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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2010, Vol. 31 ›› Issue (5): 975-982.

• Avionics and Autocontrol • Previous Articles     Next Articles

Analysis of Winding Short-circuit in Electrical/Mechanical Hybrid 4-redundancy Brushless DC Torque Motor

Wang Wei; Guo Hong; Li Yanming   

  1. School of Automation Science and Electrical Engineering, Beijing University of Aeronautics andAstronautics
  • Received:2009-04-15 Revised:2009-07-07 Online:2010-05-25 Published:2010-05-25
  • Contact: Wang Wei

Abstract: This article investigates the effect of winding short-circuit on the performance of the electrical/mechanical hybrid 4-redundancy brushless direct circuit torque motor (BLDCTM) in direct drive actuator (DDA). Based on the mathematic model of the electrical/mechanical hybrid 4-redundancy BLDCTM, the motor electrical parameter variations due to winding short-circuit are analyzed, and the equivalent circuit models are established for both interturn short-circuit and interphase short-circuit situations. The simulation results of the motor system demonstrate that the proposed low speed redundancy BLDCTM can ensure the normal executive functioning of the DDA when the interturn short-circuit in one of the phases or the interphase short-circuit between two phases occurrs. The electrical/mechanical hybrid 4-redundancy BLDCTM can overcome completely the effect of winding short-circuit and enhance the reliability of the DDA system.

Key words: brushless direct circuit motor, redundancy, actuator, interturn short-circuit, interphase short-circuit

CLC Number: