Fracture mechanism of Ti60 alloy at high temperature in very high cycle fatigue regime and fatigue life prediction

Author:

Zhou Qikai12,Huang Zhiyong1,Qian Hongjiang1,Wang Jian1,Shen Zeshuai1,Pan Kai3,Chen Yonghui4

Affiliation:

1. School of Aeronautics and Astronautics Sichuan University Chengdu China

2. Facility Design and Instrumentation Institute China Aerodynamics Research and Development Center Mianyang China

3. Chinese Aeronautical Establishment Beijing China

4. National Key Laboratory of Strength and Structural Integrity Aircraft Strength Research Institute of China Xi'an China

Abstract

AbstractThis study aimed to investigate the failure mechanism of Ti60 titanium alloy in the high cycle fatigue (HCF) and very high cycle fatigue (VHCF) at 500°C. Ti60 specimens were characterized before and after the 500°C VHCF test, and the fracture surfaces were observed. The results show that there are three different fatigue failure mechanisms at 500°C: (i) equiaxed primary α phase (αp) cleavage, forming small unsmooth facets and rough fracture area (RA), and fusion of non‐adjacent facets to grow into the main crack. (ii) αp grains gather into large grain with triple junction, and large grain slip to form large fusion facet. (iii) Oxide shedding and then cracks form. A dynamic recurrent neural network model is used to predict the fatigue life of Ti60 alloy, 91% of the overall predictions were within the scatter band of 3.0, and 100% were within the scatter band of 5.0.

Funder

National Natural Science Foundation of China

National Major Science and Technology Projects of China

Key Research and Development Program of Sichuan Province

Publisher

Wiley

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