Crack initiation and propagation in Ti-6Al-4V-0.55Fe alloy subjected to the low-cycle dwell-fatigue

Hui Du, Baofei Liu, Qinghua Deng, Wanli Ren, Feng Li, Liang Feng, Hui Chang, Jie Ding
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Abstract

This paper investigated the crack initiation and propagation behaviour of Ti-6Al-4V-0.55Fe alloy under the low-cycle dwell-fatigue. It found that cracks were preferred to initiate at the α/β-phase boundaries, the α/α-phase boundaries, and the twinning boundaries within the α-phase. Twinning played a key role in the crack initiation, for the reason that it changed the phase orientation on its sides. Besides, grain orientation was another important factor in the crack nucleation. The soft/hard grain boundaries may become the crack nucleation sites due to the dislocation pile-up. In addition, as the dwell time increased, the fraction of the high Schmid factor of prismatic slip was increasing, which resulted in more cracks. Furthermore, the fracture mode of the alloy was intergranular fracture with microporous aggregation.
低循环驻留疲劳下 Ti-6Al-4V-0.55Fe 合金的裂纹萌生和扩展
本文研究了 Ti-6Al-4V-0.55Fe 合金在低循环驻留疲劳下的裂纹起始和扩展行为。研究发现,裂纹更倾向于在α/β相边界、α/α相边界以及α相内部的孪晶边界萌生。孪晶对裂纹的产生起着关键作用,因为孪晶改变了裂纹两侧的相取向。此外,晶粒取向也是裂纹成核的另一个重要因素。由于位错堆积,软/硬晶界可能成为裂纹成核点。此外,随着停留时间的增加,棱柱滑移的高 Schmid 因子部分也在增加,这导致了更多的裂纹。此外,合金的断裂模式是晶间断裂和微孔聚集。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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