Fault tolerant topology structure of high-speed rotor inverter of magnetic suspension control torque gyroscope

A technology for controlling torque gyroscopes and high-speed rotors, which is applied in fields such as excitation or armature current control, control systems, and motor control. Achieve the effects of avoiding fault isolation and system reconfiguration time increase, improving system reliability, and consistent topology

Active Publication Date: 2014-11-05
安徽华驰动能科技有限公司
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Problems solved by technology

However, for the Buck DC-DC converter plus three-phase full-bridge inverter structure, its fault performance is different from that of the traditional three-phase full-bridge inverter, specifically: the system cannot work after the Buck power tube fails open circuit; After the short-circuit fault of the power tube, the motor winding will over-current, which will cause the winding to burn out; after the single-circuit fault of the three-phase bridge power tube, the motor will run without phase, the current will increase, and the efficiency will decrease. Long-term operation may cause the system to overheat, which will cause Secondary fault; after a short-circuit fault of a single tube of a three-phase bridge power tube, due to the switching of the conduction logic, the faulty bridge arm will pass through, and t

Method used

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  • Fault tolerant topology structure of high-speed rotor inverter of magnetic suspension control torque gyroscope
  • Fault tolerant topology structure of high-speed rotor inverter of magnetic suspension control torque gyroscope
  • Fault tolerant topology structure of high-speed rotor inverter of magnetic suspension control torque gyroscope

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[0020] Such as figure 1 As shown, the present invention includes a regulated DC power supply 1, a Buck DC-DC converter with redundant power tube 2, a fault protection circuit 3, a four-leg phase redundant inverter 4, a small armature inductance permanent magnet brushless The DC motor 5, the stabilized DC power supply 1 passes through the Buck DC-DC converter 2 with redundant power tube, and is connected to the four-leg phase redundant inverter 4 to drive the small armature inductance permanent magnet brushless DC motor 5. At the same time , A fault protection circuit 3 is added between the Buck DC-DC converter with redundant power tube 2 and the four-leg phase redundant inverter 4 to realize isolation protection after a fault; Buck DC- with redundant power tube The DC converter 2 is composed of the main Buck DC-DC converter 11, the redundant MOSFET tube 10 and the Buck power tube failover circuit 9. After the MOSFET Q7 fails, the Buck power tube failover circuit 9 performs the ...

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Abstract

A fault tolerant topology structure of a high-speed rotor inverter of a magnetic suspension control torque gyroscope is mainly composed of a Buck DC-DC converter with a redundancy tube, a four-leg phase redundancy inverter, a fault protection circuit, a small armature and inductance permanent magnet brushless DC motor and the like. According to the characteristics of the small armature and inductance permanent magnet brushless DC motor, the redundancy topology structure is designed based on a motor drive circuit with the Buck DC-DC converter and a three-phase full-bridge inverter, reliability of a high-speed rotor drive circuit of the magnetic suspension control torque gyroscope is improved, and fault tolerant control is achieved after a power tube is disconnected or short-circuits; meanwhile, a drive system has the advantage of low power consumption before and after a fault happens, and the structure has high application value for spacecrafts paying attention to low power consumption and high reliability.

Description

technical field [0001] The invention relates to a fault-tolerant topological structure of a maglev control moment gyro high-speed rotor inverter, which is used for the fault-tolerant control of a permanent magnet brushless DC motor with a small armature inductance, and is especially suitable for the high-speed drive components of attitude control actuators such as satellites and space stations. reliable control. Background technique [0002] Space applications require high precision, high torque, low power consumption, high reliability and long life for attitude control actuators. The magnetic levitation control moment gyroscope has the advantages of no friction and wear, no lubrication, long life, and high precision through active vibration control because its high-speed rotor is supported by magnetic levitation. It is an important attitude control actuator on the spacecraft. The high-speed rotor of the magnetic levitation control torque gyro is driven by a brushless DC mo...

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Application Information

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IPC IPC(8): H02P29/02H02P7/29H02M7/537
CPCY02B70/10
Inventor 李海涛李文琢郑世强朱敏金浩
Owner 安徽华驰动能科技有限公司
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