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Stator rotation type magnetic-suspension sensitive gyroscope

A magnetic levitation gyro and sensitive gyro technology, which is applied in the field of gyroscopes, can solve the problems of large power consumption and large size, and achieve the effects of low power consumption, small size, and elimination of gyro drift

Active Publication Date: 2017-08-04
UNIV OF SCI & TECH BEIJING
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide a stator rotating magnetic levitation sensitive gyroscope to overcome the disadvantages of large volume and large power consumption of the existing rotation modulation system

Method used

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  • Stator rotation type magnetic-suspension sensitive gyroscope
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Embodiment Construction

[0028] In order to make the technical problems, technical solutions and advantages to be solved by the present invention clearer, the following will describe in detail with reference to the drawings and specific embodiments.

[0029] The invention provides a stator rotating magnetic levitation sensitive gyroscope.

[0030] Such as figure 1 , 2 As shown in and 3, the stator rotating magnetic levitation sensitive gyroscope is mainly composed of four parts: magnetic levitation bearing system, magnetic levitation gyro rotor system, torquer stator rotation system and gyro house, mainly including: upper axial magnetic levitation bearing 1, lower axial Magnetic suspension bearing 2, radial magnetic suspension bearing 3, magnetic suspension gyro rotor 4, high-speed motor 5, torquer rotor assembly 6, photoelectric code disc 7, end bearing 8, rotation modulation rotor skeleton 9, rotation modulation motor 10, rotation modulation motor mount 11. The torquer stator adapter plate 12 and ...

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Abstract

The invention provides a stator rotation type magnetic-suspension sensitive gyroscope, belonging to the technical field of gyroscopes. The gyroscope comprises a magnetic-suspension bearing system, a magnetic-suspension gyroscope rotor system, a torque stator rotating system and a gyroscope chamber, wherein the magnetic-suspension bearing system comprises an upper axial magnetic-suspension bearing, a lower axial magnetic-suspension bearing and a radial magnetic-suspension bearing; the magnetic-suspension gyroscope rotor system comprises a magnetic-suspension gyroscope rotor, a high-speed motor and a torque rotor assembly; the torque stator rotating system comprises a photoelectric code disc, an end surface bearing, a rotary modulating rotor skeleton, a rotary modulating motor, a rotary modulating motor mounting seat, a torque stator changeover panel and a torque stator assembly; and the gyroscope chamber comprises a lower gyroscope chamber, a middle gyroscope chamber and an upper gyroscope chamber. The stator rotation type magnetic-suspension sensitive gyroscope has a rotary modulating function, so that the measurement accuracy of the angular rate of the magnetic-suspension sensitive gyroscope can be increased; and a system has a relatively small volume and relatively low power consumption.

Description

technical field [0001] The invention relates to the technical field of gyroscopes, in particular to a stator rotating magnetic levitation sensitive gyroscope. Background technique [0002] As the main angular rate detection equipment for inertial navigation, gyroscopes play an important role in both military and civilian fields. Existing high-precision, high-bandwidth angular rate sensitive devices such as fiber optic gyroscopes, laser gyroscopes, and magnetic levitation sensitive gyroscopes are used for a long time The angular rate detection error caused by gyro drift including gyro zero bias, random drift and temperature-related error is unavoidable. The impact of gyro drift on the detection accuracy of high-precision gyroscope is fatal. [0003] Rotational modulation technology, by rotating the sensitive axis of the inertial device, it rotates around a fixed coordinate system (generally the carrier coordinate system), so that the gyro drift error in the direction orthogo...

Claims

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Application Information

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IPC IPC(8): G01C19/02G01C19/24
CPCG01C19/02G01C19/24
Inventor 缪存孝张贺孙志辉胡纯楚焕鑫卢明华邢国柱
Owner UNIV OF SCI & TECH BEIJING
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