OPTIMAL SIMULATION DESIGN OF SPACEBORNE CONNECTOR

In the design and research on the spaceborne connector of aerospace satellites, a joint optimization method is proposed. In order to reduce the problem of excessive bolt axial force of the spaceborne connector, a method with the variance of the bolt axial force as the objective function and constrai...

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Bibliographic Details
Main Authors: YU ChengYue, LIU Bo, WANG ChunPeng, XUE Chuang, AN MingXin
Format: Article
Language:zho
Published: Editorial Office of Journal of Mechanical Strength 2022-01-01
Series:Jixie qiangdu
Subjects:
Online Access:http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2022.05.036