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Ultrasonic Fatigue Testing in the Tension-Compression Mode
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超声波辅助加工中疲劳的机械模型
Reza Teimouri1, Marcin Grabowski1
1Faculty of Mechanical Engineering, Cracow University of Technology, 31-864 Cracow, Poland.
Materials (Basel, Switzerland)
|October 16, 2024
概括
超声波辅助削通过提高表面完整性,显著提高了Inconel 718的疲劳寿命. 这种先进的加工工艺优化了表面性能,以实现航空材料的最大疲劳性能.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 制造过程 制造过程 制造过程
背景情况:
- 优化航空材料的疲劳寿命需要先进的加工来提高表面完整性.
- 当前的流程需要整体模型来最大限度地提高疲劳寿命.
研究的目的:
- 为了研究轴向超声波辅助磨削对Inconel 718疲劳寿命的影响.
- 开发一种混合模型,通过表面完整性方面将加工因素与疲劳寿命相关联.
主要方法:
- 在Inconel 718的轴超声波辅助削.
- 混合模型结合了回归分析和分析建模.
- 映射过程输入到表面完整性方面 (粗度,硬度,残余应力).
- 使用基于压力的方法将表面完整性方面映射到疲劳寿命中.
主要成果:
- 测量和预测疲劳寿命之间的密切一致 (误差<2x分散).
- 超声波振动,高振幅,料速率和切割速度显著提高了疲劳寿命 (3倍改善).
- 增强的压力余应力和工作硬化有助于改善疲劳寿命.
结论:
- 轴性超声波辅助削是有效提高Inconel 718疲劳寿命.
- 开发的混合模型准确地预测了疲劳寿命.
- 优化工艺参数,特别是超声波振动,对于最大限度地提高疲劳性能至关重要.
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