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涡轮叶盘数控加工优化方法的研究与实现
引用本文:郭连水,刘秋丰,曹浩波.涡轮叶盘数控加工优化方法的研究与实现[J].新技术新工艺,2005(10):19-21.
作者姓名:郭连水  刘秋丰  曹浩波
作者单位:1. 北京航空航天大学机械工程及其自动化学院,100083
2. 香港精品机械有限公司北京办事处,100083
摘    要:为提高涡轮叶盘的加工效率和质量,提出了涡轮叶盘数控加工工艺方案,在粗加工阶段,采用插铣方法代替传统的点铣加工,分层加工,减小加工变形。采用UGNX进行涡轮叶盘建模,NERC-Max数控编程,VERICUT刀轨仿真。结果表明,采用插铣方法,切削效率高,刀具和叶片未发生干涉,加工阶段划分、刀轨设计合理。提出的涡轮叶盘数控加工工艺方案可行。

关 键 词:涡轮叶盘  五轴数控加工  插铣方法  粗加工优化

Research and Realization of Optimized 5-axis NC Machining Method for Turbine Blade
Guo LianShui;Liu QiuFeng;Cao HaoBo.Research and Realization of Optimized 5-axis NC Machining Method for Turbine Blade[J].New Technology & New Process,2005(10):19-21.
Authors:Guo LianShui;Liu QiuFeng;Cao HaoBo
Abstract:In order to improve the efficiency and quality of turbine blade milling, a new method of turbine blade NC milling is presented in this paper, plunge milling is a good method, especially for rough milling of blade. Layered milling method can reduce shape distortion in machining. This article provides solid model of blade using UG-NX, and NC programming by NERC-Max, simulating and analyzing by VERICUT, the result indicate that layered milling, optimization tool path and plunge milling can obtain much better quality and efficiency than traditional manufacturing method.
Keywords:turbine blade  5-axis milling  plunge milling  rough optimization milling
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