This paper describes a high-speed electrical machine for an aircraft starter-generator. A surface mounted permanent magnet machine is designed to have minimal rotor losses and a novel cooling system for the stator. An inner stator sleeve is adopted to allow for a flooded stator whilst minimizing rotor windage losses. Different slot-pole combinations are compared in view of attaining an optimal combination that provides minimum losses whilst satisfying the electromagnetic, mechanical and thermal constraints.


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    Titel :

    Permanent Magnet Starter-Generator for Aircraft Application


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    La Rocca, Antonino (Autor:in) / Gerada, Chris (Autor:in) / Zhang, He (Autor:in) / Arumugam, Puvan (Autor:in) / Bozhko, Serhiy (Autor:in) / Pickering, Stephen (Autor:in) / Fernando, Weeramundage (Autor:in)

    Kongress:

    SAE 2014 Aerospace Systems and Technology Conference ; 2014



    Erscheinungsdatum :

    16.09.2014




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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