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Materials Science and Engineering A 483–484 (2008) 184–187
Influence of addition elements on the stacking-fault energyand mechanical properties of an austenitic Fe–Mn–C steel
A. Dumay a,∗, J.-P. Chateau a, S. Allain b, S. Migot a, O. Bouaziz b
a Laboratoire de Physique des Mat´ eriaux, Ecole des Mines, Parc de Saurupt, CS 14234, F-54042 Nancy cedex, Franceb Arcelor Research SA, Voie Romaine, BP 30320, F-57283 Maizieres-les-Metz cedex, France
Received 6 June 2006; received in revised form 2 October 2006; accepted 7 December 2006
Abstract
We present a thermochemical model of the stacking-fault energy (SFE) in the Fe–Mn–C systemwith few percent of Cu,Cr, Al and Si in addition.Aluminium strongly increases the SFE, contrary to chromium, while the effect of silicon is more complex. Copper also increases the SFE, but
strongly decreases the Neel temperature. The SFE is the relevant parameter that controls mechanical twinning, which is known to be at the origin
of the excellent mechanical properties of these steels. Using this model, copper containing Fe–Mn–C grades were elaborated with SFE below
18 mJ/m2, in the range where -martensite platelets forminstead of microtwins duringplastic deformation. This substitution of deformation modes,
confirmed by X-ray diffraction, does not significantly damage the mechanical properties, as long as the SFE is greater than 12 mJ/m2, which avoids
the formation of -martensite.
© 2007 Elsevier B.V. All rights reserved.
Keywords: Fe–Mn–C; Stacking-fault energy; Martensitic transformation; Strain hardening
1. Introduction
The Fe22Mn0.6C fcc steel developed by Arcelor exhibits
mechanical twinning in addition to dislocation gliding when
deformed at room temperature [1–3]. The fine microtwins
formed along with plastic deformation act as strong obstacles,
such as grain boundaries, and lead to a “dynamical Hall and
Petch effect”, a high strain hardening rate and consequently
both excellent elongation to fracture (>50%)andultimate tensile
strength (>900 MPa). The relevant parameter for twinning is the
stacking-fault energy (SFE) which depends on temperature and
composition.
The best hardening rate is obtained at room temperature in
this steel, where its SFE is intermediate (≈20 mJ/m2) [1,3].
At higher values, twinning tends to disappear, while below18 mJ/m2 microtwins are replaced by hcp-martensite platelets.
In an alloy design approach, it is necessary to predict the tem-
perature and composition dependence of the SFE, in order to
adjust an alloy’s grade to its forming or service conditions.
∗ Corresponding author. Tel.: +33 3 8358 4143; fax: +33 3 8358 4344.
E-mail address: [email protected] (A. Dumay).
We first present a thermochemical model based on the one
previously developed for the Fe–Mn–C system, in order to pre-dict the effect of adding few percents of copper, chromium,
aluminium or silicon on the SFE. An example of the influ-
ence of the SFE on the mechanical properties and deformation
microstructure, in connection with the model’s prediction, is
presented in the second part in the case of copper.
2. Thermochemical modelling of the stacking-fault
energy
In fcc structures, twinning is due to stacking faults (SFs)
extending in parallel adjacent dense planes. Extending them
every twoplanes leads to the formationof -martensite. A stack-
ing fault can be modelled by two atomic layers of ε-martensitewithin the dense planes. This allows to write the SFE as [4]:
Γ = 2ρ Gγ →ε+ 2σ γ / ε (1)
with Gγ →ε, the free molar enthalpy of the transformation
γ → ε, ρ the molar surface density of atoms in the {1 1 1} planes
and σ γ / ε =8mJ/m2 [1] the energy per surface unit of a {1 1 1}interface between γ and ε.
Accordingto thesimplifiedprevious model for theFe–Mn–C
system [3], the free molar enthalpy of martensite formation can
0921-5093/$ – see front matter © 2007 Elsevier B.V. All rights reserved.
doi:10.1016/j.msea.2006.12.170
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A. Dumay et al. / Materials Science and Engineering A 483–484 (2008) 184–187 185
be written as follow:
Gγ →ε= G
γ →εFeMnX + xc G
γ →εFeMnX/C +Gγ →ε
mg (2)
Using the regular and subregular solution model, Gγ →εFeMnX is
the chemical contribution of all the elements in substitution in
the fcc lattice. The Fe–Mn excess term is taken into account but
the others involving the addition elements are neglected becauseof the little quantities considered, except for silicon:
Gγ →εFeMnX =
i
xi Gγ →εi + xFexMn[C + D(xFe − xMn)]
+xFexSi[E + F (xFe − xSi)] (3a)
Gγ →εi = Ai + BiT, i = Fe, Mn, Cu, Cr, Al, Si (3b)
with x i the molar fraction of element i, T the temperature and
{ Ai}, { Bi}, C , D, E and F fitting parameters.
Carbon in insertion is simply introduced as a disturbance of
the former fcc solid solution [5]. An empirical law has beenimproved since [3], to account for an increasing carbon effect
with manganese content:
Gγ →εFeMnX/C =
a
xC(1− e−bxC )+ cxMn (4)
where a, b and c are fitting parameters according to Ref. [1].
Gγ →εmg is a magnetic term, due to the Neel transition (para-
magnetic to antiferromagnetic) of each phase ϕ:
Gγ →εmg = Gε
m − Gγ m (5a)
where
Gϕm = RT ln
1+βϕ
µB
f T
T ϕN
, ϕ = γ, ε (5b)
with βϕ and T ϕN , respectively, the magnetic moment and Neel
temperature of phase ϕ, µB the Bohr magneton and f a polyno-
mial function which expression can be found in Ref. [6].
ρ, Gγ →εFe , G
γ →εMn and T εN are unchanged compared to Ref.
[3]. βγ , βε have been improved in Ref. [1] to take the effect
of carbon into account (additional elements in substitution are
neglected):
βγ = β
γ FexFe + β
γ MnxMn − β
γ FeMnxFexMn − βCxC (6a)
βε= βε
MnxMn − βCxC (6b)
with βϕi the contribution of element i in phase ϕ and β
ϕij the
excess i– j term. An empirical expression of T γ N has been fitted
to data of literatures [7–10] and measurementsconductedon our
FeMnCuC alloys. T εN is given in Ref. [3]:
T γ N = 250 ln(xMn)− 4750xCxMn − 222xCu
−2.6xCr − 6.2xAl − 13xSi + 720 (K) (7a)
T εN = 580xMn (K) (7b)
A current assumption [11,12] is that the -martensitic (and
the reverse austenitic) thermal transformations occurs when
Table 1
Summarised parameters of the model from Refs. [1,3] and the present work for
addition elements (T in K)
ρ 2.94× 10−5 molm−2 [3]
σ γ / ε 8mJm−2 [1]
Gγ →εFe −2243.38+ 4.309T Jmol−1 [3]
Gγ →εMn −1000.00+ 1.123T Jmol−1 [3]
G
γ →ε
FeMn C =2873Jmol
−1
; D =−
717Jmol
−1
[1]Gγ →ε
FeMnX/C a =1246Jmol−1; b = 24.29 J mol−1; c =−17,175 J mol−1 [1]
βγ / µB 0.7 x Fe + 0.62 x Mn −0.64 x Fe x Mn −4 x C [1]
βε / µB 0.62 x Mn −4 x C [1]
Gγ →ε
Al 2800+5T Jmol−1
Gγ →ε
Cr 1370−10T Jmol−1
Gγ →ε
Cu 2273J mol−1
Gγ →ε
Si −560− 8T Jmol−1
Gγ →ε
FeSi E = 2850J mol−1; F =3520Jmol−1
Gγ →ε≈−100 J/mol (respectively, +100 J/mol; we find that
+80 J/mol gives better results). The parameters for FeMnC have
beenobtainedfirst[1]. Then,the parametersconcerning theaddi-
tion elements are fitted to give the best accordance with 120transformation temperatures of different compositions with less
than 5 wt.% of alloying elements. All data have been found in
Refs. [6,7,11,13–23]. The set of parameters which give the best
estimation of the transformation temperatures over the whole
database is summarised in Table 1 (results from Refs. [3,1] and
the present paper).
Fig. 1 shows the result when adding each element to the
Fe22Mn0.6C steel. Petrov measured the SFE by loss-energy
method and deduced the influence of chromium [23], which
is rather weak; our model is in good agreement with his results.
Copper and even more aluminium increase the SFE, contrary
to chromium. Copper is shown to strongly decrease T N. Sili-
con have a complex effect on SFE, increasing SFE for small
quantities and decreasing it at higher ones. Previous studies on
silicon effect showed that Si decreases the SFE but their range
of validity is over 4wt.% [21,24].
Fig. 1. Predicted influence of alloying elements on the SFE of the Fe22Mn0.6C
reference.
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186 A. Dumay et al. / Materials Science and Engineering A 483–484 (2008) 184–187
Fig. 2. (a) Strain hardening rate n = ε / σ dσ /dε and SFE predicted for samples A–D. (b) X-ray patterns (θ , 2θ ) of deformed samples.
This model is used to predict the SFE in accordance with
the deformation modes activated in copper containing alloys
presented in the following part.
3. Mechanical properties of a low SFE austenitic steel
The effect of the SFE on the mechanical properties was stud-ied in the Fe22Mn0.6C alloy by changing the temperature of the
tensile tests [1,3]. The decrease of the elongation to fracture and
hardening rate below room temperature was attributed to the
occurrence of -martensitic transformation instead of twinning
at lower SFE values (below 18 mJ/m2 [3]). However, disloca-
tion glide also depends on temperature: dislocation pinning by
carbon atoms is strongly thermally activated below room tem-
perature.
In order to discriminate between martensitic transformation
and thermal activation of glide, the SFE value was varied this
time by using different grades elaborated by Arcelor and all
tested at room temperature. The grades tested are four ironbase alloys containing 0.6 wt.% C, 2 wt.% Cu and increasing
Mn amounts (from 10 up to 20 wt.%). Our model predicts a
SFE increasing with the Mn content: 10, 12, 15 and 17mJ/m2,
labelled A, B, C and D, respectively, well in the -martensitic
transformation range. The SFE of the Fe22Mn0.6C reference is
23 mJ/m2.
Samples were cut out from 4 mm thick sheets obtained by hot
rolling. Metallography and X-ray analyses show that they are
100% austenitic, fully recrystallised with equal average grain
sizes of 6m. Static uniaxial tensile tests were performed up to
fracture at room temperature. Samples are analysed after tensile
testing by X-ray diffraction (θ , 2θ method) to detect the pres-
ence of -martensite and simply tested with a magnet to detectthepresence of -martensite (bodycentred tetragonal structure,
ferromagnetic).
The mechanical characteristics of each alloy are shown in
Table 2. The evolutions of the strain hardening rate with true
strain are shown in Fig. 2(a) and the X-ray diffraction patterns
after deformation in Fig. 2(b). They confirm the presence of
-martensite in all samples. Samples A and B with the lowest
valuesof theSFE(austenitestronglyunstable)are ferromagnetic
after deformation, thus containing -martensite.
Except for alloy A, the homogeneous elongation ends at
the Considere’s criterion n = ε, leading to high elongations to
fractureandultimatetensile strengths, as forthe Fe22Mn0.6Cref-
Table 2
Yield stress (YS), ultimate tensile strength (UTS), elongation at fracture (EF)
and phases observed after tensile testing on A, B, C and D Cu-containing grades
YS (MPa) UTS (MPa) EF (%) Phases observed after testing
A 337 825 37.7 γ , ε, α
B 343 914 64.4 γ , ε, α
C 345 908 62.7 γ , εD 351 883 68 γ , ε
erencesteel. Inall samples ofsteel A,and somesamples ofB,the
nucleation of -martensite, which is a hard phase, at the inter-
sections of two variants of -martensite platelets promotes pre-
mature fracture before this criterion by concentrating stresses.
4. Conclusion
Based on experimental measurements and numerous
bibliographic data of Neel temperatures and -martensite trans-
formation temperatures, we extend the SFE prediction modelfor the Fe–Mn–C system to alloys containing Cu, Cr, Al and
Si in addition. Except for the more complex case of silicon, the
results are in good agreement with other experimental results.
Chromium is the only element decreasing the SFE. All elements
decrease the Neel temperature, especially copper which has a
strongeffect. Themodelwas successfullyused in analloydesign
approach to elaborate steels containing copper with SFEs below
the lower limit of 18 mJ/m2 for the activation of mechanical
twinning.
The prediction is in good agreement with the observation of
-martensite in these steels after tensile testing at room tem-
perature. The substitution of mechanical twinning by athermal
-martensite transformation does not significantly damage the
mechanical properties of Fe–Mn–C steels. The sequential acti-
vation of two -martensite variants also leads to a “dynamical
Hall and Petch effect”, by reducing the mean free path of the
dislocations, and consequently a high hardening rate. However,
attention must be paid to the formation of -martensite, which
occurs for SFEs below 12mJ/m2 and reduces ductility.
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