Diffusion of carbon in alpha iron

Diffusion of carbon in alpha iron

DIFFUSION OF CARBON C. G. IN ALPHA IRON* HOMAN? The diffusion of carbon in alpha iron using a tracer technique was performed in the temperatur...

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DIFFUSION

OF

CARBON C.

G.

IN

ALPHA

IRON*

HOMAN?

The diffusion of carbon in alpha iron using a tracer technique was performed in the temperature range of 616°C to 844°C. 9 plot of the In D versus l/T in this temperature range deviates from the usual straight line behaviour. An empirical model which includes the possibility of a carbon-vacancy interaction is proposed to explain this deviation.

DIFFUSION DU CARBONE DANS LE FER ALPHA L’auteur Btudie par une technique de traceur, la diffusion du carbone dans le fer alpha pour une gamme de temp6ratures s’6tendant de 816°C it 844°C. la relation ln D = f(l/T) ne poss&de pas les caract&istiques Dans cette gamme de tempkratures, d’une droite. Pour expliquer ce r&,ultat, l’auteur propose un modAle empirique qui fait intervenir la possibilite d’une interaction entre les atomes de carbone et les lacunes. DIFFUSION

VON

KOHLENSTOFF

IN

ALPHA-EISEN

Die Diffusion van Kohlenstoff in alpha-Eisen wurde im Temperaturbereich 616°C bis 844°C mittels Trilgt man In D gegen l/T auf, so erhtilt man Abweichungen vom einer Isotopentechnik verfolgt. Zur Erkliirung der Abweichungen wird ein empirisches Model1 vorgeschlagen, iiblichen linearen Verlauf. das die Miiglichkeit einer Wechselwirkung zwischen Kohlenstoff und Leerstellen einschlieot.

agreement

INTRODUCTION

By implicitly

assuming that every diffusional

made by carbon performed

atoms in an alpha iron matrix

with identical

local surroundings,

perature

jump was

Wert’l’

of our results with the previous high temresults of Smithc4) indicated

extrapolation questionable. The implicit

from

low

that a linear

temperature

assumption

made

data

by Wert

was

may

be

was able to derive an elegant theory based on a simple random walk model. This model leads to an

correct for low temperature

studies in pure iron, but

expression

it is perhaps not completely

accurate in the tempera-

for the diffusivity characterized by a single parameter 7. Wert was able to qualitatively

relaxation fit experimental

data representing

approximately However, which

fourteen

the low

has been

decades

not be extrapolated

of

An empirical

diffusivity.

Furthermore,

data, could

atoms could have two different surrounding

data(3$4) at

anelastic

techniques(5)

result of an extremely

of carbon

a t’racer

technique

simple single relaxation

to examine

model and to provide

of t’his investigation

showed

with

a

st)raight

line.

Furthermore,

neighbor

iron sites is

The agreement of this model with the low temperasmall, is assured. However,

and room pressure

was impossible to fit the high temperature

configuration

exist on all the nearest neighbor

ture results,(2) where the population

was to redetermine

in order

configu-

vacant.

the anomalous

a zero that

of vacancies

A calculation

it

diffusivities quantitative

indicates

is

at the higher temperature,

the proposed model includes the possibility vacancy interactions.

the

point for a high pressure diffusion experiment. The results

The first one is the normal

is when one of these nearest

iron by

small pressure effect.

the diffusirit)y at high temperature

in

in which the moving carbon

sites of the carbon atoms and the second configuration

of the pressure

in alpha

have indicated

The purpose of this experiment using

rations.

where iron atoms

recent measurements

iron

of carbon

experimental

to the experimental

on t’he diffusion

model for the diffusion

determined,c2)

the high temperature. effect

neighbor

sites to a diffusing carbon atom may be vacant. alpha iron was developed

t,emperature

quant.itatively

measurements of the

ture range where one of the nearest

based on this model

a high temperature

of carbon

(Appendix

A)

pressure effect on the

diffusivity

of carbon in alpha iron proportional

activation

volume of formation

to the

of vacancies.

THEORY

* Received, Janua,ry 20, 1964; revised February 20, 1964. Submitted to the Physics Department, Rensselaer Polytechnic Institute, Troy, N.Y. in partial fulfillment of the requirements

In developing an empirical model for the diffusion of C in a-Fe which would include the possibility of

of the lMast)er of Science degree. ‘j’ Work performrad at Watervliet York.

vacancy-carbon interaction, the following conditions.

ACTA

METALLURGICA,

VOL.

Arsenal,

Watervliet,

12, SEPTEMBER

1964

New

1071

it is necessary

to satisfy

SCT_4

1072

1. The

diffusivity

independent

carbon

in

alpha

iron

is

derived

with

from

changes

of

VOL.

3. A good empirical

the model vacancy

should

be

fit be obtained

range.

x exp -

equation

diffusion couple

-

I = erf “-z.

i

‘22/m

tracers are used, equation

(2) may

2 22/11)t

+%&+?x])~~ ‘c

in the free state; (All energies carbon

atoms

the

(6) v2

vacancy

concentration

in atom

percent *B -

?,=6:exp

E,,

RT

(

(7

i

where E,, is the energy of forn~ation of a vacancy.

The

radioactivities

to CO, C,, and C$. Therefore,

effe&ive

formulated

diffusion

coefficient

De

may

be

to be:

from a

plot of

De = (1 -

qP,

+ rlD,

(8)

where erf-l

~oncentratioll

(9)



it is possible to determine

if D is independent

and if this is true,

its value

of the at the

annealing temperature.

is the diffusivity

II,=

The :proposed reaction is c+v+c...v The forward

reaction

atom

assumed

requires the presence of a free

bimolecular

(Experimental

(3)

(C) and a “free” and

evidence

carbon-vacancy

hence,

also suggests

The reverse reaction

differential

vacancy

governing

(V), and is

second

with unpaired motion

Ds,exp-

unimolecular.

The

this model is :

From

anelastic

the concentration

vacancy

concentrations,

respectively.

and

If one

g

relaxation

(19)

measurements,

of vacancies

D, = 0.008 exp -

where

is negligible’s’

19,800 cal/mole

(11)

)

RT

i

And for the case when q < I; (q < 1O-2 at SO%.) ,__ _^_ _, . I 19,WO cal/mole 6V1 ~... .0.008 exp -+

i

where C,, C, and C, are the pair, total carbon

of

where E,, is the motional energy of the carbon atom when paired with a vacancy.

order.

this assump-

requires only a paired

and is assumed

equation

associated

a carbon atom and for the other eon~guration,

B ~on~e~tr~,t~o~ sf ~r~or~-~~~~~e~ pa+s

total

of E,,,

C. Effective difSusion coeficient

where oO, ab and a, are the measured

tion.ti))

frequencies

con~gurations;

energy for a carbon

or expressing on the

t,o read 1 = erf-

carbon

in t,he two

At equilibrium, the ratio of paired to total carbon concentration, rj, is

tration at distance x from the interface.

corresponding

(5)

“)

and B is the binding energy of tOhepair.

high and low side of the couple and C, is the concenIf radioactive

atom

(2)

where (7, and CO are the initial concentrations

be modified

(Em;,

(I) can be shown to be S6)

C, c,

C?,v,

are expressed in kcaljmole.) of the concen-

In the case of a semi-infinite

C 2 _-5 ( c;, -

the carbon

(I)

D is independent

the solution of equation

-

!

where y1 and V, are the vibrational the motional

!z.=Dazc at ax2

tration.

(

E *g

for measured

Pick’s second law of diffusion may be written as:

when t,he diffusivity

(4) ma,y be written:

dC -2 = Gv,C,C, exp clt

concentration

over the entire ~m~)erature

A. Solution qf d$usion

1964

assumes that the carbon atoms are the more mobile

at different temperatures. diffusi~ities

12,

defect, then equation

of carbon concentration.

2. Equations consistent

of

METALLURGICA,

B ex!?

!

E”,, RT

RT

E,,

1

,

y2

112)

HOMAN:

A plot

D,)

of In (11, -

literature

value

vs.

l/T

DIFFUSION

together

OF

with the

of Bc8) and Efvcg) should

yield

the

value of [SCv,/v,) D,,] and E,,.

C IN

ALPHA

evacuated

2 ,u, radiomethane

to about

mitted

to a pressure

vessel

was

sealed.

A. Counting An

procedure

end

GM.

PROCEDURE

window

tube

(window

was mounted

thickness

as shown

1 mg/cm2)

in Fig.

1.

This

fixture insured constant geometry for surface counting sample

ends.

The

counting

end shield was concentric diameter for

of 0.120 in.

counting

counting

geometry was

chi-square

tests.

in the aluminum

with the samples and had a

The V block held the samples

and grinding.

equipment

port

The reproducibility

and the reliability

checked

of

of the counting

periodically

by

means

of

Cylinders

of 0.187

in. dia. and from

99.98%

18 in. long

were

zone refined

iron

machined

stock.oO)

The cylinders were then etched in a solution

of 10 g of oxalic acid, 20 cc of 30 ‘A hydrogen peroxide 300 ml

of

H,O

at 45°C

0.020 in. were removed

until

approximately

from the diameter

and the

surface was very bright and shiny. The cylinders

Carbon

was deposited

surface

heating

with

by

approximately

burized

vessel

the gases remaining and cylinders

furnace

which

to be carburized

Mettler

Grammatic

microbalance

quartz

carburizing

vessel.

were weighed on a

After

and placed the

in a

vessel

was

butt

in an

The car-

and shiny

to determine

to insure a uniform

The uniform

welding,

cylinder

to

in the vessel,

were placed

were bright

were reweighed

gain and counted tribution.

furnace

at 750°C for 72 hr.(l”)

cylinders,

appearance,

induction

The temperat’ure was t)hen raised to 850°C for about

90 min. After evacuating annealing

an

in the

on the cylinder

500°C for 30 min.

of the cylinder

the entire

of the methane

concentrations

cylinders.)

tion treatment.

carefully

and

pressure

different

was ad-

cm of Hg and the

in

the weight carbon

dis-

count rate of a cylinder

was

between 50 and 200 cpm depending

Sample preparation

B.

of 0.5-4.0 (The

was varied to obtain EXPERIMENTAL

1073

Fe

The diffusion in a helium

to a carburized

on the carburiza-

couple was formed

atmosphere, cylinder

by

a pure iron

(using

a special

fixture and after suitably preparing the weld surfaces). The weld was made amperes load.

through

The time

Metallographic

by passing

3-5

pulses of 900

the sample under a small pressure of a pulse never examination

exceeded

of similar

5 sec.

cylinders

of

Armco iron welded with the same procedure indicat,ed good

welds with no discernible

entrapments

at the

interface. Since this diffusion experiment high pressures,

a new technique

sample was developed.03)

will be extended

Because

the

(1) the solubility

of Carbon in Cu is low,(14) (2) the diffusivity a-Fe is low with respect to the diffusivity Feo5) and (3) Cu is an extremely

to

to encapsulate

of Cu in of C in a-

good “getter”

of O,,

it was decided

to plate the diffusion couples with 0.003 in. of Cu. After a diffusion anneal, it was possible to remove part of the copper oxide layer to obtain a bright Cu color. The solubility of C in Cu was GM END

qualitatively

investigated

C. Diflusion

anneal

by a counting

technique.

‘WIN”C)ul .. ..__.. COUNTING

A temperature 05°C GM TUBE SUPPORT

control

over the sample length of

at 725°C during a diffusion anneal was possible

by means of a diffusion furnace and controller. temperature

fluctuations

during

the

measured by means of a chromel-alumel ENDWINDOW SHIELD AND COUNTING PORT V-BLOCK

of counting

assembly.

The were

thermocouple

imbedded in the Cu heat bath of the diffusion furnace. The thermocouple potential was measured with a L&N K-3 potentiometer against a cold junction of glycerine in a dewar. The chromel-alumel couple was calibrated

FIG. 1. Schematic

anneal

before and after a diffusion run with

a Leeds and Northrup standard Pt-Pt 10% Rh thermocouple using an ice bath cold junction. The

1074

ACTA

METALLURGICA,

temperature of the cold junction was measured with a ~alibrate~l thermometer. The sample was inserted into the furnace with a chrome]-alumel thermocouple welded to the low activity side of the couple. Measurements of the heating time of this thermocouple as compared to the furnace thermocouple indicated that a maximum time of 1 minute was needed to heat from 0.8 T, to TD for diffusion runs lasting from 60 to 90 min. After the anneal, the sample was quenched within 10 set to R.T. The data has not been corrected for the heat-up time.

The sample was mounted in the V block and the Cu plating was removed from the end with a precision surfacegrinder. The grinder has an accuracy of 0.0001 in. and produced a #lS finish on the sample end. Sectioning and counting from the high carbon (activity) end showed that the original cpm measured before the anneal could be obtained within 0.005 in. of the end. This result qualitatively confirmed the fact of the extremely low solubility of C in Cu. At least three sections were made to within 0.2 in. of the weld to be sure t,hat the concentration in the carburized portion of the sample was uniform after the anneal. All samples reported in this paper were within 1 “/;; of the original value of a0 determined before the anneal in this region. The penetration was measured from this point. For samples #I & #lo, every section was counted for at least 10,000 counts; samples fA, 2A. 3A, 5 and 7 have at least three

VOL.

12,

1964

sections counted for at least 10,000 counts; and for sample #6, every section was counted for at least 3,000 counts. Background measurements were made periodically during the counting procedure and varied between 23.4 and 24.3 over several months of counting. A summary of experimental data has been tabulated in Table #I. TABLE 1. Diffusion annealing data -. ._ -

z.-. Couple no. 1 1A 2A 2B 3A 5 6 7 10

&vt.y$J

a0 iwm)

(%!

0.022 0.022 0.021 0.021 0.009 0.006 0.006 0.006 0.008

191 191 184 184 80 55 53 52 209

721.0 f 721.0 f 732.0 * 732.0 * 730.9 & 814.9 + 823.5 & 616.0 * 844.2 i -

tn x 10s sec. 0.3 0.3 0.3 0.3 0.4 1.0 1.0 0.3 1.0

4.56 4.56 4.20 4.20 3.60 3.54 4.08 5.40 3.60

RESULTS

A. Measurement of Dexp. Figure 2 is a typical penetration curve which was obtained from the measurements of the activity of Sample #l after a diffusion anneal of 76 min at 721.0%. If one plots (erf)-r

% ~ a0 -

‘b

%

vs. distance

from the interface on probability paper, the data may be fit with a straight line. Results of this experiment, some of which are plotted in Figs. 3-8 indicates that in the ranges of carbon concentration and temperature st,udied the diffusivity is independent of carbon

HOMAN:

DIFFUSION

OF

C IN

THE

ALPHA

1075

Fe

99.99

ox-(lb (lo-oh

98

9e

95

95

yo

90

ox-Ob (lo-(lb

e.

so

70

70

60

60

50

50

40

40

30

30

20

20

10

10

5

5

2

2

98

9.9

95

95

90

so

80

80

70

70

60

60

50

50

40

40

30

30

20

20

10

10

5

5

2

2

1

-30.0

-15.0

DISTANCE

FIG. 3.

0.0

FROM

I5.0

INTERFACE

( lu3

Probability plot of (a, - ab)/(q, from weld: sample #lA.

-60

30.0

-

a,) vs. distance

9999

3A

FIG. 5.

t20

0.0 FROM

WELD

(1631N.)

Probability plot of (a, - ab)/(rzO from weld: sample #5.

ub) vs. distance

99.99

99 99

DC*

6

To=730.9+.4”C

To =823.5

to=3.6Xl03sec

1D =4.OBXlO3sec

Cl4

IN

Ci41N

w-Fe

D = Ii 6 X10-’

i

I.O°C

d-Fe

D = 4 7.1 X 10-7cmz/sec

cm2/sec

98

96

95

95

90

90

80

80

‘0

70

70

70

60

60

60

60 50 40

a*-Ob oa-Ob

-20 DISTANCE

99.99

DC#

-40

IN.)

50

98

98

95

95 90

-90 armgo

80

50

M

40

40

‘la

30

30

30

30

20

20

20

20

10

IO

10

5

5

5

2

2

IO

5t-+

2

-80

-60

DISTANCE

FIG. 4.

-40 FROM

-20 WELD

(10-31N.)

Probability plot of (a, - aJ/(aO from weld: sample #3A.

0.0

+10

’ q,) vs. distance

-80

-60

DISTANCE

-20

-40 FROM

WELD

(lO-3

0.0

+10

IN.1

FIG. 6. Probability plot of (a, - ~+,)/(a,, from weld: sample #6.

aa) vs. distance

1056

ACTA

99 99

DC*

METALLURGICA,

1

7

VOL.

99 99

12.

1964 99.99

99.99

To =616.0-+0.5°C to=5.4x103 set C’41Noc-Fe D= 2.36X IO-‘cm hec

=644.2f

D =62.0 98

98

95

90

90

8o

EO O_

70

‘0

ao-(lb

60 50 40

60 50 40 30

30

20

20

10

IO

5

5

2

2

I

WELD

( lCj3

IN.)

Fro. 7. Probability plot of (a, - aa)/(ao from weld: sample #7.

concentration.

Table

experimental

#2

values

I*

is a summary

of all the

of the diffusivities of the diffusivity

the temperature

to study

pre-exponential

determined

activation

of carbon

indicates

(D, Hence

studied

a subsidiary

0.0

WELD

(lO-3

+20

IN.)

to

(B -

be

2.2 cm2/sec

Efv -

E,,)

to

and

the

be 29,300

DISCUSSION

is not

A. Comparisovb with the results of other measurements

of the

Comparison

two

Rewriting

plot was made of

diffusivities

good

competing equation

Figure

mechanisms

10

RT

3.

Summary

to x 103 SW

Couple no.

carbon indicate

effect,

if any, is not detectable.

Most

for

C-14

of the low temperature a quenching

approximately

1

721.0 * 0.3 721.0

f

0.3

4.56 4.56

+0.044 +0.032

;?q 3A 5 6 7 10

732.0 730.9 814.9 823.5 616.0 844.2

f & * + + +

0.3 0.4 1.0 1.0 0.3 1.0

4.20 3.60 3.54 4.08 5.40 3.60

-0.035 10.063 +0.060 +0.060 + 0.080 +0.045 +0.100

c, -

cbt

c0 -

cb

0.850 0.800 0.820 0.200 0.950 0.860 0.850 0.988 0.88*5

erf l#J

diffusion

technique

0.700 0.600 0.640 0.600 0.900 0.720 0.700 0.976 0.770

4 0.733 0.595 0.647 0.595 0.617 0.831 0.733 1.596 0.849

7 x,

carbon. measure-

in the sample

of diffusion calculations

X* (in.)

It

that an isotope effect would yield

of diffusivities

ments involve

1A

* z is some arbitrary distance from weld. i_ Values determined from straight line fit at r. $ See appendix B.

616”C-

Smith’s14) work using nonradioactive

smaller than for the nonradioactive

(13)

range

of this data with

values

from Fig. 10, one may find the value of the TABLE

D values(314) indicate

temperature agreement

would be expected

(12)

reported

in the

The quantitative

that an isotope

are in

B - E,, - En%,

D,) == 6 ii D,, exp

agreement

844°C.

D, from low

measurements.@)

of the D, values obtained in this experi-

ment with previously

shown in Fig. 9 minus the

extrapolated anelastic

that

operation.

range

diffusivities

corresponding temperature

terms

energy

in

form as shown in Fig. 9. In order

this effect

the measured

-20 FROM

5

Cal/mole.

a plot

simple exponential

I

FIG. 8. Probability plot, of (a, - ab)/(aO - (lb) vs. distance from weld: sample # 10.

a*) vs. distance

alpha iron measured in this and other(3s4) experiments over

-40

DISTANCE

in this experiment. However,

I

I

-60

FROM

X 10-7cm%ec

98

95

DISTANCE

I.O’C

lo-’ 12.0 10.3 11.5 12.9 11.8 32.6 47.1 2.4 62.0

11 cm2/sec f i_ * k $+ + f i

0.6 0.5 0.5 0.6 0.6 1.6 2.4 0.1 3.1

HOMAN:

DIFFUSION

OF

The

C IN

proposed

formation abrupt

model

indicates

transition. magnetic

magnetically

the vacancy

changes

occurring

the

Curie

of a possibly

factor [6(v1/v2) Do,]

magnitude

of the

pre-exponential

several orders of magnitude normally

at

the mobility

by the that the

inert C-12 or C-14 atom.

B. Pre-exponential

DIcmt&,

that

One is led to speculate

may not influence

The

1075

Fe

energy of alpha iron is unaffected

magnetic point

ALPHA

measured.(2,3)

factor

is

greater than the value

However,

this value

is of

the same order for the Do of self-diffusion measurements in alpha iron. %lg) This would appear to mean

4 83 IO-

that

2

the

relaxation

mechanism

associated

of self-diffusion

with

the

partially

diffusion

influences

the

carbon mobility. If one accepts to estimate entropy

changes.

vJv2 would IO

proposed,

of the factor

A reasonable

probably

corresponding

IO-

the model

the value

be

it is possible containing

value

between

the

of the ratio

1 and

10, the

range of Do, being 0.37 too.037

cm2/sec.

This compares to a value for Do, of 0.008 cm2/sec. C. Activation 1.50

1.40

1.30

1.20

1.10

1.00

.90

.50

9.5 kcal/mol

FIG. 9. Plot of diffusivity vs. 103/ToK for carbon in alpha iron. A Chemical technique (Stanley); 0 tracer technique E] Phase boundary migration (Smith).

preparation

fraction

Depending

stage.

quenching

should

the dispersion the

-

B of a carbon

B) vacancy

may be assigned from radiation

pair of damage

individual

present at the quench tem-

be ‘(frozen”

effect of these excess vacancies in

the

energy (E,, + E,, energy

statisttics ; e.g., the quench rate, a certain

of the vacancies

perature

on

A binding

noticed

anelastic

annealing

into

by several

relaxation

technique

the lattice.

was

The

may be the cause of investigators(2J6)

measurements.

developed

by

lO-63

An

KW6)

2

to

eliminate this dispersion. It has been shown series

of

damaged carbon pair.

on

atoms

indicating

Furthermore, annealing

atom may encounter precipitation

iron

radiation

that vacancies

a binding

energy

G,)

trap

7 6

it was suggested in these radiation kinetic

studies

that

many vacancies

the

I 9 8

for the

5

carbon

4

on its way to a

site.

The smoothness the

et &.(7~8J7) in a

alpha

at low temperatures,

damage

over

by Damask

measurements

3

of the curves

temperature

range

in Figs. 9 and 10

6OO”C-850°C

implies

lO-7 2

that the diflusivity of carbon in alpha iron is unaffected by the magnetic change at 77O”C, the Curie temperature. This result is in striking contrast to the abrupt changes in the self-diffusion coefficientW in alpha iron, the diffusivity of nickel in iron,(l5) and the diffusivities of hydrogen in nickel which occur at the Curie temperature.

and iron@O)

I IO’

FIG. 10. Plot of De,,, alpha, iron.

-

D, vs.

/ To tl

103/ToK

for carbon

I

.

in

ACTA

1078

calorimetric

studies at Brookhaven;@)

value may be appreciably solution

does

not

either t,o previous of vacancy The

participate

in the

precipitation

microscopy

however, reaction

studies

by various

of the reaction.

at Brookhaven(17)

activation 10 kcal/mol. activation or vacancy

A

has been

investigators.(s~1a~~9) From the

of this experiment,

an upper

energy for the motion

of the

of the pair is about

This energy is sufficiently energies of motion

limit

of either

less than the

13, 1964

results.c5) equation

value for AV,,

is pressure

on a plot of In D, versus l/T

at high temperatures. be

The value

diffusivities

may

fit

expression.

An empirical

of the measured

with

a

model

which includes

of a carbon-vacancy

two

interaction

mechanism the

is proposed

to explain this deviation.

A possible counting bution rate.

error in the radioactive

low energy /3 particles of subsurface

The

(14)

l3, has been shown to be pressure independentc5) pressure independent,

to the surface

counting

thickness

of

count

b of

each

6

f0

n, exp - (FK) (LX

(171

where a, is the countrate measured at the surface due to the distribution

a, in the section.

If ,u is the bulk

then b will be in the order of the range

absorptivity,

of cc particles in the material. All the count rates measured in this experiment were looking

into a decreasing

the exception

gradient

of the a0 determination.

of activity, with In the extreme

gradient, is very

steep, our

the a0 determina.tion

would appear to be a

This error may be cxpressed

by

(8) may be rewritten

B, = D, + @, D,,,

technique

section can be expressed by the relation

However,

Y&,

in

is due to the contri-

activity

effective

volume effect.

Assuming

the decrease

B. Nonstatistical experimental errors

case where the activity

For the case 7 < 1, equation

then

a

Furthermore,

count rate would be due primarily to surface activity.

APPENDICES

4000 atm.

sensitive,

from

assuming

D, will be larger.

in alpha iron.

a straight line behavior

of 0.5 atomic volumes.

a, =

The diffusion of carbon in alpha iron deviates from

in D, is predicted

A 15 ‘A decrease

(16) at 82B’C and 4000 atm.

the carbon

CONCLUSIONS

possibility

T’OL.

if E,,

or to an insu&ieney

range of EfWfrom 29 kca,l/mol to 40 kcal/mol results

due

that the latter effect may be occurring.

suggested

this

higher if all the carbon in

traps at the temperature

electron

indicate

METALLURCICA,

B and E,,

to

to be

it is clear that

(18) for the conditions Using

of this experiment.

equation

(18)

we

= I -

2

may

write,

neglecting

background, X

erf --.2dtDe,,

2a exl,

a0 X

=

erf I___ 21/tD,,t

(19)

D exp I D,,t

(20)

or (15) under the conditions The room pressure values are indicated script 0. Integrating

by the sub-

one obtains

D,(P. 117) = D, + yoD,, exp -

of this experiment.

This effect has been investigated the diffusivity activity

side.

by redetermining

of sample #2B

looking

In this counting

situation

from the low (21)

D exp 2 Dact

The results of this determination indicate a diffusivity approxima~ly 10 % higher than the results of 3A. Another source of error is in neglecting to correct the diffusion time for the heat-up time. Such a correction In the low temperature region where D, 4 D, the model agrees qualitatively with the high pressure

would

any temperature. Comparison of

tend to increase the diffusivity all

the

errors

involved

in

at the

HOMAN:

measurement to

the

indicated

subsurface

that the constant

activity

contribution

OF

DIFFUSION

error due described

above is the largest, hence the reported limit of error

10.

reflects this uncertainty. ACKNOWLEDGMENTS

I would

like

to

acknowledge

many Prof.

helpful

Huntington

and to thank him for the encouragement

he provided to

colleagues

throughout

acknowledge at Watervliet

thesis

the

with

like

my

adviser,

discussions

this research. the

help

B.

I would also

received

Arsenal, especially

Cox for his aid and ideas,

H.

from

my

Mr. J. F.

REFERENCES

6. 7. 8. 9.

12. 13.

and Dr. L. Meisel and

Mr. J. Frankel for their discussions.

1. 2. 3. 4. 5.

11.

C. A. WERT, Phys. Rev. 79, 601 (1950). C. A. WERT and C. ZENER, Phys. Rev. 76, 1169 (1949). J.K. STANLEY, Trans. AIME 185,(1949). R. P. SMITH, Trans. AZME 224, 105 (1962). J. BASS and D. LAZARUS,J. Phys. Chem. Solids 23, 1820 (1962). Also A. ROSMAN et al.,Physica 23, 1001 (1957); Physica 26, 533 (1960). P. SHEL~MON,D@&on in Solids, Chap. 1. McGraw-Hill (1963). F. FUJITA and A. DAMASK, Acta Met. 12, 331 (1964). R. ARNI)T and A. DAMASK, Acta Met. 12, 341 (1964). H. BROOKS, Impurities and Zmperfections. ASM Monograph (1957). R. MEHI. et rtl., A& Met. 9, 256 (1961).

14. 15. 16. 17.

18. 19.

20.

C IN

ALPHA

Fe

1059

R. DOREMUSand E. KOCH, Trans. AZME 218,591(1960). E. SMITH, Indirect Observations of Imperfections in Crystals, p. 207. Interscience (1962). The Batelle Iron used in this experiment was provided through the kind offices of J. W. Halley, Chairman of the Pure Iron Subcommittee of the American Iron and Steel Institute Research Committee. The analysis provided is Al-15 ppm; 0-5 ppm; Co-5 ppm; Cu-7 ppm; Ni-20 ppm; P-9 ppm; Si-10 ppm; C-10 ppm; O-10 ppm; N-2 ppm; S-18 ppm. Other metallic impurities were not detected. The radioactive methane used to carburize the specimen was purchased from two soumes, Tracerlab and Nuclear Chicago. The activity of the three ampules used was 4.9, 2.0 and 2.0 mc/mM. See L. 8. DARKEN, in Atom Movements. SSM Monograph (1951). The author is indebted to Prof. F. Lenel, Rensselaer Polytechnic Institute, for suggesting this method of reducing decarburization effects. M. HANSEN, Constitution of Binary Alloys, 2nd edition, p. 353. McGraw-Hill (1958). C. J. SMITHELLS Metals Reference Book, 3rd edition, Vol. 9. Butterworths (1962). T. S. Kfi Metals Tech. T.P. No. 2370 (June 1948); Phys. Rev. 74, 9 (1948). H. WAGENBLASTand A. DAMASK, J. Phys. Ch,em. Solids 23, 221 (1962). H. WAGENBLAST,F. FUJITA and A. DAMASK, Actu Met. 12, 347 (1964). D. LAZARUS, in Solid State Physics, Vol. 10. Academic Press (1960). R. BORG and C. BIRCHENALL, Trans. AZME 218. 980 (1960). P. BUFFINGTON,K. HIRANO and &M.COHEN, Actn Met. 9, 434 (1961). See F. N. RHINES, in Atom Novem7nt.v. 8SM Monograph (1951).