7
ISIJ International, Vol. 35 (1 995). No, 1 1, pp. 141 5-1421 Assessment of the Mobilities ot Cr. Fe and Ni in bcc Cr-Fe-Ni AlloYS Bj6rn JONSSON Department of Materials Science and Engineering. Division of Physical Metallurgy. Royal Institute of Technology. S-1 OO 44 Stockholm, Sweden. E-mail: [email protected] (Received on March 2. l995, accepted in final form on May 26. 1995) Experimental data on the diffusional mobilities of Cr, Fe and Ni in bcc Cr-Fe-Ni alloys are assessed by means of a model which takes the effect of a ferromagnetic transition in multicomponent alloys into account. Comparison between experimental data and calculations are made and a satisfactory agreement is found, A set of parameters describing the variations of the mobilities with temperature and composition are given. KEYWORDS: Cr; Fe; Ni; diffusion coefficients; mobilities; assessment. 1. Introduction The diffusivities of Cr, Fe and Ni determines the rates of many important phenomena such as, diffusional creep, and phase transformations in a wide range of technologically important materials, e.g. stainless steels. Consequently, it is important to accurately know the transport properties in this type of materials, if one want to be able to analyse/predict their transformation behaviours. Recently, a software package for simulation of dif- fusional phasetransformations in multicomponent alloys called Dictral) was developed. Dictra relies on the so- called local equilibrium hypothesis. In order to simulate diffusional phase transformations adopting local equi- librium you need: l) thermodynamic data and 2) dif- fusional data. Thermodynamic data for many alloy sys- tems are today readily available from the SGTE2) solu- tion database of the Thermo-Calc databank system.3) Unfortunately, in general, diffusional data has not been systematically assessed yet, especially not for multi- component alloy systems. This work is part of an effort to remedy this situation. In most phases, the temperature dependency of the experimental diffusion data may be properly accounted for by an ordinary Arrhenius behaviour. However, there are exceptions. For instance, it has been known for- a long time that ferromagnetic ordering may have a significant influence on the value of the diffusion coef- ficient. This topic was recently addressed by Jdnsson4'5). a model, which will be adopted here, was presented. 2. Modelling of Diffusivities One may recognize different types of expermjental data concerning diffusion, e.g, tracer diffusion data and chemical diffusion data. Tracer diffusion data are more easily analysed than the chemical diffusion data. This is becausethere is a very simple relation betweenthe tracer diffusion coefficient D~ for an element B and its atomic mobility coefficient MB if one neglects correlation fac- tors. Assuming a mono-vacancy mechanism,the follow- ing relations holds6) D~=RTMB .... ..........(1) The small fraction of thermal vacancies on the sub- stitutional sublattice is not explicitly present, but their contribution is included in the mobility coefficient. R is the gas constant and T is the temperature. The chemical diffusivity is given by a more complex relation, where the concentration of one element has been chosen to be dependent on the others. Thechemical or reduced diffusivity is expressed as6) :=1 - ll Dkj ~(8Lk xk)xM api ap axj ax . (2) where n, k andj are the dependent, the diffusing and the gradient element, respectively. 8ik is the Kronecker delta, i.e. ~ik = I if i=k and 6ik = O otherwise. xk is the ordinary mole fraction of element k. It is the derivatives of the ordinary chemical potential eklilaxj that make chemical diffusion data less attractive than the tracer diffusion data, becausein order to make use of the former we also need to have access to the thermodynamicproperties of the alloy under consideration while the latter can be analysed without such knowledge. As a consequence, the MB determined from chemical diffusion data depends critically on the accuracy of the thermodynamicdescrip- tion used. In this work, we have employed a tool capable of assessing MB from different types of experimental data. It is called Parrot7) and it has recently been im- plemented into the Dictra software4'8). a diffusivity is typically calculated from Eq, (1) or (2) and is sub- 1 41 5 C 1995 ISIJ

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ISIJ International, Vol. 35 (1 995). No, 11, pp. 1415-1421

Assessmentof the Mobilities ot Cr. Fe and Ni in bcc Cr-Fe-NiAlloYS

Bj6rn JONSSONDepartment of Materials Science and Engineering. Division of Physical Metallurgy. Royal Institute of Technology. S-1 OO44Stockholm, Sweden.E-mail: [email protected]

(Received on March2. l995, accepted in final form on May26. 1995)

Experimental data on the diffusional mobilities of Cr, Fe and Ni in bcc Cr-Fe-Ni alloys are assessed bymeansof a modelwhich takes the effect of a ferromagnetic transition in multicomponent alloys into account.Comparisonbetween experimental data and calculations are madeand a satisfactory agreement is found,Aset of parameters describing the variations of the mobilities with temperature and composition are given.

KEYWORDS:Cr; Fe; Ni; diffusion coefficients; mobilities; assessment.

1. Introduction

The diffusivities of Cr, Fe and Ni determines therates of manyimportant phenomenasuch as, diffusional

creep, and phase transformations in a wide range oftechnologically important materials, e.g. stainless steels.

Consequently, it is important to accurately know thetransport properties in this type of materials, if onewant to be able to analyse/predict their transformationbehaviours.

Recently, a software package for simulation of dif-

fusional phasetransformations in multicomponent alloyscalled Dictral) was developed. Dictra relies on the so-called local equilibrium hypothesis. In order to simulatediffusional phase transformations adopting local equi-librium you need: l) thermodynamic data and 2) dif-

fusional data. Thermodynamicdata for manyalloy sys-tems are today readily available from the SGTE2)solu-tion database of the Thermo-Calc databank system.3)

Unfortunately, in general, diffusional data has not beensystematically assessed yet, especially not for multi-

componentalloy systems. This work is part of an effort

to remedythis situation.

In most phases, the temperature dependencyof theexperimental diffusion data maybe properly accountedfor by an ordinary Arrhenius behaviour. However, there

are exceptions. For instance, it has been known for-

a long time that ferromagnetic ordering mayhave asignificant influence on the value of the diffusion coef-ficient. This topic wasrecently addressed by Jdnsson4'5).

a model, which will be adopted here, waspresented.

2. Modelling of Diffusivities

Onemay recognize different types of expermjentaldata concerning diffusion, e.g, tracer diffusion data andchemical diffusion data. Tracer diffusion data are more

easily analysed than the chemical diffusion data. This is

becausethere is a very simple relation betweenthe tracerdiffusion coefficient D~for an element Band its atomicmobility coefficient MBif one neglects correlation fac-

tors. Assuminga mono-vacancymechanism,the follow-ing relations holds6)

D~=RTMB.... ..........(1)

The small fraction of thermal vacancies on the sub-stitutional sublattice is not explicitly present, but their

contribution is included in the mobility coefficient. Ris

the gas constant and T is the temperature.The chemical diffusivity is given by a morecomplex

relation, where the concentration of one element hasbeenchosen to be dependenton the others. Thechemical

or reduced diffusivity is expressed as6)

:=1 - llDkj ~(8Lk xk)xM

api ap

axj ax .(2)

wheren, kandj are the dependent, the diffusing and thegradient element, respectively. 8ik is the Kronecker delta,i.e. ~ik = I if i=k and 6ik =Ootherwise. xk is the ordinarymole fraction of element k. It is the derivatives of theordinary chemical potential eklilaxj that makechemicaldiffusion data less attractive than the tracer diffusiondata, becausein order to makeuse of the former wealso

need to have access to the thermodynamicproperties ofthe alloy under consideration while the latter can beanalysed without such knowledge. As a consequence,the MBdetermined from chemical diffusion data dependscritically on the accuracy of the thermodynamicdescrip-tion used. In this work, wehaveemployeda tool capableof assessing MBfrom different types of experimentaldata. It is called Parrot7) and it has recently been im-plemented into the Dictra software4'8). a diffusivity is

typically calculated from Eq, (1) or (2) and is sub-

141 5 C 1995 ISIJ

ISIJ International, Vol. 35 (1995) No. 11

sequently comparedto the experimental value. The dif-

ference between calculated and experimental values areused in a least square type of method which auto-matically finds the optimal set of model parameters.

3. Modelling of the Atomic Mobility

Recently, Jbnsson8) modified AnderssonandAgren's6)

model for the temperature, pressure and compositiondependencyof the atomic mobility in a multicomponentsolution phase. Fromabsolute-reaction rate theory argu-ments the mobility coefficient for an element BMBWasdivided into a frequency factor M~and an activationenthalpy QB, i,e.

RQ~~~~~; RIT~gQMB=M~exp ... ....

...(3)

where ~gQis a factor taking into account the effect ofthe ferromagnetic transition.5) ~gQis a function of thealloy composition. The frequency factor is given by

M~=exp(6,B). ......

..........(4)

Both OBand QBWill in general dependupon the com-position, the temperature, and the pressure. In the spirit

of the Calphadapproach,9) the composition dependencyis represented with a linear combination of the values ateach endpoint of the composition space and a Redlich-Kister expansion, viz.

m~. ' ~~xixJ ~rc~j(x, x )cB= xic~ +i j>i r=0

+~~~ s s ij'k (s=i,j,k) ..,...(5)~l j k vijk c~x'x xi j>ik>j

where cB represents a composition dependentproperty,i.e. (9B or QB, and the parameters v,~jk are given by

vijk =x.+(1 -xi-xj~xk)/3.......

..........(6)

Each individual c parameter on the R.H.S of Eq. (5)

maybe expressed as a polynomial in temperature andpressure, if necessary. Limiting the binary interactions

to secondorder (m= 1), weget, for our ternary CrFe-Nisystem:

cB=xcrc~• +xF*c~e+xNiep~i

+xcrxFe[oc~r.Fe + (xcr ~xFe) I c~r.Fe]

+xcrxN,[occ. Ni + (xc.~xN,) c '']

. B' .I CB'Nl

+XFeXNi[o c~e,Ni + (xFe ~xN~)I c~e,Ni]

+xc,xFexNi[xc c.c~r.Fe,Ni +xF.Fec~r,Fe,Ni Ni c. Fe N~+xNi cB' ' J.(7)

4. Experimental Data

Experimental data on diffusion coefficients are quiteplentiful for the binary Cr-Fe system. Whereas, for thebinary systems Cr-Ni and Fe-Ni data are very sparse,and so are data for ternary diffusion in the O~Fe-Nisystem. Thedifferent pieces of experimental informationused in the present assessmentare briefly listed in TablesI~5. Thepredominant experimental technique for deter-

mining tracer diffusion coefficients used by the different

Table 1.

Reference

lO)

l l)

l2)

l3)

l4)

l5)

16)

17)

Table 2.

Experimental Cr self diffusion data.

Temperature range('C)

95(~1 250

l OO0-1250

1080-1 320

l 058-1 393

l 200-1 600

1200-1 550

l OO0-1900

l 100-1 820

Experimental Fe tracer diffusion data in Cr.

Reference

Table 3.

Reference

l6)

Table 4.

Reference

20)

Table 5.

Reference

18)

l9)

21)

22)

23)

24)

25)

26)

27)

28)

29)

3O)

31)

32)

33)

34)

35)

36)

18)

l9)

Temperature range('C)

9831413980-1 230

Experimental diffusion data in binary CrFe al-

loys.

Measuredquantity

D~*

Compositionmasso/.

20 Ni

Temperature

range ('C)

l 16()-1 400

Experimental diffusion data in binary Fe-Ni al-

loys.

Measuredquantity

D*Fc

Compositionmasso/*

[1.62, 2, 14] Ni

Temperature

range ('C)

747-820

Experimental diffusion data in binary Cr-Fe al-

loys.

Measuredquantity

* *Dcr' DFO*DFC

FcDcrCr

D*CrFcDcrCrFeDcrCr

*DFOFeDCrCr

* n*Dcr' UFeD*FeD*Pc

* *DFe' DCr*Dcr

FcDcrCr

D*Pe*DFe

DFeCrCr

DFeCrCr

Composition

mass"/o

17 Cr[2(~90] Cr[0-30] Cr[2-19] Cr[0-25] Cr

[1850] Cr[6.8-8.9] Cr

[0-22] Cr[3.C~14.6] Cr[3.0-7.8] Cr[0-1 1.8] Cr

[27, 51, 85] Cr[20-lOO] Cr[30-lOO] Cr[920] Cr

[21-8l] Cr[1220] Cr[ll~28] Cr

Temperature

range ('C)

861-1 422980-1 230675-1 485797l 402642-869

180

650-820823, 1415-1 440

65(~82065082066(~890

950-1 275

1250757-8259571250

l 200-1 300800=1OOO

authors, is the so-called residual activity method ofGruzin: Onedeposits a thin layer containing a radioac-tive tracer element on the samplesurface. After diffusion

anneals, one removes layers of material, parallel with

C1995 ISIJ 141 6

ISIJ International, Vol. 35 (1995), No. 11

Table 6. Experimental diffusion data in binary Cr-FeNialloys.

-9

T/ [K]

2200 1800 1600 1400

Reference

1200Measured Composition Temperaturequantity range ('C)masso/*

37)

38)

39)

40)

D* [14,1, 20.l] Cr IOOOl300NiDP* F* Variousc*c*, DNiNi 1100DF* P* 29Cr+4Nic*c*, DNiNi I 13(~1 300

* 25.3Cr +4.6Ni 60(~1 OOODc*

the surface. After removing each layer, onemeasurestheresidual activity that is emitted from the sample surface.

Using this procedure, one obtains activity (concentra-tion) vs. distance profiles which are subsequently usedfor fitting an exponential solution of the diffusion equa-tion in order to establish a diffusion coefficient value.Chemical diffusion data are in general determined bythe so-called BoltzmannMatanoanalysis: Concentra-tion profiles are measuredfrom diffusion couples. Theseprofiles are subsequently fit to the equations of theBoltzmann-Matanoanalysis in order to obtain diffusioncoefficient data. For more information on experimentaltechpiques see somegeneral text book on diffusion, e.g.Ref. 41).

5. Assessmentand Results

Someof the parameters describing the mobilities hasalready been assessed by J6nsson,s) That is the param-eters for the mobilities in Fe. Wewill adopt his valuesin this work. As was pointed out by J6nsson: due toinferior sectioning techniques old experimental data of-

ten showinfiuence of grain boundary diffusion for tem-peratures below roughly I OOOK. Wewill keep this in

mind during the assessmentand accept larger deviationsbetween the experimental data and the calculations at10w temperatures. It should also be kept in mind thatoften during the assessmentprocedure one finds out thatdifferent pieces of experimental data are not mutuallyconsistent. Thus, one has to accept that one cannot atthe sametime fit all sets of data.

Acomplication with the Calphadmethodused for as-sessing the mobility data, is that one may need pa-rameters also for hypothetical states. In this case, thatis the mobilities in bcc Ni. In general, for such a case,one would like to try to extrapolate data from Ni-richbcc alloys. Unfortunately, the stability region of bcc doesnot extend very far towards Ni. Moreover, data are verysparse awayfrom the Cr-Fe binary side. Consequently,

we are forced to makesome assumption about themobilities in bcc Ni. It was assumedthat they are the

sameas those in paramagnetic Fe. Dueto lack of datasomefurther assumption weremade: l) Thebinary inter-actions in Fe-Ni wereassumedequal for all three species.2) Thebinary interactions in CrNi were assumedequalfor all three species. 3) The mobilities of Fe and Niin Cr were assumedequal and furthermore, in the spirit

of the findings of Fridberg et al.,42) we assumedtheactivation energy to be the sameas that for Cr selfdiffusion.

In the usual wayof the Calphadtechnique, Iower order

~~ -12co

c\lE

- -15*,,~O~O)O -18

-21

~A Askill&Tomlin 1965~] Paxton&Gondolf1959~ Hagel 1962

~~~+~

Askill i971v Mundyet al. 1976+ Ivanov 1962x Gruzin et al. 1959o Bogdanov1960

X +~

. ~~

Fig, l

40 45 50 55 60 65 70 75 80 85 90104 /T •

[K]

Tracer diffusion of Cr in Cr. Symbolsare experimentaldata due to various authors. Solid line is from ourassessment.

systems are, if data is sufficient, assessed separately andthe parameters thus determined are later kept fixed whenadvancing to higher order systems. Consequently, theassessment was divided into several different steps: l)

the self-diffusion coefficient of Cr was determined. Theparameters for this unary system was thereafter con-sidered fixed. 2) the mobilities in the binary Cr-Fe, Cr-Ni and FeNi systems were assessed separately and weresubsequently kept fixed. 3) the rest of the data, i.e. datafor the ternary CrFe-Ni, was used to assess the re-maining interaction parameters. Additionally, due to thefact that the present modelling allows for quite a fewmodel parameters, and that the available experimentaldata is not sufficient to determine them all with a highdegree of confidence, it wasquite arbitrarily decided to

use interaction parameters for the Q's only. It can bementioned that using the interactions for the (9's worksas well. However, data is not sufficient for using themboth at the sametime. All resulting parameters are givenin the appendix. A11 thermodynamic data were takenfrom the SGTEsolution database.2)

If nothing else is stated solid lines are our calcula-tions and symbols are expcrimental data due to variousauthors. A fit between calculations and experimentswithin a factor of 2will be considered as reasonable.

Cr Self Diffusion ~

There is quite a large amount of data on Cr selfdiffusion. The scatter of the data is very large below1600K, up to about 3orders of magnitude, see Fig. l.

Except for temperatures very close to the melting pointof Cr, the two most recent investigations showreason-able agreement over the whole temperature range ex-amined. Most of these data points are for single crystalsamples (filled symbols) in order to avoid effects of grainboundary diffusion, which appears to have affccted theresults of most of the other investigations. For this rea-son, it was decided to trust only the data of Askilll6)

and Mundyet al.17) in the present assessment. The cal-

culations and the selected experimental data are in fair

agreement.

141 7 C 1995 ISIJ

ISIJ International, Vol. 35 (1995), No. 11

-121800 1600

T/ [K]

1400 1200 11oo

-14

(,)

c\] -16E_,,

a) 18LL-aa)~~ 20

~1[1]~

Cll AA

~Shinyaev 1965~] Wolfe&Paxton1964

[1]

-225 6 7 8 109

104 /T •[K]

Fig. 2. Fe tracer diffusion in 'pure' Cr. Symbols are experi-

mental data due to Wolfe and Paxtonl8) (squares) andShinyayev*9) (triangles). sohd hne is from our assess-

ment.

Diffusion in Cr-Fe AlloysDiffusion in the Fe-Cr system has been the topic of

manyreports, Not surprisingly, most investigators hasbeen interested in diffusion in Fe-rich alloys, for various

reasons. Fortunately, somehave examinedalso Cr-basealloys, so that the entire composition range has been

spanned.Not manydata concerns D~* in pure Cr, see Fig. 2,

wherewecompareour calculations with the experimentaldata of Wolfe and Paxton,18) and Shinyayev. 19) Wenotethat both sets of data indicate a lower activation energythan that assumedin this assessment, i.e. the sameasthat for Cr self diffusion. The experimental activationenergies are more in accordance with those for Cr self

diffusion as derived from data from the sameperiod oftime, i.e. the early 1960's, see Fig, I .

As was discussedin the previous section, this is probably due to grain

boundary diffusion effects.

Dueto the large amountof experimental data pointsfor the Fe-Cr system, and the limited space available forthis paper, explicit comparison betweenexperiments andcalculations are only madefor a sample of experimentaldata, see Figs. 3-8. In Fig. 3, we compare calculatedD~~c, data with experiments from Braun and Feller-

Kniepmeier23) (notice the technique of shifting the dif-

ferent curves with the amount S in order to makeit

possible to plot several curves in the samediagram).

Wenotice non-linear curves due to the effect of the

ferromagnetic transition. The fit to these data are good.In Fig. 4, we trace the composition dependencyof theD~~c* at somedifferent temperatures. Wetypically find

a reasonable fit to the experiments at high temperatures,at lower ones there is often a larger descrepancy, as for

the Heumannand B6hmer26)823'C-data shown. Theirdata does not even extrapolate to the accepted value at

the pure Fe side. Onemaysuspect that their data areinfluenced by grain boundary diffusion. In connectionto this figure, it can be mentioned that the Curie tem-perature is 770'C at the pure iron side and that it haslowered to about 680'C when it hits the bcc/(bcc+(T)

C 1995 ISIJ

-8

(D _10+

(/) -12c\I

E_

~ 14~~6C~

_16~5~

o-18

1200 11ooT/ [K]

1000 950 900 850

OoloCr

5010Cr

1OoloCr

15"loCr

20010Cr

25010Cr

S=0

S=5S=4S=3s=2S=1

Fig.

8.0 8.5 9.0 9.5 10.0 10.5 11.0 11.5 12.0

104 /T .[K]

3. Chemical diffusion coefficient in six different FehCralldys. Symbols are experimental data due to Braunand Feller-Kniepmeier.23) Solid lines are from ourassessment.

- I0.5

(D ~11.0

+~ -1 1.5

(1)

c\1 ~12.0E- -12.5\ o**

LLO__o-1 3.0

o)o -13.5

-1 4.0

o~~(~)o

4400c

41 5'C

1180'C

230c

o Sulayev et al. 1970ACarter 1974[~l Heumann&Bbhmer1960

S=0

S:: -0.5

S=0

S=2

1418

Fig. 4.

O OI O2 O3 O4 O5 0.6

Xcr

Chemical diffusion coefficient in Fe-Cr alloys at dif-

ferent temperatures. Symbols are experimental datadue to Carter24) (triangles). Heumannand B6hmer26)(squares), and Sulayev el al.35) (circles). Solid lines arefrom our assessment.

phase boundary at about 28wto/o Cr. In Figs. 5-6, wetrace the composition and temperature dependencyofD~., respectively. The fit to most data is quite reason-able. In the sameway, Figs. 7-8, showD~*. Also thesecalculations showa reasonable agreement with the ex-periments. ~

Diffusion in Cr-Ni AlloysThe only pieces of experimental information on dif-

fusion in the C~Ni system are the D~, data reportedby Askill,16) see Fig. 9. Unfortunately, only the filled

symbols are from single phase specimens. The fit to thedata is satisfactory.

Diffusion in Fe-Ni A110ysD~. data by Okada,20) see Fig. 10, are the only experi-

mental data on diffusion in the Fe-Ni alloys. The fit tothe data is satisfactory.

Diffusion in Cr-Fe-Ni AlloysIt has not been possible to satisfactorily account for

ISIJ Intemational, Vol. 35 (1 995), No. 11

-1 1-12

~=~ -13u)

c\1~14

E- -15~.aLLa'

_1 6~-17

-18

-1 9

l!~ 1250'C[ll 1145'C

I060'CVV960'C

A l!~

vvv v

v

0.6 1.OO 0.2 0.4 0.8

Xcr

Fe tracer diffusion in different Fe-Cr alloys. Symbolsare experimental data due to Shinyayevl9) (filled sym-bols), and Shinyayev34) (open symbols). Solid lines arefrom our assessment.

T/ [K]

1700 1400 1200 1000 900 800

-9

-1 O(/)

+ -11

u) -12c\l

13*~C:) -14~a)~2 _15

-16

S=2ll:]

[] 12750C~12500C

S=1 AAA

S=0S=0S=0

Fig. 5.

o 1200'C~11oo'Cv Iooo'c

O

v

JL

I

~l

-6

-8(D+ _10

a) _12c\'

E:

- -14

~+a -16a)o- -18

-20

Fig. 8.

S=5 )1 Fe- 5wt'/oCr[i Fe-20 wtoloCr~>Fe-40 wto/oCr

-10

-1 1

~ -12c~J(1) _13

14*~5iO ~15o)o -16

-17

-18

o 0.2 0.4 0.6 0.8 1.O

Wcr

Cr tracer diffusion different Fe-Cr alloys. Symbolsare experimental data due to Paxton and Kunitake31)(open symbols), and Paxton and Pasierb32) (filled sym-bols). Solid lines are from our assessment.

s=3S=2S=1

S=0

OFe-60 wt"/aCr

v Fe-80 wtoloCr

e

lii

Fig. 6.

5 6 7 8 9 10 11 12 13

104 /T •[K]

Fe tracer diffusion in different Fe-Cr alloys. Symbolsare experimental data due to Shinyayev34) (filled sym-bols), Shinyayevl9) (open symbols), Rayand Sharma33)(half filled symbols), and Ku6eraet a/.29) (stars). Solidlines are from our assessment.

T/ [K]

1800 1500 1300 1100 1000

T/ [K]

1900 1700 1500 1300 1200 1100

ll

-6

[ll

I Askill 1971 (single phase)~! Askiil 1971 (two phase)

Cll

50

Fig. 9.

-13

55 60 65 70 75 80 85 90 95104 /T •

[K]

Cr tracer diffusion in Cr-20wto/,Ni. Symbolsare ex-perimental data due to Askill. 16) Filled symbols single

phase bcc, opensymbols two phase bcc/fcc. Solid lineis from our assessment.

CD~8

- -10~a)

c\~

E -12

, ~-14O_o)o -16

-18

T/ [K]

1200 1100 1000 950 900

S=S=3S=2S=i

S=0

AFe-25010Cr[1] Fe-50010Cr

Fe-75010Cr

[1]

Cl]

[1]

OFe- 9010Cr

* Fe-1 7010Cr

oo(~~

5 6 7 8 10 119104 /T •

[K]

Cr tracer diffusion in five different FeCralloys. Sym-bols are experimental data due to Wolfe and Paxtonl8)(stars), Huntz et al.27) (circles), and Paxton andKunitake31) (other symbols). Solid lines are from ourassessment,

C/) ~14

+~::~ -15u)

c\i it~~ -Iv

~-17*O~;iO -18

-1 9

S=1

S=0

Okada1966~ Fe*2. 14wt'/•Ni~l Fe-1 .62wt'/.Ni

Fig. 7.

~~

8.0

Fig. lO.

85 90 95 100 10.5 11.0 11.5

104 /T •[K]

Fe tracer diffusion in two different Fe-Ni alloys. Sym-bols are experimental data due to Okada.20) Solidlines are from our assessment.

141 9 C 1995 ISIJ

ISIJ International, Vol. 35 (1995), No. 11

-101650 1550 1450

T/ [K]

1350 1250 1200

C/) ~11

~,) -12c\l\E_

13

O~O)o -14

-15

Fe-29Wto/oCr-4WtoloNi

[~] D~eNi

DFecrcr

S=1

S=0

6,0 6.4 6.8 7.2 7.6 8.0 8.4104 /T •

[K]

Chemical diffusion coefficient of Cr and Ni in an Fe-29wto/oCr~Vwto/oNi alloy. Symbolsare experimentaldata due to Malik el al.39) Solid lines are from ourassessment.

Ni

1OO

90

80

~~ 70\s:c;e)~

60 1473Ke,

~: *~*,h*~5~~

40~~~

30

20

1O K6 eK4

OE~]~ K8

Y+0c

Fig. Il.

-121400 1200

T/ [K]

1000 900

e o;K9

800

Feo

Fig. 13.

-14

(,)

c\] -16E~'Oo* -1 8~a)~2 -20

-22

CD

[ll Fe-25.3wto/oCr-4.6wto/aNi

C~l

7 8 9 10 11 12 13 14

104 /T •[K]

Fig, n. Cr tracer diffusion in an Fe-25.3wt'/.Cr~1:.6wt"/,Nianoy. Symbols are experimental data due to Smithand Hales.'o) Solid nne is from our assessment.

D~i data reported by Hancockand Leak37) (not shownin plot). The difference between the assessmentand theexperiments is very large, about two orders of magni-tude. The D~~c, and DF' data of Malik et al.39) areNiNiwell reproduced by the present assessment, see Fig. 11,

whereas the D~* data of Smith and Hales40) are not asnicely represented, see Fig. 12.

6. Test of SomePredictions: AnApplication

In Fig. 13 wehave markedwith squares the composi-tions at which experimental diffusion data are availableoutside the binary Cr-Fe side. Wenotice that large areasof the bcc (oc) phase field has not been investigated.

In order to independently test the quality of theassessmentwork on an application, Engstr6m43) madeand annealed three different diffusion couples K4-K6,KI~K8, and K8-K9 (alloys markedwith solid circles)

at 1200'C. Simulations madewith DICTRAusing ourassessed data are comparedwith Engstrdm's measured

70

60

~ 50o(,~40CL

J::_a) 30'(a)

~ 20

10

O

20 40 60 80 1OOWeight Percent Cr Cr

Calculated isothermal section in the CrFe-Ni sys-tem at 1473K. Squares mark alloy compositionswhere diffusion data are available due to variousauthors. Solid circles mark the alloy compositionsof Engstr6m's diffusion couples.

oeo Crc]l~ Ni

o

o

C 1995 ISIJ

e

o

1420

-2.0 -1.5 -1.0 -0.5 0.0 0.5 1.0 1.5 2.0

Distance / [mm]Fig. 14. Comparison between predicted and experimental

composition profiles in diffusion couple K4-K6(filled

symbols), KI~K8 (half filled symbols), and K8-K9(open symbols). Annealed at 1200'C for 21 h. Ex-periments are due to Engstr6m.43)

composition profiles in Fig. 14. The predicted profiles

are in reasonable agreementwith the experiments, evenfor couple K8-K9which alloys are quite far awayfromcompositions where experimental diffusion data areavailable.

7. Summary

Thediffusional mobilities of Cr, Fe and Ni in bcc Cr-Fe-Ni alloys has been assessed by meansof a Calphadtype of method. Using a modelwhich takes the effect ofthe ferromagnetic transition into account, most experi-mental data could be successfully accounted for with afairly reasonable accuracy.

Although there are manyexperimental data in this

system, most data are from Fe-rich alloys leaving large

areas of the ternary in the dark. Thus, more ternarydiffusion data are welcome. However, as tested above,

ISIJ International, Vol. 35 (1 995), No. 11

the present assessmentpossesses a reasonable predictive

power.

Acknowledgement

This work has been sponsored by TFR(SwedishResearch Council for Engineering Sciences).

l)

2)

3)

4)

5)

6)

7)

8)

9)

10)

1l)

l2)

13)

l4)

l5)

16)

l7)

18)

l9)

20)

21)

22)

23)

24)

25)

26)

27)

28)

29)

3O)

31)

32)

33)

34)

35)

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Fundamentalsand Applications of Ternary Diffusion, ed. by G.R. Purdy, PergamonPress, NewYork, (1990), 153.

SGTE(Scientific GroupeThermodataEurope) solution databaseof Jan. 1994. Editor: B. Sundman,Division of ComputationalThermodynamics. Royal Institute of Technology, S- 10044Stockholm, Sweden,E-mail: [email protected]. Sundman.B. Janssonand J.-O. Andersson: Calphad, 9(1985),

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A. Engstr6m: Private communication, augusti 1994.

Appendix

R= 8.3 1451Jmol- I K- I.

given in SI units.

Mobility of CrOCr

CroFe

CroNi

CrOIC]~Cr,Fe

I~rcr

1H Cr,PeOCrOH Cr,Ni(~Cr

l l(:)1:y~f Cr,NiCr

OI~]IC!H Fe,NiCr

I~'nH Fe,NiCr

= - 35.6/R

= In(8.5 • 10~5)

= In(8.5 • lO~ 5)

= - 116/R

= +37.5/R

=0=0=0=0

crn~ cr,Fe,Ni_O~'cr ~pen~cr,Fe,Ni_O~' cr ~Nin~cr,Fe,Ni_O'c7cr ~

Mobility of FeCre)FeFeOFeNi(9Fe

On~Cr,FeC!Fe

1IC]~ Cr,FeC' pe

OIC]~Cr,Ni'~fFe

1167HCr*NiFe

Ot~'nHFe,NiFe

l ICIFe,NiUHFe

= - 17.21R

= In(4.6 • 10~ 5)

= In (4.6 • IO~ 5)

= - 1171R

= +348/R

=0=0=0=0

crn~cr'Fe'Ni_OI~yFe ~Fen~cr'Fe,Ni_O':y Fe ~Nin~cr'Fe'Ni_Olc' Fe ~

Mobility of Ni6) Cr

NioFe

Ni6,Ni

NiOn~Cr,Fe

':7Ni

l n~Cr,Fec,Ni

O~]~Cr,Ni,~rNi

1n~Cr,Nic,Ni

On~Fe,Ni,orNi

l n~Fe,Nic,Ni

= - 17.21R

= In(1.8 • lO- s)

= In(1 .8 • 10~s)

= + lO/R

=0=0=0=0=0

Crn~Cr,Fe,Ni_Ot~,Ni -PenHCr,Fe,Ni_Ot:yNi -Nin~Cr,Pe,Ni_Olc,Ni -

A11 parameter

CrQCrPeQCrNiQCr

OnCr,Fe'~Cr

l nCr,Fe~~Cr

OnCr,Ni!:~ Cr

1nCr,Ni~iCr

OnFe,Ni~Cr

l nFe,Ni~Cr

values are

= +407OOO

= +218OOO

= +218OOO

= - 361 OOO

= -2 820

= - 350OOO

=0= - 150OOO

=0cr(]cr,Fe,Ni

=O~crFencr,Fe,Ni = +2400OOO!:~ crNincr,Fe,Ni

::; O'4cr

CrQFeFeQFeNiQFe

O(]Cr,Fe':~ Fe

l nCr,Fe~iFe

OnCr,Ni~i Fe

l nCr,Ni~~Fe

OnFe,Nik~Fe

1nFe,Ni~i Fe

= +407OOO

= +218OOO

= +218OOO

= - 267OOO

= +416000

= - 350OOO

=0= - 150OOO

=0crncr,Fe,Ni =O~~FeFencr,Fe,Ni = +1400OOO~FeNincr,Fe,Ni

=O'~ Fe

CrQNiFeQNiNiQNi

OnCr,Fe!~~Ni

l nCr,Fe'4Ni

OnCr,Ni~5i Ni

l nCr,Ni~iNi

OnFe,Ni~iNi

1nFe,Ni~iNi

= +407OOO

= +204OOO

= +204OOO

= +88 OOO

= -O= - 350OOO

=0= - 150OOO

=0crncr,Pe,N'

_l O,4Ni -Fencr,Fe,Ni_ +500OOO~CNi -Nincr,Fe,Ni_O~~Ni -

1421 C 1995 ISIJ