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Research on the Technology of NC Abrasive Belt Grinding for the Leading and Trailing Edges of Aero-engine Blades

机译:航空发动机叶片前缘和后缘数控砂带磨削技术的研究

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摘要

This paper provides an analysis of the processing status and the existing problems of leading and trailing edges,and proposes a new seven-axis linkage CNC grinding method.What's more,the paper carries out the forging blade edge abrasive belt grinding experiment.Finally,on the basis of experimental result,grinding process parameters are optimized,and the improved scheme is put forward,Through the experiment,the feasibility of the seven-axis CNC abrasive belt grinding method is verified.
机译:本文分析了加工状态以及前缘和后缘存在的问题,并提出了一种新的七轴联动数控磨削方法。此外,本文还进行了锻造刃口砂带磨削实验。在实验结果的基础上,优化了磨削工艺参数,提出了改进方案,并通过实验验证了七轴数控砂带磨削方法的可行性。

著录项

  • 来源
  • 会议地点 Hangzhou(CN)
  • 作者单位

    The State Key Laboratory of Mechanical Transmission,Chongqing University,China;

    Chongqing Engineering Research Center for Material Surface Precision Machining and Whole Set Equipments,Chongqing,China;

    The State Key Laboratory of Mechanical Transmission,Chongqing University,China;

    Chongqing Engineering Research Center for Material Surface Precision Machining and Whole Set Equipments,Chongqing,China;

    The State Key Laboratory of Mechanical Transmission,Chongqing University,China;

    Chongqing Engineering Research Center for Material Surface Precision Machining and Whole Set Equipments,Chongqing,China;

    Avic Xi'an Aero-engine LTD.Xi'an,China;

  • 会议组织
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 磨料;
  • 关键词

    precision forging blade; leading and trailing edges; abrasive belt grinding; seven-axis linkage;

    机译:精密锻造刀片;前缘和后缘;砂带磨削;七轴联动;

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