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首页> 外文期刊>Journal of spacecraft and rockets >Local effects of piezopolymer patches on inflatable space-based structures
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Local effects of piezopolymer patches on inflatable space-based structures

机译:压聚合物贴片对可充气天基结构的局部影响

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Inflatable structures are often characterized as membranes (that is, structural elements that cannot resist bending moments). This simplification raises the question of whether membrane theory can account for the effects of active, surface-mounted piezopolymer patches. This work discusses these effects on the dynamic behavior of a flat, rectangular coupon section and assesses the patch's ability to sense and actuate transverse deflections of the thin-film substrate using traditional membrane theory. The Rayleigh-Ritz method was employed to approximate the natural frequencies and mode shapes of this layered system. Although including the additional mass of the patch, traditional membrane theory was unable to account for the added stiffness of the patch layer. When the piezoelectric behavior of the patch was considered, membrane theory failed to model the piezopolymer as a useful sensor. Also, excitation of transverse vibrations was not possible using membrane theory, which does not allow application of bending moments. However, piezoelectric actuation was modeled as applied in-plane forces, which enabled the patch to suppress out-of-plane disturbances by altering the tension in the base layer as a function of applied voltage. References: 12
机译:充气结构通常被描述为膜(即不能抵抗弯矩的结构元件)。这种简化提出了一个问题,即膜理论是否可以解释活性表面贴装压聚物贴片的影响。这项工作讨论了这些对扁平矩形试样截面动态行为的影响,并评估了贴片使用传统膜理论感知和驱动薄膜基板横向挠度的能力。采用Rayleigh-Ritz方法近似该分层系统的固有频率和振型。尽管包括了贴片的额外质量,但传统的膜理论无法解释贴片层增加的刚度。当考虑贴片的压电行为时,膜理论未能将压电聚合物建模为有用的传感器。此外,使用膜理论无法激发横向振动,膜理论不允许应用弯矩。然而,压电驱动被建模为施加的面内力,这使得贴片能够通过改变基层中的张力作为施加电压的函数来抑制面外干扰。[参考资料: 12]

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