aec research ent report

53
ORN L-2278 AEC RESEARCH ENT REPORT Reactors-Special I I i ~ 3 4456 0351470 2 VBSCOS8TY MEASUREMENTS ON MOLTEN FLUORIDE MIXTURES So I, Cohen To No Jones * . OAK RIDGE NATIONAL LABORATORY OPERATED BY A '.- UNCON CARBIDE NUCLEAR COMPANY A Division of Union Carbide and Carbon Corporation m POST OFFICE BOX X OAK RIDGE, TENNESSEE

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Page 1: AEC RESEARCH ENT REPORT

ORN L-2278 AEC RESEARCH ENT REPORT Reactors-Special

I

I

i ~

3 4456 0351470 2

VBSCOS8TY MEASUREMENTS ON MOLTEN

FLUORIDE MIXTURES

S o I, Cohen T o No Jones

* . OAK RIDGE NATIONAL LABORATORY OPERATED BY A ' . -

UNCON CARBIDE NUCLEAR COMPANY A Division of Union Carbide and Carbon Corporation

m POST OFFICE BOX X OAK RIDGE, T E N N E S S E E

Page 2: AEC RESEARCH ENT REPORT

This document consists of 50 pages. Copy 3- 208 copies. Series A.

Contract No, W-7405-eng-26

Aircraft Reactor Engineering Division

VISCOSITY MFASURIXEIVTS ON MOLTER

FLUORIDE MIXTURES

S. I, Cohen T. N. Jones

DATE ISSUED

OAK RIDGE NATIOIUL LABORATORY Operated by

UNION CARBIIE NUCLEAR COKF'lWY A Division of Union Carbide and Carbon Corporation

Post Office Box X Oak Ridge, Tennessee

Page 3: AEC RESEARCH ENT REPORT

\

-it- ORNL-2278 Reactors-Special Features

of Aircraf t Reactors

8ak INTWNAL DISTRIBUTION

1. C. E. Center 2. Biology Library 3. Health Physics Library 53. R. ,I?. Gray

51. E. J. $$eding 52. E. R.,:Dgtko

54. D,w’Pe Gregory 4-5. Central Research Library Reactor Ekperimental

ory Records Department R. D. Peak 258. W, B, Cot t re l l

59. S. J. Cromer .r,

,.,’ 60. J, H. D e V a n

16. J. A. Swa 620 A. P. Fraas 17. E. H. Ta 63. W. T. F’urgerson 18. E. D. Shipley 19. M. L. Nelson 65. W. H. Jordan 20. S. C. Lind 66. F. F. Blankenship 21. F. L. Culler 67. W. R , Grimes 22. A. H. Snel l 68. F. Kertesa

69. H. W, Savage 70. W. D. Manly

23. A. Hollaender

‘71. E. P. Blizard 72. R. E. MacPherson 73. E, R. Mann 74. L. A. Mann 75. W. B. McDonald 76. R. V. Meghreblian

24. M. T. Kelley 25. J. H. Frye, Jr. 26. K. 2. Morgan 27. C. P. K e i m 28. R. S. Livingston ,’ 29. T. A. Lincoln ,

30. A. S. Householder 31. C. S. Harrill I “

32. C. E. Winters ; * . 78. D. H, Platus 33. D. W. Cardwel3p‘ ’79. D. L. Platus 34. E. M. King i 80, R. D. Schultheiss 35. A. J. m11eqi 81. ?. B. Trauger 36. R. A. Char$e 82. M. M. Yarosh 37. J. A. Lane.’ 83. W. F. Boudreau 38. M. J. Ski&er 84. €3. B, Lindauer 39. S. I. Cohen 85. D. C . Kamilton 40. W. R. &&bill 86. R. E. Moore 41. N. D. Greene 87. G. J. Nessle 42. H. W, H o f f m a n 88. R. F. Newton 43. T. N . Jones 89. L. G. Bverholser 44. J. J. Keyes 90. R , E. mom 45- A. I. Krakoviak 46. F. E. Lynch 47. L. D. Palmer 48. W. D. Powers 49. W. J. Stelzrnan 50. J. L. Wantland

< 61. W. K. Ergen

64. A. G. Grindell

’s, 77* A. M. Perry

91. G. M. Watson 92. C. J. Barton 93. C. M. Copenhaver 94. ORNL - Y - 1 2 Technical Library,

Document Reference Section

pi i ” . 9 c

Page 4: AEC RESEARCH ENT REPORT

EXPERNAL 'DSSTRIBVTION

.

Technical Intelligence Center

med Forces Special Weapons Project, Wash

Energy Commission, Washington s International

Memorial Institute

onautics (Code 24) onaut ic s General Rfjlhre sent at ive

I

121. Convair-Gener amics Gbrporation 122. Curt iss -Wrigh

124-127. General Electric 128. General Nuclear 129. Glenn L. Martin 130. Hartford Area Of

133. Idaho Operations,, Offi 134. Knolls Atomic J$wer L 135. Lockland Area (Off ice 136. LOS Marnos Sg5entifi.c

Aeronautic s , cle-lsnd Aeronautic 8 , Washington

to L. Richards)

sile Development Division) Operations Office rican Aviation, Inc.

r Development Corporati of the Chief of Naval

er son-Moos t and Whitney Aircraft Divisio x Project) (1 copy to

San Francisco Operations Office Sandia Corporation . School of Aviaition Medicine

9. Sylvania Electric Products, Inc. 0. Technical Research Group

Q

183-207. Technical Information Service Extension, Oak R 208. Division of Research and Development, AEC, OR0

Page 5: AEC RESEARCH ENT REPORT

-iv- '8 . L

E k E

ABSTRACT ............................................................. 1

INTRODUCTION ......................................................... 2

I2XPER-G APPfSiATUS AND TECHMIQUES ................................ 5

The Drybox ......................................................... 5

The Furnace ........................................................ 7

The Capillary Visconteter ........................................... 12

The Brookfield Viscometer .......................................... 16 INSTRta'lEMT CALIBRATIOM ............................................... 19 EXPERIMENTAL RESULTS ................................................. 29

CORRELATIORS ......................................................... 34

m c E S ........................................................... 45

.

.

Page 6: AEC RESEARCH ENT REPORT

-1-

ABSTRACT

.._c

!This report is a sumnary of the experimental viscosi ty

program on fused fluoride mixtures which has been carried

out i n support of the ANP e f fo r t a t the Oak Ridge National

Laboratory.

veloped a re described, data on the viscosi ty of 36 mixtures

are tabulated, and several correlations involving these data

The experimental techniques which have been de-

1 are discussed. 1

Page 7: AEC RESEARCH ENT REPORT

-2-

IN'lRODUCTIOIV

The value of fused fluorides as coolants and fuels for high tempera-

ture, circulating-fuel reactors was recognized early in the Om-ANPprogram.

However, the scarcity of known and reliable data on the thermal properties

of these fluids seriously hampered the initial design efforts. To remedy

this situation, a program was outlined to obtain experimental data on the

viscosity, enthalpy and heat capacity, density, and thermal conductivity of

the fused fluorides and their mixtures.

portion of this program concerned with the measurement of the viscosity of

the fused fluoride salts.

This report is a s n r y of the

The experimenter is confronted with a number of difficulties in the

measurement of the viscosity of these fluids:

(1) The high melting points and wide extent of the liquid state

of the fluoride salts establishes a temperature region of

experimental interest between 5OO0C and l,OOO°C.

All of the common materials available for the construction

of the experimental apparatus corrode in the molten fluoride

salts.

water vapor, the corrosion rates are greatly accelerated.

Since these salts in the molten state combine strongly with

both oxygen and water vapor, the purification of the salt is

difficult. Further, to insure a continuing purity, and hence

avoid large amounts of contaminating corrosion products, it is

(2)

In the presence of even s m a l l amoun%s of oxygen or

(3)

.

.

Page 8: AEC RESEARCH ENT REPORT

x

-3- 5

necessary to maintain the molten salts in an inert atmosphere.

Some of the salts, such as beryllium fluoride, present prob- (4)

. *, :$

lems in handling due to their toxicity.

The fluid viscosity in the tenperatwe range of interest

l o w , varying from approximately 2 to 15 centipoises.

( 5 )

These difficulties impose severe requirements on the measuring equ

is

praent DY

limiting the choice of techniques, construction laateriala, and instrumentation

and by complicating the experiraentalmnipulation of the apparatus.

A number of techniques have been investigated by the experimental groups

at the Oak Ridge National Laboratory in developing suitable instruments for

measuring the viscosities of fused salts.

and Cisar used a modified fora of the Brookfield rotational viscometer.

developed a gravity flow capillary efflux viscometer.

ated a capillary device in which fluid flow was accomplished by gas pressqre.

A "falling-ball" viscometer using a radioactive cobalt-plated Pyrex bead was 6 developed by Redmond and &plan .

1 2 Knox and Kertesz and later RedPlond

3 4 Tobias

5 -ox and Kertesz oper-

After review of this early work on the measurement of the viscosity of

the fluoride salts, it was decided that the most expedient route to results

of the desired accuracy was through further refinements of the apparatus and

techniques for the modified Brookf'ield and capillary efflux viscometers. hrr-

ing this sme period of apparatus development, salt preparation techniques

were greatly advanced by the bfaterials Chemistry Division.

reported are in general for high purity salt mixtures.

B u s , the results

The general techniques for fused salt viscosity measurements have been

developed sufficiently to place these measureaents in the category of routine.

Page 9: AEC RESEARCH ENT REPORT

ir :: 2 c_ -4-

The detailed discussion of these techniques and the apparatus modifications

is contained in the section of this report

procedures.

Some 36 mixtures have been studied at

on experiuental equipment and

O m * . These have included

binary, ternary, and quaternary mixtures of the following fluorides:

NaF, LiF, KF, RbF, BeF2, ZrF4, UF3, UF4, and ThF4.

A modest program of viscosity measurement on fused fluorides will be

continued. As new mixtures are formulated and found to be of sufficient

interest, viscosity data will be supplied to the various design groups

studying fused fluoride reactors. In addition, a program to investigate

fused salt systems other than fluorides is planned. At present this plan

includes studies on chlorides, and mixtures of chlorides and fluorides.

Some data 7 have already been obtained in the chloride system. Other sys-

tems will be studied as they become of interest.

* In addition to the ORWL, program, the Mound Laboratory is involved in an extensive Investigation of the viscosity of fluorides comprised mostly of

mixtures of the alkali fluorides with BeF2 and UF

carried out by €3. C. Blanke using a rotational viscometer developed at

the Mound Laboratory.

This work is being 4’

‘I f Y, mm

Page 10: AEC RESEARCH ENT REPORT

-5-

The experimental apparatus and techniques used in the measurement

of the viscosity of the fused fluoride mixtures are described in the

paragraphs which follow.

(capillary efflux and rotational), the viscometer furnace, and the dry-

box.

This equipanent includes the two viscometers

The Drybox.

inert atmosphere, all measurements were made in a drybox under an argon

blanket.

and front consisting completely of Plexiglas windows.

inches high, 30 inches wide, and 24 inches deep.

attached to Plexiglas rings located on the front at shoulder height to

Because of the necessity for handling these salts in an

This box was constructed froxu l/B-inch mild steel with the top

The box was 50

Long rubber gloves were

enable convenient and cowortable manipulation of the equipment located

within the box. A photograph of the box is shown in Figure 1.

One side of the drybox was constructed as a door to provide access

t o the inside.

its weight and was sealed against a live rubber tubular gasket by W - V I S E

H-200 clartlps located around its periphery. Shelves and a bracket to support

the Brookfield viscometer were welded to the inside walls and a cooling coil

made fra l/k-inch copper tubing was located on the w a l l opposite the door.

This coil was provided to reduce the temperature rise in the drybox due to

prolonged operation of the furnace.

increased for high heat loads by the use of a 14.cfb blower to establish a

forced draft across the tubes.

Tbis door was constructed of l/k-inch aluminum to reauce

The efficiency of this coil could be

Page 11: AEC RESEARCH ENT REPORT

-6-

UNCLASSIFIED

Page 12: AEC RESEARCH ENT REPORT

-7-

A number of precautionary measures w e r e taken during construction of

the box t o insure gas t ightness. Thermocouple leads were brought through

the drybox wall i n Conax f i t t i n g s and attached t o terminal blocks on both

the inside and outside surfaces of the w a l l t o eliminate s t r a i n on the

seal.

These f i t t i n g s , as well as the f i t t i n g s used for the cooling coi l , gas in -

l e t , and gas out le t , were welded i n place. The welds were heavily painted

w i t h GlyptaP before the final paint was applied t o the drybox.

was periodically checked fo r t ightness with a Freon leak detector.

E lec t r ica l leads were introduced through similar special f i t t i n g s .

The box

A ser ies of t e a t s was conducted t o ascer ta in the optimum procedure 8 fo r obtaining argon drybox atmospheres It was found that best r e su l t s

were produced by introducing argon a t the bottom of the box and allowing

it t o ex i t near the top through an o i l bubbler.

i n t h i s manner overnight wfth a flow of from 4 t o 8 cubic feet per hour of

argon before the test mixture was exposed t o the drybox atmosphere.

The box w a s usually purged

The Furnace.

t o design a tube furnace which would bring a capsule consisting of a

14-inch section of one-inch I .P .S . pipe f i l l e d with a fused fluoride t o

red heat quickly, hold the temperature constant along the en t i re length

of the capsule, and a t t a i n equilibrium rapidly after adjustments i n the

temperature set t ing. A diagram of the furnace along with the ternperatwe

measurement and control systems i s shown i n Figure 2, and a photograph of

It was necessary i n carrying out t h i s experimental program

the furnace i s shown i n Figure 1,

The furnace s h e l l was a cylinder 16 inches high and 10 inches i n dia-

meter, mounted on casters and equipped with leveling screws which can be

L

Page 13: AEC RESEARCH ENT REPORT

8

-

1 0

K

1

t

-

v)

W 1

a

3 0

0 0

H

K

W I

I- -

3 K

W

-1

K

W

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C 0

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m

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KO

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Page 14: AEC RESEARCH ENT REPORT

-9-

operated

circular

from several inches above the furnace. It was insulated with semi-

blocks cut f r o m slabs of JN-3000, an aluminum silicate insulating

brick ramufactured by Johns-Manville.

Two pairs of 3-inch I . D . "clam-shell" resistance heaters made up the

furnace element.

3-1/2 inches, were located in the furnace with the short section on top

and were controlled separately (see furnace diagram, Figure 2). The lower

unit heated the liquid wad the upper unit served as a "guard zone" heater.

This guard heater was necesssry for two reasons.

above t h e liquid surface must be kept at the temperature of the liquid or

t h e resulting temperature gradients w i l l cause convection currents giving

These two units, having lengths of lO-l/2 inches and

First, the zone just

slightly erroneous readings on the Brookfield vi8cmeter. Second, it is

essential, that the efflux cup visccmeter be held in a zone at the tempera-

ture bf t h e liquid while it is draining or an error is obviously introduced.

It was found that two separately controlled elements provided the simplest

mems of maintaining the temperature of this zone at the liquid temperature.

Temperatures of the two elements were controlled by circuits containing

chromel-alumel thermocouples, relays, and "Sinaplitrol~.~

included in these circuits to afford mre sensitive adjust;ment.

junctions of t h e thermocouples were imbedded in the outer face of a heavy

copper pipe ocmpying the annulus between the furnace e$eznerrk and the capsule

containing the sample,

one inch, served as a them1 diffuser to provide very even taperatwe dis-

tribution in the sampLe.

Variaes were also

!Be hot

This copper pipe, having a w a l l thickness of almost

t . **

Page 15: AEC RESEARCH ENT REPORT

-10- 5 ’$

Liquid tmperatures were measured using four chromel-alumel thermo-

couples inserted in wells of 0.08-inch O.D. thin-walled tubing which were

snapped into 0.08-inch square grooves machined longitudinally in the outer

wall of the capsule (see Figure 2 ) . The wells were cut to such length that

the junctions of two thermocouples were located in the liquid zone and two

were in the zone above the liquid.

of the four thermocouples to the two viscometers in operation may be found

in Figure 3.

Brown multipoint recorder

A diagram showing the relative positions

Tenperatures measured by these four couples were read on a

Measurements were made with both the capillary and rotational instru-

About ments using the same sample of salt diiing a single heat-up period.

100 cc of molten salt were required to fill the capsule to sufficient depth

to operate the two instruments. A complete viscosity-temperature curve was

determined using one of the instruments before measurements were begun with

the other.

After a satisfactory inert atmosphere had been obtained in the drybox,

the furnace controls were set at a temperature 25 to 50 degrees above the

liquidus temperature of the salt and the system was allowed to come to

equilibrium.

preparation equipment rose to the surface as the salt melted. This graphite

was removed by touching the surface of the salt with a cold tanaper, allowing

the superficial layer containing the graphite t~ freeze on the tamper.

The small quantity of graphite present in the salt from the

The capillary cup was usually used in making the first measurements

To establish the entire viscosity-temperature e w e , the on a new salt.

temperature of the melt was incrementally raised and measurements were made

Page 16: AEC RESEARCH ENT REPORT

m +

0

A-

i

I -

-

I

A

1

L

3

Lc n

J

W

m

a, a,

0

V

m

Y

0

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0

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m

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. .

Page 17: AEC RESEARCH ENT REPORT

-l2-

after attainment of equilibrium at each temperature step.

was allowed to cool to the original starting temperature, and a similar

experimental procedure was followed with the Brookfield viscometer.

Then, the salt

The Capillary Viscometer. The efflux cup or capillary viscometer, origin-

ally designed by Tobias 3 , is still being used with slight modifications. The instrument consists of a reservoir, containing the test fluid, located

above and integrally connected with a capillary tube. A photograph of the

device is shown in Figure 4, and a detailed diagram is given in Figure 5.

The fluid drains through this capillary and the time of efflux is obtained.

By comparing the efflux time for the test fluid with the times for fluids

of known viscosity flowing through the same cup, the unknown viscosity is

established. The determination of the calibration curve will be discussed

in detail in the section on instrument calibration.

This viscometer, while it does not provide an absolute measurement,

does possess the advantages of simplicity of operation, ease of cleaning,

and l o w cost of fabrication, Various construction materials can be used

to provide compatibility with many elasses of liquids, and the capillary

bore can be varied to cover a wide viscosity range.

advantage of the instrument, plugging of the capillary, has been virtually

eliminated by improvements in fuel preparation and drybox atmosphere tech-

niques.

by reaming with a fine, stiff wire,

The principal dis-

The occasional partial plugging which does occur is easily remedied

The cup used in these studies had a reservoir of approximately 6 cc

capacity, connected to a capillary one inch in length, Two capillary bore

Page 18: AEC RESEARCH ENT REPORT

-1 3-

F i g . 4 . Photograph of E f f l u x Cup or Capi l lary Viscometer a n d Sp ind le o f

B r o o k f i e l d V iscomete r .

Page 19: AEC RESEARCH ENT REPORT

-1 4-

UNCLASSIFIED ORNL- L R - DWG 49836

CAPILL 0.033

.ARY DIAMETER in. OR 0.039 in

Fig. 5. Diagram of Capillary or Ef f lux Cup Viscometer.

Page 20: AEC RESEARCH ENT REPORT

I diameters were used, 0.0330

-15-

inch and 0.0394 inch. Liquids with a kinematic

viscosity of one centistoke, the lowest value usually encountered in measure-

ments of fluorides, will drain from the smaller bore cup in about 45 seconds.

Measurements were made with the efflux cup using a visual procedure.

The cup was submerged in the molten salt until complete thermal equilibrium

m s attained.

heated "guard zone, '* and allowed to drain (see Figure 3). ance between the outside walls of the cup and the inner walls of the tube

containing the salt afforded assurance that the cup was uniformly vertical

from reading to reading.

It was then raised above the surface of the salt, held in the

The close clear-

A timer was started as the top edge of the reservoir cleared the sur-

The cup drained while being held face on being withdrawn from the liquid.

in the heated zone above the liquid, and the timer wss stopped when the

liquid level in the cup reached the bottom of the conical section of the

reservoir.

a number of times at the stme temperature.

ture was within - + 2 - 3 per cent. due to partial plugging of the capillary. In the event of plugging, the

capillary was reamed and the procedure was repeated until a series of meas-

urements of satisfactory precision was obtained.

The time of efflux xas recorded, and the procedure was repeated

The precision at a given tempera-

Results with greater spread were ususally

Because of the high purity of the salts and the improve4 inert atmos-

pheres, corrosion has been slight enough to enable cleaning, recalibration

and continued use of the cups on an almost indefinite basis.

Page 21: AEC RESEARCH ENT REPORT

The Brookfield Viscometer. This

consisting of a spindle which is

instrument is a rotational viscometer

immersed in the liquid being studied and

a synchronous motor which rotates the spindle.

spindle by the viscous forces of the l iquid produces a deflection on a

calibrated spring made of a Copper-beryllium alloy.

centipoises rotates with the motor and a pointer attached below the spring

indicates the deflection of the spring on this dial.

The torque applied to the

A dial graduated in

As with the capillary cup viscometer, this instrument does not pro-

vide an absolute measurement and requires frequent calibration.

even though more complex than the capillary device, it possesses similar

advantages for measurements on fused salts.

the system which comes into contact with the Baits, is easily fabricated

from a choice of metals. It is simple to construct, easily cleaned, and

may be reused indefinitely.

ment results from its application to a lower viscosity range (2 tt, 15 cen-

tipoise) than that for which it was designed.

cations of the Hlanufacturer's design were necessary.

will be discussed in the section on instrument calibration.

However,

The spindle, the only part of

The principal disadvantage with this instru-

Thus, a number of modifi-

These modifications

For measurements with the fluorides, the spindle was connected to the

motor by a long, linked drive shaft. This isolated the delicate mechanism

of the instrument from the extreme temperatures at the top of the furnace.

A shiny metallic reflector, placed just beneath the motor housing, served

as additional thermal protection for the motor.

field in operating position in the drybox is shown in Figure 1, and a photo-

graph of the spindle is presented in Figure 4.

A photograph of the Brook-

r 4 II)

Page 22: AEC RESEARCH ENT REPORT

-17-

Centering of the spindle i n the

and even temperatures throughout the

salt capsule,

en t i re sample

leveling of the motor,

of salt are a l l essen-

t i a l if accuracy is t o be obtained with the Brookfield.

the -tor causes bumpy, uneven rotat ion and a resulting error.

bulb on the motor housing provided a neans of avoiding this diff icul ty .

A uniform annulus was produced between the surface of the spindle and the

wall of the capsule by carefulLy adjusting the capsule t o an exactly ver t i -

c a l position, This m s done by placing a level on the machined top surface

of the capsule which extends out of t he furnace and making necessary adgust-

ments with the leveling screws on the furnace (see Figure 1).

vection was niniraized by adjustment of the "guard zone" heater.

Poor leveling of

A leveling

Thermal con-

Errors produced by ilaproper centering of the spindle result i n high

readings.

moving the spindle wfthin the capsule t o give the lowest consistent reading.

Once t h i s was done, only ve r t i ca l adjustments were made during the course

of the experimentalnieasurements over the complete temperature range so as

t o maintain the l iqu id l eve l a t the notch located on the spindle shaft.

This w&s necessary t o compensate f o r the expansion of the l iquid with in-

creasing teaperatwe.

It was therefore possible t o properly center the instrument by

The results obtained with the Brookfield viscometer a t a single t a p e r -

ature are highly reproducible.

even though the clutch is disengaged and the spring allowed t o completely

relax between readings.

Variation seldom exceeds + - 0.1 centipoises

The Brookfield instrument Eased is designated Model LVF by the m u -

f a c k r e r a It has four speeds: 60, 30, l2, and 6 rp. Only the 30 rpm

Page 23: AEC RESEARCH ENT REPORT

-18-

speed was used in this progrr~m.

lence in the lower viscosity liquids.

Operation at 60 rprn resulted

The apind2.es used were

*;

in turbu-

modified

to give a larger shear surface than those provided by the Iganufacturer.

This m s done by doubling the spindle length while maintaining the stme

cylinder diameter.

Q ,

Page 24: AEC RESEARCH ENT REPORT

L 9 - 1E- :b

Il'?Smm CALIBRATION

The viscosities of nearly all fluoride mixtures of practical interest

fall between 2 and 15 centipoises over the pertinent temperature range.

Since the minhanm full-scale reading of the Brookfield viscometer as manu-

factured was 100 centipoises, it was clear that its use in an absolute

manner would result in readings of only a few per cent of full scale and

would introduce large errors.

modify the instrument to produce a higher reading at a given viscosity and

then carsfully calibrate the modified instrument i n liquids of known pro-

perties.

cometers as it ma found that the capillaries were not bored with sufficient

precision to allow theoretical determination of their characteristics;

calibration curves were found to vary substantially between cups. The

following paragraphs will describe the development of the calibration tech-

niques presently used.

To avoid this pitfall, it was necessary to

It was also necessary to calibrate the individual capillary vis-

Early Brookfield measurements were made at 60 rpm using a spindle

identical io geometry with the lowest range spindle provided by the manu-

facturer. This spindle was cylindrical, having an B.D. of about 3/4 inch

and a length of about 2-3/4 inches.

made from 1-1/2 inch, Schedule 40 I .P.S. pipe.

in a series of glycerol-water solutions having the proper viscosities, and

a calibration curve of Brookfield reading versus actual viscosity was plotted

from the data. Capillary viscometers were also calibrated in these solutions

and the reslllts were plotted in the form: kinematic viscosity in centistokes

The salts were contained in a capsule

Calibration was carried out

Page 25: AEC RESEARCH ENT REPORT

-20- $A.

versus time of efflux in seconds.

their viscosities were determined in 0stwkd.d viscometers in a constant temper-

ature bath.

of 1-1/2 inch pipe to reproduce the annulus in the salt capsuJ.e. However,

these solutions were somewhat disadvantageous in that they were subject to

property changes due to evaporation m d those of lower glycerol concentration

had a tendency to grow molds. In an, effort to avoid these disadvantages, a

series of pure alchols were tried in place of these solutions and used with

some success.

These solutions were easily prepared and

The solutions were kept in wide-mouth jars containing a length

The results obtained on fused fluorides wlth the two separate instru-

ments calibrated in this way differed substantially.

30 per cent were found, and it was noted that the Brookfield readings in-

variably were high.

liquid around the Brookfield spindle by operating it in a dilute solution

of Milling Yellow MGS, a commercially available dyestuf"f having double re-

fracting properties. Lines of &rain ana consequently, flow patterns, are

visible in this liquid when viewed with polarized light, Fortunately, solu-

tions in the concentration range exhibi%ing this effect also had viscosities

i n the desired range.

about the same geometry as the 1-l/2 inch pipe used for the salt capsules

and i n the calibrating liquids.

Deviations up to

A visual study was made on the flow patterns of" the

The solution was held in a g l a s s container having

Turbulent cells were observed between the*spindle and c~~p6u.l.e surfaces

when the instrument was operated at 60 rpm.

2 to 4 times more dense than the dye or calibrating soLutions, the Reynolds

Since the fluoride melts were

Page 26: AEC RESEARCH ENT REPORT

-21-

modulus in the annular region between the capsule and the spindle was 2 to 4

tiaes higher in the salts than in the calibrating liqulds.

this turbulence would be even more pronounced in the salts.

As a result,

In view of these observations, a number of modifications were made in

The speed of rotation was reduced calibration and operation procedures,

to 30 rpan, and the length of the spindle was doubled to compensate for the

loss in shear resulting from this reduction in speed. Further, the salt

capsules were constructed of one-inch Schedule 40, I.P.S. pipe to reduce

the thickness of the salt annulus. The net result of these changes was an

increase in the shear, and hence larger in$tnarment readings. At the same

time the turbulent flow cells were eliminated. The effect of a reduction

in annul= tHickness in a rotational viscoaeter on the critical speed, or

speed at which vortices begin to form, can be determined from the following

relation for rotational viscometers with the outer cylinder stationary':

where

U = critical speed at which vortices begin to be produced

R1 = outer radius of annulus

R2 = inner radius of annulus

t = R1 - R2 = thiCknFSS of annulus

v = kinematic viscosity of liquids.

Solving equation (1) using the dimensions of the one-inch capsule and a

kinematic viscosity of one centistoke (the lowest value usually encountered

in measurements on fluorides) ylelded a critical speed of 58 qm. Thus,

Page 27: AEC RESEARCH ENT REPORT

-22 -

operation at 30 rpm assured lminar f l a w in this capsule.

was solved using the same kinemtic: viscosity and the dimensions of the

1-3-12 inch capsules, a critical speed of 13 r p was obtained.

fore likely that considerable turbulence existed in the salt in the 1-1/2

inch capsules, ptieularly at the operating speed of 60 r p ,

was solved far v using the dimensions of the large capsule and a value of

4.64 centistokes was indicated as the minimum viscosity which could be

measured with laminar f low at a spindle speed of 60 ~pm,

studied in this program have viscosi%ies less than 4.64 centistokes.

When equation (1)

It was there-

The equation

Most of the salts

Since the nature of flow is a func%iola of density as well as viscos-

ity, a search was made to find calibrating liquids ha7Jing both densities

and viscosities comparable to fPuorides.

s-tetrabromoethane, were found t o have suitable properties.

liquid principally used, is a fused salt mixture having the composition:

NaE\T02-NaM0 -KNO

air, and melts a% 142’6.

1.965 gus/cc at 160’6 to a b u t 1.79 &cc at kOO°C.

from about 14.5 centipoises at B60°C $0 about 2 centipsises at 400°C,

Density-temperature and viscosity-taperatwe ewves for HTS are given in

Figure 6. Regular checks were easily and precisely made on, the viscosity

of the samples of HTS used for calibration in an Ostwetld viscometer sus-

pended in a bath of HTS.

Two liquids, HTS’O and

HTS, the

40-7-53 weight $ o It is noncorrosive, easily handled in

The density of this mfxture varies from about 3 3;

The viscosity varies

Both instruments were calibrated in this liquid using a capsule and

Measurements were furnace identical with those used with the fluorides.

made at several tmperetttepes, and calibration curves were plotted in a

m@ .;$$ 0

Page 28: AEC RESEARCH ENT REPORT

-23-

18

16

14 F I- cn 0 0 cn

0

-

5 - c

2

4

2

0

UNCLASSIFIE ORNL-LR-DWG 19837

2 .05

100 150 200 250 300 350 TEMPERATURE ( " C )

&Pi$. ,,* &;-

Fig. 6. The Densi ty and Viscos i ty of IIHTS".

1.85 6 0

i.75

4 0 0

Page 29: AEC RESEARCH ENT REPORT

-24-

manner similar to that described in conjunction with the glycerol solution

calibrations.

it reduced the already small error resulting from the slightly different

dimensions of the instruments in the glycerol solutions at room tempera-

ture and the fluorides at high temperatures.

Use of this salt mixture had the additional advantage that

The other calibrating liquid, s-tetrabromoethane, is a heavy, highly

toxic, organic halogen compound having a room temperature density of

2.964 gm/cc.

poises at 20'~ t o about 3.8 centipoises at 65Oc .

curves for this liquid may be found in Figure 7.

out in this liquid by containing it in one of the capsules used for the

fluorides and supporting this capsule in a constant temperature bath.

liquid was used less frequently than HTS because of its toxicity

The viscosity of this liquid varies from about 11.5 cemti-

The viscosity-temperature

Calibration was carried

This

11 . A complete calibration curve was detemined for each new cup o r spindle

before it was put into use. After each set of measurements on a fluoride

mixture, two or three recalibmtion points were made to insure that the in-

strument had not been altered during use. Representative calibration curves

fo r the Brookfield and capillary visconeters are shown in Figures 8 and 9,

respectively.

field reading to viscosity becomes: constant at 1-1/2.

Above a reading of about 10 centipoises, the ratio of Brook-

The changes made in the use of the Brookfield, coupled with the furnace

design employing two elements and the use of calibrating liquids of higher

density, have

two different

virtually eliminated the earlier poor agreement between the

viscometers. The results with the two instruments now agree

Page 30: AEC RESEARCH ENT REPORT

-25-

U N C L A S S I F lED ORNL-LR-DWG 19838

14

12

IO

8

6

4

2

0 0 10 2 0 30 40 50

TEMPERATURE ( " C ) 60 70

5

4

3

2

Fig. 7. The V iscos i ty of s -Tet rabromoethane.

Page 31: AEC RESEARCH ENT REPORT

0 2 4 6 a 10 12 14 16 2 0 BROOKFIELD READING ( c e n t i p o i s e s )

U N C L A S S I F I E D ORNL-LR-DWG 49839

I h) OI I

Fig. 8. Brookfield Viscometer Calibration Curve .

Page 32: AEC RESEARCH ENT REPORT

7.0

6.0

- 5.0 v) Q) Y 0 v) c c 0)

+ .-

2 4.0

k >- cn 0 0 cn 5 3.0 0 l- a E w z y 2.0

-

-

1.0

0 0

CUP NO. 22 (INTERMEDIATE RANGE) CAPILLARY DIAMETER = 0.039 in. I

2 0 40

-I- +

I UNCLASSIFIED

ORNL-LR-DWG 19840

r' CAPILLARY DIAMETER = 0.033 t in. CUP NO. 41 (LOW RANGE) I

Y I 0 ORIGINAL CALIBRATION I

I

T 100 120 140 160 180 2 0 0 60 80

TIME OF EFFLUX ( s e c )

Fig. 9. Capil lary Viscometer Calibrat ion Curves.

Page 33: AEC RESEARCH ENT REPORT

- -28-

to within + - 10 per cent. taken after this technique developaent program had been completed and the

changes instituted .

A11 of the data presented in this report were

Page 34: AEC RESEARCH ENT REPORT

-29-

EXPERIMENTAL RESULTS

r--- Experimental viscosity measurements have been made on 36 fluoride

mixtures.

BeF2, ZrF4, UF4, and ThF'b.

the ANP project at the present time is I?aF-ZrF4-UF4, seven binaries and

ternaries from this system have been studied.

50-46-4 mole $) is presently being planned for use in the ART.

The constituents of these mixtures were NaF, LiF, KF, RbF,

Since the system of principal interest to

Mixture 30 (NaF-ZrFk-UF,+;

This mix-

ture will be formed in the reactor and the reactor made critical by the

addition of Na2UF6 (mixture 43) to NaZrF (mixture 31). 5 I - Conaiderable interest has been shown in mixtures in the ITaF-LiF-BeF2-

Up4 systa.

excessive amounts result in very high viscosities, the other properties

Although the proportion of BeF2 must be somewhat limited as

of many of these mixtures make them highly desirable fo r reactor appli-

cations. Measurements have been made on several mixtures at this labora-

tory, and the viscosity program of Blanke, et al, at Mound Laboratory

has been devoted almost entirely to an extensive and complete examination

12

of this system.

Another mixture which has attracted considerable attention is the

eutectic of KF, LiF, and NaF' known as Flinak. This salt has the most de-

sirable combination of physical properties, including viscosity, of any salt

studied to date. However, its use has been limited because of associated

corrosion problems. Measurements are reported on Flinak (mixture l2) and

on two fuels formed by the addition of varying amounts of UF4 to Flinak

(mixtures 14 and 107). !g :%

Page 35: AEC RESEARCH ENT REPORT

-30-

In addition to the mixtures from

others from various systems have been

these three systems, a number of

studied a8 part of a continuous pro-

gram devoted to finding the optimum fused fluoride mixture for use in re-

actor work . viscosity standpoint.

* Mixtures containing RbF show considerable promise from a

Table I presents the viscosity data on the mixtures which have been

studied to this time. Mixture numbers, compositions in mole per cent,

liquidus temperatures, and viscosities in cenkipoises at 100 C intervals

are given.

0

Equations for the viscosity in the form

are given for liquids where the experimental data when plotted as log p

versus l/T(OK) yields a straight line. The initial reference is also given.

Nearly all of these measurements have been previously reported in memos and

quarterlies; all except Mos. 117, 118, and 119 may be found in the recently

published physical properties sutma~y . This summary report supplies the data in engineering units as well as centipoises and also provides kinematic

viscosities in CGS and engineering units.

13

The accuracy of these aeasurements is indicated by the agreement between

values obtained with the two completely different viscometers described in

the experimental section; one of these instruments involves flow through a

* A tabulation of all the mixtures that have been formulated to date within the A m project may be found in reference 13. This tabulation is complete except for mixtures 117, 118, and 119, which are given here and any compo- sitions which may have been m e d since this report u&s written.

- 4 t

Page 36: AEC RESEARCH ENT REPORT

.

TABU I

"HE VISCOSITIES OF FLUORIDE MIXTURES STUDIED TO DATE

Composition (Mole $I) Liquidus Viscosity (Centipoises) Temp. p = Ae B/T('K) Initial C '500 '600 '700 '"800 '"9 A B Ref.

Mixture NaF LiF XF RbF BeF2 ZrF4 m4 ThF4 0

2 12 14 20 30

31 33 35 43 44

45 70 72 74 78

81 82 86 87 88

90 95 96 97 98

46.5 11.5 46.5 10.9 44.5

5.0 50.0

50.0 50.0 57.0 66.7 53.5

53.0 56.0 20.9 38.4

69.0 56.0 16.0

22.0 55.0 20.0 55.0 32.0 35.0

64.0 5.0

49.0

53.0 24.0 49.0 36.0 56.0 21.0

26.0 42.0 43.5 52.0

27- 5

1.1 43.0 46.0 4.0

50.0 25.0 25.0

43.0 33.3

40.0 6.5

47.0

35.7 5.0 39.0 5.0

31.0 28.0

23.0

29.0 4.0 21.0 4.0

48.0 48.0 4.0 31.0

1 5 0 . 0 36.0

23.0 15.0 20.0 3.0

50.0 46.0 4.0

530 454 452 42 5 520

510 610 360 66 5 540

520 530 4 9 505 478

570 545 445 425 555

555 500 535 597 505

17.3 9.2 4.75 8.8 4.6 io. 5 6.1

8.5

8.4

12.8

8.5

7.5 8.1

20.0 9.9 7.5 6.0

12.0 12.0

20.5 10.5 7.1 7.1

8.0 7.05 5.9 5.65 7.3

9.8 2.9 2.75 4.1 5.4

5.2 8.5 7-0

10.25 5.7

4.6 5.2 6.0 4.9 4.0

7.0 7.0 6.45 4.65 4.75

5.0 4.35 4.1 3.95 4.6

6.3 4.35 1-95 1.85 3.1 3.7

3.45 5.0 3.5 4.25 7.0 5.15 4.2

3.2 3.6 4.25 3.45 2.85

4.45 4.45 4.55 3.3 3.4

3.4 2-95 3.0 2.95 3.1

0.0767 0.0400 0.0348 0.161 0.091

0.0709

0.0346

0.194 0.181

0.104

0 . ~ 8 0.111

0.585 0.0585

0.116 0.138

0.0811 0.0657 0 157 0.173 0.0737

4731 4170 4265 3171 3895

4168

5164 3927 3302

3798

3486 3624

4647 4647

3590 3435

4008 4081 3168 3043 4012

1 5 16 16 17 18

19 1 w P

14 20 1

21 13

13 22 23 l2*, 20 l2*, 24

25 25 26 27 12*, 28

29 27 29 30 30

&* &fTurements were made by B. C. Blanke a t Mound Laboratory as w e l l as by the authors. Results were in satisfactory agreement. Ave age values are listed.

Page 37: AEC RESEARCH ENT REPORT

f ' .3

TABU?, I (Continued)

THE VISCOSITIES OF FLUORIDE MIXTURES STUDIED TO DATE

Composition (Mole $) Liquidus Viscosity (Centipoises) Temp. p = Ae C '500 '600 '700 '800 '1900 A B Ref. Mixture NaF LiF KF RbF EkF2 ZrF4 UF4 ThF4 0

100 40.0 60.0 652 3.2 2-35 0.116 3225 1 4 104 43.0 57.0 475 9.0 4.5 0.0212 4678 27

113 50.0 50.0 380 15.3 8.4 5.25 0.0493 5009 31

107 11.2 45.3 41.0 2.5 4 9 5.1 3.0 0.0292 4507 16 1I.l 71.0 16.0 1.0 12.0 13.0 7.1 4.8 0.0620 4666 13

114 50.0 50.0 445

116 79.0 21.0 730 117 5.0 54.5 34.5 6.0 545 118 44.5 15.0 34.5 6.0 540

115 50.0 50.0 400 15.3 6.7 3.45 0.00517 6976 31 I

w 10 11.5 5.2 2.75 0.00534 6701 13

8.0 4.8 3.3 32: 7.5 4.75 3.5 32

2.2 0.0770 3600 29 I

119 37.5 9.5 47.0 6.0 540 9.5 5.2 3.5 32

&* P .*

I .

Page 38: AEC RESEARCH ENT REPORT

-33-

. capillary and the other is concerned with shear in an anrnulus with the inner

cylinder rotating.

+ 10 per cent of the true value.

An error analysis indicates %ha.t the results are within

- Measurements were made on all of the salts reported here except those

containing 13eF with both of the instruments previously described. Salts

containing BeF2 were studied with only capillary viscometers in a separate

drybox facility built for this purpose from a 55-galLon drum.

capillary viscometers were used in studying each beryllium salt mixture to

furnish a check.

2

Two or three

!Phe agreement between cups was within + PO per cent. -

Page 39: AEC RESEARCH ENT REPORT

-34-

CORRaATIONS

One of the purposes of any experimental program is the development of

correlations based on the experhuelatally determined data.

describe the behavior of the materials studied and, if possible, serve as a

basis for prediction of the properties of similar materials.

attempts have been made to correlate the viscosity data obtained in this

program, and these attempts have not been without some degree of success.

However, because of' the complex nature of the phenomenon of fluid viscosity,

these correlations cannot be depended on for predicting the viscosities of

mixtures far from the measured compositions.

the various trends observed in the data.

These correlations

Several such

They do serve to illustrate

Before describing the correlations which have been developed, the ob-

served trends in the data w i l l be discussed.

of the fluorides are fond to be a function of the fluid density and molec-

ular weight.

behave in this manner.

correlation does not hold.

amounts of BeF2, the least dense of the fluorides studied, exhibit very high

viscosities.

responding BeF2-free mixtures, and the introduction of amounts of BeF2 in

excess of 30 - 40 mole per cent results in very sharp increases in viscosity.

Blard~e~~ obtained a reading of about 9 0 centipoises on NaF'-BeF2 (21.9-78.1

mole 8) at 60OoC.

planation of the high viscosities of BeF2-containing mixtures.

In general, the viscosities

This relationship is as predicted since most classes of liquids

However, for some mixtures of fluorides this general

For example, mixtures containing appreciable

Mixtures containing BeF2 have much higher viscosities than cor-

The fact that pure BeF2 is a glass provides a partial ex-

Page 40: AEC RESEARCH ENT REPORT

-35-

Another pronounced trend which has been noted involves the relative

effect of each alkali fluoride on the viscosity of a mixture. It was found

that the viscosity of a fluoride mixture w i l l decrease as the lower molecular

weight alkali-metal fluorides are replaced by those of higher molecular weight.

Thus, the viscosity of a RbF-containing mixture w i l l be considerably lower

than that of a prototype mixture containing EiF in place of the RbF.

These trends can be seen in Figure 10 in which the viscosity at 700°C

of each salt is plotted as a function of its room temperature density. The

room temperature density values were calculated from the mixture composition

using the equation:

1 P = N

where :

p = density at room temperature of the mixture ( d c c )

M. = molecular w e i g h t of a component of the mixture

= mole fraction of that component fi

= density at room temperature of that component (gm/cc). Pi

1

Values obtained from this relation represent well the room temperature experi-

mental values.

liquid densities of the fluoride34 mixtures.

This equation was used in the correlation for predicting the

An average line drawn through the non-BeF2 points on Figure 10 indicates

the trend of the relationship between density and viscosity. The two extremes, -

Page 41: AEC RESEARCH ENT REPORT

-36-

! NON-BeF2 MIXTURES

0 ORNL-LR-DWG 19844

+ 3 0 O/O

.

2 . 3 2.5 3.0 3.5 4.0 4.5 5 .O 5.5 CALCULATED ROOM TEMPERATURE DENSITY ( g / c c )

Fig,&. Viscos i ty a t 700°C vs. Ca lcu la ted Room Temperature * Densi ty .

Page 42: AEC RESEARCH ENT REPORT

-37-

mixtures I 2 and 43, are the lightest and densest salts, respectively, that

are likely to be encountered in non-BeF2 fluoride mixtures.

with the exception of two mixtures, the data f a l l within + - 30 per cent of this average line.

BeF2 are above the + 30 per cent line and that the viscosities of the BeF2

salts vary as their BeF2 content over the concentration range (15 to 50 mole

per cent) studied.

It is seen that,

Figure 10 also shows that all of the uixtures containing

The relative effect of the various alkali fluorides on the viscosity is

indicated in Figure 10, Mixtures 81, 82, 86, and 72, which are considerably

above the average line, are zirconium-base fuels containing LiF as the prin-

cipal alkali fluoride, Salts 87, 95p and 117, which fall somewhat below the

average line, are zirconium-base fuels comt;etinirpg rubidium as the alkali flu-

oride.

similar mixtures containing HaF.

The mixtures of intermediate viscosity, such as 30, 44, and 70, are

A l l of tbese trends are substantiated by a correlation resulting from

a statistical treatment of the data. This approach was based on a number of

empirical equations cited by Hatscheka5 relating $he viscosities of nixtures

to their coanpositions.

ideal mixture should be additive.

The simplest assmp%fon is that %he viscosity of an

T'h.Ls,

where p is the viscosity

components, and x is the

CL = CLp + P2 0 - x> (4)

of the mfxture, pl and p are the viscosities of the

mole fraction of one o f the two conaponents. Binghm

2

stated that the reciprocal of viscosity, the fluidity (a), was additive. Thus,

. , ,;A i

(B = "x + e2 (1 - x> (51 -

Page 43: AEC RESEARCH ENT REPORT

m -38-

Arrhenius proposed the purely empirical function,

log p = x

Kendall and Monroe found for some mixtures of nonassociated

(6)

liquids that

From these empirical equations and the observed data trends, a corre-

lation based on equation ( k ) , assuming the viscosities of the fluorides to

be approximately additive, was indicated.

represented by the equation

The viscosity

+ ~ H ~ H p = p f f p f f ...... A A B B

of the mixture was

(8 )

where p represents the viscosity of pure component A, f is the mole frac-

tion of that component, and so forth, for the eight components. A matrix

containing as its elements the mole fractions of the components in all the

mixtures studied along with the viscosities of the mixtures at 6OO0C, 700 C,

and 800°C was programmed for the ORACLE.

three temperatures for the viscosities of the pure components.

understood that these "pure component viscosities" are merely empirical rep-

resentations for use in this relationship since the pure components are not

liquids at these temperatures.

temperatures using the same matrix along with the viscosities expressed as

log p and as fluidity, or l/p, as in equations (5) and (6). Comparison of

experimental and calculated viscosities using equations (4) , (5), and (6)

indicated that the three correlations were of about equal merit.

A - A

0

Solutions were obtained at the

It must be

Solutions were also obtained at the three

1 A &

Page 44: AEC RESEARCH ENT REPORT

-3.9-

. However, the degree of correlation was only fair. Viscosfties ealcu-

lated by this correlation for four salts at 7OO0C differed from the experi-

mental values by more than 20 pes cent.

experimental and calculated viscosities at 7OO0C for all of the mixtures

The average deviation between

studied was approximately 10 per cent. It must be concluded, therefore,

that this correlation would not be a safe basis for predicting the viscos-

ities of new mixtures. The "pure component viscosities" obtained fron the

ORACLE for the equation involving linear additivity, the simplest of the

three functions tested, are found in Table 11.

mental and calculated viscosities at 7OO0C based on this function is given

in Table 111.

A comparison of" the experi-

Another correlation which may be applied to the experimental results

involves the relationship between fluidity and the number of "holes" in a

liquid.

as has been postulated by E y r i ~ ~ ~ , it is reasonable to assme that the

fluidity of a liquid will be proportiom1 to the number of holes,

If holes must be present in a liquid before flow can take placep

Ira addi-

tion, the essential difference between a solid and a liquid m y be regarded

as the introduction of holes. If V is the molar volume o f +&e l i qu id and

Vs is the molar volume of the unexpanded solid, the difference, (V - Vs), is proportional to the number of holes and, hence, to the fluidity. Since

the fluidity is the reciprocal of the coefficient o f viscosity, it follows

that C

p = v - v s 37 where c is a constant. This equation was originally proposed by Ea$schiaaaki .

and foyd to hold for a large number of nonassoeiated liquids.

-7

Page 45: AEC RESEARCH ENT REPORT

-40-

.

TABLE I1

"F'URE COMPONENT VISCOSITIES" BASED OM EQUATION (8)

"Pure Component Viscosity" (Centipoises)

Component 600°C 700Oc 8OO0C

(A) - 1.33319 0.414287 0 495901

LIF (3) 8.58465 5 27885 3 38107

KF (c> 1.03168 0.367723 0.332103

RbF (D) - 2.90961 - 1.43543 - 1.93418 BeF2 (E) 27.3054 13.4185 8.10863

ZrF4 (F) 15. ig88 g.og101 6,54347

uF4 (a 60.9819 31.2966 200 5855

m 4 (E) 16.0516 7 9 43398 7.46834

.

Page 46: AEC RESEARCH ENT REPORT

T A B U I11

COMPARISON OF EXPERIMENTAL VISCOSITIES AT 7OO0C

AND PREDICTED VALUES MSED ON EQUATION (8 )

Viscosity at 7OO0C, Centipoises Per Cent Mixture Experimental Predicted Deviation

*

2 I 2 14 20 30

31 33 35 43 44

45 70 72 74 78

81 82 86 87 88

90 95 96 97 98

9.8

2*75 4.1 5.4

2.9

592 8.5 7.0

10.25 5.7

4.6 5.2 6.0 4.9 4.0

7.0 7.0 6.45 4.65 4.75

5.0 4.35 4.1 3.95 4.6

8.89 2.66 2.90 4.12 5.64

4.75 10.30 6.01

10.70 5.89

4.49 5.34 6.92 7.80 4.83

5.09 6.15 5.87 4.93 4.69

5.09 4.71 4.57 4.12 4.96

9$ 84 5%

4$ 0

* Per cent deviation is defined as (difference/experimental) x 100.

Page 47: AEC RESEARCH ENT REPORT

-42 -

TABU I11 (Continued)

COMPARISON OF MPERIMENTAL VISCOSITIES AT 700°C

AND PREDICTED VALUES BASED ON EQUATION ( 8 )

Viscosity at 7oo0c, Centipoises Per Cent

Mixture Experimental Predicted Deviation *

100 3.2 3.33 4qh, 3.0 3.37 12% 107

111 7.1 7.10 8.4 6.92 18%

3% 113 114 6.7 6.89

0

5.2 4.8 4.75 5.2

5.99 4.25 4.98 6.17

IC Per cent deviation is defined as (diff erence/experimental) x 100.

Page 48: AEC RESEARCH ENT REPORT

-43 -

This relationship was applied to the experimental data on fluorides

reported here, and the results are shown graphically in Figure 11. The

tern p in the equation is the viscosity at 70OoC, V is the molar volume

or reciprocal of

ciprocal of the density at room teaperatwe calculated from equation (3 ) .

Experimental values are used for the liquid density where available; cal-

culated values are used in the other instances.

sity at 70OoC, and Vs is the molar volume or re-

Although the points shown on the figure exhibit considerable scatter,

the hyperbola described by the equation can be discerned. In contrast to

the density-viscosity trend shown in Figure 10, this relationship appears

to correlate the data f o r liquids containing BeF2 as well as for the

non-BeF mixtures, However, the BeF -bearing liquids studied have contain-

ed only moderate proportions of this constituent. Calculations using some

of the data taken at Mound Laboratory on liquids containing enough BeF2 to

sharply increase the viscosity* result in greatly increased scatter.

2 2

Some of the scatter shown in Figure U. is probably due to the error

limits to which the experimental and predicted data are subject.

it is safe to assume that most of the divergence encountered with this

correlation, as well as with the others described, is due to factors such

as the general complexity of the viscosity phenomenon and the wide varia-

tion in the physical nature of the fluoride mlxtures.

However,

Page 49: AEC RESEARCH ENT REPORT

t u

-44-

.

0.12

0.10

0.08

9 I x 0.06

3 0.04

0 BeF2-BEARING SALTS

0

0

0 2 4 6 8 10 12 VISCOSITY AT 700°C (cent ipo ises)

Fig. 1 1 . Viscosity at 700°C vs. ( 1/7000c - 4 ) .

Page 50: AEC RESEARCH ENT REPORT

-45-

1.

2.

3.

4,

5-

6.

7-

8.

9.

10.

11

12.

13

14.

1 5

16.

&ox, F. A., and Kertesz, F., AMP Quarterly Progress Report f o r Period Ending September 10, 1951, Om-1154, p. 136.

Redmond, R. F., MW Quarterly Progress Report f o r Period Ending June 10, 1952, - ORNL-l29h, p. 124.

Cisar, J. M., ibid.

Tobias, M., AMP Quarterly Progress R e p o r t fo r Period Ehding December 10, 1951, om-1170, p. 124.

Knox, F. A., and Kertesz, F, , ANP Quarterly Progress Report fo r Period Ending September 10, 1952, ORNL-1375, p. 145.

Redmond, R. F., and KapW, S, I., "Remarks on the Falling Ball Viscometer, '' ORWL CF 53-1-248, January 14, 1953.

Cohen, S . I., ANP Quarterly Progress Report f o r Period Ending December 31, 1956, ORNL-2221, p. 228.

Cohen, S . I., and Peele, J. PI., "Determination of the Opt imum Procedure f o r Obtaining Ine r t Atmospheres i n Non-Vacuum Dryboxes," ORNL CF 55-10-132, October 26, 1955.

"Modern Developnents i n Fluid Dynamics," V O ~ . 11, pp. 388-390, Oxford Press, Oxford, (1938).

Kirst, W. E., Nagle, W. M., Csstner, J. B., "A New Heat Transfer Medim fo r H i g h Temperatures, " Trans. AIChE, 36, p. 371, (1940).

New York, (1951). Sax, N. Irving, "Handbook of Dangerous Materials," p. 5, Reinhold,

Blanke , B. C., MLN CF 55-U-14, Novernber 7, 1955+

Cohen, S. I., Powers, W. D., a d Greene, M I D., "A Physical Property Summary for ANP Fluoride Mixtures," OFEG-2150, August 23, 1956.

Cohen, S. I., ANP Quarterly &ogress R e p o r t for Period Ending

Cohen, S . I., and Jones, T. E., ORNL CF 55-4-32, April 1, 1955.

December 10, 1955, OW-2012, p. 180,

Cohen, S. I., and Jones, T. N., ORJXL CF 56-5-33, W Y 9, 19569

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-46- jcr

REFWWCES (Continued)

17.

18.

Cohen, S. I., and Jones, T. N., ORML CF 55-2-20, February 2, 1955.

Cohen, S, I., and Jones, T. MI, OF@& C F 56-4-148, April 17, 1956.

19. Cohen, S . I., and Jones, T. I?., O m CF 55-12-128, Decenber 23, 1955.

20.

21.

22.

Cohen, S . I., and Jones, T. N., ORNL CF 55-2-89, February 15, 1955.

Cohen, S . I., and Jones, T. N., ORWL CF 55-3-137, March 16, 1955.

Cohen, S . I., and Jones, T. N., ORNL C F 55-9-31, September 6, 1955.

23. Cohen, S. I., and Jones, T. ll., ORNL C F 55-3-61, March 8, 1955.

24.

25.

Cohen, S. I., and Jones, T. N., ORNL CF 55-5-59, May 16, 1955.

Cohen, S . I., and Jones, T. N., ORNL C F 55-5-58, May 16, 1955.

26. Cohen, S. I., and Jones, T. N., ORNL CF 55-7-33, July 7, 1955.

27. Cohen, S. I., and Jones, T. N., ORmL CF 55-11-27, November 4, 1955.

28. Cohen, S. I., and Jones, T. M., ORNL CF 55-8-21, August 1, 1955.

d

29. Cohen, S. I., and Jones, T. N., ORNL CF 55-u_-28, November 8, 1955.

30. Cohen, S . I., and Jones, T. N., ORNL CF 55-12-127, December 23, 1955.

31. Cohen, S. I., and Jones, T. N. , ORNL C F 55-8-22, August 1, 1955.

32. Cohen, S. I., and Jones, T. N., Unpublished data.

33. B l a n k e , B. C., KLM CF 55-10-34, October 24, 1955.

34. Cohen, S. I., and Jones, T. N., "A Summary of Density Measurements on Molten Fluo,ride Mixtures and a Correlation for Predicting Densities of Fluoride Mixtures," ORwL-l7O2, July 19, 1954.

35. Hatschek, Rnil , "The Viscosity of Liquids," pp. 135-139, D. Van Mostrand, London, (1928).

36. Glasstone, S., Laidler, K. J., and w i n g , H., "The Theory of Rate Processes, " p. 481, M c G r a w - H i l l , New York, (1941).

37. Batschinski, A. J., Z. physik Chem,, 84, p. 643, (1913).

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