Multi-operating points PM Motor Design Methodology for Electric Actuation systems

被引:0
|
作者
Sarigiannidis, A. G. [1 ]
Beniakar, M. E. [1 ]
Kakosimos, P. E. [1 ]
Kladas, A. G. [1 ]
机构
[1] Natl Tech Univ Athens, Dept Elect & Comp Engn, Lab Elect Machines & Power Elect, Zogyafou Athens 15780, Greece
关键词
Actuators; aerospace engineering; fault tolerance; finite element method; machine design; particle swarm optimization; permanent magnet motors; redundancy; AEROSPACE APPLICATIONS; OPTIMIZATION;
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
In this paper, a comparative optimal design of Permanent Magnet Motors (PMMs) for aerospace actuation applications based on single and double layer Fractional Slot Concentrated Winding (FSCW) topologies with different motor segmentation strategies is undertaken, by means of a combined electromagnetic, fault tolerance and thermal evaluation. Initially, analytical machine equations and 2D Finite Element (FE) analysis are employed for the determination of the motors basic dimensional and operating characteristics. Both configurations considered are in a next step optimized regarding the mean torque, efficiency, torque ripple, induced Electromotive Force (EMF) quality and motor weight. The proposed methodology involves appropriate handling of mean torque and induced EMF as constraints through the application of a particular single-objective Particle Swarm Optimization (PSO) technique accounting also for multiple motor operating conditions. Fault tolerance and thermal robustness of the optimized motors are also examined. Both single layer and double layer FSCW PMM optimal configurations present complementary advantages for this class of applications.
引用
收藏
页码:2506 / 2512
页数:7
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