2014
DOI: 10.1016/j.actamat.2013.10.017
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Build direction dependence of microstructure and high-temperature tensile property of Co–Cr–Mo alloy fabricated by electron beam melting

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Cited by 176 publications
(70 citation statements)
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“…The tensile testing of specimens fabricated by EBAM produced average UTS of 1.45 GPa, YS of 0.51 GPa, and an elongation of 3.6%, which are better than wrought or cast Co-Cr-Mo alloys. Sun et al [49] Ramirez et al [50] investigated the effects of precipitate (Cu 2 O) on the microstructure and mechanical properties of EBAM Cu parts. These precipitate-dislocation architectures create increased hardness, ranging from a base-plate hardness of HV 57 to an EBAM part hardness of HV 88, referenced to the precursor powder containing Cu 2 O precipitates that has a hardness of HV 72.…”
Section: Other Materials Used In Ebammentioning
confidence: 99%
“…The tensile testing of specimens fabricated by EBAM produced average UTS of 1.45 GPa, YS of 0.51 GPa, and an elongation of 3.6%, which are better than wrought or cast Co-Cr-Mo alloys. Sun et al [49] Ramirez et al [50] investigated the effects of precipitate (Cu 2 O) on the microstructure and mechanical properties of EBAM Cu parts. These precipitate-dislocation architectures create increased hardness, ranging from a base-plate hardness of HV 57 to an EBAM part hardness of HV 88, referenced to the precursor powder containing Cu 2 O precipitates that has a hardness of HV 72.…”
Section: Other Materials Used In Ebammentioning
confidence: 99%
“…Hereafter, the CCM alloy subjected to HPT and subsequent annealing at the temperature T for the duration of t, is designated by CCM HPTA(T/t) as CCM HPTA(1273 K,0.3 ks) for the case of T = 1273 K and t = 0.3 ks. The equivalent strain ε eq at a distance r from the disk center was estimated by the following equation: 10) ε eq = 2πrN/t √ 3 (1) where N is the rotation number and t is the specimen thickness. ε eq was calculated according to eq.…”
Section: Materials Preparationmentioning
confidence: 99%
“…[1][2][3] The mechanical properties of CCM alloys need to be further improved to reduce the probability of failure in biomedical applications. 4) Grain re nement is effective to improve the mechanical properties of CCM alloys.…”
Section: Introductionmentioning
confidence: 99%
“…Furthermore, EBM additive manufacturing can produce arti cial implants in different shapes and sizes for different patients at the same time, so it is an attractive way to manufacture Co-Cr-Mo alloy implants. Many studies [21][22][23][24][25] are now conducted on these alloys. In a Co-Cr-Mo alloy at equilibrium, the face-centered cubic (fcc, γ, or γ-fcc) phase is stable at temperatures above 800 C, while the hexagonal close-packed (hcp, ε, or ε-hcp) phase is stable at lower temperatures.…”
Section: Introductionmentioning
confidence: 99%