Rotating bending fatigue mechanisms of L-PBF manufactured Ti-6Al-4V alloys using in situ X-ray tomography

被引:8
|
作者
Wu, Zhengkai [1 ]
He, Ziang [1 ]
Wu, Shengchuan [1 ]
Gao, Xi [1 ]
Lei, Liming [2 ]
Liu, Changkui [3 ]
Chen, Bingqing [3 ]
Dong, Chengli [3 ]
机构
[1] Southwest Jiaotong Univ, State Key Lab Rail Transit Vehicle Syst, Chengdu 610031, Peoples R China
[2] Taihang Lab, Chengdu 610213, Peoples R China
[3] AECC Beijing Inst Aeronaut Mat, Beijing 100095, Peoples R China
基金
中国国家自然科学基金;
关键词
Titanium alloys; Additive manufacturing; Rotating bending fatigue; Multiple cracks; In situ X-ray computed tomography; HEAT-TREATMENT; MICROSTRUCTURE; POROSITY;
D O I
10.1016/j.ijfatigue.2023.107876
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Lightweight titanium alloys are being increasingly used in high value structures, but in-depth knowledge of the rotating bending fatigue (RBF) mechanism remains insufficient, particularly for additively manufactured components. In response, an in situ RBF test rig was developed for the first time, using time-lapse synchrotron radiation X-ray microtomography (SR-& mu;CT) to identify the failure behavior of laser powder bed fused Ti-6Al-4V alloys. The RBF damage evolution was characterized by combining the non-destructive SR-& mu;CT with post-mortem scanning electron microscopy, and electron backscatter diffraction. Compared with RBF life data and fatigue long crack growth from standard specimens, in situ RBF tests proved to be reliable, in revealing the fatigue mechanism. However, fatigue short cracks in the representative mini RBF testing campaign were found to initiate from microstructural features of outer surfaces, instead of gas pores or lack of fusion defects. It is demonstrated that neither the standard nor the improved Kitagawa-Takahashi diagrams are unable to correlate the fatigue strength to manufacturing defects. The equivalent defect should include the effect of surface microstructural defects, in addition to internal defects, when studying additively manufactured alloys.
引用
收藏
页数:13
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