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高速电火花加工微孔中重铸层诱导的疲劳降解:实验表征

Recast Layer-Induced Fatigue Degradation in High-Speed EDM Microholes: Experimental Characterization.

作者信息

Zhang Yaou, Zheng Qian, Wu Zeyu, Liao Hualin, Lu Yifan, Lu Juncheng

机构信息

State Key Laboratory of Mechanical System and Vibration, Shanghai Jiao Tong University, Shanghai 200240, China.

出版信息

Materials (Basel). 2025 Apr 27;18(9):1985. doi: 10.3390/ma18091985.

Abstract

High-speed electrical discharge machining (EDM) is crucial for drilling aerospace components, but the fatigue effects of its recast layer are still not well understood. This study investigates the fatigue behavior of high-speed EDM-processed specimens using ultrasonic fatigue testing and microscopic analysis. The recast layer showed a 20.4% increase in hardness and a 16.5% decrease in elastic modulus compared to the base material. Fatigue cracks originated from microcracks, pores, and inclusions within the recast layer, as well as at its interface with the substrate. Microscopic crack initiation was influenced by defect interactions, while macroscopic crack initiation occurred near the maximum hole diameter perpendicular to the loading direction due to stress concentration. The specimens exhibited bimodal fatigue life: shorter lifetimes were observed when macroscopic stress concentrations overlapped with recast layer defects such as cracks and voids, while defect-free regions significantly extended durability. The non-uniform distribution of the recast layer critically links microstructural heterogeneity to variations in fatigue failure. These findings highlight how recast layer characteristics influence crack nucleation and life variability in EDM-processed components, offering valuable insights for optimizing machining parameters to reduce fatigue risks in critical aerospace applications.

摘要

高速放电加工(EDM)对于航空航天部件的钻孔至关重要,但其重铸层的疲劳影响仍未得到充分理解。本研究使用超声疲劳测试和微观分析来研究高速电火花加工试样的疲劳行为。与基体材料相比,重铸层的硬度提高了20.4%,弹性模量降低了16.5%。疲劳裂纹起源于重铸层内的微裂纹、气孔和夹杂物,以及重铸层与基体的界面处。微观裂纹萌生受缺陷相互作用影响,而宏观裂纹萌生则由于应力集中发生在垂直于加载方向的最大孔径附近。试样表现出双峰疲劳寿命:当宏观应力集中与重铸层缺陷(如裂纹和孔隙)重叠时,观察到较短的寿命,而无缺陷区域显著延长了耐久性。重铸层的不均匀分布将微观结构的不均匀性与疲劳失效的变化紧密联系起来。这些发现突出了重铸层特性如何影响电火花加工部件中的裂纹形核和寿命变异性,为优化加工参数以降低关键航空航天应用中的疲劳风险提供了有价值的见解。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/e852/12072793/4d558c66bd23/materials-18-01985-g001.jpg

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