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   Potentials to Improve the Post-Fault Performance of a Fault-Tolerant Inverter System in Electrified Aircraft Propulsion System   [View] 
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 Author(s)   Yongtao CAO 
 Abstract   Due to the increased exposure to cosmic radiation at higher flight altitude, a significant voltage derating of power semiconductors is required to reduce the failure rate of the inverters designed for electrified aircraft propulsion systems. By utilizing the necessary oversized block-voltage capability of the power semiconductors while employing the concept of variable DC-link voltage, post-fault performance of the inverter system can be improved. 
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Filename:0275-epe2022-full-17512433.pdf
Filesize:616.2 KB
 Type   Members Only 
 Date   Last modified 2023-09-24 by System