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Slicing Recognition of Aircraft Integral Panel Generalized Pocket

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文摘 To automatically obtain a machining area in numerical control (NC) programming, a data model of generalized pocket is established by analyzing aircraft integral panel characteristics, and a feature recognition approach is proposed. First, by reference to the practical slice-machining process of an aircraft integral panel, both the part and the blank are sliced in the Z-axis direction; hence a feature profile is created according to the slicing planes and the contours are formed by the intersection of the slicing planes with the part and its blank. Second, the auxiliary features of the generalized pocket are also determined based on the face type and the position, to correct the profile of the pocket. Finally, the generalized pocket feature relationship tree is constructed by matching the vertical relationships among the features. Machining feature information produced by using this method can be directly used to calculate the cutter path. The validity and practicability of the method is verified by NC programming for aircraft panels.
来源 Chinese Journal of Aeronautics ,2008,21(6):585-592 【核心库】
DOI 10.1016/s1000-9361(08)60178-8
关键词 numerical control ; aircraft integral panel ; feature extraction ; computer aided manufacturing
地址

1. School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing, 100191  

2. Shenyang Aircraft Co. Ltd, Shenyang, 110034  

3. Beijing Zhongke Fulong Computer Technology Co. Ltd, Beijing, 100085

语种 英文
文献类型 研究性论文
ISSN 1000-9361
学科 航空
文献收藏号 CSCD:3443735

参考文献 共 13 共1页

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引证文献 7

1 于芳芳 基于几何特性的槽加工刀具选取算法 计算机辅助设计与图形学学报,2010,22(11):1984-1989,1997
被引 5

2 Yu Fangfang Principal Face-based Recognition Approach for Machining Features of Aircraft Integral Panels Chinese Journal of Mechanical Engineering,2011,24(6):976-982
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