Power Electronics Circuits Design and Validation of a 2 kV 1 MW Integrated Modular Motor Drive for Electric Aircraft Propulsion-Reference-Cited by-同舟云学术

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Power Electronics Circuits Design and Validation of a 2 kV 1 MW Integrated Modular Motor Drive for Electric Aircraft Propulsion

Published:2023-07-18 Issue: Volume: Page:
ISSN:
Container-title:2023 IEEE Workshop on Power Electronics for Aerospace Applications (PEASA)
language:
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Author:

Cong Yizhou¹,Borjas Rob¹,Schnabel Alec¹,Shi Yifan¹,Fu Pengyu¹,Wang Jin¹

Affiliation:

1. The Ohio State University,Center for High Performance Power Electronics (CHPPE),Department of Electrical and Computer Engineering,Columbus,OH,USA,43210

Funder

NASA

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10235329/10235365/10235373.pdf?arnumber=10235373

Reference12 articles.

1. Submodule Design of a 2 kV 1 MW Integrated Modular Motor Drive for Aviation Applications

2. 2-kV 1-MW 20,000-RPM Integrated Modular Motor Drive for Electrified Aircraft Propulsion

3. Low Pressure Partial Discharge Tests with Ultra High dv/dt PWM Voltages for Aircraft Motor Windings

4. Laminated bus bars for power system interconnects

5. A cryogenically-cooled mw inverter for electric aircraft propulsion;chen;2020 AIAA/IEEE Electric Aircraft Technologies Symposium (EATS),2020

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