用于混合动力航空应用的碳化硅推进驱动器的开发、集成与飞行测试

This article details the design, development, and successful flight testing of an 800 V, 250 kW silicon carbide (SiC) inverter built for a hybrid-electric aircraft propulsion system. Using custom 1200 V SiC modules with pin-fin baseplates and integrated CMOS gate drivers, the inverter achieves high performance and reliability, while a direct cooling approach yields a high power density of approxim...