Design of Electric Machine for Electric Aircraft: A Case Study of Rotor-stator Configurations and Magnet Arrangements-Reference-Cited by-同舟云学术

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Design of Electric Machine for Electric Aircraft: A Case Study of Rotor-stator Configurations and Magnet Arrangements

Published:2020-08-17 Issue: Volume: Page:
ISSN:
Container-title:AIAA Propulsion and Energy 2020 Forum
language:
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Author:

Mitsuda Hiroshi¹,Miyama Yoshihiro¹,Ito Kazumasa¹,Yamada Masaki¹,Fukumoto Hisatoshi¹

Affiliation:

1. Mitsubishi Group

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. FAA. Aviation Emissions, Impacts & Mitifation. 2015.

2. IATA. Technology Roadmap 2013. 2013.

3. Parallel Hybrid Gas-Electric Geared Turbofan Engine Conceptual Design and Benefits Analysis

4. Partially Turboelectric and Hybrid Electric Aircraft Drive Key Performance Parameters

5. Overview of NASA Electrified Aircraft Propulsion (EAP) Research for Large Subsonic Transports

Cited by 3 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. Development of Double-Rotor Motor for Aircraft Electrification;IEEJ Transactions on Industry Applications;2024-07-01

2. Design and Fabrication of Dual-Rotor Motors with Axially Extended Stator for Electrified Aircraft Propulsion;2022 25th International Conference on Electrical Machines and Systems (ICEMS);2022-11-29

3. An Overview of High Specific Power Electrical Machines and Drives Technologies for Electrified Aircraft;2022 IEEE Energy Conversion Congress and Exposition (ECCE);2022-10-09

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