A Surface Fairing Method Based on Torus Tool Machining
In order to solve the problems of failure of tool-path generation or a relatively narrow processing row span,which are initiated by unfairness of surface of engine blade,this paper according to the blade actual design,machining and testing method,combining End-points error controlling method for tool position optimization in five-axis,and a dual drive tool path planning strategy,develop surface smoothness checked tools oriented to ring tool machining,and fairing surface contours where detected data points have influenced the row span.Repeating this progress,until surface machining yow-span is satisfied.At this time,it is considered that surface conform to the requirement of smoothing.With an aeroengine blade,for example,verify the validity of the proposed method.
Fairing Energy optimization method Tool position optimization
Zhang Bochang Xu Rufeng Ning Tao Chen Zhitong
School of Mechanical Engineering and Automation Beijing University of Aeronautics and Astronautics Beijing, China, 100191
国际会议
沈阳
英文
746-749
2012-07-27(万方平台首次上网日期,不代表论文的发表时间)