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基于CAD模型的涡轮叶片误差检测系统
引用本文:席平,孙肖霞.基于CAD模型的涡轮叶片误差检测系统[J].北京航空航天大学学报,2008,34(10):1159-1162.
作者姓名:席平  孙肖霞
作者单位:北京航空航天大学,机械工程及自动化学院,北京,100191;北京航空航天大学,机械工程及自动化学院,北京,100191
摘    要:涡轮叶片型面误差检测是其制造过程中的重要环节.研究了涡轮叶片型面误差检测关键技术的实现方法,提出了基于测量数据的叶片截面关键参数的自动提取方法以及测量数据与计算机辅助设计(CAD)模型的坐标配准方法,制定了衡量叶片截面轮廓度、倾斜度、弯曲度和扭曲度的评估指标,并基于UG平台开发了叶片型面误差检测系统.应用实例表明,该系统可显著提高叶片的误差检测速度和分析质量.

关 键 词:涡轮叶片  误差评估  特征提取  坐标配准
收稿时间:2007-10-19

Error analysis system of turbine blade based on CAD model
Xi Ping,Sun Xiaoxia.Error analysis system of turbine blade based on CAD model[J].Journal of Beijing University of Aeronautics and Astronautics,2008,34(10):1159-1162.
Authors:Xi Ping  Sun Xiaoxia
Institution:School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:The error analysis of blade surface is very important during the process of turbine blade manufacture.Firstly,key technologies of surface inspection were studied,and the crucial parameters automation extraction algorithm for blade section from measured data was proposed.Next,the registration method between measured data and computer aided design(CAD) model was given.Meanwhile,several indexes of evaluation for blade were put forward,such as profile error,angularity error,camber error and twist error.Finally,...
Keywords:turbine blade  error analysis  feature extraction  coordinate registration  
本文献已被 CNKI 维普 万方数据 等数据库收录!
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