首页> 外文会议>Conference on Smart Structures and Materials 2001: Smart Structures and Integrated Systems Mar 5-8, 2001, Newport Beach, USA >Modeling and Characterization of Piezoelectric and Magnetostrictive Induced Strain Actuators
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Modeling and Characterization of Piezoelectric and Magnetostrictive Induced Strain Actuators

机译:压电和磁致伸缩感应致动器的建模与表征

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This paper presents the results of theoretical modeling and experimental characterization of PiezoSystems Jena P-177-00 large stroke piezoelectric actuator and of Etrema AA-140J025-ES1 large stroke/large power magnetostrictive actuator. An improved smart-material actuators measurement method suited for static and low frequency actuation was devised. Analytical and finite element modeling (ANSYS) of the experimental setup to determine stiffness component characteristics was performed. The output displacements of the active material actuators were recorded in quasi-static and dynamic regimes, under varied pre-stress level, voltage and frequency values. The measurements indicated a strong dependence of the actuator stiffness and piezoelectric properties on the electromechanical loading conditions. The study also identified and calculated the parameters of the induced strain actuators electro-mechanical model. These parameters are necessary for performing design optimization to achieve maximum energy transfer and minimum power requirements. Experimentally verified data characterizing piezoelectric and magnetostrictive actuators in the full stroke/full power regime required for designing an effective airborne induced strain activated aerodynamic control system for air and space vehicles is provided.
机译:本文介绍了PiezoSystems Jena P-177-00大行程压电致动器和Etrema AA-140J025-ES1大行程/大功率磁致伸缩致动器的理论建模和实验表征结果。提出了一种适用于静态和低频驱动的改进的智能材料驱动器测量方法。进行了确定刚度部件特性的实验设置的分析和有限元建模(ANSYS)。在变化的预应力水平,电压和频率值下,以准静态和动态方式记录了活性材料促动器的输出位移。测量结果表明,致动器刚度和压电特性对机电负载条件的依赖性很大。该研究还确定并计算了感应应变致动器机电模型的参数。这些参数对于执行设计优化以实现最大的能量传递和最小的功率要求是必需的。提供了经实验验证的数据,该数据表征了设计用于航空航天器的有效机载感应应变激活空气动力学控制系统所需的全行程/全功率状态下的压电和磁致伸缩执行器。

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