Grain refinement of biomedical Co–27Cr–5Mo–0.16N alloy by reverse transformation
Introduction
Cobalt–chromium–molybdenum (Co–Cr–Mo) based alloys have been used in various medical applications, such as hip and knee joint replacements, metallic coronary stents, and denture bases, because of their good biocompatibility and mechanical properties, and their excellent resistance to wear and corrosion. Improved reliability and safety are required for hip and knee joint replacements, since these replacements are being performed in younger patients, greatly lengthening the implants' period of service.
One of the most effective methods of achieving higher mechanical reliability is grain refinement, because it increases the toughness of the material. So far, conventional grain refinement techniques for medical Co–Cr–Mo based alloys have involved thermomechanical treatment with recrystallization, such as hot forging, swaging, and rolling, and do result in greatly improved mechanical properties [1], [2], [3]. However, when inhomogeneous strains are introduced during the hot working process, uniform fine grains are not produced. Thus, the mechanical properties vary from area to area, owing to the non-uniform grain size distribution. Another grain refinement technique is heat treatment using the solid-phase transformation without any hot or cold plastic deformation process. In carbon steels and high-nitrogen stainless steel, grain refinement was successfully achieved without any deformation process by reverse transformation from a lamellar structure to austenite [4], [5]. It may be possible to apply a similar technique to the Co–27Cr–5Mo–0.16N alloy, because it also undergoes a eutectoid transformation (γ → ε + Cr2N), analogous to that observed in high-nitrogen stainless steels.
This work examines the grain refinement of Co–27Cr–5Mo–0.16N alloy by reverse transformation from a lamellar structure consisting of ε-hcp and Cr2N to the γ-fcc phase, without any hot or cold deformation processes.
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Material and methods
A commercially purchased Co–27Cr–5Mo–0.16N alloy, in the form of a cylindrical bar 30 mm in diameter, was used in this study. The composition by mass% was: 27.2Cr, 5.5Mo, 0.12Ni, 0.04C, 0.16N, with Co making up the balance. A cubic specimen (10 mm on a side) for microstructural observation, and a rectangular bar specimen (7 × 7 × 30 mm) for tensile testing were cut using an electric discharge machine. The microstructures were observed at the center of the cross-sectional area of the cubic specimen.
Microstructure prior to reverse transformation treatment
Fig. 1(a) and (b) shows an image quality map and an XRD pattern, respectively, of the Co–27Cr–5Mo–0.16N alloy after solution treatment at 1473 K for 3.6 ks. The microstructure consisted of equiaxed, uniform γ grains with no precipitates. The average grain size with standard deviation of the specimen after solution treatment was 201 ± 8.1 μm.
Fig. 2 shows (a) an SEM micrograph, (b) an XRD pattern, and (c) and (d) inverse pole figure orientation maps with a boundary map of the Co–27Cr–5Mo–0.16N alloy
Conclusions
An advanced grain refinement technique, based on heat treatment utilizing a reverse transformation, and variation in the tensile properties with various heat treatments of biomedical Co–27Cr–5Mo–0.16N alloy were investigated. The results obtained are summarized as follows:
- 1.
The γ phase transformed due to a eutectoid reaction during aging at 1073 K for 90 ks, forming a lamellar structure of ε-hcp and Cr2N phases in the alloy, which was quite similar to the “pearlite” formed in carbon steels and
Acknowledgements
This research was supported by a grant for Cooperation of Innovative Technology and Advanced Research in Evolutional Area from the Ministry of Education, Culture, Sports, Science, and Technology of Japan.
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