期刊文献+

空间可展结构能量节点的设计和动力分析 被引量:1

Design and Dynamic Analysis of Energy-loaded Joints for Deployable Space Structures
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摘要 设计了一种用于空间可展抛物面天线的能量节点机构 ,并分析其展开机理 ,对杆件及其端部的扭簧组成的宏单元的缩减刚度矩阵进行了讨论 .结果表明 ,在结构体系中设置能量节点可显著改善结构的共振性能 ,证明该设计是可靠。 A kind of energy\|loaded joint used for deployable space structures is proposed and designed, and its deploying mechanics is also studied. The curtail rigid matrix of macrocell which is composed of the rod and its torsiomal springs has been analyzed. It has been shown that the resonant behaviour of structure was significantly improved by introducing the energy\|loaded joints into it. It's proved that this design is reliable and feasible.
出处 《工程设计学报》 CSCD 2001年第2期53-56,共4页 Chinese Journal of Engineering Design
基金 国家自然科学基金资助项目 !(6 9982 0 0 9)
关键词 空间可展结构 能量节点 扭簧 缩减刚度短阵 设计 动力分析 共振性能 航天器 deployable structure energy\|loaded joint torsional spring reduced stiffness matrix
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参考文献3

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同被引文献12

  • 1张淑杰,李瑞祥,丁同才.盘绕式杆状展开机构的设计与力学分析[J].力学季刊,2006,27(2):341-347. 被引量:12
  • 2袁家军,于登云,陈烈民.卫星结构设计与分析(下)[M].北京:中国宇航出版社,2009.
  • 3DENG Zongquan, HUANG Hailin, LIU Rongqiang. Synthesis of deployable/foldable single loop mechanisms with revolute joints[J]. Journal of Mechanisms and Robotics, 2011, 3(3) :031006.
  • 4PUIG L, BARTON A, RANDO N. A review on large deployable structures for astrophysics missions [ J ]. Acta Astronautica, 2010, 67(1): 12-26.
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  • 7National Aeronautics and Space Administration. Solar Power 0rigami-Style [ EB/OL ]. [ 2014- 08- 14 ]. http ://www. nasa. gov/jpl/news/origami-style-solar-power-20140814/.
  • 8ZIRBEL S A, WILSON M E, MAGLEBY S P, et al. An origami-inspired self-deployable array [ C ]// ASME 2013 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. Utah : ASME, 2013 : 3296.
  • 9JONE P A, BRIAN R S. Spacecraft solar array technology trends [ J ]. Aerospace and Electronic Systems, 2011,26 (8) :17-28.
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