首页> 外文会议>International symposium on advances in abrasive technology >Research on the Technology of NC Abrasive Belt Grinding for the Leading and Trailing Edges of Aero-engine Blades
【24h】

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NC磨料带研磨技术研究

获取原文

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:本文提供了对处理状态和领先和尾边的现有问题的分析,提出了一种新的七轴联动数控磨削方法。此外,纸张执行锻造刀刃磨料带磨削实验。最后,实验结果的基础,研磨工艺参数经过优化,并通过实验提出了改进的方案,验证了七轴CNC磨料带研磨方法的可行性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号