Supercritical Carbon Dioxide (sCO2)-Cooled Current Source Inverter-based Integrated Motor Drive for MW-scale Electric Aviation Applications

Hang Dai, John Yagielski, Thomas Jahns, Kum Kang Huh, Vandana Rallabandi, Libing Wang, Tarak Saha, Wenda Feng, Bulent Sarlioglu

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

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 languageEnglish
Title of host publicationAPEC 2025 - 14th Annual IEEE Applied Power Electronics Conference and Exposition
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages3174-3180
Number of pages7
ISBN (Electronic)9798331516116
DOIs
StatePublished - 2025
Event14th Annual IEEE Applied Power Electronics Conference and Exposition, APEC 2025 - Atlanta, United States
Duration: Mar 16 2025Mar 20 2025

Publication series

NameConference Proceedings - IEEE Applied Power Electronics Conference and Exposition - APEC
ISSN (Print)1048-2334
ISSN (Electronic)2470-6647

Conference

Conference14th Annual IEEE Applied Power Electronics Conference and Exposition, APEC 2025
Country/TerritoryUnited States
CityAtlanta
Period03/16/2503/20/25

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

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