| 空间充气展开天线支撑结构尺寸优化 |
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| 引用本文： | 陶宏新,胡振东.空间充气展开天线支撑结构尺寸优化[J].计算机辅助工程,2007,16(3):132-135. |
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| 作者姓名： | 陶宏新 胡振东 |
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| 作者单位： | 同济大学,航空航天与力学学院,上海,200092 |
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| 摘 要： | 为优化充气展开天线支撑结构,采用四边形四节点薄壳单元建立充气支撑管和支撑圆环的有限元分析模型.利用ANSYS软件,首先计算内压作用下结构的应力和固有频率,然后依次采用0阶和1阶优化算法对结构尺寸进行参数优化,有效地降低结构整体质量.该尺寸优化可以大大缩短设计周期,提高设计水平.
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| 关 键 词： | 充气展开天线 优化设计 结构分析 有限元 ANSYS 空间 充气展开 天线支撑 结构尺寸优化 antenna space structure support optimization on 设计水平 设计周期 整体质量 参数优化 优化算法 固有频率 应力 作用 内压 计算 软件 |
| 文章编号： | 1006-0871（2007）03-0132-04 |
| 收稿时间： | 2007-05-23 |
| 修稿时间： | 2007-06-15 |
Size optimization on support structure of
inflatable space antenna |
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| TAO Hongxin and HU Zhendong.Size optimization on support structure of
inflatable space antenna[J].Computer Aided Engineering,2007,16(3):132-135. |
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| Authors: | TAO Hongxin and HU Zhendong |
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| Affiliation: | School of Aerospace Eng.& Applied Mechanics,Tongji Univ.,Shanghai 200092, China;School of Aerospace Eng.& Applied Mechanics,Tongji Univ.,Shanghai 200092, China |
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| Abstract: | To optimize the support structure of inflatable space antenna, the finite element analysis model for inflatable tube and torus is established by four node quadrangular shell elements. By using ANSYS, the static and natural frequency of the structure subjected to inner pressure are obtained, and two optimization methods with zero order and first order are used to optimize the structure size parameters. The total mass of the structure is reduced efficiently. The optimization can shorten its design cycle greatly and improve its design level. |
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| Keywords: | inflatable space antenna optimum design structural analysis finite element ANSYS |
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