HBAR应力敏感系数

Baron Thomas, Petrini Valerie, M. Gilles, C. Guillaume, Clairet Alexandre, Dulmet Bernard, Lesage Jean-Marc, Laroche Thierry, Ballandras Sylvain
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引用次数: 1

摘要

振动灵敏度是专用于航天或机载系统的振荡器的一项重要指标。振动灵敏度可能是由于谐振器,振荡器环路或非振荡器组件,如电线,例如。通常,加速度灵敏度的主要来源是由于谐振器。主动补偿可以用来减少这种影响,但这样的系统不容易小型化。本文介绍了高泛音体声谐振器的频率应力敏感系数的计算,并设计了一种简单的封装,以减小振动灵敏度。最终目标是控制专用封装的高泛音体声谐振器的振动灵敏度。计算结果与实验结果进行了比较。理论与实验结果的一致性约为50%。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Stress sensitivity coefficients of HBAR
Vibration sensitivity is an important specification for oscillators dedicated to space or airborne systems. Vibration sensitivity can be due to the resonator, the oscillator loop or non-oscillator components like wire, for instance. Commonly, the main source of acceleration sensitivity is due to the resonator. Active compensation can be used to decrease this effect, but such systems are not easily miniaturized. This paper presents computations of the stress sensitivity coefficients of frequency for the high-overtone bulk acoustic resonators and the design of a simple packaging to minimize vibration sensitivity. The final goal is to control vibration sensitivity of the high-overtone bulk acoustic resonators with dedicated packaging. The computed results are compared to experimental ones. The agreement between theoretical and experimental results is about 50%.
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