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Pin type piezoelectric solid wave mode matching gyroscope

A technology for driving modes and pins, which is applied to the gyro effect for speed measurement, gyro/steering sensing equipment, measuring devices, etc., which can solve the problems of limited application, inconvenient detection accuracy, and large gyro bandwidth, and reduce the temperature. Sensitivity, mass production, and the effect of improving sensitivity

Active Publication Date: 2016-11-16
SHANGHAI JIAOTONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] This technology has the following disadvantages: the structure of the micro-gyro resonator of the spring mass system is fragile, which limits its application in many shock-resistant conditions; the processing technology of the gyro is relatively complicated, and the processing cost is high, which is not suitable for mass production and Encapsulation; the frequency split between the gyro drive mode and the detection mode is large, resulting in a large bandwidth of the gyro, and it is difficult to improve the quality factor; the gyro noise is large, and the generated signal is small, which is not easy to improve the accuracy of detection

Method used

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  • Pin type piezoelectric solid wave mode matching gyroscope
  • Pin type piezoelectric solid wave mode matching gyroscope
  • Pin type piezoelectric solid wave mode matching gyroscope

Examples

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Embodiment Construction

[0042] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several modifications and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0043] Such as figure 1 , 2 As shown, this embodiment provides a pin type piezoelectric solid wave mode matching gyroscope, including:

[0044] A cuboid harmonic oscillator 1 with a square top surface;

[0045] A columnar frame 2 hollowed out in the middle;

[0046] Four thin beams 3 connecting the cuboid resonator 1 and the cylindrical frame 2;

[0047] Two driving electrodes 4 symmetrically distributed in the center of the top surface of the cuboid resonator 1;

[0048] Four detection elect...

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PUM

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Abstract

The invention provides a pin-type piezoelectric gyroscope for matching solid fluctuation modes. The pin-type piezoelectric gyroscope comprises a cuboid harmonic oscillator with a square top surface, an internally-hollow double-square-frame-shaped cylindrical frame, four thin beam connected with the cuboid harmonic oscillator and the double-square-frame-shaped cylindrical frame, two drive electrodes symmetrically distributed at the centre of the top surface of the cubiod harmonic oscillator, four detection electrodes symmetrically distributed at the four corners of the top surface of the cubiod harmonic oscillator, and six pins extensionally distributed along the double-square-frame-shaped cylindrical frame, wherein the cubiod harmonic oscillator is located at the centre of the hollow part of the double-square-frame-shaped cylindrical frame and connected with the double-square-frame-shaped cylindrical frame by the four thin beams; the drive electrodes and the detection electrodes are connected to the pins by a metal connection wire through the thin beams. The pin-type piezoelectric gyroscope provided by the invention has the characteristics of being simple in structure, convenient to machine, small in size, high in Q value and the like, and is beneficial to package.

Description

technical field [0001] The invention relates to a solid wave mode matching gyroscope in the field of micro-electromechanical technology, in particular to a pin type piezoelectric solid wave mode matching gyroscope. Background technique [0002] Gyroscope is an inertial device that can be sensitive to the angle or angular velocity of the carrier, and it plays a very important role in the fields of attitude control, navigation and positioning. With the development of national defense technology and aviation and aerospace industries, the requirements of inertial navigation systems for gyroscopes are also developing in the direction of low cost, small size, high precision, multi-axis detection, high reliability, and adaptability to various harsh environments. The micro gyroscope based on MEMS technology is processed by micro-nano batch manufacturing technology, its cost, size, and power consumption are very low, and its environmental adaptability, working life, reliability, and ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C19/5642G01C19/5656
CPCG01C19/5684
Inventor 张卫平汪濙海刘亚东成宇翔唐健张弓许仲兴孙殿竣陈文元
Owner SHANGHAI JIAOTONG UNIV
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