Effects of microstructure on the short fatigue crack initiation and propagation characteristics of biomedical α/β titanium alloys

被引:0
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作者
Toshikazu Akahori
Mitsuo Niinomi
Kei-Ichi Fukunaga
Ikuhiro Inagaki
机构
[1] Toyohashi University of Technology,the Department of Production Systems Engineering
[2] Osaka Steel Works,the Railway Parts & Forging Manufacturing Department
[3] Kansai Division,undefined
[4] Sumitomo Metal Industries,undefined
[5] Ltd.,undefined
关键词
Fatigue; Material Transaction; Fatigue Crack; Crack Initiation; Fatigue Strength;
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学科分类号
摘要
This article presents the results of a study of the effects of microstructure on the fatigue strength and the short fatigue crack initiation and propagation characteristics of a biomedical α/β titanium alloy, Ti-6Al-7Nb. The results are compared to those obtained from a Ti-6Al-4V extra-low interstitial (ELI) alloy. Fatigue crack initiation occurs mainly at primary α grain boundaries in an equiaxed α structure, whereas, in a Widmanstätten α structure, initiation occurs within the α colonies and prior β grains, where α plates are inclined at around 45 deg to the stress-axis direction. In an equiaxed α structure, the short fatigue crack initiation and propagation life, where the length of the crack (a) is in a microstructurally short fatigue-crack regime (2a < 50 µm), occupies around 50 pct of the total fatigue life. On the other hand, the fatigue crack in a Widmanstätten α structure initiates at very early stages of fatigue, and, therefore, the fatigue crack-initiation life occupies a few percentages of the total fatigue life in an α structure. Then, the short fatigue crack propagates rapidly and is arrested at the grain boundaries of α colonies or prior β grains for a relatively long period, until the short crack passes through the boundaries to specimen failure. Therefore, the short fatigue crack-arrest life occupies more than 90 pct of the total fatigue life in a Widmanstätten α structure. These trends are similar between the Ti-6Al-7Nb and Ti-6Al-4V ELI alloys and biomedical α/β titanium alloys. The total fatigue life for the Ti-6Al-7Nb alloy with an equiaxed α structure is changed by the volume fraction of primary α phase and the cooling rate after solution treatment. By increasing the volume fraction of the primary α phase from 0 to 70 pct, the fatigue limit of the Ti-6Al-7Nb alloy is raised. Changing the cooling rate after solution treatment by switching from air cooling to water quenching improves the fatigue limit of the Ti-6Al-7Nb alloy significantly.
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页码:1949 / 1958
页数:9
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