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Circular and multi-ring shaped axial and radial magnetizing permanent magnetism antimagnetic rotor electrostatic rotating micro gyroscope

An axial-radial, magnetic rotor technology is applied in the field of circular and multi-annular axial-radial magnetized permanent magnet diamagnetic rotor electrostatic rotating micro-gyroscopes, which can solve the problems of complicated process and increased rotor suspension lifting requirements, etc. Achieve the effect of improving the axial stiffness, enhancing the stable suspension performance, reducing the start-up process and the difficulty of start-up control

Inactive Publication Date: 2009-12-02
SHANGHAI JIAOTONG UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

Its shortcoming is that radial control electrodes for controlling the radial (X, Y) position of the rotor are arranged on the radially inner and outer sides of the rotor; Axial control electrodes for axial position suspension control, so that the suspension support of the rotor needs to control 5 degrees of freedom, which greatly increases the requirements for the suspension support of the rotor, and the process is also more complicated

Method used

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  • Circular and multi-ring shaped axial and radial magnetizing permanent magnetism antimagnetic rotor electrostatic rotating micro gyroscope
  • Circular and multi-ring shaped axial and radial magnetizing permanent magnetism antimagnetic rotor electrostatic rotating micro gyroscope
  • Circular and multi-ring shaped axial and radial magnetizing permanent magnetism antimagnetic rotor electrostatic rotating micro gyroscope

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Embodiment Construction

[0024] The embodiments of the present invention are described in detail below in conjunction with the accompanying drawings: the present embodiment is implemented on the premise of the technical solution of the present invention, and detailed implementation methods and processes are provided, but the protection scope of the present invention is not limited to the following implementations example.

[0025] Such as figure 1 As shown, this embodiment adopts a three-layer structure, which is composed of three parts: the upper stator 1, the rotor 3 and the lower stator 2. The upper stator 1 is inverted on the lower stator 2, so that the upper stator 1 and the lower stator 2 are two top Face to face, the assembly is completed, thereby forming a cavity, and the rotor 3 is suspended in this cavity. During assembly, the surface facing the rotor 3 in the structure of the upper stator 1 is called the top surface, and the corresponding other surface is called the bottom surface. Similar...

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Abstract

A circular and multi-ring axial radial magnetization permanent magnet anti-magnetic rotor electrostatic rotating micro-gyroscope in the field of micro-electromechanical systems, consisting of an upper stator, a rotor and a lower stator, relying on cylindrical and multi-ring shapes in the upper and lower stators Axial and radial magnetized permanent magnets provide levitation force and lateral stabilizing force to the anti-magnetic rotor to realize uncontrolled self-stabilizing suspension. The rotating electrodes of the upper and lower stators and the rotor form a variable capacitance motor, which pulls the rotor to rotate at high speed, and at the same time Use the axial detection of the upper and lower stators, the feedback electrodes and the lateral detection of the lower stator, and the electrostatic force between the feedback electrodes and the rotor to improve the axial stiffness, lateral stiffness and impact resistance of the micro gyroscope, enhance the stable suspension performance, and reduce the It eliminates the starting process of the rotor and the difficulty of starting control. It can achieve self-stabilization without complicated control mechanism. It has low power consumption, convenient implementation, and small size. X, Y two-axis angular acceleration.

Description

technical field [0001] The invention relates to a miniature gyroscope in the field of micro-electromechanical technology, in particular to an electrostatic rotating micro-gyroscope with a circular and multi-ring axially and radially magnetized permanent magnet antimagnetic rotor. Background technique [0002] The inertial navigation system is an autonomous navigation technology that directly calculates the navigation parameters such as the position, heading and attitude of the carrier according to Newton's law of inertia. During the working process, it neither transmits energy to the outside world nor obtains information from the outside. It has unique advantages such as being free from interference, can be used anywhere, has good dynamic performance, and rich navigation output information. It is widely used in the fields of aviation, aerospace and navigation. It has been widely used, and the emergence of MEMS (Micro-electromechanical Systems, micro-electromechanical systems...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01C19/24H02N15/00B81B7/02
Inventor 张卫平陈文元刘武张忠榕
Owner SHANGHAI JIAOTONG UNIV