Title :
The study of expansion method based on geometry modeling for high rib integral panel
Author :
Yin, Haijun ; Meng, Biao
Author_Institution :
Shenyang Aircraft Co., Shenyang, China
Abstract :
Combined the roughcast expansion technology for double curvature high rib integral panel part from a certain type of aircraft, a rapid and precise expansion method for the part is realized. The part base expansion method uses geometric simulation modeling method based on the hypothesis of the siding material deformation in thickness direction is negligible and the siding neutral layer surface area is unchanged, and determines reinforced structure and internal milling information on panel body based on mapping theorem and intersection algorithm. Finally, a machine panel as an example, the geometry simulation modeling approach is introduced step by step.
Keywords :
aerospace components; aircraft; computational geometry; deformation; design engineering; structural engineering computing; structural panels; aircraft; geometric simulation modeling; high rib integral panel; internal milling information; intersection algorithm; machine panel; mapping theorem; panel body; part base expansion method; reinforced structure; roughcast expansion technology; siding material deformation; siding neutral layer surface area; thickness direction; Aircraft; Aircraft manufacture; Atmospheric modeling; Deformable models; Geometry; Mathematical model; Ribs; expansion; geometry modeling; integral panel; mapping;
Conference_Titel :
Computer Science and Automation Engineering (CSAE), 2012 IEEE International Conference on
Conference_Location :
Zhangjiajie
Print_ISBN :
978-1-4673-0088-9
DOI :
10.1109/CSAE.2012.6272940