摘要
阐述一种用于全电飞机机电作动系统的双绕组永磁无刷直流电动机。该电动机定子上有双重绕组,由两套独立的功率电路驱动形成双通道控制系统。该系统能够实现容错控制以提高可靠性。论文研究了该电动机的数学模型与转矩特性,并给出试验结果。
A permanent magnet brushless DC motor was presented, which will be used for a Electro-Mechanical Actuator (EMA) in a All-Electric Aircraft(AEA). This motor includes double-windings in stator, which are driven by two independent sets of power electronic circuits, thereby it is formed that a electrical driven system with dual control channels. A fault-tolerated operation mode can be used in this system for high reliability. The model of the motor and the torque characteristics are researched, and finally the test data are given.
出处
《电工技术学报》
EI
CSCD
北大核心
2004年第4期12-16,共5页
Transactions of China Electrotechnical Society
基金
航空科学基金资助项目(01F51016)
关键词
无刷直流电动机
机电作动器
容错工作
Brushless DC motor,electro-mechanical actuator (EMA),fault-tolerated operation