航空推进电源系统研究综述  

Review of Research on Power Systems for Aerospace Propulsion

作　　者：齐扬 李伟林[1] 吴宇[2] 赵宏卫 祝文涛 何林珂 QI Yang;LI Weilin;WU Yu;ZHAO Hongwei;ZHU Wentao;HE Linke(School of Automation,Northwestern Polytechnical University,Xi’an 710072,China;School of Civil Aviation,Northwestern Polytechnical University,Xi’an 710072,China)

机构地区：[1]西北工业大学自动化学院,西安710072 [2]西北工业大学民航学院,西安710072

出　　处：《电源学报》2022年第5期51-59,共9页Journal of Power Supply

基　　金：国家自然科学基金资助项目(52272403)。

摘　　要：随着电力电子技术的进步和航空产业绿色发展的需求,以电能作为主体推进动力的航空飞行器受到了广泛关注,特别是航空推进电源系统的设计对于优化飞机结构、减少碳排放和提高飞机可靠性具有重要意义。同时,多电/全电背景下的飞机电源系统在转换效率、功重比和能量综合管理等方面也面临着新的问题与挑战。围绕电推进飞机的关键技术,对航空推进电源系统的能源体系架构、电力电子变换器拓扑结构、协同控制方法和能量管理等方面进行了研究现状的梳理。在此基础上,归纳和展望了飞机电推进系统,包括宽禁带半导体器件、大功率脉冲性负载以及分布式电推进等方面的未来研究趋势。With the advance of the power electronics technology and the demand of carbon-free airline industry, the electric propulsion aircraft which utilizes electricity as its main driving force has gained much attention. In particular,the design of power systems for aerospace propulsion is crucial for the optimization of aircraft architecture, carbon reduction, and the improvement of aircraft reliability. Meanwhile, the power systems for more/all electric aircraft also face new problems and challenges, such as power conversion efficiency, power-to-weight ratio, and comprehensive energy management. The key technologies for electric propulsion aircraft are focused. Specifically, the state-of-the-art research works on the energy system architectures of aerospace propulsion power system, topologies of power electronics converters, coordinated control methods, and energy management are reviewed. On this basis, the future research trends including wide-band-gap semiconductor devices, high-power impulsive load, and distributed electric propulsion are also summarized and forecasted.

关 键 词：多电飞机 电推进系统 电能转化 电力电子变换器 协同控制 能量管理 

分 类 号：TM92[电气工程—电力电子与电力传动]