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Piezoelectric Energy Harvesting from an L-Shaped Beam-Mass Structure

机译:从L形梁质量结构中收集压电能量

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Cantilevered piezoelectric harvesters have been extensively considered in the energy harvesting literature. Mostly, a traditional cantilevered beam with one or more piezoceramic layers is located on a vibrating host structure. Motion of the host structure results in vibrations of the harvester beam and that yields an alternating voltage output. As an alternative to classical cantilevered beams, this paper presents a novel harvesting device; a flexible L-shaped beam-mass structure that can be tuned to have a two-to-one internal resonance to a primary resonance ω(≌)2 = 2ω_1(which is not possible for classical cantilevers). The L-shaped structure has been well investigated in the literature of nonlinear dynamics since the two-to-one internal resonance, along with the consideration of quadratic nonlinearities, may yield modal energy exchange (for excitation frequency ω (≌ )ω_1) or the so-called saturation phenomenon (for ω (≌) ω_2). As a part of our ongoing research on piezoelectric energy harvesting, we are investigating the possibility of improving the electrical outputs in energy harvesting by employing these features of the L-shaped structure. This paper aims to introduce the idea, describes the important features of the L-shaped harvester configuration and develops a linear distributed parameter model for predicting the electromechanically coupled response. In addition, this work proposes a direct application of the L-shaped piezoelectric energy harvester configuration for use as landing gears in unmanned air vehicle applications.
机译:悬臂式压电收集器已在能量收集文献中得到广泛考虑。通常,具有一个或多个压电陶瓷层的传统悬臂梁位于振动主体结构上。主体结构的运动会导致收集器束发生振动,并产生交流电压输出。作为经典悬臂梁的替代方案,本文提出了一种新型的收割装置;灵活的L形束质量结构,可以将其调谐为与初级共振ω(φ)2 =2ω_1具有二对一的内部共振(这对于经典的悬臂梁是不可能的)。 L型结构已在非线性动力学文献中进行了深入研究,因为二对一内部共振以及二次非线性的考虑可能会产生模态能量交换(对于激发频率ω(≌)ω_1)或所谓的饱和现象(对于ω(≌)ω_2)。作为我们正在进行的压电能量收集研究的一部分,我们正在研究通过利用L形结构的这些特征来改善能量收集中的电输出的可能性。本文旨在介绍这一思想,描述L形收割机配置的重要特征,并开发一种用于预测机电耦合响应的线性分布参数模型。此外,这项工作提出了将L形压电能量收集器配置直接用于无人飞行器应用中的起落架的建议。

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