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基于全桥半桥切换LLC谐振变换器的霍尔电源设计
电子技术应用
徐霆豪,王少宁,刘澳慧
兰州空间技术物理研究所
摘要: 针对深空探测等空间任务电推力器高输入电压的需求,设计出一种适用于霍尔电推进系统的电源处理单元,对LLC谐振变换器对半桥全桥动态拓扑切换和软启动进行研究,实现高效率、宽范围的输出。通过建立LLC谐振变换器的基波模型,分析频率与增益的特性曲线,K值和Q值的选值,实现变频率控制输出电压,并设计基于同时变频和变占空比的低尖峰全桥半桥切换模式。同时为满足电推进所需的软启动功能,根据移相全桥软启动设计出基于改变LLC谐振变换器MOSFET移相角的分段线性的软启动模式。为了验证设计性能,设计了一款5 kW的全数字样机,输入400 V输出200 ~1 000 V,能够实现LLC谐振变换器宽范围、高效率的输出。
中图分类号:TN86 文献标志码:A DOI: 10.16157/j.issn.0258-7998.245587
中文引用格式: 徐霆豪,王少宁,刘澳慧. 基于全桥半桥切换LLC谐振变换器的霍尔电源设计[J]. 电子技术应用,2025,51(2):108-114.
英文引用格式: Xu Tinghao,Wang Shaoning,Liu Aohui. Design of Hall power supply based on full bridge half bridge switching digital LLC resonant converter[J]. Application of Electronic Technique,2025,51(2):108-114.
Design of Hall power supply based on full bridge half bridge switching digital LLC resonant converter
Xu Tinghao,Wang Shaoning,Liu Aohui
Lanzhou Institute of Space Technology Physics
Abstract: A power processing unit suitable for Hall electric propulsion systems is designed to meet the high input voltage requirements of space missions such as deep space exploration. The LLC resonant converter is studied for half bridge full bridge dynamic topology switching and soft start, achieving high efficiency and wide range output. By establishing a fundamental model of LLC resonant converter, analyzing the characteristic curves of frequency and gain, selecting the values of K and Q, variable frequency control output voltage is achieved, and a low peak full bridge half bridge switching mode based on simultaneous frequency conversion and variable duty cycle is designed. At the same time, in order to meet the soft start function required for electric propulsion, a segmented linear soft start mode based on changing the phase shift angle of LLC resonant converter MOSFET is designed according to the phase-shifting full bridge soft start. In order to verify the design performance, a 5 kW all digital prototype was designed, with an input of 400 V and an output of 200 V to 1 000 V. The results showed that it can achieve a wide range and high efficiency output of the LLC resonant converter.
Key words : power processing unit;LLC resonant converter;full bridge half bridge switching;digital control;soft start

引言

电推进技术是一种将航天器储备或收集的电能转化为动能的技术,通过将气体工质电离,并通过高压电场将离子加速喷出而产生推力。与化学推进相比,电推进具有高比冲、高精度、长寿命的特点。随着电推进技术的发展和深空探测需求的提升,电推进技术依靠着其优良的性能从仅仅用于位置保持和轨道转移开始转向深空探测主推力器的任务。

电源处理单元(Power Processing Unit,PPU)作为电推进系统的关键单机之一,它的功能不限于电源转换和调节、输出稳定电流和电压、点火控制、保护功能、监测和诊断、通信接口等。为了满足电推力器各个模块实现各个功能的供能需求,PPU的技术发展起着至关重要的作用[1]。

目前在超大功率卫星平台上,太阳能电池阵提供电推进系统的输入电压一般为60~120 V,但未来应用在深空探测电推进主推力器的输入电压将会提升至400 V[2],这要求采用高压DC-DC转换技术,因此本文设计了基于全桥半桥切换LLC谐振变换器的电源处理单元以确保能够高效地将输入电压转换为电推进系统所需的各级电压。


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作者信息:

徐霆豪,王少宁,刘澳慧

(兰州空间技术物理研究所,甘肃 兰州 730000)


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