' = tabulated coefficients 2-APshutoff = shutoff pressure drop f'

For inflatable seal, B &B2 = 0.

1 Torque @ o*-(in-lbs) = AAPACT-o* + B + CAPDYN-o*

3 Where A,~B,~C = Tabulated coefficients APACT-o. = Ac ua pressure drop at angle a*

APDYN-o* = Dynamic pressure drop at angle ao

/

Procedure:

1.

Determine shaft class.

Using Table 1, determine the shaf t class by valre size and shaft diameter.

W12J1

/

W p.

sQ ' ~~ _

,.y 4

• .es n w nou.o ses,. w e e.

.s -...

m "L U 5e;tet St Bushint % t'll H (Select Scaling Type or Anele)

-.JI Graphite

>#ne.

_ M ius table t) 0*

In fla t aLie to O'

,.sy

Stae L a r.ad Titled Bronz2 Alloy-B Otner "Elastcmers" viton (Select OnN 90.'-

10

~ !a.

Brente 6

8 8-3 y.

'O.299 0.800 1.00 1.60

$2.2 79 1.6 212.2 372.2 52.2

'5 0.357 1.25'

-1.56 2.50 54.0 138 1.9 254 454 54.0 6

0.503 1.75 2.19 3.50

$(. 8 197 2.2 294.8 534.8 54.8*

8 1.07 3.75 4.67 7.50 76.0 313 2.5 396 716 76.0 IG 2.24 7.85 9.81 15.7 116 469-3.2 516 916 116

- 12 3.29 11.5 14.4 23.0 123 665 4.1 603 1,083 123 14 5.14 18.0 22.5 36.0 185 889 5.0

• 715 1,245 185 la 6.71-~

23.5 29.4 47.0 198'

~ 1,212 6.6 808 1,418 198 15 10.3 36.0 45.0 72.0 260 1,603 8.1 940'

'1,620 260 N-12.6' 44.0 55.0 88.0 316 2,188 11.3 1,076 1,836 316 24 21.4 75.5 34 2 151 471 3.634

-24.1 1,*391

'2.311~

471

~

l ??'

18.7 136 169' 271-782 5,860 62.3 1,942 3.102 782-36 54.9 192 240 384 995 8.110 101.3 2,395 3,795 995 52 94.3 330 413 660 2,040 10,360 140.3

[

3,680 5.320 2,040

~

1S' 154 434 543 A68 2, 00 12,610 179.3 4,080 5.960 1.200

{

34 189 662 828 1,320 2,420 14,860 21b.3 4,540 6,660 2.420 64 234 820 1.020 1,840 4,520 17.110 25 7.3 6,880 9,240 4,520

_f6 332 1.160 1,450 2,320 5,760 19,360 296.3 8,360 10,960 5,760

~

lM.

396 1.390 1,730 2.770 6.860 21,610 335.3 9,700 12,540 6,860 f 84 619 2,170 2,710 4.330 9,150 26,110 413.3

<12,470 15,790 9,150

~

l 94 911 3.190 3,990 6380 11,400 30,610 491.3 15,200 19,000 11.400 c* ST. lisad SST or TTE lined f aber814ss.

W M

TA3:J. 4 TYPE 9200 A/S LW'.*E COETT*C: ins - CL*ds 3-4.setee: ene iusnine :at t i 3

• select s e a. :.: 4 T-_ce sr Aneles

,i::t 277.

Grapntte hone.

4 :! u s t a::.e e

• Mitatante s 0*

'St:e Lased Titled Bronze Alloy (Setect ones

0**

bronze.

6 B

B; 3,

.:4ser 'Elastseers*

Vttas 90*

0.27.4 0.960 1.20 1.92 67.2 79 1.6 227.2 337.2 67.2 5

0.429 1.50 1.88 3.00 63.0 13S 1.9

'69 469 69.0 1

0.600 2.10 2.63 4.00 61.8 197 2.2 309.8 549.8 69.8 5

1.43 4.99 6.23 9.98 111 313 2.5.

431.

751

.111

!23 2.80 9.81

• 12.3 19.6 156 469 3.2 556 956 156 I ?!

a 11 14.;

19 0 23 4 163 465 41 643%

1,123 163 1

6.17 21.6 27.0 43.2 229 389 5.0 759 1,289 229 16 S.06 28.2 35.3 56.4 242 1,212 6.6 852 1,462 242

?? O f.2 1

.7 Ra.2 308 1 603 9.1

• • 1 1,f64 303 k;!

14.7 51.5 64.4 103 304 2,183 11.3 1.124 1.S84 364 24.6 66.1 105

!?:

521 3.634 24.1 1.;41 2,261 5:1

t a 169

• 1 339 06

• .!60 62.3 2.056 3.216 a*6 23 63.6 240 303 480 1.110 8,110 101.3 2.510 3.910 1.110

-2

!!3 -

396 415 792 2.1( 0 10,360 140.3 3.!:0 5.440 2.160 F-t 144 5:t 651 1,040 2,3*3 12.(10 t*9 3 4.200 6.080 2.120 M

221 775 969 1.550 3,500 14,S60 218.3 5,680 7,800 3.560 274 959 1.200 1,920 4.640 17,110 257.3 7.020 9,330 4.660

{

UA 1,3 0 1,660 2,650 5.90 19.360 Ois 3 9.4C0 11,100 5 aco t*

7 451-1,580 1,970 3,140 7,000 21.610 335.3 9,8:0 12,680 7.000.

L.

~.699 2.450 3,040 4,310 9.310

~ 26.110 413.3 12,630 15.950 9.310 3

t,033 3.610 4.510 7,210 11 f00 30.610 411.3 14.800 18.600 11,600

.g r--

.--r--,

y

.a

, Disc Shaft-'

Torq1e factor C (Select One Ar.gle)

.elve '

Typ2 Dia.

.'s ise.

. Flew -

lShsts h.

Direction classi-c' 10*

20' 10' 40*

$0*

60*

70*

goe.go.

Cast-Flat-All 0

10.3 21.0 33.0 12.0 129 245 495 763

, Cast-Hub All 0

15'.4 31.5 49.5 TOS 194 365 742 1140 1 1/4 [2l 0

IG.3 29.0 29.0 29.0 64.8 144 323 392 I l/2 131 0

16.2 27.8 27.8 27.8 65.0 139 276 313 14 Flate 1 3'/4 [4]

o 16.3 29.0 29.0 29.0 64.8 134 239 280 T'

2 ($1 0

16.4 28.2 23.2 28.2 65.8 134 216 254 2 1/2.16f 0,

16.5 23.2 28.2 28.2 65.8 113 151' 177 3 f71 0

16.4 23.3 28.3 28.3 65.8 94.1 120 144 Cast-Tlat All o'

15.0-31.0 -

51.0 108,

195 370 750 1,160 Cast-Hob All' 0

22.5 46.5 76.5 162 292 555 1.120 1.740 1 1/4 121 0

24.7 42.3 42.3 42.3 99.0 224 515 627

+

1 1/2 13l 0

24.8 42.6 42.6 42.6

'99.3 220 475 572 16 Plate 1 3/4 (4) 0 24.7 42.3 42.3 42.3, 99.0 210 402 472 2 [5]

0 25.1

,42.9 42.9 42.9 100

- 207 365 426 2 1/2,l6l 0

25.1 42.9 42.9 42.9 100 201 305' 355 3 f71 0

25.1 42.9 42.9 4*.9 100 154 201 236 Cast-Tlat All 0

22.0 45.0 73.0 156 282

535, 1,08C 1,710 Cast-Hub All 0

33.0 67.5 110 234 423 802,

1,620 2.560 1 1/2 (2) 0 34.3 58.8 58.8 58.8 136 315 720 892 la 1 3/4 (3) 0 34.4 58.9 58.9 58.9 137

~299 627 750 Plate 2 (41 0

34.3 58.8 58.8 58.8

'136 290 535 630 /

2 1/2 (51 0

34.4 58.9 58.9 58.9 137 279 452 529 3 [6]

O 34.4 58.8 58.3 58.8 138 260 373 442 3 1/2 (71 0

34.4 58.A

$8.9 58.8 137 206 260 309 Cast-Flat All 0

32.0 61.0 99.0 210 381 720 1,460 2,310 Cast-Hub All 0

48.0 11.5 144 315 572 1.080 2.190' 3.460 I 1/2 121 0

48.0 8, 2.0 32.0

$2.0

91 438 1,030 1.230 1 3/4 (31 0

48.0 82.3 32.3 52.3 193 425 920 1,;10 22 Plate 2 (4) 0 48.0 82.0

$2.0 22.0

91

• 18 857 1,220 2 1/2 151 0

47.9 82.3 32.3

$2.3 192 398 688 303 3 (6]

o 47.9 32.3

$2.3 32.3 11 2 384 583 678 3 1/2 (71 0

47.9 82.3

!2.3 92.3 112 129 453 534

$17.3 M.i 03.ato*7 g w 155Dwy.

l260 Cast-Tlat All 0

$3.0 106 Cast-Mub A!!

0 79.5 159 260

!!2

!.:00 1.s90 3.820 6.080 1 3/4 (2) 0 85.0 146 146 146 140 783 1.910 2.410 2 l3l 0

85.C 146 146 146 40

' 766 1,730-2,100 24 Plate 2 1/2 141 0

85.0 146 146 146 240 730 1.470 1,720 3 15l 0

85.2 146 146 146 341 706 1,300 1.540 3 1/2 161 0

85.2 146 146 146 241 682 1,070 1,270 4 I?!

0 95.2 146 146

!;6 "I.1 621 376 1.?;0 Cast Flat All 0

105 211 34-734

,22 0 2.;20 5,090 5.*5

Cast-Hab All C

154 116 516

!.!00

2. 20 3.!to

?.640

12. 20 2 (21 0

171 293 293 293 i10 1.'30 3.950 5.200 2 1/2 131 0

171 293 293 293 il2 1,4!0 3.510

4. 20 92 Plate I'l 0

171 293 293 293 iso 1.510 3,240 3.723 3 1/ 15l 0

171 293 293 293 633 1,480 2.830 2.320 4 161 0

171 293 293 293 is) 1,390 2,270 2.650 1/2 I?!

0 17 291 293 293

,4 1,170 2.100 2,440 L

l 5

TA:.0.VL *.hMT 3:tJ:ITEPS TABLE 1.

SILATT DI AMETERS (!NCKIS) 10R TYPE 9200 b

halve size In Shaft 2

3 4

5 6

7 l

c!ss.

3 4

5/8 3/4 1

1 1/4 5

5/8 3/4 1

1 1/4 6

5/8 3/4 1

1 1/4 1 1/2 l

8 3/4 1

1 1/4 1 1/2 1 3/4 10 1

I t/4 1 1/2 1 3/4 2

2 1/2 12 1

1 1/4 1 1/2 1 3/4 2

2 1/2 14

'l 1/4 1 1/2 1 3/4 2

2 1/2 3

16 13/4 1 1/2

' 1 3/4 2

2 1/2 3

18 1 1/2 1 3/4 2

2 1/2 3

3 1/2 2

--)6 1 1/2, 1 3/4 2

2 1/2 3

3 1/2 Dk 2

2 1/2 3

3 1/2 4

24 --+

10

2

~ 2 1/2 3

3 1/2 4

4 1/2

~

36 2

2 1/2 3

3 1/2 4

4 1/2 42 2 1/2 3

3 1/2 4

4 1/2 5

48 2 1/2 3

3 1/2 4

4 1/2 5

54 3

3 1/2 4

4 1/2 5

5 t/2 60 3

3 1/2 4

4 1/2 5

5 1/2 66 3

3 1/2 4

4 1/2 5

5 1/2 72 3 1/2 4

4 1/2 5

5 1/2 6

84 4

4 1/2 5

5 1/2 6

6 1/2 96 4 1/2 5

5 t/2 6

6 1/2

?

I2 ETTECTIVE ??ISS*,71

• ROP TASLI 2

<> c f Type of Anele of ' isc Oeening J

.s?

Fluid 0*

to*

20'

0*

.0*

50*

e0*

0*

10* 1;*

t Liquid A#* t 0*

0.570P 0.730P 0.500P 0.690P 0.650P 0.450P 0.390P 0.35CP, c

1 I

1 1

1 1

1 I

iP Cas act 0 act-10" 0.500P, 0.250P, 0.250P, 0.200P, 0.200P.

0.140P.

0.140P.

I 2

Laqund act 0*

0.700P 0.700P, 0.7CGP; 0.700P 0.670P 0.600P 0.500P 0.45GP; g

g 3

g g

Cas aet 0*

0.2t0P.

0.!!cP, S.?!:P.

0.?!0P, 0.2!0P; 0.120P.

0 ! 0P.

L CC:P g P. 8 L'pstream pressure (psna) et tric andscated angle of cpetics (o').

J i

e ii

CFG 200-20 PAGE 17 JANUARY 1973 SectionbA. Type 9200-Flow Against llub Side of Disc (Continued)

T-Ring !!aterial: Adjustable,-All Except TFE(I)

Inflatible-All Except TFE(I) and Viton(2)

,n., v e:. a, ans.. o. van uu a n,t usun.uu c,

,i rAA c, or 17 4 3r tunes c m, a l'.a:n t.u a.

sus.mc ros cis. c.tc j

0, e f.mu a a y,.,,

1..e.+ r isau a*.;ts:

lau aut:5l tan a,.mts:

0* l to' l 20' I C!M*l Wl WlO*W D '

• I ' h _ _ _ __ ___

f l

t 136 l 86lLoh22 l 12.

]

h 92C0 IE ADJ 109 161 397 136 l 86 l LOl 22 l 12 6l~h M LATE 109 1 23h y

UlO 35 20 nl 6l h snu.

ADJ.

m l 127

+

1 1/2, M LATE 109 l 167 133 93l 67 35 20 11 6

h 213 l 136 ;

63 l J5 ll 19 9

6

}

9200 TFE A0J-153 l256

-=-

g 213 l 136 l 63 l 35 l 19 il 9 6

VLATE 153 l 3L8 16e 3

ILO l..M l Sh ' 32 l 18 9

6 1 34

$ ntt..

ADJ 153 l 180 s3 269 NrLatt 153 N233 190 ILO i 102 l Sh 32 l 18 9

6 l

283 ll 3L9 l-*

31512c1 l 93 l 52 l 28 IL ! 9 IFt DJ 9200

['

VL ATEl

?!S 1L27l-~ l 31L l 201 93 I 52 i 28 IL l 9_

I 2LL l-*

l 197 I IL6 79l L7 I 26 l IL l 9 5 :t.

ADJ 288 351 V LATE 235 N 311 l 257 l 107 I IL6 i 79 i L7 i 26 l 1L! 9 l

2'

,3 lfIL7'l-* l 98 l 62 l 29 l 23 l 8l kl 3 9200 TFE ADJ. k 12h g

.VL ATEl 12h 11190lIthl 95 l 62 l 29 l 23 4 8j hl 3 2

,"i hi 3

.gu ADJ. !

12h y 1ch l 103 ! To! L9 1 25 l 15l 5

1.in i

15s l

,3 JJ L AT El 12h ll135l103l 70 t L9 I 25 l 15 l 6l

=1 3

l l

g.

! L5 25 l 13 6 7 l g F

l tsg t0J l 161 210 l

• I !!Li 93 215 161 E 252 l-** ! 15L ' 95 i Ls i 25 ' 13 i 7t a

9200 i

i

• .'L A7El 5?ttt A0J l 161 h IL7 !-*" I 1C51 75l LO ! 23 i 13j 7} L 1 3 A.

215

1. 3

>#L ATE l 161 II 100iIL7l1c5 I

'S ! Lo l l Is I 7l

?)

!i ?!L l - l 225 i 1L5 l 67l 37 l 20 ! 10 I 6 l

ti ADJ l 125

,,E 9200 2e1 l 229 l 115 l 67! 37 I 20 l 10 l 6 V LA*E 188 ll353 g

142 l 108 ! 53 ! 3h ! 19 ! 10 [ 6 l Setit, t0; les ll 200

-~

2*

281 l#3

' rt t.;El 188 d253 1 200 ILS l 10$ l 58 l 3h ' 19 10 l 6

!l ILS l- ~ ! !! l 56 l 26 ! IL I iI Ll 2 l

f

% ll,n g A0J l 105 9200 I

IL7

-*/ L A'!g I $

'L!

2

- ~

2 1

105 '

!I 193 l 155 I !S f 56g 26I IL I Aa; i 105 l' 101 l 95 l 63 i LL l 23 l 13 7

h! 2 2

5 l

IL7

1. ) A a

.%s t r.* f.,f 105 l!127_l 95 l 63 ! LL I 23 0 13 i 7

2 I

f I

I

! L 123

_I.77

!?O I 33 39 21 11 120c I

I'E f.UUJ]

-~

t i 2.3j y L.; e e, u _,1 u__;

2'-

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1,,

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123 1 ) *,

129 I O' 6k

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'1 6 i 3 I

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l l

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-._171- _129 O -

3 I

f*l

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22.._~-_ _. _5 D 1D

%..._j,1_. _2 ?. _1 -

l 9200

)'

f

[#'

g.3**y__202 3"

' L93

'_250 1159 i 22 11 7

%q L1 q

21 11 i 7

t i g,,n I

';J 202

. ??) i 215 in 118 ' 63 t ja:

2*I # l lJa 300 t.,, t f,.I !

202 l, 272 l 215 l 161 1118 l 6) i 1 83 i 21 8 11 1 7

l I

! AdJ l 80

!?Ll* l 66 ' L 2 i 19 t 11__ { 6_

3 ! 2 1

9700 to g l

i f*E j,157 l 1M l 66 i L2 l 19 l 11I 66 ) l 2 I#

eo 33, p

f 85 _ l 7h l L8 I 3h l 17 l to l 5_I_ 3 l 2 l

suu 20J eo r---

l l

jg37[

0

' 107 I 7h LS l 3h 17 l 10 i 51 3 l 2 p.

J3 10 1.

Con. ult tietory.

2.

See Section 2C.

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Marshalltown, ** wea 50158 Beceiving P2nnt Marshalltown, Iowa

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