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Analytical Modeling of a Double-Rotor Multiwinding Machine for Hybrid Aircraft Propulsion

Hang Zhao, Chunhua Liu*, Zaixin Song, Wusen Wang

*Corresponding author for this work

Research output: Journal Publications and ReviewsRGC 21 - Publication in refereed journalpeer-review

Abstract

In this article, a new double-rotor multiwinding machine (DRMWM) that utilizes the flux modulation principle is proposed for propulsion system of hybrid electric aircrafts (HEAs). First, the operation principle of DRMWMs and the corresponding HEA propulsion configuration are introduced, where different operation modes of two rotors and three sets of windings of DRMWMs to cope with various flight tasks of HEAs are elucidated. Then, an improved subdomain method is utilized to solve the magnetic field distribution of DRMWMs with the consideration of saturation effect of soft-magnetic material (SMM). Finally, a prototype is manufactured to verify the effectiveness of the proposed improved subdomain method in predicting the electromagnetic performances of DRMWMs. The experiment shows that the DRMWM is a good candidate to be applied in HEA with different operation modes. © 2020 IEEE.
Original languageEnglish
Pages (from-to)1537-1550
JournalIEEE Transactions on Transportation Electrification
Volume6
Issue number4
Online published25 May 2020
DOIs
Publication statusPublished - Dec 2020

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

  1. SDG 7 - Affordable and Clean Energy
    SDG 7 Affordable and Clean Energy

Research Keywords

  • Aircraft
  • electrified transportation
  • flux modulation
  • hybrid propulsion
  • operation modes
  • permanent-magnet machine
  • subdomain method
  • unmanned aerial vehicle (UAV)

RGC Funding Information

  • RGC-funded

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