适合更多电动飞机的高频转换器拓扑结构

A. Dannier, G. Brando, I. Spina, A. Raciti, S. Rizzo, G. Susinni
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引用次数: 1

摘要

在过去的几年里,航空航天业在发展机载电气化方面付出了越来越大的努力。在向未来飞机过渡的过程中出现的困难,首先涉及到飞机应用需要遵守的所有限制(可靠性、小尺寸、减少维护时间等)。本文对满足机载应用要求的功率器件和合适的变换器拓扑结构进行了分析和讨论,特别是对其可靠性和性能匹配问题进行了研究。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
High frequency converter topologies suitable for more electric aircraft
In the last years the aerospace industry has put a growing effort to develop on-board electrification. The difficulties, which have emerged to implement the transition to the future aircraft, concern above all the constraints to be respected for aircraft applications (reliability, small size, reduced maintenance time, etc.). The present paper proposes to analyze and discuss the power devices and suitable converter topologies that bring the requirements of the airborne applications, especially devoted to match with the reliability and performance issues.
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