Optimal design of spaceborne antenna supporting structure with load-bearing barrel-brackets configuration by topology optimization method

被引:0
|
作者
Yang Jungang [1 ]
Liu Bingshan [2 ]
Huang Yongbin [2 ]
Zhang Qiao [1 ]
Gao Tong [2 ]
Xiao Yong [1 ]
Duan Hao [1 ]
Yu Zeliang [1 ]
机构
[1] Xian Space Radio Acad Inst, Xian 710068, Peoples R China
[2] Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
Topology optimization; spaceborne antenna; supporting structure; load-bearing barrel-brackets configuration;
D O I
10.1117/12.2639006
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper, the optimal design of the large spaceborne antenna supporting structure with load-bearing barrel-brackets configuration is studied. In this form of structure, the satellite and the antenna supporting structure are provided with a central load-bearing barrel, and the two are connected to each other as the main bearing structure; the antenna parts are connected to the load bearing barrel through a series of brackets. A topology optimization design model of the antenna supporting structure of the load-bearing barrel-bracket configuration is constructed. The layout of the supporting brackets structure is ensured through methods such as design space segmentation and independent material volume control.
引用
收藏
页数:6
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