计算机集成制造系统 ›› 2016, Vol. 22 ›› Issue (第9期): 2118-2126.DOI: 10.13196/j.cims.2016.09.008

• 产品创新开发技术 • 上一篇    下一篇

航空发动机叶片保形加工中的定位误差数值建模与分析

王辉,周明星,余杰,王文宇,黄博浩,融亦鸣   

  1. 1.清华大学机械工程系精密超精密制造装备及控制北京市重点实验室
    2.西安航空发动机集团公司
  • 出版日期:2016-09-30 发布日期:2016-09-30
  • 基金资助:
    国家自然科学基金资助项目(51575310);清华大学自主科研计划资助项目。

Positioning error modeling and analysis for jet-engine blade's keeping-aerofoil machining

  • Online:2016-09-30 Published:2016-09-30
  • Supported by:
    Project supported by the National Natural Science Foundation,China(No.51575310),and the Tsinghua University Initiative Scientific Research Program,China.

摘要: 针对航空发动机近净成形转子叶片保形加工中的误差控制问题,基于叶片3D点云数据模型,提出了定位误差向叶片加工误差的传递作用机制及其分析模型。进一步建立了叶片工件定位误差的随机模拟与数值分析方法,以实现对叶片定位误差的准确估计。以某型低压转子叶片的机械加工为例,对工件的定位误差进行了分析和评估,验证了所提方法的可用性和有效性。

关键词: 近净成形转子叶片, 精密加工, 定位误差, 数值仿真, 航空发动机

Abstract: As a typical thin-walled workpiece,the machining performance of jet-engine rotor blade was affected very much by its positioning errors when held by fixtures.Aiming at the error control problem in keeping-aerofoil machining of jet-engine blade's near-net shaped formed,the dimensional errors accumulative process was modeled and its numerical calculation method was proposed based on 3D point cloud model of rotor workpiece.A Monte-Carlo random simulation method was presented to evaluate the positioning tolerance of rotor workpiece.A rotor blade in a jet-engine low pressure compressor was milled precisely,and the effectiveness of proposed method was validated by analyzing,evaluating and verifying the positioning error of workpieces.

Key words: near-net shaped formed rotor, precision machining, positioning error, numerical simulation, jet-engine

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