航空学报 > 1994, Vol. 15 Issue (5): 636-640

叶片型面刀位计算方法分析

魏源迁   

  1. 浙江大学机械系,杭州,310027
  • 收稿日期:1993-01-04 修回日期:1993-05-10 出版日期:1994-05-25 发布日期:1994-05-25

AN ANALYSIS OF CUTTER-LOCATION CALCULATING METHOD FOR TWIST TURBINE BLADE SURFACES

Wei Yuanqian   

  1. Dept.of Mechanics,Zhejiang University,Hangzhoti,310027
  • Received:1993-01-04 Revised:1993-05-10 Online:1994-05-25 Published:1994-05-25

摘要: 为实现汽轮机700mm扭叶片型面的数控砂带磨削精加工,通过分析研究有关现有文献的刀位计算方法,提出采用鞍形曲面法,对由离散型值点给出的汽轮机扭叶片,可以确定其宽行线接触加工的刀位轨迹,以实现叶片型面的数控砂带磨削精加工。

关键词: 刀具-位置, 计算, 扭曲-涡轮叶片

Abstract: he abrasive belt precision grinding for a 700mm long twist balde surface is realized.Through analysis and discussion of some related references on surface cutter-position calculating methods,it is proposed that the cutter-location paths of twist blade surface given by discrete points for fulfilling line-contact machining in width rows should be determined by use of a saddle surface method.

Key words: cutters-location (position), computation, twisting turbine blades

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