Abstract
Wide-bandgap enabled current-source inverter (CSI) is a promising power converter topology that has cleaner output voltage waveform, higher fault tolerance, and higher temperature operation capability than conventional voltage-source inverters (VSI). This paper presents a WBG-enabled CSI for a 2-MW integrated motor drive (IMD) for electric aviation application. The CSI system consists of two series-connected CSI that forms as a unit, and three such units are connected in parallel to drive a specially designed surface permanent magnet synchronous motor (PMSM) that has six individual groups of three-phase windings. Furthermore, the CSI's dc-link inductor and power modules are cooled with supercritical carbon dioxide (sCO2), and also cools the integrated PMSM's stator windings. The proposed CSI-based MW-scale IMD achieves an estimated 97.3% efficiency and 18.1 kW/kg power density. Its high-power density and promising fault-tolerance characteristics make it a competitive solution for MW-scale electric aviation applications.
Original language | English |
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Title of host publication | APEC 2025 - 14th Annual IEEE Applied Power Electronics Conference and Exposition |
Publisher | Institute of Electrical and Electronics Engineers Inc. |
Pages | 3174-3180 |
Number of pages | 7 |
ISBN (Electronic) | 9798331516116 |
DOIs | |
State | Published - 2025 |
Event | 14th Annual IEEE Applied Power Electronics Conference and Exposition, APEC 2025 - Atlanta, United States Duration: Mar 16 2025 → Mar 20 2025 |
Publication series
Name | Conference Proceedings - IEEE Applied Power Electronics Conference and Exposition - APEC |
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ISSN (Print) | 1048-2334 |
ISSN (Electronic) | 2470-6647 |
Conference
Conference | 14th Annual IEEE Applied Power Electronics Conference and Exposition, APEC 2025 |
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Country/Territory | United States |
City | Atlanta |
Period | 03/16/25 → 03/20/25 |
Funding
The authors gratefully acknowledge the support from U.S. Advanced Research Project Agency-Energy (ARPA-E) under Project Number DE-AR0001353. The views and opinions expressed in this paper are those of the authors and do not necessarily reflect those of the U.S. ARPA-E.
Keywords
- current source inverter
- electric aviation
- integrated motor drive
- sCO