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Three-axis gyroscope

A gyroscope and gyroscope technology, applied in gyroscope/steering sensing equipment, gyro effect for speed measurement, instruments, etc., can solve the problems of low sensitivity, large orthogonal error, and low integration, and achieve a reasonable and compact overall structure, The effect of reducing the quadrature error and improving the detection accuracy

Pending Publication Date: 2021-08-03
美新半导体(天津)有限公司
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Problems solved by technology

In current consumer applications, it is generally a single-chip three-axis gyroscope, which is characterized by drive sharing and a reasonable layout of the X / Y / Z gyro masses. However, the three-axis gyroscope is also faced with large size and low integration High, the problem of large quadrature error
[0006] See Chinese invention patent CN108225295A, which discloses a three-axis gyroscope with tuning fork driving effect. The three-axis gyroscope disclosed in this patent has a cleverly designed steering structure. The left and right mass blocks are used to detect the Y / Z axis angular rate. The block is used to detect the X-axis angular rate, but obviously its integration is not high, and the Y / Z mass blocks share the mass block to easily generate coupling; continue to refer to the Chinese invention patent CN110926445A, which discloses a three-axis MEMS gyroscope, the patent The disclosed micro-gyroscope structure is a shared drive, and its innovation is that the X / Y gyroscope structure is novel in design, and the X / Y-axis gyroscope interacts and is arranged in the middle of the drive frame, and is supported by a central anchor point. The Z-axis gyroscope The gyroscopes are distributed on both sides of the X / Y gyroscope and connected to the middle gyroscope structure
Its overall structure design is novel and reasonable, and its integration is high, but its Z-axis gyroscope is not directly decoupled, so it may face the problems of low sensitivity and large quadrature error
[0007] Therefore, it is urgent to propose a new technical solution to solve the problems of low integration and large orthogonal error of the three-axis gyroscope in the prior art

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Embodiment Construction

[0026] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0027] Reference herein to "one embodiment" or "an embodiment" refers to a particular feature, structure or characteristic that can be included in at least one implementation of the present invention. "In one embodiment" appearing in different places in this specification does not all refer to the same embodiment, nor is it a separate or selective embodiment that is mutually exclusive with other embodiments. Unless otherwise specified, the words connected, connected, and joined in this document mean that they are electrically connected directly or indirectly.

[0028] In describing the present invention, it is to be understood that the terms "upper", "lower", "left", "right", "top", "bottom", "inner", "outer" etc. indicate an orie...

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Abstract

The invention provides a three-axis gyroscope, which comprises a first driving frame, a second driving frame, an X / Y gyroscope structure and a Z gyroscope structure, wherein the first driving frame can perform resonant motion along the X axis; the second driving frame is parallel to the first driving frame and is spaced from the first driving frame by a preset distance, and the second driving frame can perform resonant motion opposite to the first driving frame along the X axis; the X / Y gyroscope structure is coupled between the first driving frame and the second driving frame; the Z gyroscope structure is coupled between the first driving frame and the second driving frame and is positioned on one side of the X / Y gyroscope structure; and the X / Y gyroscope structure and the Z gyroscope structure are mutually independent, and the X / Y gyroscope structure and the Z gyroscope structure are both driven by the first driving frame and the second driving frame together. The three-axis gyroscope is reasonable and compact in overall structure and high in integration level, orthogonal errors can be reduced, and the detection precision is improved.

Description

【Technical field】 [0001] The invention relates to the technical field of micromechanical systems, in particular to a three-axis gyroscope. 【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 the fields of modern industrial control, aerospace, national defense and consumer electronics. [0003] The development of gyro can be roughly divided into three stages: [0004] The first stage is the traditional mechanical rotor gyro, which has high precision and plays an irreplaceable role in military strategic weapons such as nuclear submarines and intercontinental strategic missiles. However, it has a large volume, complicated manufacturing process, expensive price, long cycle and It is not suitable for mass production; the second stage is optical detection gyroscope, mainly including laser gyroscope and fiber optic gyroscope, mainly using the Sagnac effect, which has...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01C19/5691
CPCG01C19/5691
Inventor 凌方舟丁希聪蒋乐跃刘尧
Owner 美新半导体(天津)有限公司