A SiC MOSFET propulsion inverter design with power redundancy, considering unwanted events, for electrical aircrafts-Reference-Cited by-同舟云学术

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A SiC MOSFET propulsion inverter design with power redundancy, considering unwanted events, for electrical aircrafts

Published:2024-06-19 Issue: Volume: Page:1-6
ISSN:
Container-title:2024 IEEE Transportation Electrification Conference and Expo (ITEC)
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Author:

Kim Simon¹,Lee Donghyun²,Mier Ainhoa Puyadena³,Kim Myeonghyo⁴,Kwak Byunggil⁴

Affiliation:

1. Infineon Technologies Korea Ind., Inf., Consum., Comp & Comm.,Seoul,Korea

2. Hanwha Systems Power Control Team,Yongin,Korea

3. Infineon Technologies Germany Green Industrial Power (Technical Marketing),Warstein,Germany

4. Hanwha Aerospace Co., Ltd. E-Propulsion Biz. Group,Seongnam,Korea

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10598816/10598836/10599039.pdf?arnumber=10599039

Reference12 articles.

1. Electric Aircraft System Co-Simulation Including Body, Propeller, Propulsion, and Energy Storage Models

2. A Comparison of Electrical Vehicle Power Systems to Predict Architectures, Voltage Levels, Power Requirements, and Load Characteristics of the Future All Electrical Aircraft;Alexander

3. Fault Tolerant More Electric Engine/Aircraft Architecture with Integrated Condition-Based Control

4. Aviation battery monitoring electronics in lithium-ion based battery systems for electrified sailplanes and aircrafts

5. DC Link Voltage Control Strategy for Electric Propulsion Aircraft

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