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Aircraft skin stretch-forming die light-weight design using topology optimization

  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节会议稿件同行评审

1 引用 (Scopus)

摘要

The purpose of this paper is to use the topology optimization method to solve the light-weight design problem of large aircraft skin stretch-forming die. The platform of ABAQUS is firstly used for numerical simulation of skin stretch-forming. And the surface load conditions are therefore obtained. The topology optimization is carried out accordingly to maximize the structural stiffness with the material properties and the boundary conditions properly defined. Referring to the obtained topology design, the optimal structure is reconstructed and then evaluated by the non-linear numerical simulation of stretch-forming. Compared with the traditional design, the numerical results have shown that the topology design can improve the stiffness and strength of the stretch-forming die significantly.

源语言英语
主期刊名Advances in Materials Manufacturing Science and Technology XIV
编辑Tian Huang, Dawei Zhang, Bin Lin, Yanling Tian, Weiguo Gao, Anping Xu
出版商Trans Tech Publications Ltd
600-603
页数4
ISBN(印刷版)9783037852378
DOI
出版状态已出版 - 2012
活动14th International Manufacturing Conference in China, IMCC2011 - Tianjin, 中国
期限: 13 10月 201115 10月 2011

出版系列

姓名Materials Science Forum
697-698
ISSN(印刷版)0255-5476
ISSN(电子版)1662-9752

会议

会议14th International Manufacturing Conference in China, IMCC2011
国家/地区中国
Tianjin
时期13/10/1115/10/11

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