Abstract:This paper demonstrates a topology-device selection and multi-objective optimization tool for a 350 V dc, 27 kVA aircraft inverter system. The design space is generated with the topology-device combination as the primary variable and the switching frequency as the secondary variable, which considers two-level vs. three-level topologies and Silicon (Si) vs. Silicon Carbide (SiC) devices. The proposed optimization tool conducts automated design of each component and estimation of their performances regarding pow… Show more
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