| 多电飞机电气系统关键技术研究 |
| |
| 引用本文： | 齐蓉,林辉,周素莹.多电飞机电气系统关键技术研究[J].航空计算技术,2004,34(1):97-101. |
| |
| 作者姓名： | 齐蓉 林辉 周素莹 |
| |
| 作者单位： | 西北工业大学,自动控制系,陕西,西安,710072 |
| |
| 摘 要： | 介绍了多电飞机电气系统关键技术的研究现状和发展趋势,阐述了电源系统结构,PSP和ELMC的结构与功能,电源系统BIT技术与容错技术以及电力作动技术等关键技术,并探讨了上述关键技术的设计方案。
|
| 关 键 词： | 多电飞机 供电处理机 电气负载管理中心 自检测与容错 电力作动 |
| 文章编号： | 1671-654X(2004)01-0097-05 |
| 修稿时间： | 2004年1月6日 |
Study on Key Techniques for Electrical System of More- Electric'Aircraft |
| |
| QI Rong,LIN Hui,ZHOU Su-ying.Study on Key Techniques for Electrical System of More- Electric''''Aircraft[J].Aeronautical Computer Technique,2004,34(1):97-101. |
| |
| Authors: | QI Rong LIN Hui ZHOU Su-ying |
| |
| Abstract: | In this paper the key techniques and developing trends for electrical power system of more electric aircraft are firstly explained. Then, it particularly introduces the key techniques of electrical power system. These key techniques include the architecture of more electric aircraft power system , the structure and function of PSP and ELMC, demand of BIT technique and fault tolerant design of electrical power system, and electrical actuation technique etc. Apart from these, it refers design scheme of these key techniques. |
| |
| Keywords: | more electric aircraft power system processor electrical load management center autotest and fault tolerant electrical actuation |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
