| 包带连接力学分析与建模 |
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| 引用本文： | 白绍竣,梁鲁,张静,郑钢铁.包带连接力学分析与建模[J].上海航天,2011,28(6):43-48. |
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| 作者姓名： | 白绍竣 梁鲁 张静 郑钢铁 |
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| 作者单位： | 1. 哈尔滨工业大学航天学院,黑龙江哈尔滨,150001
2. 清华大学航天航空学院,北京,100084 |
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| 摘 要： | 研究了卫星包带连接的有限元力学建模。基于对包带预紧力、卡块与连接环间的接触力，以及两连接环间的接触力的分析，将接触力等效为有限单元节点力。对所建模型中的非线性项，用Newton-Raphson法求得给定包带顸紧力的平衡位置，再以该平衡位置处的切线刚度对模型作线性化，分析了模态和固有频率等动力学特性。某卫星的算例验证了模...
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| 关 键 词： | 卫星 包带连接 有限元 线性化 动力学特性 |
Modeling and Analysis of Marman Clamp Joint |
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| BAI Shao-jun,LIANG Lu,ZHANG Jing,ZHENG Gang-tie.Modeling and Analysis of Marman Clamp Joint[J].Aerospace Shanghai,2011,28(6):43-48. |
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| Authors: | BAI Shao-jun LIANG Lu ZHANG Jing ZHENG Gang-tie |
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| Institution: | BAI Shao-jun1,LIANG Lu2,ZHANG Jing1,ZHENG Gang-tie2(1.School of Astronautics,Harbin Institute of Technology,Harbin 150001,Heilongjiang,China,2.School of Aerospace,Tsinghua University,Beijing 100084,China) |
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| Abstract: | The modeling of the marman clamp joint of satellite in this paper.Based on the analysis of the band,the contact forces between the two adaptor rings and between the V-segments and adaptor rings,the contact forces were equivalent to element node forces.The linearization technique was applied for modal and natural frequency analysis as the clamp joint model was nonlinear,and Newton-Raphson method was applied to determine the equilibrium position.The linearized equation was obtained by expanding the nonlinear ... |
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| Keywords: | Satellite Marman clamp joint Finite element method Linearization Dynamic characteristic |
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