随机振动环境下航天器结构强度设计方法综述

张玉梅; 韩增尧; 邹元杰

doi:10.6052/1000-0992-12-016

随机振动环境下航天器结构强度设计方法综述

doi: 10.6052/1000-0992-12-016

中国空间飞行器总体设计部, 北京 100094

基金项目: 国家“973” 项目(613133) 资助

详细信息

通讯作者:
韩增尧

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出版历程
- 收稿日期: 2012-02-24
- 修回日期: 2012-05-10
- 刊出日期: 2012-07-25

AN OVERVIEW OF STRUCTURAL STRENGTH DESIGN METHODS FOR SPACECRAFTS IN RANDOM VIBRATION ENVIRONMENT

Beijing Institute of Spacecraft System Engineering, Beijing 100094, China

Funds: The project was supported by the National Basic Research Program of China (613133).

More Information

Corresponding author: HAN Zengyao

摘要

摘要: 随机振动环境是航天器结构强度设计重点考虑的因素之一. 目前, 在随机振动环境条件下, 航天器结构强度设计采取的方法主要为等效的准静态设计方法, 其等效原则可分为加速度响应等效、位移响应等效以及应力响应等效. 本文重点介绍了3 种等效原则的基本原理、处理方法、国内外发展现状及工程应用情况, 并在综合分析的基础上推荐使用基于位移和应力峰值响应等效的设计方法. 最后针对需进一步开展的研究工作提出了建议.
- 准静态载荷 /
- 随机振动 /
- 设计载荷 /
- 响应等效
Abstract: Random vibration is an important part of spacecraft structure design. Now, the main method used in the structural strength design of spacecrafts is equivalent static design method. Its equivalent principles include equivalent acceleration response, equivalent displacement response and equivalent stress response. Respective theories, methods, domestic and overseas research status, advantages and disadvantages and engineering applications are presented. The design method based on the peak values of displacement and stress response is recommended. And the problems in need of further research are finally suggested.
- equivalent static loads /
- random vibration /
- design load /
- equivalent response

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参考文献(47)

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