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多孔涂层Ti-6%Al-4%V植入合金的疲劳强度

The fatigue strength of porous-coated Ti-6%Al-4%V implant alloy.

作者信息

Yue S, Pilliar R M, Weatherly G C

出版信息

J Biomed Mater Res. 1984 Nov-Dec;18(9):1043-58. doi: 10.1002/jbm.820180908.

Abstract

The fatigue behaviour of Ti-6Al-4V (extra low interstital) alloy coated with Ti-6Al-4V powder was investigated using rotating bending fatigue testing. It was found that the high cycle fatigue strength of porous coated specimens exhibited a substantial decrease compared to uncoated specimens of the same microstructure. Chemical analysis of the sintered surface revealed significant increases of interstitials compared to the bulk analysis, but it is concluded that this would not adversely affect the fatigue strength. Scanning electron microscopy revealed crack initiation close to particle/substrate contact interfaces and it is concluded that stress intensification due to these interface regions are major sources of weakness with respect to fatigue strength. Finally it was found that subjecting a polished Ti-6Al-4V specimen to the heat treatment required for sintering resulted in delineation of prior beta grain boundaries and it is suggested that this also contributes to the inferior fatigue strength of porous coated Ti-6Al-4V.

摘要

采用旋转弯曲疲劳试验研究了涂覆Ti-6Al-4V粉末的Ti-6Al-4V(超低间隙)合金的疲劳行为。结果发现,与具有相同微观结构的未涂层试样相比,多孔涂层试样的高周疲劳强度显著降低。烧结表面的化学分析表明,与整体分析相比,间隙元素显著增加,但得出的结论是,这不会对疲劳强度产生不利影响。扫描电子显微镜显示裂纹在颗粒/基体接触界面附近萌生,得出的结论是,由于这些界面区域导致的应力强化是疲劳强度方面的主要薄弱来源。最后发现,对抛光的Ti-6Al-4V试样进行烧结所需的热处理会导致先前β晶界的 delineation,并且认为这也导致了多孔涂层Ti-6Al-4V疲劳强度较低。 (注:“delineation”这个词可能有误,推测可能是“delamination”分层之意,但按要求未修改)

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