Queen Mary University of London University of Cambridge

Tempered Martensite

H. K. D. H. Bhadeshia

Introduction

Tempering is a term historically associated with the heat treatment of martensite in steels. It describes how the microstructure and mechanical properties change as the metastable sample is held isothermally at a temperature where austenite cannot form. The changes during the tempering of martensite can be categorised into stages.

During the first stage, excess carbon in solid solution segregates to defects or forms clusters within the solid solution. It then precipitates, either as cementite in low-carbon steels, or as transition iron-carbides in high-carbon alloys. The carbon concentration that remains in solid solution may be quite large if the precipitate is a transition carbide. Further annealing leads to stage 2, in which almost all of the excess carbon is precipitated, and the carbides all convert into more stable cementite. Any retained austenite may decompose during this stage. Continued tempering then leads to the coarsening of carbides, extensive recovery of the dislocation structure, and finally to the recrystallisation of the ferrite plates into equiaxed grains.

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This is a useful description but it is revealing to consider first, the factors responsible for driving the process in the first place.

Deviation from Equilibrium

Tempering is a process in which the microstructure approaches equilibrium under the influence of thermal activation. It follows that the tendency to temper depends on how far the starting microstructure deviates from equilibrium. It is interesting therefore to consider how metastable a material can be, before dealing specifically with martensite. Turnbull characterised metastability in terms of the unit RTm where R is the universal gas constant and Tm is the absolute melting temperature. This coarse unit is a measure of the thermal energy in the system at the melting temperature; it represents a large amount of energy, typically in excess of 20,000 J mol−1.

Table 1: Degree of metastability
Metastable structure RTm
Supersaturated solutions1
Amorphous metal0.5
Modulated films, nanostructures0.1

Supersaturated solutions are prominent in this list and the extent of metastability depends both on the excess concentration and on the equilibrium solubility. It can be demonstrated that excess carbon which is forced into solution in martensite is the major contributor to the stored energy of martensite.

The calculations presented in Table 2 show the components of the stored energy of martensite in a typical low-alloy martensitic steel Fe-0.2C-1.5Mn wt%. It is necessary to define a reference state, which is here taken to be an equilibrium mixture of ferrite, graphite and cementite, with a zero stored energy. Graphite does not in fact form because it is too slow to precipitate; the effect of replacing the graphite with cementite is to increase the stored energy by some 70 J mol−1.

When transformations occur at low temperatures, it is often the case that substitutional elements like manganese and iron cannot diffuse during the time scale of the experiment, whereas carbon is still mobile. The transformation then happens in such a way that the Fe/Mn ratio is maintained constant whilst the carbon redistributes subject to this constraint, until its chemical potential becomes uniform. This is known as paraequilibrium. Unlike the equilibrium state, because the iron and manganese atoms are trapped during transformation, their chemical potentials are no longer uniform. This adds a further 315 J mol−1 to the stored energy.

When bainite forms, the transformation mechanism is displacive, there is a shape deformation, which leads to an additional 400 J mol−1 of stored energy. Since there is no diffusion during transformations, but the carbon partitions following growth, the total stored energy is that for the paraequilibrium state added to the strain energy term, giving a net value of 785 J mol−1.

Martensite is not only a diffusionless transformation, but it frequently occurs at low temperatures where its virgin microstructure is preserved. Even the carbon remains trapped in the product crystal. Furthermore, the strain energy term associated with martensite is greater at about 600 J mol−1 because the plates tend to have a larger aspect ratio (thickness/length). There may also be twin interfaces within the martensite plates, which cost about 100 J mol−1. The trapping of carbon inside the martensite adds a further 629 J mol−1, which makes the total stored energy in excess of 1700 J mol−1!

Table 2: Stored energies of a variety of microstructures
Phase Mixture in Fe-0.2C-1.5Mn wt% at 300 K Stored Energy / J mol−1
1. Ferrite, graphite and cementite0
2. Ferrite and cementite70
3. Paraequilibrium ferrite and paraequilibrium cementite385
4. Bainite and paraequilibrium cementite385 + 400 = 785
5. Martensite385 + 600 + 100 + 629 = 1714
6. Mechanically alloyed ODS metal55

Figure 1: The free energy due to the trapping of carbon in martensite, as a function of its carbon concentration. The results are for a temperature of 473 K.

Graph of free energy vs carbon concentration

Virgin Microstructure

The virgin microstructure obtained immediately after quenching from austenite consists of plates or laths of martensite which is supersaturated with carbon. In the vast majority of steels, the martensite contains a substantial density of dislocations which are generated during the imperfect accommodation of the shape change accompanying the transformation. The plates may be separated by thin films of retained austenite, the amount of untransformed austenite becoming larger as the martensite-start temperature MS is reduced.

Micrograph of martensite and austenite

(a) Transmission electron micrograph of as-quenched martensite in a Fe-4Mo-0.2C wt% steel. The mottled contrast within the plates is due to a high density of dislocations. (b) Corresponding dark-field image showing the distribution of retained austenite.

Carbon Atoms

Carbon is an interstitial atom in ferritic iron, primarily occupying the octahedral interstices. There are three such interstices per iron atom. At a typical concentration of 0.4 wt% or about 2 at%, less than 1% of these interstices are occupied by carbon. Furthermore, there is a strong repulsion between carbon atoms in nearest neighbour sites. This means that carbon atoms almost always have an adjacent interstitial site vacant, leading to a very high diffusion coefficient when compared with the diffusion of substitutional solutes. In the latter case, the substitutional vacancy concentration is only 10−6 at temperatures close to melting, and many orders of magnitude less at the sort of temperatures where martensite is tempered. It follows that carbon diffuses much faster than substitutional atoms (including iron), as illustrated below.

Carbon in ferritic iron

(a) A carbon atom in an octahedral interstice in body-centred cubic iron.

Diffusion in iron

(b) The ratio of the diffusivity of a substitutional atom to that of carbon in body-centred cubic iron.

Precipitation of Iron Carbides

In high-carbon steels, the precipitation of excess carbon begins with the formation of a transition carbide, such as ε (Fe2.4C). ε-carbide can grow at temperatures as low as 50 °C. Indeed, most of the iron carbides can precipitate at low temperatures, well below those associated with the motion of substitutional solutes. This is because they grow by a displacive mechanism which does not require the redistribution of substitutional atoms (including iron); carbon naturally has to partition. This corresponds to a process known as paraequilibrium transformation in which the iron to substitutional solute ratio is maintained constant but subject to that constraint, the carbon achieves a uniform chemical potential.

Martensite is said to be supersaturated with carbon when the concentration exceeds its equilibrium solubility with respect to another phase. However, the equilibrium solubility depends on the phase. The solubility will be larger when the martensite is in equilibrium with a metastable phase such as ε carbide. Some 0.25 wt% of carbon is said to remain in solution after the precipitation of ε-carbide is completed.

Although most textbooks will begin a discussion of tempering with this first stage of tempering, involving the redistribution of carbon and precipitation of transition carbides, cementite can precipitate directly. This is particularly the case when the defect density is large. Trapped carbon atoms will not precipitate as transition carbides but cementite is more stable than trapped carbon.

Martensite tempered at 190 degrees

(a) Transmission electron micrograph of martensite in a Fe-4Mo-0.2C wt% steel after tempering at 190 °C for 1 hour. The carbon has in this case precipitated as fine particles of cementite. (b) Corresponding dark-field image showing the distribution of retained austenite, which has not been affected by the tempering.

Decomposition of Retained Austenite

Tempered martensite at 295 degrees

Tempering at higher temperatures, in the range 200–300 °C for 1 h induces the retained austenite to decompose into a mixture of cementite and ferrite. When the austenite is present as a film, the cementite also precipitates as a continuous array of particles which have the appearance of a film.

Dark field transmission electron micrograph of martensite in a Fe-4Mo-0.2C wt% steel after tempering at 295 °C for 1 hour. Only the cementite is illuminated. The film of cementite at the martensite plate boundaries is due to the decomposition of retained austenite.

Further Tempering

Tempering at even higher temperatures leads to a coarsening of the cementite particles, with those located at the plate boundaries growing at the expense of the intra-plate particles. The dislocation structure tends to recover, the extent depending on the chemical composition. The recovery is less marked in steels containing alloying elements such as molybdenum and chromium.

Bright field transmission electron micrograph of martensite in a Fe-4Mo-0.2C wt% steel after tempering at 420 °C for 1 hour.

Tempered martensite at 420 degrees

The recovery of the dislocation structure and the migration of dislocation-cell and martensite boundaries leads not only to a coarsening of the plates, but also an increase in the crystallographic misorientation between adjacent plates, as illustrated in the adjacent figure. The data are from Suresh et al., Ironmaking and Steelmaking 30 (2003) 379–384.

Misorientation graph

Precipitation of Alloy Carbides

Diffusion distance graph

Alloy carbides include M2C (Mo-rich), M7C3, M6C, M23C6 (Cr-rich), V4C3, TiC etc., where the 'M' refers to a combination of metal atoms.

However, all of these carbides require the long-range diffusion of substitutional atoms. They can only precipitate when the combination of time and temperature is sufficient to allow this diffusion. The figure on the left shows the calculated diffusion distance in ferrite for a tempering time of 1 h. It is evident that the precipitation of alloy carbides is impossible below about 500 °C for a typical tempering time of 1 h; the diffusion distance is then just perceptible at about 10 nm.

The alloy carbides grow at the expense of the less stable cementite. If the concentration of strong carbide forming elements such as Mo, Cr, Ti, V, Nb is large then all of the carbon can be accommodated in the alloy carbide, thereby completely eliminating the cementite.

Mo carbide micrograph Mo carbide dark field

Fe-0.1C-1.99Mn-1.6Mo wt% quenched to martensite and then tempered at 600 °C. (Photograph courtesy of Shingo Yamasaki). The precipitates are needles of Mo2C particles. The needles precipitate with their long directions along ⟨100⟩α.

Vanadium carbide micrograph Vanadium carbide dark field

Fe-0.1C-1.99Mn-0.56V wt% quenched to martensite and then tempered at 600 °C for 560 h (Photograph courtesy of Shingo Yamasaki). The precipitates are plates of V4C3 particles which precipitate on the {100}α planes.

Severe Tempering

Severe tempering micrograph

Fe-0.98C-1.46Si-1.89Mn-0.26Mo-1.26Cr-0.09V wt% tempered at 730 °C for 7 days. This transmission electron micrograph shows large cementite particles and a recovered dislocation substructure. The plate microstructure is coarsened but nevertheless retained because the carbides are located at plate boundaries.

Spheroidised cementite micrograph

Fe-0.98C-1.46Si-1.89Mn-0.26Mo-1.26Cr-0.09V wt% tempered at 730 °C for 21 days. The optical micrograph shows some very large spheroidised cementite particles. The ferrite has completely recrystallised into equiaxed grains.

Hardness

Hardness vs temperature graph

Fe-0.35C-Mo alloy quenched to martensite and then tempered at the temperature indicated for one hour (data from Bain's Alloying Elements in Steels). Whereas the plain carbon steel shows a monotonic decrease in hardness as a function of tempering temperature, molybdenum in this case leads to an increase in hardness once there is sufficient atomic mobility to precipitate Mo2C.

Secondary hardening is usually identified with the tempering of martensite in steels containing strong carbide forming elements like Cr, V, Mo and Nb. The formation of these alloy carbides necessitates the long-range diffusion of substitutional atoms and their precipitation is consequently sluggish. Carbides like cementite therefore have a kinetic advantage even though they may be metastable. Tempering at first causes a decrease in hardness as cementite precipitates at the expense of carbon in solid solution, but the hardness begins to increase again as the alloy carbides form. Hence the term secondary hardening.

Kinetics

Tempering kinetics flow chart

Typical time scales associated with the variety of processes that occur during tempering. Elements such as silicon and aluminium have a very low solubility in cementite. They greatly retard the precipitation of cementite, thus allowing transition iron-carbides to persist to longer times.

Case Studies: AerMet 100

AerMet 100 is a martensitic steel which is used in the secondary-hardened condition; its typical chemical composition is as follows:

Composition of Aermet 100 in wt%
CCoNiCrMoMnSiAlTiSP
0.2313.411.13.01.20.030.030.0040.0130.0010.003

The cobalt plays a key role in retarding the recovery of martensite during tempering, thereby retaining the defect structure on which M2C needles can precipitate as a fine dispersion. By increasing the stability of body-centred cubic iron, it also reduces the tendency of martensite to revert to austenite during tempering. The carbon concentration is balanced such that all the cementite is replaced by the much finer alloy carbides during secondary hardening.

The optimum combination of strength and toughness is obtained by tempering at 470 °C. Tempering at 430 °C, 5 h is associated with a minimum in toughness because of the precipitation of relatively coarse cementite platelets in a Widmanstätten array.

Strength of AerMet 100 Toughness of AerMet 100

Landing gear critical components are made from tempered martensite.

Landing gear part 1 Landing gear part 2 Landing gear part 3 Landing gear part 4

Temper Embrittlement

Tempering can lead to embrittlement when the steel contains impurities such as phosphorus, antimony, tin and sulphur. These impurities tend to segregate to the prior austenite grain boundaries and reduce cohesion across the boundary plane, resulting in intergranular failure.

Role of Prior Austenite Grain Boundaries

Ordinary steels are ferritic or pearlitic; both of these phases can grow by reconstructive transformation across austenite grain boundaries. By contrast, the coordinated motion of atoms accompanying displacive transformations cannot be sustained across austenite grain boundaries. Therefore, a vestige of the austenite grain boundary (prior austenite grain boundary) remains in the microstructure.

Martensite hindered by boundaries Intergranular failure illustration

Figure: (a) Martensite (α') is hindered by austenite grain boundaries whereas allotriomorphic ferrite (α) is not. (b) Failure at the prior austenite grain boundary.

650 °C Reversible Temper Embrittlement

Tempering at temperatures around 650 °C promotes the segregation of impurity elements such as phosphorus to the prior austenite grain boundaries. The tendency for embrittlement correlates strongly with an empirical J factor:

J = Mn + Si + 104 (P + Sn)

where the concentrations of elements are in weight percent.

To summarise, the impurity-controlled temper embrittlement occurs in bainite as it does in martensite; after all, neither of these transformation products cross austenite grain surfaces and hence leave them open for impurity segregation. By comparison, reconstructive transformation products such as allotriomorphic ferrite, can grow across and consume the austenite grain surfaces, thereby removing them entirely from the final microstructure.

Finally, it is worth noting that although the science of the embrittlement is well understood, for reasons of cost, commercial steels always contain more impurities than is desirable. Steps must therefore be taken to mitigate the impurity effects, for example by alloying with molybdenum to pin down the phosphorus and prevent it from segregating.

300–350 °C Temper Embrittlement

Fracture is again intergranular with respect to the prior austenite grain boundaries which become decorated with coarse cementite particles during tempering. At the same time, the grain boundaries are weakened by impurity segregation. The cementite particles crack under the influence of an applied stress and in this process concentrate stress at the weakened boundaries. These factors combine to cause embrittlement.

300–350 °C Tempered-Martensite Embrittlement

This effect is common in clean steels, with fracture occurring transgranularly relative to the prior austenite grain boundaries. It is attributed to the formation of cementite particles at the martensite lath boundaries and within the laths. During tempering, the particles coarsen and become large enough to crack, thus providing crack nuclei which may then propagate into the matrix. As a consequence, untempered low-carbon martensitic steels sometimes have a better toughness than when they are tempered, even though the untempered steel is stronger. The cementite behaves like a brittle inclusion.

Both of the impurity-controlled embrittlement phenomena can be minimised by adding about 0.5 wt% molybdenum to the steel. The Mo associates with phosphorus atoms in the lattice thereby reducing mobility and hence the extent to which they segregate to boundaries. Larger concentrations of molybdenum are not useful because precipitation occurs.

In many bainitic microstructures, tempering even at temperatures as high as 550 °C has only a small effect on cementite size and morphology. Consequently, the low-temperature embrittlement phenomena are not found in conventional bainitic microstructures.

Related Topics

Martensitic transformations

Transformation hardening

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Tempered martensitic steel band holding log in position.

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Tempered martensitic steel band holding log in position.

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Study guide: tempered martensite

Detailed review of microstructural and mechanical changes in steels

This study guide provides a detailed review of the microstructural and mechanical changes that occur during the tempering of martensite in steels. It covers the thermodynamic driving forces, the stages of precipitation, the role of alloying elements, and the phenomena associated with temper embrittlement.

Part 1: Short-Answer Quiz

Instructions: Answer the following questions in 2–3 sentences based on the provided text.

1. What is the technical definition of "tempering" in the context of martensitic steels?
2. Why is the stored energy of martensite significantly higher than that of bainite or ferrite?
3. Explain the concept of "paraequilibrium" during the transformation process.
4. How does the diffusion rate of carbon compare to substitutional solutes like iron or manganese in a ferritic lattice?
5. What microstructural changes characterise "Stage 1" of the tempering process?
6. Under what specific conditions can cementite precipitate directly rather than following the formation of transition carbides?
7. What is "secondary hardening," and which alloying elements are typically responsible for it?
8. How does the addition of cobalt influence the properties of AerMet 100 during tempering?
9. Why do displacive transformations like martensite leave "prior austenite grain boundaries" intact while reconstructive transformations do not?
10. Describe the mechanism of "650 °C Reversible Temper Embrittlement."

Part 2: Quiz Answer Key

  1. Tempering is a heat treatment where a metastable martensitic sample is held isothermally at a temperature where austenite cannot form. This process allows the microstructure and mechanical properties to evolve as the system approaches equilibrium through thermal activation.
  2. The stored energy of martensite is high (in excess of 1700 J mol−1) because of the trapping of carbon atoms within the product crystal, high strain energy from plate-like deformations, and the presence of twin interfaces. Carbon forced into solid solution is the largest single contributor to this stored energy.
  3. Paraequilibrium is a state where the ratio of iron to substitutional alloying elements remains constant because these atoms cannot diffuse, while carbon atoms redistribute until their chemical potential becomes uniform. This occurs during low-temperature transformations where carbon is mobile but substitutional elements are trapped.
  4. Carbon has a much higher diffusion coefficient because it is an interstitial atom occupying octahedral sites, which are mostly vacant. In contrast, substitutional solutes require vacancies to migrate, and the concentration of such vacancies is extremely low at tempering temperatures.
  5. During Stage 1, excess carbon in solid solution segregates to defects or forms clusters. It then precipitates as transition iron-carbides (like ε-carbide) in high-carbon alloys or as cementite in low-carbon steels.
  6. Cementite can precipitate directly when the defect density in the martensite is large. In these cases, trapped carbon atoms do not form transition carbides because cementite is more stable than the trapped carbon state.
  7. Secondary hardening is an increase in hardness at high tempering temperatures caused by the precipitation of fine alloy carbides (such as those containing Mo, Cr, V, or Ti). These carbides form through the long-range diffusion of substitutional atoms, which is only possible at temperatures typically above 500 °C.
  8. Cobalt retards the recovery of martensite during tempering, which helps retain the defect structure necessary for a fine dispersion of M2C needles. It also increases the stability of body-centred cubic iron, reducing the tendency for the martensite to revert to austenite.
  9. Displacive transformations involve coordinated atomic motion that cannot cross austenite grain boundaries, leaving them as "prior" boundaries in the final structure. Reconstructive transformations (like allotriomorphic ferrite) grow across and consume these boundaries, effectively removing them from the microstructure.
  10. 650 °C Reversible Temper Embrittlement is caused by the segregation of impurities like phosphorus to prior austenite grain boundaries, reducing cohesion and causing intergranular failure. It is "reversible" because these impurity atmospheres can be evaporated by increasing the temperature, followed by quenching to prevent re-segregation.

Part 3: Essay Questions

Instructions: Use the provided source context to develop comprehensive responses to the following prompts. (Answers not provided).


Part 4: Glossary of Key Terms

Term Definition
AerMet 100 A high-strength martensitic steel used in secondary-hardened conditions, known for its use in large aircraft landing gear.
Alloy Carbides Carbides formed with strong carbide-forming elements (Mo, Cr, V, etc.) that require long-range diffusion of substitutional atoms.
Cementite Fe3C; a stable iron carbide that precipitates during tempering, often coarsening at higher temperatures.
Displacive Transformation A transformation mechanism (like martensite formation) involving coordinated atomic motion and shape deformation without diffusion.
ε-carbide A transition iron carbide (Fe2.4C) that forms at low temperatures (as low as 50 °C) during the early stages of tempering high-carbon steels.
Isothermal A process occurring at a constant temperature.
J-factor An empirical formula (Mn + Si + 104(P + Sn)) used to correlate a steel's susceptibility to impurity-controlled embrittlement.
Martensite-start (MS) The temperature at which the transformation of austenite to martensite begins upon cooling.
Octahedral Interstices Specific sites within the iron crystal lattice where small interstitial atoms like carbon typically reside.
Paraequilibrium A kinetic state where carbon redistributes to achieve uniform chemical potential, but substitutional atoms remain immobile.
Prior Austenite Grain Boundary The original boundaries of the austenite grains that remain visible/functional after a displacive transformation to martensite or bainite.
Recovery The process during tempering where the dislocation density decreases and the internal structure of the martensite plates begins to reorganise.
Recrystallisation The final stage of severe tempering where ferrite plates transform into equiaxed grains, typically after long times at high temperatures.
Retained Austenite Austenite that remains untransformed after quenching to ambient temperature; it may decompose into ferrite and cementite during tempering.
Secondary Hardening A localised increase in hardness during tempering caused by the delayed precipitation of fine alloy carbides.
Tempering The heat treatment of martensite at temperatures below the austenite formation range to alter microstructure and mechanical properties.

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