Electromagnetic Design of Dual Winding Permanent Magnet Synchronous Motor for Electromechanical Actuators of Flight Control Systems

被引：0
|
作者：
Terao, Yutaka [1 ]
Hirayama, Hiroshi [2 ]
Sugawara, Hirotaka [3 ]
Oyori, Hitoshi [3 ]
机构：
[1] Univ Tokyo, Grad Sch Frontier Sci, Chiba, Japan
[2] Akita Univ, Grad Sch Engn Sci, Akita, Japan
[3] IHI Corp, Aeroengine Space & Def Business Area, Tokyo, Japan
来源：
2022 INTERNATIONAL POWER ELECTRONICS CONFERENCE (IPEC-HIMEJI 2022- ECCE ASIA) | 2022年
关键词：
Electromechanical actuator; flight control systems; more electric aircraft; permanent magnet synchronous motor;
D O I：
暂无
中图分类号：
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号：
0807 ; 0820 ;
摘要：
This paper deals with PM motors using multi-pole anisotropic ring magnet for electro mechanic actuators (EMAs) of future aircraft flight control systems. The electromagnetic design via FEM software and evaluations of motor torque, losses in healthy and failure state are carried out. The results showed that even if one-phase open circuit of an inverter occurred or one-side of the 3-phase current supply system failed, the PM motor could operate at 100% of the average torque of 5.5 Nm or over 14.6 Nm, which is over 97 % of the maximum torque of 15.0 Nm.
引用
收藏
页码：2135 / 2140
页数：6
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