Of THE ORIGINAL IS QOOR

( N A S A -Ca -1 20 227) flEASURECEIT COClPOl E l T R34-27186

HEASUREHENT Ah0 CRYOGENIC L I Q U i D DETECTION TECHNOLOGY. VOLUflIE 2: CIYOGEHlC FLOY

MEASUEENEN r IECHNOLOGY (North Aaericaa Unclas 93 p nc $7.75 CSCL ~ O L 63/23 45513

REPf@O(KIBJLITY Of THE ORIGINAL PAGE IS QOOR.

REPROCNCIBILITY OF THE ORIGINAL PAGE IS P O O R .

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REPROMX:IBILI’IY OF THE ORIGINAL PAGE IS P O O R

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i

I


1.c l2maxTIm. . . . . . . . . 2.0 SmmY . . . . . . . 3.0 L ~ W O G E N I C F L ~ ~ I Y E Z & S . ~ " ~ ~ ~ ~ . . . . .

3.1 lBchnicalDFacussicm . . . . . . 3.2 F'lcwbtwnmmntDesignCarsideratims . 3.3 SurueyIIesultscfAvailableDeaigns . . . 3.4 De-si-ter-tes . . . . 3.5 AFplicatianof an Available Des~gn . . .

. .

4.0 CRYOMTC LlWID DE3"ICN TEUMXLGi

4.1 ~ C a i D l s c u s s i c n . . . . . . 4.2 EvaltntaonofAvailahleDesiqm . . . . 4.3 SrnvqrWtsofCurmnt lyAwUableSys tars . 4.4 Tahlaticn -~LiquidDetectuxlsygtans . .

BlBLlCGRAPUl . . . . . .

- 1

5

. 11

* 15 . '8 . 19 . 59 . 60

. 69

. 69 . 70 . 71 . 80

82


Fiqure

3.3.1-1 3.3.3-1 3.3.4-1 3.3.4-2 3.3 4-3 3.3.5-1 3.3.6-1 3.3.7-1 3.3.7-2 3.3.8-1 3.3.9-2 3.3.9-1 3.3.10-i 3.3.10-2 3.3.11-1 3.3.11-2 3.3.12-1 3.3.12-2 3.3.13-1 3.3.14-1 3.3.15-1 3.3.15-2 3.3.16-1 3.3.16-2 4.3.1-1 4.3.3-1 4.3.4-1 4.3.5-1 4.3.8-1 4.3.8-2

. ,.2 . 25 27

. 2 9 . 29

. 32

. 33

. 3 4 . 35

. 36 . 38 . 40 . 41 . 42 . . 45 . 46 . 48 . 49 . . 50 . . 52 . . 54 . . 55 . 57

. 5 8 . . 7 1 . . 73 . . 74 . 71 . . 77 . 78

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REPRODUCIBJLJTY OF THE ORIGINAL PAGE 1s POOR.

- paqe

3.6-1 Flcsaeter &mufacture SlpVFy Table . . . . . 64 3.6-2 candidate -sign Capwism Table . . . . . 6 i 3.6-3 Aaeptahle FLowaeter ‘hble . . . . . . . 68 4.4-1 L i q u d Detection Sysvan Design and perfantlance Feat*mes . 81

-n- mn2-c#-oua-2

REPROMK31BILITY Of THE ORIGlbIAL PAGE IS POOR.

Cryogeruc - Any teipereture 1- than -100 F.

&ymlds No. - A d i ~ ~ ~ ~ ~ l o n l e s ~ ratio of inertia forces divlded by viacum fcnxea.

o x - m2skol56-2

REPRODUClBJllTY OF THE ORIGINAL PAGE IS P O O R -

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REPRODUCIBILITY OF THE ORIGINAL PAGE IS POOR.

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REPROMK:lBlLlTY OF THE ORIGINAL PAGE IS POOR.

REPROM)CIBJLITY OF THE ORIGINAL PAGE IS P O Q R .

- 4 -

REPRODUCIBILITY Of THE OC(IGlP4AL PAGE IS P O O R

REPROOKIBILITY Of THE WlGINAL PAGE IS POOR.

Rue invastigaticm primarily addressee itself bo the search for a netallic d for myoqmic tenpersture arr9 q~ LO 5000 p i g pressure wlicationa.

Ths rate for a real deperds on fluid w i e s , surf- W m , aprrsuse differential, hardne~ of the smaliw~ material, ard seal- amtact StmSE.

- 6 - m2-sA-ow-2

KtmunUclMLlTY Of THE OfclGlNAL PAGE IS POOR.

- 7 - m*w-2

REPRODUCIBJLITY Of THE OKIGINAL PAGE IS POOR

REPRODUClSlLlTY OF THE ORIGINAL PAGE IS POOR.


REPROMX:INLITY of THE ORIGINAL PAGE IS POOR.

- 11 - m72-skol5b-2

REPRODUClSlLlTY OF THE ORIGINAL PAGE IS POOR

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KtYK(XXK, -1BJLITY OF THF ORIGINAL PAGE IS POOR.


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REPRODUCIBILITY OF THE ORIGINAL PAGE IS POOR.

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REPRODUClBlLlTY OF THE ORIGINAL PAGE IS POOR.

- 2 3 -

REPROOKIBJLITY Of- THE ORIGINAL PAGE IS POOR

REPPOWCIBILITYOF THE &IC~NAL + I PAGE IS POOR

KEPROMX:INLlTY Of THE OCclGINAl PAGE IS P O O K

- 2 0 -

REPRODUClBlLlTY OF THE OCcIGINAL PAGE IS POOR,

ssceian 3.3.5 3.3.6 3.3.7 3.3.8 3.3.9 3.3.1C 3.3.11 3 . 3 . u 3.3.13 3 3.14 3.3.15 3.3.16

REPROOKIBILITY OF THE ORIGINAL PAGE 15 POOR.

Mi V YULTfPLIZR

sa-

p 1 '#&

c-cayciunce p =Actual density hMrtaase botweea capmitance dement

g m D h h c t r i c eoartoat kronotant

P p m i c a u d deaolty

l . A c h ~ l maar flow rate

A . A r u V.Velodty

and k &re co~f . ( l tO

Figure 3.3.1-1 (91

The BendLC Inferentlrl M a r Symtcm

REPRODUCIBILITY OF TH€ OFcIGINAL PAGE IS P o h .

-23-

REPRODUCIBILITY W THE OfcIGINAL PAGt IS P O O R


.‘huLxKi OUTPUT ( 4 - Z O U ETC) J-ulnn-

SOURE WAVE O u - r p u ~ o m5y) BLUFF BODY

-2s -


- 2 6 - m72-Bkow-1


MtDU F L O W

IMPELLER

Figure 3.3.4-1 Meme Momentum Motor Ammomblp

- 2 7 -


Flgurc 3.3.4-2 a4 Flow Meter fartallation


-29- m7zIBIcow-2


Le.,

i.e., 8 - k p t vhm kj is a crm8-t

k2 k p t = k l h


- 31 -


Plgure 3, 3.5-1 Tha Fisher And Po rer Turbine Mater


Fiauure 3.9.6-1 Tb4 Fbr Technology Turbine &tat

-33-


Figure 3.3.7-1@4 Tba Fadoro M a o r Momentum Mater

- w - 8(m%kol%-2


-PICKUP COIL

/ ,ROTOR S H A F T ASSEMEL FLOW l;i

S d - H V S T E R E S I S . c

F,C-7==&!?= 2.. - - 7 1F - -I--_-_ .r DRIVE

S T R A I 6 H T E R E R: --- >

Figure 3.3.7-2@1 Tha Forboro Maar Meter Installat,on

- 3 s - m2ak0156-2


3.3. The General Electric M a e m Flow Meter

-36-


*re V is tl.n transnittPr cut@ ml-.siqal, kB i s t!! ratio of flw +- the sens~f to the total flou, n is the tctal mass rate of flou, P is t9e inpeller f l a r e l o c i t y , kv is the pxkoff wl- gradient, and ks is the turbrne restrairhq- spring ornotant. systan. It is a direct statermt of ?&&XI'S lar umbr steady-state mrditicns, umrporatirq necessary mid aoc~stu 1 . i of the oanporrnts am*iikutuq to the raeacnrremnt.

'I% f u r t i i o n of the bvpkos el-t SB the sare m prirri$e as a t of a shunt resistor in paral! ii vith a maillivoltmter in the mas- of e-ic current. The basu operational mqukemmt is that the div.'bm of f lau u e m sasor ard bypass be rn omstant ratio. Hydraulic &sign nust & such that the f l m rate to pressure drwp ratio of the bypass eLanent and that of the flcw mmsor are equal over th operating range. abviouply mxlld be met i f both ehamts follared -isely the aquare hw of pressure drcp wrms mlds maker. the square lad, but they deviate by eqwll BIDults. - y , thc diVisl0n of flow is ranqe.

&I importMt design fector ie nuntamirq -at flcr*. anditirns in the senmx arrd bypeos over the operatirq rangp. Cthena 'se a precisely constant division of flow WGlld be d i f f i c u l t to maintab c ~ ~ l e r t ! ~ tmraitiion reg-. Fluid turtdenoe pxwalir in the #Mor f lu id charber a t dl f h rates, even zero, by vim of amtinuous i n p e l k mtm. Ouer any practical flow range, turkrlenoe rn the bypass can be maintained +hrough prppcr selection of pipr. and o r i f i a e d m i c m s .

Wditiinal lat l th of ducing a n i f i c e in the f l m 8er .m~ piplng. to l~arpmate the maxrl orifice, althaagh test deta indicrrte tiut it is not a furticMl requhmmt *herr, d y a enrll f r a c t - m of total f l m P=f=thraWh*-.

rdius of gyration, w is the q e l l e r angular

'Re equation is m a l am3 bids for my amsistent unit

Ihi. d t i a ~

Both elenmts &rate s l igh t ly f m n

mt to a high degmz of precision o\Rr the er.tira cparatbq

d immiana l an-1 m y be obtained .y L"- 'h~ f-tar is Qsrgrd

-37- mz%k-Ol!j6-2


F L U I D IWPELLER- ,- FLOY smsswe ELLRENT

F L U I D

I '. - = - = ' I -SA- Y - \c - PATH 1


- 3 9 -


- 4 0 -



T 8 ?(n f2)

- 4 2 -


- 43 - RY72.skOw-2


- 4 4 -


-Oh1 PI) ESSIO?' Fl r TD'C T\ CONNECTOR

----!I4 SENSING V A N T 7

--- I>- I

- .-- - -

1'- - m - - - J SUPPORT ROD'

I31 Figure 3. 3.11-1 ITT Darton Denritometrr

- 49 - m2-6kOl.56-2


' Y r--- Lcl (291


- 47 - m72-6kol56-2


Figura f . 3. kZ-r33bwntum Dynamic8 Turbine Meter Cutaway


' I I J

- 49 -


FLOW

?ObCE XDU

f FORCE)

(F FORCE LEVER ARM

(341 Figure 3.3.13-1 Rampo Dr.8 Body Volumetric Meter

- 9 - anHm-ol56-2



CONTROL ClRCUlT

* t -I:

f

(bo1 Figure 3.3.16-1 Thermo-systems Thermal Mare Meter Schcmattc

- 57 - 8Dn-Skol56-2


- 53 - m*w-2


-n-

REPRODUClSlllTY OF THE ORIGINAL PAGE IS POOR.

Figure 3.3.19- Pa S i m m o d Precision Flow Moss System Schematic


- % - g72-skolM-2


- 57 - m72-a-01Sbz


COYPEHSA LMLET SCREEm \

FLOW tLEMENT

TOR

TRANSZUCEP 'IENTU31 SECTION

Thorum-eyatoma Mass Motor Inuta!lation Cutaway

- 9 -


* 59 -


- 6 0 -


- 61 - mz%kOuB-2


- 6 2 -


- 63 -


GAS

clrs

LXQ.

I

LIQlChS

L I Q / S L W

SOLIn??

LIQ/GAS

LIQlGAS

LLQIcnS

LIQ.

LIQ/SLvPar

6bs

tIQ/sas LIQ/66S

u p 8

c*s/LIQ/ StBILn LIQ/CAs

UQ/W

L I Q l W

L I Q l W

LXQ/Ollll/ SLCpll l

394

711513

358

- 2PQ/W4

b 50

2771333

20 /422

- 588

19

350lb22

2?3/ 339

2 7 3 l U 9

19

161610

227 /810

339

CPPOIbl?

20190

217/322

SI533


FISHER rw) PORTER

CLW c a har TEOl.

FLUID DATA

FOXBORO

m u 0 cw CaSERu L L E c r . CtNEirU ELECT.

CILllowT

CL'RLEY

HALL1 LL'RTON

HAST!NGS-RAYDIST

HONMUELL

HONEWELL

1ND. UEAS.

I S - V A L - m

:TT BARTON

In M R T a

K I N G W N - U % I T E

KOIUTCS

KOUTES

LLN

L I B U S C O P E

LINDSEY

LIQUID CONTROlS

ma HANOSTATE

LIQ I SLURRY

LIQ1SLUUV

L I Q I W

LIQ . LIP. LIQlcrrS LIQ.

LIQICAS

LIQICAS

LIQICAS

LIQ.

LI:] *

GAS

LXQfCX5

LIQ/SAS

LIQ.

LXQ.

LIQIGhS

LIQlGAS

L I p/cAs /!'AP@R

GAS

CAS

LIQlGAS

GAS

LIQICJS /SLURRY

LIQ.

L I O I W

LIQIGAS

2131455 141533

l L l 4 S O

89/&77

761333

191810 355

2 0 1 9 0

24413513

2551373

2731339

?00ih78

21?0:1310

366

19

2 5 5 / 3 5 3

2001700

191810

2 2 2 I366

ULtPR

3u j

340

2 391 344

2271333

331810

222

2221477

2001417

ELECTPD?lACNETIC

n ' U 1 N E METER

T V U I N E NETER

ULTlUSOWLCS mnrrm puss TURBINE METER

VAXIMLE AREA ROTAMETER

?iCWT'JX MASS

DIFFELEXTIAL PRESSUKE

VUAIABLE AREA ROTMETCR

TUWIYE XETER

RRBIXE METER

T H E W L

DIPFEREWIAL PMSSURE

DRAG BODY

P X I T I V E UiSfLALEniNT

IJRBINE HETER

NEBINE EaTER

DIFFERENTIAL PRESSURE

DIFFERENTIAL PESSl'RE

DIFRILE?;TIX PRTSSL'XF.

VAXlAELE AREA, ROTMETER

f L X T B D M E T I C

F!!W Q)WVTER

TURBINE (OUT OF aus. ) Pa ITIVE Dl S P U C k n E W i

-- VARIABLE M E A . R O T W T E l l


!U XHESOS

a€. h.0

YFG4)-?(ETER

Y E R I M

';A1 i 3 S U INSTR.

XPTLWE

' U . U r n D Y W I C S

hCW0

RAMP0

ROBINSOW

.WCKUTLL

ROSCUJLW ENG.

ROTROX

SCHROEDER

SENTRY

S 1 . W N S P R E C I S I o l

STATHAH

TAYLOR

KAILOR

T E N YEf64tRfWICf

THfIUWL INST. cb.

THERHO-SYSTfn INC. " LAS

VALLACE 6 T I E W

UACKLE

LIQ . w LIQ. -- GAS

LIQ . LIQICAS LIQ/GAE

L IQ lclrs Ayy

LIQ.

CASILIQ.

LIQICAS

LIQ. LIQ. LIQ . BLOOD

t1q/ SLURRY

LIQ. CAS/SLURRY

w CA.. I LI v. cns/Lrq.

LIQ/GAs CASILIQ.

GAS

396

294

-- 233/ 700

2 s i m -

31511

219/810

751616 -- 372

158/311

23 3IL50

2171378 -- 201422

289/111 2551394

233f810

2301339

TO 921

227f 366 2191344

394

339

PkcE 3 OF 3 -66-

VARIABLE Aa€A. mMEIen VARIABLE ABU. m r m R DIFFERENTIAL PlKSSUBE

LANIIOA. F t o v aaEIT

DIrnBLl l f '4L P m s m N P B I N E llETU

N B B I S E METER

VARIABLE AREA. ROTAMIXER

STIUIH CAGE La.'.cT BODY

D I F F E M I A L PRESSURE

TURBINE METFR

T H E W W S

VORTEX

DIFFEREX IAL PRESSURE

TUBBIM HETER

TURBINE ?anR

ELECTROUCSETIC

ELE(3EOIIACMTIC

DIFFERENTIAL PRESSURE

T H E W %ASS

r n u m u luss

'IHEIMAL W S

OIFFEDEWTIAL FLOU

VARIABLE AREA. RmMETEk

VARIMLt AREA. R O T M E T E U

m 2 b k o w - 2


rYPE Of SYSTRl msxr(pILm WIDIMTE AYD PUIQCIPAL H E ' D TYPE

B U O I X

COI INST

EASTECli

ELECTRO DEV. COW.

FISHEU 6 PORTER

F t W lTcI1

FoQulBo

C E L E W ELECTRIC

HMTIIQCS-RAYDIST

HOH€YUEU

IlT w m

D8& BE-BAWICIIIC

NBBIIQE - B(dDQ AltD Bp PICKOFF

BLUFF BOW - VORTEX SWEEDIWG

N U B I N E WTER - BLADE M I ) iv 08 SAC PICIOFF NBBIIE ?lETtR - B U D € AWD UP OR ldAc PIQLOFP WEENTUN. ANGULAR - IOkQUE A!D ANGULAR SPEED m 1 K E METER - B L m Z Am H U PICKOFF I(wlfwNH. ANGULAR - TOaqvE. RADII All0 ANGULAR SPEED THHERnnL - UEAT TMWSFER

THERHAL - H U T TRAhSFER

TURBINE METER - BLARE Am) PICKOFF

T H E W - H U T TRANSFER

PACE I OF 1 - 67 -

YES - DIELECTRIC- 'co-DENSIIY

wo - VOLmETRIC OUTPUT ONLY

NO - V O L U M B I C OUTPUT ONLY

NOT NECESSARY, TRUE #Ass OUTPUT

NO - YOLuIIErnC ptow ONLY

No - VOLUHETRIC F W ONLY

NOT NECESSARY. TRUE HAS5 OUTPUT

NO - MLUlQTRIC FLlx ( W t Y

NOT NECESSARY. TRUE W S OUTF'UT

NOT NECESSARY. TQLR: PIASS OUTPUT

NOT NECESSARY. T W E luss OUTPUT

YES - O S C I L U T I N C VAtJE

YES - DIELECTRIC- TD-DFWSI'IY

NO - VOLUMETRIC F L W ONLY

NOT NECESSARY, TRUE MSs OUTPUT

YES - DIELECTRIC- TO-DENSITY llOT NECESSARY, TRUE MASS m

Q72-m-0156-2


Y 9

2 i

w

H




Flgum 4.3.1-1 Acoustlca Ultrasonic Samnr Systw,

- 71 -


- 72 - s m 2 ~ l % - 2


I e 1

* 13 -


J

I---- I

Film?. 4. S. 4-1 Bond& Cryogedc O p t 1 4 Soknror




"\\ /' Figuro 4.3.8-1 Simmondo Prociaion Coaxial Capacitance Syatem

-77-


Figure 4.3.8-2 Simmond8 Prscieiorr Point Sansor Ring System


- 7 9 -


- 8 0 -


I %


BIBLIOGFWHY

111 F. F. Liu, 'Dytwmic Phase T r a n s i t h l PherrmreM Associated -A& W C Q w n Flew m the Fenp?rature &urge of Fmm 20.K to 2YK; .sen: €&ermmtal observations"

D. H. Weitzel, J. E. Cruz, L. T. Rme. R. J . 3ick-d~ Md D. B. Mum, " I n ~ t n m m t a t i c n for Storage and hvufer of tlvQosen Siush,' Divisim Institute f.Jn Basic Standards, W t i n a l euteau of Stamkds

R. C. E-, "Fluid Wzhanks," rhrrd editicn, pages 203 throuQl 241.

5. L. Brittcn. Wecon, Color& mineertq -=tal Station,

(21

[31

I41

IS] D. weitzel, means, ~aucrral mma~ stand~ds, mdder, c~ lo . ,

[6] D. A. Ulerbruch, "hcrva\~ M t b d s for L ~ I C Liquid and Slush instnmmtatim," Cqacprdc Divisran, N.B.S. Ins t i tu te for Basic

1972.

1971 a d Jawry 1972.

ShmjatdS, Boulder, 810.

171 Il%aa*nt mgineeruq 8 . 8 "kmptame Tkst pmceduse for Flow

[E ] 'W449-0015, ' h n m k e r , Mass Flow" Rav. E, dated 2 3 Nmenber 1965.

[9J &nd.h, fnstnments a d Ufe SUFplrt Divisim, lUlleun 1619110 dated 15 Fcb_ruary 1%7*, a d ''S- of Flowrcter Surrrey &sults."

V Y P E 9133 Pual PZar 'Ranmittar PubliWticm 2805-5A--70(401), TYPE 9164 ~ l a w mte lhntmitter puhliaaticm 28c5-a-70 (40 ) .

septrmtrer 1971.

Sensors IEZ 1248 and 124'2 WSiD Part .W49+015.'

1101 W. 'Ireawm, R. ifrd&, Faci l i ty Cantact, Bendix, Dw-, Ram,

I l l ] COX Instnslants, RAlettinS -03, (3-7601, and 03601.1.

[12]

[131

0. Whtt 6 W. Kruq?r, F a r i l i t y Crmhct, cao< Inst., Mlch., srpt. 1971.

a r m twrpcra ta l , BLllletins VS-21970, 'ID-1, W 8 , T3-5, II)-t, iE-9, and *lo.

' . R. J. Cawunrar, " E Z Technical Propogal, eUsiness a u d Mmnagmmt Infomatiar for fhss Flolrslptars for Space Shuttle," d a x m n t M. 710527 dated Mty 5 , 1971.

Firher d %rter, Catdlw CIOC daw June 1968.

P u h r & m-r, Technical Infornution 1x4 dated .Tune 1968.

[lS]

!la] [17] F l o w It.czhnolqv fncoqmratxd, BuiletiM 0).

- 12 - m2-M-0156-2


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I291

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[301

I311

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1331

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1431

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I451

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Of THE ORIGINAL IS QOOR