[an error occurred while processing this directive]
   
 
���¿��ټ��� �߼�����
   ��ҳ  �ڿ�����  ��ί��  Ͷ��ָ��  �ڿ�����  ��������  �� �� ��  ��ϵ����
�������պ����ѧѧ�� 2006, Vol. 32 Issue (02) :190-194    DOI:
���� ����Ŀ¼ | ����Ŀ¼ | ������� | �߼����� << | >>
���п�������ˢֱ���綯���ݴ����з�ʽ
��Ԫ��, ���۷�, ����ǿ*
�������պ����ѧ �Զ�����ѧ���������ѧԺ, ���� 100083
Fault-tolerance operation of brushless DC motor for flight control
Zhou Yuanjun, Dong Huifen, Wang Ziqiang*
School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

ժҪ
�����
�������
Download: PDF (425KB)   HTML 1KB   Export: BibTeX or EndNote (RIS)      Supporting Info
ժҪ ˫��������ˢֱ���綯�����ɵ�˫ͨ����������ϵͳ(EMA,Electro-Mechanical Actuator),��һ��ͨ������ʱ���Բ����ݴ����з�ʽ.�����˵綯����˫���鹤���뵥���鹤��ʱ�Ļ�е���ԡ�ͭ���������ת��.�������Ļ�е�����������߷�����֪,����ͬ�ĵ�ѹ������,���ֹ�����ʽ�Ļ�е��������ͬ���������ת��,���ݴ���ʱ���ز�����ת�ٽ�������1��.�ڹ�����IJ����������,�ݴ���ʱ�綯�����������Ϊ�ֵ��1.4��,����ת��Ϊ�ֵ��0.7��,ͨ�������������������ݳ����֤����һ��.̽����˫��������ʱ�ĵ���������Ʒ����Լ��ݴ�����ȡ�Ĵ�ʩ,���÷������߷������ݴ�����ʽ�µĶ�̬����.
Service
�ѱ����Ƽ�������
�����ҵ����
�������ù�����
Email Alert
RSS
�����������
�ؼ����� ��ˢ���   �ݴ�   ��������ϵͳ     
Abstract�� The operation of a brushless DC motor with dual-windings for the flight control system was described. The dual-channels electro-mechanical actuator (EMA) is composed of the motor, the fault-tolerance operation mode can be obtained when any channel is failure. The mechanical characteristic, power losses and allowed torque of the motor were analyzed at two cases of normal and fault-tolerance operation modes. From the experimental mechanical characteristics curve, it can be obtained that the no load speeds of two operation modes are same under the same voltage, but the speed drop in the case of the fault-tolerance operation is greater than the normal operation because of the load. Holding the power loss not changed in the case of fault-tolerance operation, the motorallowed current is 1.4 times of the rated current and the allowed torque is 0.7 times of the rated torque, these were validated by the temperature experimental data. The balance control of the dual-windings operation and the control method of the fault-tolerance operating were researched, the dynamic characteristic of the fault-tolerance operation was simulated.
Keywords�� brushless electric machines   fault-tolerance   electro-mechanical actuator     
Received 2005-01-14;
Fund:

���տ�ѧ����������Ŀ(01F51016)

About author: ��Ԫ��(1951-),Ů,��������,����, zhouyuanjun304@163.com.
���ñ���:   
��Ԫ��, ���۷�, ����ǿ.���п�������ˢֱ���綯���ݴ����з�ʽ[J]  �������պ����ѧѧ��, 2006,V32(02): 190-194
Zhou Yuanjun, Dong Huifen, Wang Ziqiang.Fault-tolerance operation of brushless DC motor for flight control[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2006,V32(02): 190-194
���ӱ���:  
http://bhxb.buaa.edu.cn//CN/     ��     http://bhxb.buaa.edu.cn//CN/Y2006/V32/I02/190
Copyright 2010 by �������պ����ѧѧ��