Comparative Investigation of SiC Current Source Converter and Matrix Converter Topologies for Medium-Voltage Electric Aircraft Propulsion

被引：0
作者：
Luckett, Benjamin [1 ]
He, JiangBiao [1 ]
机构：
[1] Univ Kentucky, Dept Elect & Comp Engn, Lexington, KY 40506 USA
来源：
2021 IEEE TRANSPORTATION ELECTRIFICATION CONFERENCE & EXPO (ITEC) | 2021年
关键词：
INVERTER; DESIGN;
D O I：
10.1109/ITEC51675.2021.9490080
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：
Medium-voltage electric propulsion is a promising technology to enable the electrification of aircraft, especially for twin-aisle aircraft. The performance of the medium-voltage power converter plays a critical role in the overall electric propulsion performance. To pursue higher efficiency, reliability, and power density, this paper investigates the comparison of the current source converter, direct and indirect matrix converters, with respect to a multilevel voltage source converter. The emerging Silicon Carbide (SIC) MOSFET modules are used to configure the power converters to achieve higher efficiency and power density. All these converters are modeled and simulated for a megawatt-scale propulsion drive system rated at medium voltage. Simulation results are presented and analyzed to provide a reference for the future aircraft propulsion designs.
引用
收藏
页码：641 / 646
页数：6
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