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VIBRATION TESTING AND FINITE ELEMENT ANALYSIS OF INFLATABLE STRUCTURES

机译:充气结构的振动测试和有限元分析

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This paper presents vibration testing and finite element analysis of an inflated thin-film torus. Inflatable structures show significant promises for future space applications. However, their extremely lightweight, flexible, and high damping properties pose difficult problems in vibration testing and analysis. In this paper, we experimentally show that smart materials could be used as sensors and actuators for performing vibration tests of an inflated torus. In addition, we developed a predictive model that can be compared with experimental results. A commercial finite element package, ANSYS, is used to model the pre-stressed inflatable structure. Both experimental and finite element results are in good agreement with each other. The predictive model can be used for analyzing the dynamics of inflated structures, and for designing control systems to attenuate vibration in an inflated torus.
机译:本文介绍了充气薄膜圆环的振动测试和有限元分析。充气结构显示出对未来太空应用的重大希望。但是,它们的极轻量,柔性和高阻尼特性在振动测试和分析中带来了难题。在本文中,我们通过实验表明,智能材料可用作执行充气圆环振动测试的传感器和执行器。此外,我们开发了可与实验结果进行比较的预测模型。商业有限元软件包ANSYS用于对预应力充气结构进行建模。实验结果和有限元结果彼此吻合良好。该预测模型可用于分析充气结构的动力学,并用于设计控制系统以减弱充气圆环中的振动。

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