Evaluation of Fatigue Crack Growth in α-Titanium Alloys

Osamu Umezawa , Makiko Hamada , Toshifumi Tatsumi
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引用次数: 6

Abstract

The fatigue crack growth modeling that based on linear fracture mechanics under the Mode I condition provided a good estimate of the stress intensity range for subsurface crack growth in α or near α-type titanium alloys. Based on the relationship between crack growth rate and stress intensity factor range, the fatigue crack propagating life was evaluated by the Paris rule. The subsurface crack initiation process consumed a large number of cycles to failure. Microstructure may strongly affect on not only subsurface crack initiation but also crack growth. The microstructural modification to prevent microcrack growth should be taken into account.

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α-钛合金疲劳裂纹扩展的评价
基于I型条件下线性断裂力学的疲劳裂纹扩展模型可以较好地估计α型或α型钛合金亚表面裂纹扩展的应力强度范围。根据裂纹扩展速率与应力强度因子范围的关系,采用Paris准则对疲劳裂纹扩展寿命进行了评价。地下裂纹萌生过程需要大量的循环才能失效。微观组织不仅对裂纹萌生和裂纹扩展有重要影响。应考虑防止微裂纹扩展的显微组织改性。
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