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航发叶片前后缘数控砂带磨削关键技术研究

张明德 蔡汉水 谢乐 罗冲

机械科学与技术2018,Vol.37Issue(5):797-803,7.
机械科学与技术2018,Vol.37Issue(5):797-803,7.DOI:10.13433/j.cnki.1003-8728.2018.0521

航发叶片前后缘数控砂带磨削关键技术研究

Research on Key Technology of CNC Abrasive Belt Grinding for Aircraft Engines Blade Edges

张明德 1蔡汉水 1谢乐 1罗冲1

作者信息

  • 1. 重庆理工大学机械工程学院,重庆400054
  • 折叠

摘要

Abstract

In order to improve the machining accuracy and efficiency of the leading and the trailing edges (LTE) of aircraft engines blade,the existing problems in grinding of the current aircraft engines blade edges were analyzed,combined with the current requirements of machining technology for LTE and the motion control algorithms of computer numerical control(CNC) belt grinding machine,considering the influence of the grinding elements such as particle size,contact force,belt speed and feed rate,the tool trajectories are optimized,a grinding technology of the blade edges is put forward.Finally,the aircraft engines blades were subjected to actual grinding experiments.The experimental results show that the grinding method can obviously improve the machining precision and the surface roughness of the blade.

关键词

航发叶片/前后缘/运动控制算法/磨削要素/工艺方法

Key words

aircraft engines blade/edges/motion control algorithms/grinding elements/grinding technology

分类

机械制造

引用本文复制引用

张明德,蔡汉水,谢乐,罗冲..航发叶片前后缘数控砂带磨削关键技术研究[J].机械科学与技术,2018,37(5):797-803,7.

基金项目

国家科技重大专项项目(2014ZX02001031)与重庆理工大学研究生创新基金项目(YCX2016218)资助 (2014ZX02001031)

机械科学与技术

OA北大核心CSCDCSTPCD

1003-8728

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