Full-bridge phase-shifted converter design for aircraft rectifier unit

摘要

Basic requirements for the aircraft converters besides the quality of electrical power conversion are minimizing the weight of the device and reducing the volume occupied by them. In particular, soft-switching topology are used to solve these problems. The method of soft-switching DC-DC converter design for controlled rectifier unit for aircraft is described in this paper. The design of 2 kW converter and the results of modeling in software PSIM are presented as an example.