Conducted EMI Modeling and Evaluation of Si and SiC devices on Aerospace Machine

Will Perdikakis, M. Scott, K. Yost, Chad Miller, J. Scofield
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引用次数: 0

Abstract

Aerospace applications demand power electronics with high power density and high reliability. Many strategies exist to improve power density and researchers are examining new power devices as a tool to achieve this goal. Commercially available silicon carbide (SiC) power devices have Figures of Merit significantly higher than silicon (Si) components. Their smaller on-resistances facilitate lower conduction losses, and their small parasitic capacitances result in reduced switching loss and increased transient switching speed. These advantages, when applied strategically, can increase power density. The reliability of SiC power devices has also improved during the last decade, but questions remain about conducted and radiated emissions that result from SiC-based hardware due to their high switching speed. This research models the conducted electromagnetic interference (EMI) of a three-phase inverter and electric machine. Experimental results confirm the validity of the model under DO-160.
对航天机械上的硅和碳化硅器件进行了电磁干扰建模和评估
航空航天应用需要具有高功率密度和高可靠性的电力电子设备。有许多策略可以提高功率密度,研究人员正在研究新的功率器件作为实现这一目标的工具。商业上可用的碳化硅(SiC)功率器件具有显著高于硅(Si)元件的性能指标。其较小的导通电阻有助于降低传导损耗,而其较小的寄生电容导致降低开关损耗和提高瞬态开关速度。如果有策略地应用这些优势,可以提高功率密度。在过去十年中,SiC功率器件的可靠性也得到了改善,但由于其高开关速度,SiC基硬件导致的传导和辐射发射仍然存在问题。本文研究了三相逆变器和电机的传导电磁干扰(EMI)模型。实验结果证实了该模型在DO-160下的有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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