Impact of Converter Interface Type on the Protection Requirements for DC Aircraft Power Systems
AC/DC Converter with DC Fault Suppression for Aircraft +/− 270 VDC Distribution Systems
Evaluation of Paralleled Generation Architectures for Civil Aircraft Applications
Failure Analysis of a Turboelectric Distributed Propulsion Aircraft Electrical Network: A Case Study
AC/DC Converter with DC Fault Suppression for Aircraft ± 270 VDC Distribution Systems
Evaluation of Paralleled Generation Architectures for Civil Aircraft Applications
Failure Analysis of a Turboelectric Distributed Propulsion Aircraft Electrical Network: A Case Study