DocumentCode
2916595
Title
Shape optimization of switched reluctance machine for aerospace applications
Author
Naayagi, R.T. ; Kamaraj, V.
Author_Institution
Dept. of Electr. & Electron. Eng., Sri Venkateswara Coll. of Eng., Sriperumbudur, India
fYear
2005
fDate
6-10 Nov. 2005
Abstract
This paper describes the shape optimization of switched reluctance machine (SRM) using genetic algorithm (GA). To achieve the required performance within a specified space envelope, the physical dimensions of the switched reluctance machine like stator pole arc, rotor pole arc, rotor diameter and stack length were optimized using GA. The proposed strategy improves the power density by 13.97% using GA. The maximum torque throughput is enhanced by 12.1%. The proposed design, in comparison with the standard design, highlights improvement in performance with considerable reduction in size. This method maximizes flux linkage and torque per unit rotor volume of the SRM. In this paper, the design specifications are suited for 25 hp, 24/18 pole, 4 phase SRM. The simulation results obtained from the given specifications, demonstrate the efficacy of the proposed strategy.
Keywords
aerospace engineering; genetic algorithms; reluctance machines; rotors; stators; torque; 25 hp; 4 phase SRM; GA; aerospace application; flux linkage; genetic algorithm; power density; rotor pole arc; shape optimization; stator pole arc; switched reluctance machine; torque; Aerospace engineering; Circuit faults; Costs; Evolutionary computation; Genetic engineering; Reluctance machines; Reluctance motors; Shape; Stators; Temperature;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics Society, 2005. IECON 2005. 31st Annual Conference of IEEE
Print_ISBN
0-7803-9252-3
Type
conf
DOI
10.1109/IECON.2005.1569169
Filename
1569169
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