Design of High Current, High Power Density GaN Based Motor Drive for All Electric Aircraft Application

W. Khan, Armin Ebrahimian, S. I. Hosseini S., N. Weise
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Abstract

The past decade has seen noticeable advancements in the miniaturization of wide-band gap semiconductor technology making it feasible to be applied in demanding applications such as more-electric-aircrafts (MEA). Multiple high speed electric motors operating in parallel with current ratings in hundreds of amps are required to match the power delivery capability of conventional jet engines. As a result, the power electronics driving the motors require special attention to parallel multiple active switches in order to meet the high current requirements. This paper presents the design of an axially stator mounted 250 kW integrated modular motor drive for MEA applications. The design considerations presented include optimal component placement and layer stackup to minimize voltage overshoots during switch commutation, optimal gate drive layout to synchronize the current sharing of multiple GaN active switches, and the selection process of the on-board current sensor. Lastly, experimental test results are presented that verify the efficacy of the proposed design.
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全电动飞机用大电流、高功率密度氮化镓电机驱动设计
在过去的十年中,宽带隙半导体技术在小型化方面取得了显著的进步,使其能够应用于要求苛刻的应用,如更电动的飞机(MEA)。需要多个高速电动机并联运行,额定电流为数百安培,以匹配传统喷气发动机的动力输送能力。因此,驱动电机的电力电子设备需要特别注意并联多个有源开关,以满足高电流要求。本文介绍了一种用于MEA应用的250kw轴向定子集成模块化电机驱动器的设计。提出的设计考虑包括优化组件放置和层堆叠,以最大限度地减少开关换相期间的电压过调,优化栅极驱动布局,以同步多个GaN有源开关的电流共享,以及板载电流传感器的选择过程。最后,给出了实验测试结果,验证了所提设计的有效性。
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