在基于响应表面方法的TC17合金转过程中,研究表面完整性和疲劳性质
Xunqing Lai1, Yuannan Wang2, Dan Wang1
1College of Mechanical and Electrical Engineering, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China.
Materials (Basel, Switzerland)
|November 25, 2023
概括
优化合金转参数通过增加压缩余应力和最大限度地降低表面粗度来提高疲劳寿命. 在航空航天应用中,料速度是实现所需表面完整性的关键.
科学领域:
- 材料科学 材料科学 材料科学
- 机械工程 机械工程
- 航空航天工程 航空航天工程
背景情况:
- 合金对于航空航天非常重要,因为它们的强度与重量比很高.
- 提高合金组件的使用寿命对于飞机的安全性和性能至关重要.
- 表面完整性显著影响航空航天部件的疲劳寿命.
研究的目的:
- 研究转参数对合金表面残余应力和粗度的影响.
- 建立一个数学模型,将表面完整性参数与疲劳寿命相关联.
- 为了确定最佳的转向参数,以提高疲劳性能.
主要方法:
- 使用响应表面方法分析转参数 (料率,切割深度,切割速度).
- 采用多重线性回归来开发基于表面完整性的疲劳寿命预测模型.
- 进行实验测试以验证模型和发现.
主要成果:
- 转参数会影响表面残余应力 (料速率>切割深度>切割速度) 和粗度 (料速率>切割速度>切割深度).
- 余压力对疲劳寿命有最显著的积极影响,其次是表面粗度 (负面影响).
- 料速度对残余应力和表面粗性都具有关键影响.
结论:
- 优化料速率对于实现卓越的表面完整性 (Ra < 2μm) 和高余压应力至关重要.
- 建立的数学模型有效地根据表面完整性参数预测疲劳寿命.
- 这些发现为选择适当的加工参数提供了基础,以延长合金航空航天部件的使用寿命.
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