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首页> 外文期刊>Journal of Vibration and Acoustics >Precision Microscopic Actuations of Parabolic Cylindrical Shell Reflectors
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Precision Microscopic Actuations of Parabolic Cylindrical Shell Reflectors

机译:抛物线形圆柱壳反射镜的精密微观致动

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摘要

An open parabolic cylindrical shell panel plays a key role in radial signal collection, reflection, and/or transmission applied to radar antennas, space reflectors, solar collectors, etc. Active vibration control can suppress unexpected fluctuation and maintain its precision surface and operations. This study aims to investigate the distributed active actuation behavior of adaptive open parabolic cylindrical shell panels using piezoelectric actuator patches. Dynamic equations of parabolic cylindrical shells laminated with piezoelectric actuator patches are presented first. Then, the actuator induced modal control force is defined based on a newly derived mode shape function. As the actuator area varies due to the curvature change, the normalized actuation effectiveness (i.e., modal control force per unit actuator area) is further evaluated. When the actuator area shrinks to infinitesimal, the expression of microscopic local modal control force is obtained to predict the spatial microscopic actuation behavior on parabolic cylindrical shells. The total control force and its three components exhibit distinct characteristics with respect to shell geometries, modes, and actuator properties. Analyzes suggest that the control force contributed by the membrane force component dominates the total actuation effect. The bending-contributed component increases with the corresponding mode number, while the membrane-contributed component decreases. Actuation effectiveness of two shell geometries, from shallow to deep, and actuator sizes are evaluated. Analysis of optimal actuator locations reveals that actuators placed at the maximal shell curvature are more effective and maximize the control effects.
机译:开放式抛物线形圆柱壳面板在应用于雷达天线,太空反射器,太阳能收集器等的径向信号收集,反射和/或传输中起着关键作用。主动振动控制可以抑制意想不到的波动并保持其精确的表面和操作。这项研究旨在调查使用压电致动器贴片的自适应开放抛物线形圆柱壳面板的分布式主动致动行为。首先介绍了压电致动器贴片叠层的抛物线形圆柱壳的动力学方程。然后,基于新导出的模式形状函数来定义致动器感应的模式控制力。当致动器面积由于曲率变化而变化时,归一化的致动效率(即,每单位致动器面积的模态控制力)被进一步评估。当致动器面积缩小到无穷大时,将获得微观局部模态控制力的表达式,以预测抛物柱形壳上的空间微观致动行为。总控制力及其三个分量在壳体几何形状,模式和执行器特性方面表现出不同的特性。分析表明,由膜力分量贡献的控制力主导了总的驱动效果。弯曲贡献分量以相应的模数增加,而膜贡献分量减小。评估了两种壳体几何形状(从浅到深)的致动效果以及致动器的尺寸。最佳执行器位置的分析表明,以最大壳体曲率放置的执行器更有效,并且可以最大程度地发挥控制效果。

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  • 来源
    《Journal of Vibration and Acoustics》 |2015年第1期|011013.1-011013.11|共11页
  • 作者

    S. D. Hu; H.Li; H. S. Tzou;

  • 作者单位

    StrucTronics and Control Lab,School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027, China;

    StrucTronics and Control Lab,School of Aeronautics and Astronautics,Zhejiang University,Hangzhou 310027, China;

    School of Aeronautics and Astronautics,Zhejiang University The State Key Laboratory of Fluid Power Transmission and Control, Department of Mechanical Engineering, Zhejiang University, Hangzhou 310027, China;

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