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Analytical Investigation of Dynamics of Inflatable Parabolic Membrane Reflector

机译:充气抛物面膜反射器动力学的分析研究

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摘要

An analytical method for computing the dynamic characteristics of a lenticular inflatable parabolic reflector supported by an inflatable torus is presented. The system is modeled by a combined structure consisting of two pressurized paraboloidal membranes with an elastic circular ring support. Equations of motion for the transverse free vibration of the pressurized paraboloidal membrane are derived first by using the nonlinear theory of shallow shells of revolution. Then, the analytic solutions for those equations of motion are formulated. Afterward, according to the force balance and the displacement continuity between the membranes and the circular ring, the displacements of the ring are calculated as boundary conditions of the paraboloidal membranes. As a result, the frequency equation and analytic mode shape functions of the inflatable reflector are obtained, and the influences of support stiffness on the dynamic characteristics of the reflector are analyzed. The validity of these analytical modal solutions is verified by finite-element simulations.
机译:提出了一种分析方法,用于计算由可充气圆环支撑的双凸形可充气抛物面反射器的动态特性。该系统以组合结构为模型,该结构由两个加压抛物面膜和一个弹性圆环支撑组成。首先利用浅层旋转壳的非线性理论导出了加压抛物面膜的横向自由振动的运动方程。然后,制定了这些运动方程的解析解。然后,根据力平衡和膜与圆环之间的位移连续性,将环的位移计算为抛物面膜的边界条件。结果,得到了充气式反射镜的频率方程和解析模态函数,并分析了支撑刚度对反射镜动态特性的影响。这些分析模态解的有效性通过有限元仿真得到了验证。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2015年第1期|285-294|共10页
  • 作者

    Liu Fushou; Jin Dongping;

  • 作者单位

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Jiangsu, Peoples R China;

    Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Jiangsu, Peoples R China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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