多孔涂层Ti-6A1-4V合金的烧结后热处理。

S D Cook, E A Renz, R J Haddad
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引用次数: 3

摘要

先前的研究表明,多孔Ti-6A1-4V合金涂层的应用导致基体材料疲劳性能大幅降低。这种现象是由于微观结构从等轴α - β微观结构转变为层状结构和多孔涂层产生的缺口效应造成的。在Ti-6A1-4V合金中,片层组织具有最差的疲劳性能。本研究考察了不同的烧结后热处理方法,这些热处理方法可以改变材料的微观结构,从而可能提高材料的疲劳性能。经热处理后,合金的显微组织向片层组织转变,有的接近完全转变的针状α组织。在缺口状态下,Ti-6A1-4V合金的针状α组织表现出最佳的疲劳性能。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Post-sintering heat treatments for porous coated Ti-6A1-4V alloy.

Previous studies have shown that the application of a porous Ti-6A1-4V alloy coating results in a substantial decrease in the substrate material fatigue properties. This phenomenon is due to both a microstructural change from the equiaxed alpha-beta microstructure to a lamellar structure and a notch effect created by the porous coating. The lamellar microstructure has been shown to exhibit the worst fatigue properties of the most common structures obtained in Ti-6A1-4V alloy. This study examined various post-sintering heat treatments which would alter the material microstructure and possibly result in improved fatigue performance. The heat treatments examined produced alternate microstructures to the lamellar structure and some approached the totally transformed acicular alpha structure. The acicular alpha structure has been shown to exhibit the best fatigue properties for Ti-6A1-4V alloy in the notched condition.

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