LLC拓扑在飞机上大功率高升压应用中的局限性及解决方案

IF 0.2 Q4 AREA STUDIES
Shuangyi Zhong, Xin Zhao, Xuanlyu Wu, Xiliang Chen, Bei Wang, Xiaohua Wu
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引用次数: 0

摘要

在现代飞机中,对于从28V到270V甚至更高电压的大功率高升压(HPHS) DC-DC转换有巨大的需求,例如启动电源单元(SPU)和备用电源系统。由于高效率、高功率密度、低电磁干扰和软开关能力,LLC谐振拓扑受到特别关注。然而,在HPHS应用中,原有的LLC谐振拓扑会遇到一定的限制,导致参数可控性差,功率密度低,效率低。本文首先分析了造成这些局限的根本原因。然后,分别从电路拓扑和系统架构两方面给出了解决方案。设计、制造和测试了一台5kW 2SV/222V样机。验证了所提出解决方案的可行性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Limitations and Solutions of LLC Topology in High Power High Step-up Applications on Aircraft
In modern aircraft, there is a huge demand for high power high step-up (HPHS) DC-DC conversion from 28V to 270V or even higher voltage, such as Start Power Unit (SPU) and backup power supply systems. Due to high efficiency, high power density, low EMI, and soft-switching capability, LLC resonant topology are receiving special attention. However, when it comes to HPHS applications, original LLC resonant topology will encounter some limitations, resulting poor parameter controllability, low power density and low efficiency. This paper first analyzed the fundamental causes of these limitations. Then, solutions are given in terms of circuit topology and system architecture, respectively. A 5kW 2SV/222V prototype was designed, fabricated and tested. The feasibility of proposed solutions is validated.
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CiteScore
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