南京航空航天大学学报（英文版）2022，Vol.39Issue(3)：349-357,9.
航空发动机叶片数控加工区域误差识别方法
An Error Area Determination Approach in Machining of Aero?engine Blade
摘要
Abstract
As a result of the recently increasing demands on high-performance aero-engine,the machining accuracy of blade profile is becoming more stringent. However,in the current profile,precision milling,grinding or near-net-shape technology has to undergo a tedious iterative error compensation. Thus,if the profile error area and boundary can be determined automatically and quickly,it will help to improve the efficiency of subsequent re-machining correction process. To this end,an error boundary intersection approach is presented aiming at the error area determination of complex profile,including the phaseⅠof cross sectional non-rigid registration based on the minimum error area and the phaseⅡof boundary identification based on triangular meshes intersection. Some practical cases are given to demonstrate the effectiveness and superiority of the proposed approach.关键词
航空发动机叶片/误差区域/边界识别/非刚性配准/数控补加工Key words
aero-engine blade/error area/boundary identification/non-rigid registration/NC re-machining分类
机械制造引用本文复制引用
张云,朱燏,朱正清..航空发动机叶片数控加工区域误差识别方法[J].南京航空航天大学学报（英文版）,2022,39(3):349-357,9.基金项目
This work was supported by the Aero?nautical Science Foundation of China(No. 20200016112001). （No. 20200016112001）
