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

S. V. Luft, A. A. Khristolyubov
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Abstract

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.
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飞机整流装置全桥移相变换器设计
除电能转换质量外,对飞机变流器的基本要求是尽量减轻设备重量,减小设备占用的体积。特别是软交换拓扑可以解决这些问题。介绍了飞机可控整流装置软开关DC-DC变换器的设计方法。以2kw变换器的设计为例,给出了在PSIM软件中建模的结果。
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