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177

Thermal Properties of High Alumina Refractory Mortars Modified With

Lanthanide Chemical Admixtures

THOMAS NOVINSON Naval Civil

Engineering

Lab

Port

Hueneme, California

HEINZ F. POPPENDIEK Geoscience Ltd Solana

Beach, California

(Received September 16, 1986) (Revised November 17, 1986)

INTRODUCTION

I T

IS OF interest to

study

the thermal

insulating properties

of certain

chemically

modified high

alumina

refractory

mortars because of their

potential

use as heat

resistant

insulating

liners for

portland

cement concrete structures

exposed

to heat

in the range from 500 to 1000 ° F

Conventional alumina refractories are heat cured in

place,

in

engineering

ap-

plications [1].

This is not a

problem

for

refractory

liners

prepared by gunning

onto the interior steel surface of a furnace or a kiln. For

lining

pcc,

however,

this

is a

problem

since flame heat

curing

of the

refractory

liner is

likely

to

damage

the

underlying

concrete meant to be

protected.

For this reason, a

variety

of chemical

modifiers,

known as &dquo;admixtures&dquo; have been

investigated

to lower the cure

temperatures

of conventional refractories.

Among

the chemicals

reported

in this paper are various derivatives of the lanthanide

elements, lanthanum, cerium, neodymium

and

praeseodymium, plus

the

closely

related but non-lanthanide element zirconium. The lanthanide com-

pounds

were chosen for

potential

flux

properties,

that

is, ability

to lower the

fusion

point

of alumina

[2].

The unmodified controls and modified

(chemical admixtures)

refractories were

heat cured and tested for cold

crushing strength following

the ASTM C133-82a

procedure [3].

Plots of

strength

vs.

temperature

were made to determine

physical

behavior at elevated

temperatures.

Then thermal

properties, including

thermal

conductivity, specific

heat and thermal

diffusivity,

were

measured,

to ensure that

insulating properties

had not

changed

for the modified materials.

Journal

of

COMPOSITE

MATERIALS,

Vol.

22 -February

1988

0021-9983/88/02 0177-15 $4.50/0

(2)

178

EXPERIMENTAL

Crushing Strength

Measurements

Mortars were

prepared

from 1000 gm of

high

alumina calcium aluminate cement

containing

bauxite

aggregate, plus

150 ml of water

(15

%

by weight)

con-

taining

0

(control,

no

admixture), 1 % , 5 %

and 10 %

by weight

of each chemical admixture. The

refractory

mortar was cast in the

shape

of 2

by

2

by

2 inch cubes.

The cubes were moist cured 24 hours at

95 % humidity

and 75 ° R Then the molds

were

stripped

and the cubes were

slowly

baked in an oven at 220°F to remove

water. The

cubes,

which were allowed to cool to room

temperature,

were then heated in sets of

three,

to

temperatures

of

500,

750 and 1000°F The cubes were

again

cooled to room

temperature

and were crushed with a Tinnius Olsen test machine. The cold

crushing strengths

were then recorded. The results can be

seen in

Figures

1 and 2.

Thermal

Conductivity

Determinations

The thermal

conductivity

is defined

by

the Fourier’s

equation,

where

q = heat flow rate k = thermal

conductivity

t =

temperature

y = distance

along

heat flow

path

A = heat transfer area normal to the heat flow

The

guarded

hot

plate apparatus (ASTM C-177) [4]

was used to make the ther- mal

conductivity

measurements.

Figure

3 illustrates the

major

elements of the

system.

Heat from a

central,

flat

plate

heater flows

through

two hot

plates, through

two test slabs to two

cooling plates.

The

temperature

differences across

the two test

samples

are determined from

thermocouples

that are embedded in the hot and cold

plates

or in the test

samples.

As shown in the

figure,

the central heater is surrounded

by

a

guard

heater. A

thermopile

is

positioned

between the central hot

plates

and the

guard

hot

plates.

At

steady

state, when the central heater and

guard

heater have been

adjusted

so that the

thermopile output

is very small

(yielding

unidirectional heat

flow),

a data set is obtained. From a heat balance on the

system involving

heater power

inputs,

heat transfer areas, tem-

perature

differences and

sample thicknesses,

the thermal

conductivity

can be

determined.

Specific

Heat Determinations

One convenient way of

measuring

the

specific

heat of cementitious materials is

by utilizing

a

gradient layer

calorimeter. The elements of such a

system

are shown

(3)

179 Figure 1. Comparison of crushing strengths of unmodified alumina refractory and

refractory

doped with 1 % lanthanide compounds.

(4)

180

Figure 2. Comparison of crushing strength of alumina refractories with 1 % lanthanum

phosphate

and cerium oxide.

(5)

181

Figure

3. Guarded hot plate (twin plate) thermal conductivity system.

in

Figure

4. A test

sample

is

positioned

inside of the heat flux

measuring envelope

that is housed in a fluid cooled heat sink. The heat sink in turn is sur-

rounded

by

thermal insulation.

This calorimeter is based on the

principle

that all of the heat flow into or out

of the calorimeter must pass

through

its walls where the

temperature gradient

sensors are located.

Therefore,

the calorimeter

envelope integrates

the total heat flow in the

system

on an instantaneous basis. The calorimeter walls consist of

special

thermoelectric heat flux transducers* that

yield

a DC

voltage output

*A heat flux transducer is composed of a thermopile system that has &dquo;hot&dquo; junction sets at one depth within the

sensor and &dquo;cold&dquo; junction sets at another depth

(6)

182

signal.

The calorimeter walls are thin so that low time constants are involved. As heat flows

through

the

walls,

a small

temperature

difference

directly proportional

to the heat flow is

developed.

In a

properly designed calorimeter,

the

output sig-

nal is affected

only by

the rate of the heat flow.

The utilization of the calorimeter to measure the

specific

heat of a material is done as follows: An unloaded calorimeter that has come to thermal

equilibrium

at

temperature level t1

is

suddenly exposed

to a new

temperature level,

t2. The heat flow trace as the transient process

proceeds

from the initial

steady

state con-

dition to the final

steady

state condition can be obtained with a

recording poten-

tiometer. The area under this curve is

equal

to the heat added to or extracted from the calorimeter and its liner for the

superposed temperature perturbation. Next,

the calorimeter is loaded with the

specimen

to be

investigated

and

again exposed

to the

original temperature tl

and allowed to

equilibrate.

Then the loaded calorimeter is

suddenly exposed

to the new

temperature

datum t2, allowed to reach

equilibrium

and the

corresponding

transient heat flow trace recorded. The

area under this curve is

equal

to the heat added to or

given

up

by

the

calorimeter,

its liner and the

specimen.

Subtraction of the areas under the two transient traces

yields

the desired heat flow for the

specimen

alone. The trace area is related to an energy flow per unit time

by

means of an accurate resistance

heating

calibra-

tion for the calorimeter. The

specific

heat for the

specimen

is obtained from the

Figure

4. Elements of a gradient layer calorimeter system.

(7)

183

Figure 5. Thermal diffusivity measurement apparatus.

classical definition

(heat

transferred divided

by

the

product

of the mass and tem-

perature perturbation).

The

defining equation

for the

specific heat, c,.,,

is

where

q(O)

= time

dependent

heat flow

through

calorimeter when loaded with test

sample

q(6)e =

time

dependent

heat flow

through

calorimeter without the test

sample

0= time

0,=

the

equilibrium

time

period (no

further heat

flow)

ms = mass of the test

sample

tl = initial

temperature

datum

t2 = final temperature

datum Thermal

Diffusivity

Determinations

If it is desired to measure the thermal

diffusivity directly (rather

than

by

mak-

ing

the individual

property

measurements and

substituting

them into the

defining

(8)

184

property ratio),

it is necessary to work with a

time-temperature

solution of a clas- sical

boundary

value

problem

where transient heat transfer is in

operation [5].

A

typical example

of such a

system

is a slab that is

suddenly

cooled at both sur-

faces

by

forced convection

cooling. Symbolically,

the functional

relationship

of

the variable can be

expressed

as,

where tc, to

and t,

are the

centerline,

surface and initial

temperatures,

respec-

tively,

yc, is the

product

of the

specific

heat and the

density

and h is the surface heat transfer conductance.

The surfaces and centerline

temperatures

of the slab are measured as a function of time

during

the

step

function

cooling (see Figure 5).

From such data and the mathematical

time-temperature

solution for this

boundary

value

problem,

the

thermal

diffusivity

can be deduced.

Figure

6. Refractory mortar at 100 x magnification. F = flint

clay,

M = matrix area,

P = pore.

(9)

185

Figure 7. Refractory mortar with 1 % cerium oxide at 100 x magnification. F = flint clay,

M = matrix area, P = casting pore, C = cerium oxide.

RESULTS AND CONCLUSIONS

Representative samples

of the control

(refractory

without

admixture)

and 1%

cerium oxide

doped

mortar cubes were vacuum

impregnated

with an epoxy

pot- ting compound.

The cured cubes were then machine

polished,

first with diamond

grit

down to 1 ¡.tm, then with alumina

grit

down to 0.05 ¡.tm. The

samples

were

then viewed at several different

magnifications (40X, 100X,

and

200X)

for the

petrographic analysis. Photomicrographs

were taken with a Polaroid camera at- tachment. Photos at 100X are included in this paper

(Figures

6 and

7)

to illustrate

major findings.

Samples

of 8

refractory

mortar

cubes, including

one control

(no admixture)

and one

1 %

cerium oxide

doped

mortar, were examined under

high magnification using

an ISI

(International

Scientific

Instruments) scanning

electron

microscope (SEM).

The

samples

were

chipped

off the corners of the

refractory

mortar

cubes,

mounted on carbon blocks with a

special graphite adhesive,

and

placed

in an

analysis

chamber. The

samples

were

sputtered

with

gold

for

high

resolution. The chamber was

placed

under vacuum and the

samples

were scanned with x-rays for the SEM

pictures (recorded

with a Polaroid camera

attachment)

shown in

Figures

8 and 9.

Samples

of the control

(without admixture)

and 1 % cerium oxide

doped

refrac-

tory

mortar cubes were

pulverized

to - 325 mesh and

chemically analyzed using

x-ray diffraction

equipment (Kevex).

Chemical

analysis

of the mineral

phases

of

(10)

186

Figure 8. Refractory mortar before finng (75°F), at 500 x magnification.

Figure 9. Refractory mortar after firing (to 700°F) and cooling, at 500 x magnification.

(11)

187 the mortars verified the existance of cristobalite

(Si02),

mullite

(AI6Si2013)’

and

gehlenite (Ca,A1,SiO,), plus

some calcium aluminum

hydroxides

that could not

be identified. The mineral cerianite

(Ce02)

was also identified in the 1 % cerium oxide

doped samples.

No other cerium

compounds

were identified in the

doped refractory.

The cerium oxide did not

chemically

react with the

components

of the cements, since inclusions of cerianite were the

only

identifiable cerium com-

pounds

observed in the x-ray diffraction

experiments. However,

the

petrographic analysis

at 100X

magnification (Figures

6 and

7) definitely

show a difference in

casting density,

that

is,

the cerium oxide

doped samples

are denser than the

undoped

control

refractory

cubes.

Perhaps

cerium oxide acts as a

superior

fine

aggregate

to

replace part

of the aluminum oxide

(bauxite). Unfortunately,

a

similar

study

on the lanthanum oxide could not be

performed

due to time and

funding

limitations.

Lanthanum

phosphate

may

actually undergo

chemical reaction with some of the other mortar

components, however,

because

(a)

this salt is somewhat water

soluble

compared

to the insoluble lanthanide oxides and

(b)

the curve for

strength

vs.

temperature (Figure 1)

for lanthanum

phosphate

is much

steeper (hence greater strength)

than that for the lanthanum oxide

doped refractory

mortar.

Another reason for the observed

strength

increases may be due to

physical changes

in the

refractory

microstructure caused

by

the lanthanide

compounds.

Figure

8 shows the surface of the alumina

refractory

at 500X

magnification

before

firing.

The surface appears like a series of

pottery

cups or vases. After fir-

ing

at 700

degrees,

the surface

changes,

as illustrated in

Figure 9,

and the

frag-

ments appears to have melted or

annealed,

thus

forming

a denser material. The cerium oxide may have aided in the densification of the material at this

tempera-

ture,

although

it is unclear as to

why

the

strength

decreases between 700 and 1000

degrees.

It should be noted that the

peak

in

strength

is

reproducible

and was

observed in

laboratory experiments

both at NCEL and at National

Refractory

and

Minerals

Corp.

This

strange

increase in

strength

at 700

degrees

was also noted

with

refractory

cubes

containing

1 % of certain

zinc,

barium and strontium salts

(results

to be

published

at a later

date).

Refractory

mortars

containing

1 % cerium oxide exhibited the

greatest

cold

crushing strength throughout

the range of 500 to

1000 ° F,

with an unusual

peak

or increase in test

strength occurring

at 750 ° F. Lanthanum

phosphate (1 % )

also

produced

a substantial increase in

strength

for the

refractory

mortar in the range of 500 to 1000 ° F The other lanthanide

oxides, neodymium

and

praseodymium,

had little or no effect or

actually

decreased the

strength

of the heated mortar. The zirconium oxide showed

only slight

increases in

strength

when added in

1 % ,

5 %

and 10 %

by weight

increments to the calcium aluminate mortars.

The thermal

conductivity, specific

heat and thermal

diffusivity

vs. densities are

recorded in Tables

1,

2 and 3. In the case of thermal

conductivity,

the data

points

shown in Table 1 indicate that this

property

increases

slightly

with increases in

weight

concentration of the mortar

additive,

as shown for

ZrSiO3.

The thermal conductivities of solid materials are controlled

by

two

primary

mechanisms, namely,

lattice vibrations

(atomic motions)

of the material and free

(12)

188

Table 1. Thermal

conductivity

measurements for mortar with various additives.

Table 2.

Specific

heat measurements for mortar with various additives.

Table 3. Thermal

diffusivity

measurements for mortar with various additives.

(13)

189 electron flow or the electronic

component.

In the case of cementitious

type materials,

thermal

conductivity

is

primarily

controlled

by

the lattice vibration mechanism.

Generally,

one cannot

predict

thermal conductivities for such materials from first

principles.

It is

possible,

however to

predict

the

equivalent

thermal

conductivity

of a mixture of

components

if their thermal conductivities and volume or

weight

fractions are known. The

following equations

illustrate

how such

predictions

can be made.

If the

components

of a mixture were

arranged

in &dquo;n&dquo;

adjacent

slabs with heat flow

along

the

lengths

of the

slabs,

the classical

expression

for the effective or

equivalent

thermal

conductivity, keq,

is

where

~y =

density

of the

composite

material

kn

= thermal

conductivity

of the nth

component

wn =

weight

fraction of the nth

component

yn =

density

of the nth

component

If the

components

of such a mixture were

arranged

in

adjacent

slabs with heat flow

perpendicular

to the

lengths

of the

slabs,

the classical

expression

for the

equivalent

thermal

conductivity

is

For the case of one

component (small particles) uniformily

distributed in a

second

component (the carrier)

the

equivalent

thermal

conductivity (as proposed by Eucken) is

where

k~

= thermal

conductivity

of the carrier

kp

= thermal

conductivity

of the

particles

b = ratio of

particle

volume to total volume

a =

3/(2

+

kpkc)

The Eucken

equation

is valid in the range 0 < b < 0.5.

(14)

190

On the basis of the small

percentages

of admixtures

present

and on the basis that the thermal conductivities of the

components

are all of the same

order,

it can

readily

be shown from the three

equations

shown above that

only

small

changes

in thermal

conductivity

occur

(as

found

experimentally)

for the mortars contain-

ing

the admixtures used in this

study.

The

specific

heat measurements for the mortars

containing Zr02

and

ZrSiO3

illustrate the fact that the

product

of the

specific

heat and the

density

is approx-

imately

a constant.

From the classical oscillator

theory,

it can be shown that the

specific

heat of a

material is relatable to the number of

degrees

of freedom of the molecule in- volved and the universal gas constant. Such an

expression

can be used to estimate

the

specific

heat of some materials.

Dulong

and Petit related

specific

heats of

metal to their atomic

weights.

More

complicated

materials like the cementitious materials

being

considered in this

study

are more difficult to evaluate on first

principle

bases. It is

possible, however,

to describe the

equivalent specific heats,

c, , of such materials in terms of the

specific

heats of the individual

components

and

their

weight fractions, namely

where

w&dquo; = the

weight

fraction of the nth

component

C’n = the

specific

heat of the nth component

Calculations can be made for the

specific

heat of a mortar

containing

an admix-

ture,

using

the mixture

equation given

above.

Again,

because of the small admix- ture

percentages involved,

one can show that the

predicted changes

in

specific

heat are small as a result of the admixture

additions,

as found

experimentally.

The thermal diffusivities were found to be very

nearly

a constant

quantity

for

all admixtures measured. This result is

apparently

related to

corresponding changes

in thermal

conductivity

and the

product

of

density

and

specific

heat as

the

compositions change.

It has been shown that small

percentages

of admixtures which

significantly

influence the

strength

of

refractory

mortars, did not

significantly

affect the thermal

properties.

Analysis

of these data indicates that the refractories

doped

with

1 %

lanthanide

oxides differ little from the unmodified

refractory

mortar control. This informa- tion is

promising

in that it demonstrates that

insulating properties

of the modified mortars were not lost in those cases where the lanthanide oxides

imparted

in-

creased

strength

to the heated refractories.

ACKNOWLEDGEMENT

Funds for this work were

provided by

the Naval Facilities

Engineering

Command, Alexandria,

and the Office of Naval

Research, Arlington, Virginia.

(15)

191 The authors wish to thank the materials science

engineering

technicians at NCEL for assistance in

preparing

the mortar

cubes, plates

and other

specimens,

the

ceramic

engineering

research staff of National Refractories and

Minerals, Pleasanton, California,

for modulus of

rupture (cold crushing) data,

and

Geoscience staff members for their assistance in

making

the thermal

property

measurements.

REFERENCES

1. American Concrete Institute "Refractory Concrete," Special Publication SP-57, Detroit, Mich.

(1978).

2. "The Lanthanides," Chap 31, pp. 870-891 in Advanced Inorganic Chemistry, A Comprehensive Text, F. A. Cotton and G. Wilkinson, eds. New York, NY:Interscience Publishers (1962).

3. American Society for Testing and Materials, Philadelphia, PA (1982).

4. Annual Book of ASTM Standards, Part 18, Philadelphia, PA (1981).

5. "Heat Transfer Notes," L. M. K. Boelter, V. H. Cherry, H. A. Johnson and R. C. Martinelli, eds.

Chapter 1, University of California Press, Berkeley and Los Angeles (1946).

References

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