Design of an Aviation Dual-Three-Phase High-Power High-Speed Permanent Magnet Assisted Synchronous Reluctance Starter-Generator With Antishort-Circuit Ability-Reference-Cited by-同舟云学术

Design of an Aviation Dual-Three-Phase High-Power High-Speed Permanent Magnet Assisted Synchronous Reluctance Starter-Generator With Antishort-Circuit Ability

Published:2022-10 Issue:10 Volume:37 Page:12619-12635
ISSN:0885-8993
Container-title:IEEE Transactions on Power Electronics
language:
Short-container-title:IEEE Trans. Power Electron.

Author:

Guo Hong¹^ORCID,He Xu¹,Xu Jinquan¹^ORCID,Tian Wei²^ORCID,Sun Gaoyang¹,Ju Laicai³,Li Dehong⁴

Affiliation:

1. School of Automation Science and Electrical Engineering, Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing, China

2. School of Electrical and Information Engineering, Jiangsu University, Zhenjiang, China

3. Beijing Shuguang Aviation Electric Co., Ltd., Beijing, China

4. Aviation Industry Helicopter Design and Research Institute, Tianjin, China

Funder

National Natural Science Foundation of China

Aeronautical Science Foundation of China

Publisher

Institute of Electrical and Electronics Engineers (IEEE)

Subject

Electrical and Electronic Engineering

Link

http://xplorestaging.ieee.org/ielx7/63/9803836/09766450.pdf?arnumber=9766450

Reference38 articles.

1. Influence analysis of slot parameters and high torque density optimisation for dual redundant permanent magnet motor in aerospace application

2. Design study of a three-phase brushless exciter for aircraft starter/generator

3. Design and Characterization of a Three-Phase Brushless Exciter for Aircraft Starter/Generator

4. Experimental Tests of Dual Three-Phase Synchronous Reluctance Motor Under Half-Control Mode

5. Comparison of Fault Characteristics According to Winding Configurations for Dual Three-Phase Synchronous Reluctance Motor

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