DocumentCode
3037625
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
Volume
3
fYear
2012
fDate
25-27 May 2012
Firstpage
208
Lastpage
211
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;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Science and Automation Engineering (CSAE), 2012 IEEE International Conference on
Conference_Location
Zhangjiajie
Print_ISBN
978-1-4673-0088-9
Type
conf
DOI
10.1109/CSAE.2012.6272940
Filename
6272940
Link To Document