Design and modeling of a ZnO-based MEMS acoustic sensor for aeroacoustic and audio applications

D. S. Arya, M. Prasad, C. C. Tripathi
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引用次数: 10

Abstract

In previous research work related to the acoustic sensors, the researchers had focused on the individuality of the sensors for aeroacoustic application and sensors for audio range application. This paper describes a simple and novel model of acoustic sensor for aeroacoustic and audio applications (microphone). The model of the device presented in this paper shows interoperability. The sensor reported has the bandwidth of~22 KHz, which covers the entire bandwidth of microphone and aeroacoustic sensors. A LEM (Lumped Element Model) is used to determine the characteristics of the device. The device has the square diaphragm of 1.5 × 1.5 mm2 and a nominal thickness of 15 μm to sustain the high SPL (Sound Pressure Level). A piezoelectric ZnO layer 2.4 μm-thick is sandwiched between two Al-top and bottom electrodes. The top electrode is segmented to enhance the sensitivity of the device. Furthermore, a microtunnel of 100 μm wide and 21μm deep is designed to achieve the lower cut-on frequency of ~5 Hz. The theoritical results show that the sensor has sensitivity (RMS) of 126.3μV/Pa and 96.6 μV/Pa in case of central and outer electrodes respectively. The resonant frequency of ~ 85 KHz is obtained from lumped model, simulated using MULTISIM 13.0. The result is verified with MEMS-CAD TOOL COVENTORWARE®.
气动声学和音频应用中基于zno的MEMS声学传感器的设计和建模
在以往的声学传感器研究工作中,研究人员主要关注航空声学传感器和音频测距传感器的个性化。本文介绍了一种用于气动声学和音频应用(麦克风)的简单而新颖的声传感器模型。本文提出的设备模型具有良好的互操作性。所报道的传感器带宽约为22 KHz,覆盖了传声器和气动声传感器的整个带宽。LEM(集总元素模型)用于确定设备的特性。该器件具有1.5 × 1.5 mm2的方形膜片,标称厚度为15 μm,以维持高声压级(SPL)。在铝顶电极和铝底电极之间夹有一层2.4 μm厚的ZnO压电层。顶部电极是分段的,以提高设备的灵敏度。此外,还设计了宽100 μm、深21μm的微隧道,实现了~5 Hz的低通断频率。理论结果表明,该传感器的灵敏度(RMS)在中心电极和外电极分别为126.3μV/Pa和96.6 μV/Pa。通过集总模型得到了~ 85 KHz的谐振频率,并利用MULTISIM 13.0进行了仿真。结果通过MEMS-CAD工具COVENTORWARE®进行验证。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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