• 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