带有PZT有源层的100 kHz Pmuts空气耦合阵列:多物理场模型和实验

G. Massimino, A. Colombo, R. Ardito, F. Quaglia, F. Foncellino, A. Corigliano
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引用次数: 11

摘要

本文主要研究了压电微机械超声换能器(PMUTs)空气耦合阵列的多物理场有限元建模,并在时域上对其力学和声学行为进行了初步实验验证。在膜片响应的基础上,采用两种数值模型模拟了系统的完整性能。在前者中,利用系统的轴对称,解决了单个PMUT的机电声(EMA)问题,具有以下特征:制造诱导残余应力的存在,决定了压电板的非线性初始变形结构和大量线性化的基模频移;不同物理场之间的多重耦合,即有源层的压电耦合和波在周围流体中传播的声结构相互作用。当动态响应中的非线性被所涉及的大位移激活时,随着电压输入的增加,系统表现出初始跳动行为,稳态振幅增量较小。在后一种模型中,考虑了属于4 × 4阵列结构的硅模的全套pmut,其中振动板被建模为等效的振动刚性平面圆形活塞,其施加的加速度振幅减小,在由表面模的其余部分表示的刚性挡板上。在不同电压幅值的单驱动换能器TX测试的情况下,数值模拟的结果与实验结果进行了比较,即在距离膜片中心15 cm处,沿其自身声轴垂直方向上的初始静态预挠曲和压力。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Air-Coupled Array of Pmuts at 100 kHz with PZT Active Layer: Multiphysics Model and Experiments
This work is focused on the multi-physics modelling via the finite element method (FEM) of an air-coupled array of Piezoelectric Micromachined Ultrasonic Transducers (PMUTs) and its preliminary experimental validation in the time domain for the mechanical and acoustic behaviour.Two numerical models are used to simulate the complete performance of the system based on the response of the diaphragm.In the former, the electro-mechanical-acoustic (EMA) problem for the single PMUT is solved, exploiting the axial symmetry of the system, with the following features: the presence of the fabrication induced residual stresses, which determine a non-linear initial deformed configuration and a substantial linearized fundamental mode frequency shift of the piezo-plate; the multiple couplings between different physics, namely piezoelectric coupling in the active layer and acoustic-structural interaction for the waves propagation in the surrounding fluid. When the non-linearities are activated in the dynamic response, by the involved large displacements, the system shows an initial beating behaviour with small steady state amplitude increment as the voltage input increases.In the latter model, the full set of PMUTs belonging to the silicon die in a 4 × 4 array configuration is considered in which the vibrating plates are modelled as equivalent oscillating rigid plane circular pistons, with reduced imposed acceleration amplitude, on a rigid baffle represented by the remaining part of the surface die.The results of the numerical simulations are compared with the experimental ones in terms of the initial static pre-deflection and pressure at 15 cm from the centre of the diaphragm, on the vertical direction along its own acoustic axis, in the case of the TX test with a single actuated transducer for different voltage amplitudes.
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