Electromagnetic Design of Dual Winding Permanent Magnet Synchronous Motor for Electromechanical Actuators of Flight Control Systems
Author:
Affiliation:
1. Graduate School of Frontier Sciences, The University of Tokyo,Chiba,Japan
2. Graduate School of Engineering Science, Akita University,Akita,Japan
3. Aero-Engine, Space & Defense Business Area, IHI Corporation,Tokyo,Japan
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9806820/9806821/09807212.pdf?arnumber=9807212
Reference11 articles.
1. Primary Flight Control Actuation System for 787;Moog,0
2. The A380 flight control electrohydrostatic actuators, achievements and lessons learnt;bossche;25th Int Congress Aeronautical Sci,0
3. Motor Application of NEOMAX® Nd-Fe-B Anisotropic Ring Magnets;marukawa;HITACHI MATERIALS TECHNICAL REVIEW,2019
4. High Reliability Permanent Magnet Brushless Motor Drive for Aircraft Application
5. Fault-tolerant and resilient electrification for the More Electric Engine;oyori;49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition,0
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Investigation of Slot Shape and Associated Winding Configuration for Aerospace Actuator Motor;2023 IEEE International Electric Machines & Drives Conference (IEMDC);2023-05-15
2. Improvement Torque ripple characteristics of Dual-Winding Square wave Brushless DC Motor with phase difference drive;2023 IEEE International Magnetic Conference - Short Papers (INTERMAG Short Papers);2023-05
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