摘要
整体叶盘、叶轮等航空发动机零件形状复杂、精度要求高,对传统加工方法提出了很大挑战。混合加工技术结合了增、减制造技术优点,是解决复杂零件加工问题的有效手段。针对以上问题,基于几何特征将叶轮分解为叶片与叶盘两个部分,利用五轴环状切片方法规划了叶轮的增减材混合加工工艺,并在自主搭建的五轴混合加工平台基础上,对叶轮进行了加工试验,验证了该混合加工工艺规划方法的可行性。
Aero-engine parts such as blisks and impellers have complex shapes and high precision requirements,which pose great challenges to traditional processing methods. Additive-subtractive hybrid machining method can be used to machine before obstacles formed, which is an effective way to solve complex part processing problems. In view of the above problems, the impeller is decomposed into two parts, the blade and the disc based on geometric features. The fiveaxis annular slicing method is used to plan the additive-subtractive hybrid machining process of the impeller. Based on an self-built five-axis hybrid processing platform, an impeller was processed and tested to verify the feasibility of the hybrid processing planning method proposed in this paper.
作者
唐新宇
汪祥
李昊翔
邓晓鹏
赵明宇
刘长青
乔辉
TANG Xinyu;WANG Xiang;LI Haoxiang;DENG Xiaopeng;ZHAO Mingyu;LIU Changqing;QIAO Hui(College of Mechanical and Electrical Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;SIPPR Engineering Group Co.,Ltd.,Zhengzhou 450007,China)
出处
《航空制造技术》
2019年第8期81-87,共7页
Aeronautical Manufacturing Technology
基金
南京航空航天大学教师能力提升研究重点课题(1611JF0502Z)
关键词
整体叶轮
环状切片
增减材混合加工
特征分解
增材制造
Integral impeller
Annular Slicing
Additive-subtractive hybrid manufacturing
Feature decomposition
Additive manufacturing