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 language | English |
|---|---|
| Pages (from-to) | 1537-1550 |
| Journal | IEEE Transactions on Transportation Electrification |
| Volume | 6 |
| Issue number | 4 |
| Online published | 25 May 2020 |
| DOIs | |
| Publication status | Published - Dec 2020 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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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
Fingerprint
Dive into the research topics of 'Analytical Modeling of a Double-Rotor Multiwinding Machine for Hybrid Aircraft Propulsion'. Together they form a unique fingerprint.Projects
- 1 Finished
-
ECS: Development of Novel High-performance Double-stator Motor Drives for Direct-drive Robotics
LIU, C. (Principal Investigator / Project Coordinator)
1/10/16 → 15/09/20
Project: Research
Student theses
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Design, Modeling, Optimization and Application of Permanent-Magnet Harmonic Electric Machines
ZHAO, H. (Author), LIU, C. (Supervisor), 6 Jan 2021Student thesis: Doctoral Thesis
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