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REDUNDANCY TECHNOLOGY FOR AIRCRAFT MULTI-CHANNEL DC POWER SUPPLY SYSTEM 被引量:2
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作者 杨善水 魏秦华 +2 位作者 黄仙密 居蓉蓉 王莉 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2007年第4期305-309,共5页
The redundancy technology for the aircraft multi-channel DC electrical power supply system is studied. In this system, the key loads can obtain power from seven sources. The direct current bus power control unit (DC ... The redundancy technology for the aircraft multi-channel DC electrical power supply system is studied. In this system, the key loads can obtain power from seven sources. The direct current bus power control unit (DC BPCU) is put forward to manage the power supply system automatically. The redundancy innovation is also applied in both hardware and software of DC BPCU. Furthermore, redundancy fault diagnosis is discussed through the existing parts. Experiments and applications show that the proposed aircraft DC power supply system possesses many advantages of high reliability, high automation and so on. 展开更多
关键词 redundant power supply bus power control unit(BPCU) redundancy hardware redundancy software
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