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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:分析了前缘和后缘的加工现状及存在的问题,提出了一种新的七轴联动数控磨削方法。并进行了锻造刃口砂带磨削试验。最后,根据实验结果,对磨削工艺参数进行了优化,并提出了改进方案。通过实验,验证了七轴数控砂带磨削方法的可行性。

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