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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    Title :

    Permanent Magnet Starter-Generator for Aircraft Application


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE 2014 Aerospace Systems and Technology Conference ; 2014



    Publication date :

    2014-09-16




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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