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

共 50 条

[21] Comparison of Heat-Pipe Cooling System Design Processes in Railway Propulsion Inverter Considering Power Module Reliability
Lee, June-Seok
Choi, Ui-Min
ENERGIES, 2019, 12 (24)
[22] Design and Optimization of SiC MOSFET Wire Bondless Power Modules
Chen, Hao
Hossain, Md Maksudul
Castillo, David Gonzalez
Li, Xiaoling
Wallace, Andrea
Chen, Yuxiang
Mantooth, H. Alan
2020 IEEE 9TH INTERNATIONAL POWER ELECTRONICS AND MOTION CONTROL CONFERENCE (IPEMC2020-ECCE ASIA), 2020, : 725 - 728
[23] Accumulation-mode SiC power MOSFET design issues
Wang, Y
Weitzel, C
Bhatnagar, M
SILICON CARBIDE AND RELATED MATERIALS - 1999 PTS, 1 & 2, 2000, 338-3 : 1287 - 1290
[24] Inverter design for hybrid electrical vehicles considering mission profiles
Hirschmann, D
Tissen, D
Schröder, S
De Doncker, RW
2005 IEEE VEHICLE POWER AND PROPULSION CONFERENCE (VPPC), 2005, : 567 - 573
[25] Analysis of Inverter Loss Improvement According to Si-IGBT and SiC-MOSFET Utilization of 150kW Inverter for EV Propulsion
Hwang D.-Y.
Joo D.-M.
Gu B.-G.
Transactions of the Korean Institute of Electrical Engineers, 2024, 73 (01): : 63 - 68
[26] A POWER MOSFET DESIGN METHODOLOGY CONSIDERING EPI PARAMETER VARIATIONS
HWANG, SK
CHOI, YI
CHUNG, SK
LEE, K
KIM, CK
IEEE TRANSACTIONS ON SEMICONDUCTOR MANUFACTURING, 1993, 6 (04) : 377 - 380
[27] Design Considerations and Performance Test for SiC MOSFET Based 1000V/ 1.5MHz Pulse Power Inverter
Liu, Chunhui
Lei, Qin
2018 IEEE ENERGY CONVERSION CONGRESS AND EXPOSITION (ECCE), 2018, : 6641 - 6645
[28] A FULL SIC MOSFET DCDC BOOST POWER MODULE USING 2 KV SIC MOSFET FOR 1500V STRING SOLAR INVERTER APPLICATIONS
Liu, Yusi
2024 IEEE APPLIED POWER ELECTRONICS CONFERENCE AND EXPOSITION, APEC, 2024, : 188 - 191
[29] Power Loss Analysis in a SiC/IGBT Propulsion Inverter Including Blanking Time, MOSFET's Reverse Conduction and the Effect of Thermal Feedback Using a PMSM Model
Amirpour, Sepideh
Thiringer, Torbjorn
Hagstedt, Dan
IECON 2020: THE 46TH ANNUAL CONFERENCE OF THE IEEE INDUSTRIAL ELECTRONICS SOCIETY, 2020, : 1424 - 1430
[30] A Modelling Framework for Efficient Design of Electrical Power Systems for Electrical Propulsion Aircraft
Jones, Catherine E.
Norman, Patrick J.
Burt, Graeme M.
2021 AIAA/IEEE ELECTRIC AIRCRAFT TECHNOLOGIES SYMPOSIUM (EATS), 2021,

← 1 2 3 4 5 →