航空学报2025，Vol.46Issue(2)：1-39,39.DOI:10.7527/S1000-6893.2024.30689
航空发动机多电控制系统源-网-荷架构与关键技术
Source-grid-load architecture and key technologies of aero-engine multi-electrical control system
摘要
Abstract
The aero-engine,with the multi-electric technology as its new feature,optimizes the system's multiple en-ergy architectures and significantly improves system maintainability and reliability,which is now a core component of the multi-electric aero-engine research field.As the power generation system jumps from the hundred kW level to the MW level,the high-power,highly integrated multi-node power distribution system and the power-using system includ-ing high-power pumps and actuators together constitute a complex multi-electric control system.This system is charac-terized by multi-nodes and superposition of dynamic and static changes,and is facing the challenges in different appli-cation environments.Based on the electrification foundation,this paper firstly classifies the source-grid-load architec-ture of the aero-engine multi-electrical control system,and elaborates on the basic concepts,compositional character-istics,and challenges of the source,grid,and load systems.Then,the source-grid-load integrated system is ana-lyzed,and the research status of four key technologies,the lightweight and high-reliable motor technology,power conversion topology and motor drive control,multi-node microgrid networking and control research,and electromag-netic compatibility modeling analysis and suppression methods,is comprehensively analyzed.Finally,the develop-ment trend of source-grid-load system and the layout of multi-position architecture are summarized and the prospects are discussed to promote the development of aero-engine multi-electrical control system.关键词
多电技术/电气化/多电控制系统/源-网-荷/电机/驱动控制/多节点微电网/电磁兼容Key words
multi-electric technology/electrification/more-electric control system/source-grid-load/motor/drive control/multi-node microgrid/electromagnetic compatibility分类
航空航天引用本文复制引用
孔武斌,俞珏,程颐,陈文娟,罗飞腾,刘迪,范兴纲,裴雪军,郝圣桥,崔颖,马前容,李大伟,方海洋..航空发动机多电控制系统源-网-荷架构与关键技术[J].航空学报,2025,46(2):1-39,39.基金项目
国家自然科学基金(52377050) National Natural Science Foundation of China(52377050) （52377050）
