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Vibration isolation frame work decoupled silicon micro-gyroscope

A technology of silicon micro-gyroscope and frame, which is applied in the direction of speed measurement by gyro effect, gyroscope/steering sensing equipment, and technology for producing decorative surface effects, etc., to increase sensitivity, improve anti-interference ability, and reduce coupling Effect

Active Publication Date: 2011-04-27
NAT UNIV OF DEFENSE TECH
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Problems solved by technology

Although these decoupled micro-gyro structures separate the supporting beams of the driving mode and the detection mode, they do not completely separate the inertial masses of the two modes. When there is an input angular velocity, the inertial mass vibrates in both the driving mode and the The detection modal vibration caused by Coriolis force is prone to vibration coupling and affects the performance of the micro gyroscope

Method used

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  • Vibration isolation frame work decoupled silicon micro-gyroscope
  • Vibration isolation frame work decoupled silicon micro-gyroscope
  • Vibration isolation frame work decoupled silicon micro-gyroscope

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Embodiment Construction

[0039] The present invention will be described in further detail below in conjunction with the accompanying drawings and specific embodiments.

[0040] Such as figure 1 , figure 2 , image 3 with Figure 4As shown, a silicon micro-gyroscope decoupled by a vibration-isolation frame of the present invention includes a first substrate 1 and a second substrate 16 above the first substrate 1, and two detection electrodes 2 are arranged on the first substrate 1. , the second substrate 16 includes two driving masses 7 with the same structure and arranged symmetrically that can vibrate along the driving direction, two proof masses 14 with the same structure and arranged symmetrically that can vibrate along the detecting direction, driving electrodes 4, movable The drive comb 5, the fixed drive comb 6 and the vibration isolation frame assembly, the two detection masses 14 are located directly above the two detection electrodes 2 on the first substrate 16, the vibration isolation f...

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Abstract

A silicon micro-gyroscope with vibration isolation framework decoupling comprises a first substrate and a second substrate above the first substrate; two detection electrodes are arranged on the first substrate; the second substrate comprises two drive mass blocks, two detection mass blocks, drive electrodes and a vibration isolation framework component; the two drive mass blocks with the same structure are symmetrically arranged and can be vibrated along the drive direction; the two detection mass blocks with the same structure are symmetrically arranged and can be vibrated along the detection direction; the detection mass blocks are arranged on the first substrate and above the two detection electrodes; the vibration isolation framework component is arranged at the middle part of the second substrate; and both ends of the vibration isolation framework component are respectively connected with the two drive mass blocks and the two detection mass blocks through elastic beams. The silicon micro-gyroscope with vibration isolation framework decoupling has simple and compact structure, low cost, simple machining technology, easy mass production and high product quality.

Description

technical field [0001] The invention mainly relates to the field of micro-electro-mechanical systems, in particular to a silicon micro-gyroscope decoupled by a vibration-isolation frame. Background technique [0002] Compared with traditional gyroscopes, silicon micro-gyroscopes have the advantages of small size, light weight, and low price, and are widely used in aircraft stability control, weapon system navigation guidance, micro-satellite attitude control and other fields. Vibrating silicon micro-gyroscopes have become the main structural form of micro-gyroscopes because they have no rotating parts. With the development of MEMS technology, various silicon micro-mechanical gyroscopes are emerging in an endless stream in the world. Their common feature is that there are two vibration directions perpendicular to each other, that is, the vibration excitation direction and the sensitive vibration direction under the action of Coriolis force. [0003] The working principle of...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C19/56B81B7/02B81C1/00G01C19/5733
Inventor 吴学忠李圣怡肖定邦侯占强董培涛满海鸥王浩旭
Owner NAT UNIV OF DEFENSE TECH
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