典型难加工材料叶片切削加工研究  

Study on Cutting of Difficult-to-Cut Material Blade

作　　者：李美荣[1] 刘娜[1] 王钰玉[1] 

机构地区：[1]中航工业沈阳黎明航空发动机(集团)有限责任公司

出　　处：《航空制造技术》2012年第16期68-70,共3页Aeronautical Manufacturing Technology

摘　　要：本文通过建立刀具磨损预测模型,并将该模型理论和现场生产实际相结合,在保证加工质量要求的前提下,给出了难加工材料(GH2132)经济效益最大化的切削加工参数,并在航空发动机叶片型面加工中获得验证,取得了加工质量、加工效率和加工成本的最优结合,为解决航空典型难加工材料的切削参数优化问题提供了重要依据和解决途径,这对于提高航空发动机难加工材料的加工效率和降低加工成本具有重要意义。By building the tool wear forecast model and combining the model theory and production practice, and ensuring the quality requirement of machining quality, cutting parameters are given to maximize the effectiveness of difficult-to-cut material (GH2132). These parameters are verified during the blade surface machining of aeroengine, which achieves the optimal combination of machining quality, efficiency and cost and provides the important basis and solve method for cutting parameterization of aviation difficult-to-cut materials. This method is very important for enhancing machining efficiency and reducing cost.

关 键 词：难加工材料 叶片 高速加工 

分 类 号：V263.1[航空宇航科学与技术—航空宇航制造工程]