对响应表面方法和有限元方法进行研究,以在钻孔过程中模拟飞机发动机机身变形
Andrzej Matras1, Magdalena Machno2
1Department of Production Engineering, Faculty of Mechanical Engineering, Cracow University of Technology, 31-155 Cracow, Poland.
Materials (Basel, Switzerland)
|January 8, 2025
概括
本研究分析了飞机发动机组件在Inconel 718中的钻孔参数. 它开发数学模型来预测和最小化加工过程中薄壁结构的变形.
科学领域:
- 制造业 工程 制造工程
- 材料科学 材料科学 材料科学
- 航空航天工程 航空航天工程
背景情况:
- 航空业寻求高效的制造方法,在加工薄壁元件方面面临挑战.
- 加工像Inconel 718这样的超级合金由于材料特性而存在困难.
研究的目的:
- 分析钻井参数对薄壁Inconel 718飞机发动机组件变形的影响.
- 开发和验证用于预测切削力和变形的数学模型.
主要方法:
- 使用响应表面方法 (RSM) 的实验研究.
- 对于结构分析的有限元法 (FEM) 模拟.
- 同时应用实验方法和计算方法.
主要成果:
- 开发的数学模型准确地描述了切割参数,力和变形之间的非线性关系.
- 量化了钻井参数对复杂,薄壁结构变形的影响.
- 通过实验数据和FEM计算之间的强相关性来验证模型.
结论:
- RSM和FEM的综合方法为分析和优化加工过程提供了有效的工具.
- 开发的模型和方法适用于改善飞机发动机部件制造的工业条件.
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