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

被引：0

作者：

Kim, Simon ^{[1
]}

Lee, Donghyun ^{[2
]}

Mier, Ainhoa Puyadena ^{[3
]}

Kim, Myeonghyo ^{[4
]}

Kwak, Byunggil ^{[4
]}

机构：

[1] Infineon Technol Korea, Ind Inf Consum Comp & Comm, Seoul, South Korea

[2] Hanwha Syst, Power Control Team, Yongin, South Korea

[3] Infineon Technol Germany, Green Ind Power, Tech Marketing, Warstein, Germany

[4] Hanwha Aerosp Co Ltd, E Propuls Biz Grp, Seongnam, South Korea

来源：

2024 IEEE TRANSPORTATION ELECTRIFICATION CONFERENCE AND EXPO, ITEC 2024 | 2024年

关键词：

Distributed electric propulsion (DEP); SiC MOSFET; Virtual flight profile; Power redundancy;

D O I：

10.1109/ITEC60657.2024.10599039

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

This paper discusses a distributed electric propulsion (DEP) system for virtual aviation systems. The DEP system includes six propulsion inverters with SiC MOSFET modules. Through three different virtual flight profiles normal planed one, another with changed trajectory, and the other with changed trajectory and failure mode power and current sharing between these modules was investigated. Measurement-based loss simulations and thermal simulations, with defined cooling conditions, were performed to test power redundancy and loss in each propulsion inverter for all the three virtual profiles.

引用

页数：6

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