Static Modeling and Power Flow of the More Electric Aircraft Power System

被引：0
|
作者：
Xu, Ke-lu [1 ]
Xie, Ning [1 ]
Wang, Cheng-min [1 ]
Deng, Jia-wei [1 ]
Shi, Xu-dong [2 ]
机构：
[1] Shanghai Jiao Tong Univ, Sch Elect Informat & Elect Engn, Shanghai, Peoples R China
[2] Civil Aviat Univ China, Aeronaut Automat Sch, Tianjin, Peoples R China
来源：
2016 3RD INTERNATIONAL CONFERENCE ON SYSTEMS AND INFORMATICS (ICSAI) | 2016年
基金：
中国国家自然科学基金;
关键词：
MEA; power system; static modeling; power flow; steady-state analysis;
D O I：
暂无
中图分类号：
TM [电工技术]; TN [电子技术、通信技术];
学科分类号：
0808 ; 0809 ;
摘要：
This paper proposes a static modeling and power flow calculation of the More Electric Aircraft (MEA) power system to study the stability and the fault analysis. Combined with the common land power system, the structure and characteristics of MEA power system are firstly illustrated and the static models are built. Then, on the basis of the alternate iteration method, the method to calculate and analysis the AC/DC hybrid MEA power system is described. Finally, the power flow calculation results and adjust strategy under different working period are showed with an example of Boeing 787. The simulation results showed that the programmed algorithm can accord with the characteristics of MEA power system and the power flow distribution and adjustment strategy are simple and clear.
引用
收藏
页码：193 / 198
页数：6
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