航空发动机多电控制系统源-网-荷架构与关键技术

doi:10.7527/S1000-6893.2024.30689

Abstract

Abstract:

The aero-engine， with the multi-electric technology as its new feature， optimizes the system’s multiple energy 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 including high-power pumps and actuators together constitute a complex multi-electric control system. This system is characterized by multi-nodes and superposition of dynamic and static changes， and is facing the challenges in different application environments. Based on the electrification foundation， this paper firstly classifies the source-grid-load architecture of the aero-engine multi-electrical control system， and elaborates on the basic concepts， compositional characteristics， and challenges of the source， grid， and load systems. Then， the source-grid-load integrated system is analyzed， 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 electromagnetic compatibility modeling analysis and suppression methods， is comprehensively analyzed. Finally， the development 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.

Key words: multi-electric technology, electrification, more-electric control system, source-grid-load, motor, drive control, multi-node microgrid, electromagnetic compatibility

CLC Number:

Wubin KONG, Di LIU, Xinggang FAN, Xuejun PEI, Shengqiao HAO, Ying CUI, Qianrong MA, Dawei LI, Haiyang FANG, Jue YU, Yi CHENG, Wenjuan CHEN, Feiteng LUO. Source-grid-load architecture and key technologies of aero-engine multi-electrical control system[J]. Acta Aeronautica et Astronautica Sinica, 2025, 46(2): 30689.

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用电系统	电压等级	用电功率/kW
环控增压系统	270 VDC	320
液压系统	270 VDC	40
冷却装置	270 VDC	40
环控风扇	270 VDC	32
防冰系统	230 VAC	60
厨房	230 VAC	120
燃油泵	230 VAC	32
前货舱	230 VAC	60
综合通讯系统ICS	115 VAC	40
各种交流负载	115 VAC	140
飞控系统	28 VDC	14
各种直流负载	28 VDC	20

电机类型	研究单位/公司	功率/kW	功率密度/（kW·kg^-1）	冷却方式	效率/%
EMRAX 348	EMRAX	210	5.1	风冷水冷	95
SP260-DA	Siemens	260	5.9	油冷	95
Magni 650-EPU	Magnix	560	2.8
Air cooled PM	Illinois Univ.	1 000	13		96
HEMM	NASA	1 400	16		96
SP2000D	Siemens	2 000	7.7	水冷
IM	Ohio Unv.	2 700	13		96

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Source-grid-load architecture and key technologies of aero-engine multi-electrical control system

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子系统	电机驱动数量	最大功率/kW	总功率/kW
飞控系统	28	50	80
环控系统	10	10	40
滑行系统	20	5	30
气动系统	2	15	30
起动发电机	6	125	125/通道
燃油泵	10	9	35
其他	10	1	20