Completely non - contacting magnetic suspension control moment gyro of single framework
A technology for controlling torque gyroscopes and magnetic levitation, which is applied to the guidance devices of space navigation vehicles, etc., can solve the problems of large size and weight of the frame system, affect the stability of the spacecraft, and interfere with the spacecraft system, so as to reduce the size and weight, improve the Reliability and service life, the effect of reducing the bonding area
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[0022]As shown in Figure 2, the present invention is mainly composed of two parts: a magnetic levitation rotor system and a magnetic levitation frame system, wherein the magnetic levitation rotor system is mainly composed of a sealing cover 1, a gyro rotor 2, a radial magnetic bearing 3, a left axial magnetic bearing 4, and a protective bearing 5 , shaft seat 6, rotor system radial / axial integrated displacement sensor 7, rotor system base 8, drive motor 9, rotor system connector 10, right axial magnetic bearing 11, of which gyro rotor 2, radial magnetic bearing 3 The rotor part, the driving motor 9 The rotor part, the left axial magnetic bearing 4 The rotor part, the right axial magnetic bearing 11 The rotor part constitutes the rotor assembly of the magnetic levitation rotor system, the rest is the stator assembly, and the stator assembly and the rotor assembly are connected by a radial The magnetic bearing and the axial magnetic bearing realize stable suspension without mecha...
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