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Micro-silicon resonance accelerometer with temperature stress compensation and vibration decoupling capabilities

A technology of temperature stress and accelerometer, applied in the direction of speed/acceleration/shock measurement, gyro effect for speed measurement, gyroscope/steering sensing equipment, etc., can solve the problem of sensitivity dead zone, achieve suppression of common mode interference, and achieve temperature Effects of stress compensation and processing technology compatibility

Active Publication Date: 2016-01-20
BEIJING INST OF AEROSPACE CONTROL DEVICES
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  • Abstract
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Problems solved by technology

[0004] The technical problem solved by the present invention is: the present invention overcomes the deficiencies of the prior art, proposes a silicon microresonant accelerometer with temperature stress compensation and vibration decoupling capabilities, solves the problem of thermal stress release of the tuning fork under high and low temperature conditions, and The Sensitivity Dead Zone Problem Produced by the Vibration Coupling of Two Tuning Forks

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  • Micro-silicon resonance accelerometer with temperature stress compensation and vibration decoupling capabilities
  • Micro-silicon resonance accelerometer with temperature stress compensation and vibration decoupling capabilities
  • Micro-silicon resonance accelerometer with temperature stress compensation and vibration decoupling capabilities

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Embodiment Construction

[0028] The basic idea of ​​the present invention is: a silicon microresonance accelerometer with temperature stress compensation and vibration decoupling capability, the structure is two parts A and B that are independent of each other and symmetrical about the center line, and the two parts realize differential measurement. The mass blocks of each part are suspended in the air through their respective mass block support beams, which feel the acceleration input and generate acceleration inertia force. The acceleration inertial force is amplified by the force amplification of the lever, and applied to the axial direction of the tuning fork, which is converted into an axial force of the tuning fork, which changes the equivalent stiffness of the working vibration mode of the tuning fork, and the vibration frequency of the tuning fork changes accordingly. By detecting the resonance of the tuning fork The change of frequency can demodulate the magnitude of the acceleration load. Th...

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Abstract

The invention provides a micro-silicon resonance accelerometer with temperature stress compensation and vibration decoupling capabilities. The micro-silicon resonance accelerometer comprises main parts including mass blocks, a lever, a lever supporting cantilever, resonance tuning forks, mass block supporting arms and the like. When the temperature of the environment of the accelerometer is changed, the length of a resonance beam is changed. The thermal deformation size of the lever supporting cantilever is matched with the thermal strain of the resonance beam, so that axial thermal stress of the resonance beam is sufficiently released; the resonance efficiency of the resonance tuning forks is not influenced by the thermal stress. When one tuning fork vibrates, weak displacement is generated in the axial direction to draw the mass block to vibrate, and draw the tuning fork on the other side to from vibration coupling. When the vibration frequencies of the two tuning forks are the same, the vibration frequency is not changed along with the change of the load, and a sensitivity dead zone is formed. The size of the range is directly related with a vibration coupling degree. Therefore, the whole structure of the accelerometer is divided into two symmetrical parts; the two mass blocks in the middle are supported through the mass block supporting arms respectively and the sensitivity dead zone is reduced to the minimum size.

Description

technical field [0001] The invention relates to a silicon micro-resonance accelerometer with temperature stress compensation and vibration decoupling capabilities, which belongs to the field of frequency output accelerometer structure design, and the technical direction of temperature stress and vibration decoupling. Background technique [0002] The temperature compensation technology of the frequency output accelerometer is a key technical issue in the design and debugging process of the accelerometer. The differential output structure of double tuning fork is an effective way of temperature compensation, which is adopted by various frequency output accelerometer structures (French ONERA, American Kearfort, Holleywell, etc.). But this method is a follow-up processing compensation method. The resonant frequency of each single tuning fork still changes with the temperature. The temperature stress felt by the tuning fork has not been eliminated, and the problem has not been f...

Claims

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Application Information

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IPC IPC(8): G01C19/5614G01C19/5621
CPCG01C19/5614G01C19/5621
Inventor 庄海涵王岩邢朝洋刘福民刘国文徐宇新张玲
Owner BEIJING INST OF AEROSPACE CONTROL DEVICES
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