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Microscopic actuation and optimal actuator locations of paraboloidal cylindrical shells

机译:抛物面圆柱壳的微观致动和最佳致动器位置

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This study aims to investigate the distributed actuation behavior induced by piezoelectric patches on a simply-supported adaptive paraboloidal cylindrical shell panel. The transverse dynamic equation of the paraboloidal cylindrical shell panel with piezoelectric actuations is presented. Then, the actuator induced modal control force is derived with a newly defined transverse mode shape function. In order to exclude the actuator size effect, microscopic actuation behavior induced by actuator neurons is obtained by shrinking the actuator patch to be infinitesimal. Control actuations are sensitive to actuator locations and natural modes. The maximal control force in the meridional direction inclines to relatively flat regions due to the curvature effect. These results provide a design guideline on placing actuator locations to maximize the control effect.
机译:这项研究旨在调查由压电贴片在简单支撑的自适应抛物面圆柱壳面板上引起的分布式驱动行为。提出了抛物线形圆柱壳面板在压电作用下的横向动力学方程。然后,利用新定义的横向模式形状函数导出执行器感应的模式控制力。为了排除执行器尺寸的影响,通过将执行器贴片缩小到无穷小来获得由执行器神经元引起的微观执行行为。控制执行对执行器的位置和自然模式很敏感。由于曲率效应,在子午方向上的最大控制力倾向于相对平坦的区域。这些结果为放置执行器位置提供了设计指导,以最大程度地发挥控制效果。

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