Design Optimization of Switched Reluctance Motor for Aerospace Application

被引：0
|
作者：
Castellini, Luca [1 ]
Lucidi, Stefano [2 ]
Villani, Marco [3 ]
机构：
[1] Umbra Cuscinetti SpA, I-06034 Foligno, Italy
[2] Sapienza Univ Rome, Dept Comp Control & Management Engn, I-00185 Rome, Italy
[3] Univ Aquila, Dept Elect & Informat Engn, I-67040 Laquila, Italy
来源：
2015 IEEE INTERNATIONAL ELECTRIC MACHINES & DRIVES CONFERENCE (IEMDC) | 2015年
关键词：
Aerospace; actuator; electric aircraft; electric motor; design optimization; fault-tolerant; finite element analysis; multi-phase; switched-reluctance; GLOBAL OPTIMIZATION; INDUCTION-MOTORS;
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：
The switched reluctance motor, due to the high MTBF, mates properly the aerospace reliability requirements. In normal operation the electric machine operates in healthy mode but it is designed to satisfy the load specifications also with one or two faulty phases. This paper presents a design optimization for a five-phase switched reluctance motor developed to satisfy the requirements of flap actuators in medium size aircrafts. The design issues are described at the beginning in order to introduce the problem, than the optimization procedure is described. A new Controlled Random Search (CRS) algorithm is used for minimizing the optimization function. The detailed finite-element analysis validates the better performance of the optimized solution. Experimental tests on the motor prototype are included.
引用
收藏
页码：1678 / 1682
页数：5
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