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润滑组件壳体高温耐久开裂分析与改进

中文摘要英文摘要

针对配套于某航空发动机滑油系统的润滑组件在高温耐久试验过程中壳体出现开裂的问题,采用宏观和微观检查的方法对裂纹产生的原因进行了分析。仿真分析显示,开裂位置由于圆角较小且刚度不足,存在应力集中的现象,为疲劳失效的热点部位,同时壳体铸造的表面粗糙度较差,进一步促进了裂纹的萌生。对壳体结构进行了设计改进,包括增大内部圆角和增加加强筋,仿真结果显示结构优化后疲劳寿命提升了1013倍;同时对铸造工艺进行了优化,通过对铸造型芯的表面处理,改善了表面粗糙度。改进后的壳体通过了高温耐久试验验证。

Regarding the problem that the housing of the lubrication component supporting an aero-engine oil system cracks during high-temperature durability testing, macroscopic and microscopic inspection methods were used to locate the cause of the crack. Simulation analysis shows that the cracking position has a small fillet and insufficient stiffness, resulting in stress concentration, which is a hot spot for fatigue failure. At the same time, the high surface roughness of the cast further intensified the initiation of the crack. Design optimization has been made to the housing structure, including increasing internal rounded corners and adding reinforcing ribs. Simulation results show that the fatigue life has been increased by 1013 times after structural optimization. At the same time, the casting process was optimized, and the surface roughness was lowered by surface treatment of the casting core. The improved housing can pass the high-temperature durability test verification.

谢春稳、胡海波、张帆

中航工业新乡航空工业集团民机研发中心,河南新乡 453019中航工业新乡航空工业集团民机研发中心,河南新乡 453019中航工业新乡航空工业集团民机研发中心,河南新乡 453019

航空

高温耐久壳体强度结构优化铸造工艺

high temperature durabilityhousing strengthstructural optimizationcasting process

谢春稳,胡海波,张帆.润滑组件壳体高温耐久开裂分析与改进[EB/OL].(2025-06-18)[2025-07-19].http://www.paper.edu.cn/releasepaper/content/202506-78.点此复制

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