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结构-声耦合效应对非真空封装振动圆柱陀螺仪的影响。

Structural-acoustic coupling effects on the non-vacuum packaging vibratory cylinder gyroscope.

机构信息

College of Mechatronics Engineering and Automation, National University of Defense Technology, Changsha 410073, China.

出版信息

Sensors (Basel). 2013 Dec 13;13(12):17176-92. doi: 10.3390/s131217176.

Abstract

The resonant shells of vibratory cylinder gyroscopes are commonly packaged in metallic caps. In order to lower the production cost, a portion of vibratory cylinder gyroscopes do not employ vacuum packaging. However, under non-vacuum packaging conditions there can be internal acoustic noise leading to considerable acoustic pressure which is exerted on the resonant shell. Based on the theory of the structural-acoustic coupling, the dynamical behavior of the resonant shell under acoustic pressure is presented in this paper. A finite element (FE) model is introduced to quantitatively analyze the effect of the structural-acoustic coupling. Several main factors, such as sealing cap sizes and degree of vacuum which directly affect the vibration of the resonant shell, are studied. The results indicate that the vibration amplitude and the operating frequency of the resonant shell will be changed when the effect of structural-acoustic coupling is taken into account. In addition, an experiment was set up to study the effect of structural-acoustic coupling on the sensitivity of the gyroscope. A 32.4 mV/°/s increase of the scale factor and a 6.2 Hz variation of the operating frequency were observed when the radial gap size between the resonant shell and the sealing cap was changed from 0.5 mm to 20 mm.

摘要

振动圆柱陀螺仪的谐振壳通常用金属帽包装。为了降低生产成本,一部分振动圆柱陀螺仪不采用真空包装。然而,在非真空包装条件下,可能会产生内部声噪声,从而产生相当大的声压,作用在谐振壳上。基于结构声耦合理论,本文提出了在声压下谐振壳的动力特性。引入有限元(FE)模型来定量分析结构声耦合的影响。研究了几个主要因素,如密封帽的尺寸和真空度,这些因素直接影响谐振壳的振动。结果表明,当考虑结构声耦合的影响时,谐振壳的振动幅度和工作频率会发生变化。此外,还进行了实验研究结构声耦合对陀螺仪灵敏度的影响。当谐振壳与密封帽之间的径向间隙从 0.5mm 变为 20mm 时,观察到标度因数增加了 32.4mV/°/s,工作频率变化了 6.2Hz。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/318a/3892826/a141fce60df1/sensors-13-17176f1.jpg

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