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Decoupling type micro-gyroscope device for piezoelectric driving piezoelectric detection

A piezoelectric detection and piezoelectric drive technology, applied in the direction of measuring devices, gyro effect for speed measurement, gyroscope/steering sensing equipment, etc., can solve the problems of small electrostatic drive displacement, suction failure, low yield, etc., to achieve The orthogonal coupling error is small, the structure design is reasonable, and the effect of improving the detection accuracy

Pending Publication Date: 2020-04-07
ZHONGBEI UNIV
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0005] Through searching new materials in this field, it is found that Southeast University has applied for "Symmetric fully decoupled double-mass silicon micro-gyroscope with double tuning fork effect" (application number 201410362573.9), which uses electrostatic drive, capacitive detection, and overall structural design Complex, electrostatic driving displacement is small, the comb tooth voltage is easy to break down during detection, and it will also fail to attract during lateral impact, especially the comb manufacturing process requires extremely high precision and low yield
This patent designs a decoupling micro-gyro device for in-plane detection of tunnel magnetoresistance. The overall structure is reasonable and compact, with small orthogonal coupling error and high detection accuracy. The device innovatively applies electromagnetic drive and tunnel magnetoresistance detection to In the decoupling micro-gyroscope, this technical field has not yet been reported, and it is a technical field to be explored by the world's scientific and technological circles.

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  • Decoupling type micro-gyroscope device for piezoelectric driving piezoelectric detection
  • Decoupling type micro-gyroscope device for piezoelectric driving piezoelectric detection
  • Decoupling type micro-gyroscope device for piezoelectric driving piezoelectric detection

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Embodiment Construction

[0054] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention.

[0055] In the description of the present invention, it should be understood that the orientations or positional relationships indicated by the terms "center", "upper", "lower", "front", "rear", "left", "right" etc. are based on the attached The orientation or positional relationship shown in the figure is only for the convenience of describing the present invention and simplifying the description, and does not indicate or imply that the referred combination or element must have a specific orientation, be constructed and operated in a spec...

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Abstract

The invention belongs to the technical field of micro-inertial navigation instrument measuring instrument parts, and particularly relates to a decoupling type micro-gyroscope device for piezoelectricdriving piezoelectric detection. The decoupling type micro-gyroscope device for piezoelectric driving piezoelectric detection mainly comprises a supporting frame, mass blocks, a movable beam, a detection beam, a connecting block and a signal line. The mass blocks, a driving composite beam and a detection composite beam are arranged on the supporting frame; the mass blocks consist of a driving massblock, a detection mass block and a central mass block; and the driving composite beam is composed of the movable beam and the connecting block, the detection composite beam is composed of the detection beam and the connecting block, piezoelectric material structures are arranged on the driving mass block and the detection mass block, inverse piezoelectric effect driving and direct piezoelectriceffect detection are utilized, and the device is reasonable and compact in structural design, small in orthogonal coupling error and suitable for miniaturization.

Description

technical field [0001] The invention belongs to the technical field of micro-inertial navigation instrument measuring instrument components, and in particular relates to a decoupling micro-gyroscope device for piezoelectric-driven piezoelectric detection. Background technique [0002] Gyroscope is a sensor used to measure angular rate and is one of the core devices of inertial technology. It plays an important role in modern industrial control, aerospace, national defense, consumer electronics and other fields. [0003] For micromachined gyroscopes, the quadrature error is an important factor affecting its performance. For gyroscopes with undecoupled structures, the mass block and the fixed end are connected by a two-dimensional elastic beam. A single mass block has two degrees of freedom for driving and detection, and there is serious coupling between modes; decoupled gyroscopes can be divided into single decoupled And double decoupling, the single decoupling structure gyr...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C19/5656G01C19/5663
CPCG01C19/5656G01C19/5663
Inventor 金丽武绍宽李孟委张瑞
Owner ZHONGBEI UNIV