A transverse flux electrical machine for coupling to a rotating shaft of a propulsor of an aircraft is provided. The transverse flux electrical machine includes a rotor having a plurality of circumferentially distributed permanent magnets that form a number, NP, of rotor poles, wherein the rotor poles have a pole pitch angle, Pθ, equal to 2π divided by the number of rotor poles, NP. The transverse flux electrical machine further includes a stator having a plurality of current-carrying coils configured to interact with the rotor poles of the rotor to produce a torque. The transverse flux electrical machine further includes an air gap separating the rotor from the stator by an air gap distance, GAir, wherein a machine parameter, Υ, defined as: Υ=Pθ×GAir is less than 100 micro radian-meters.


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    Titel :

    ELECTRICAL MACHINES FOR AIRCRAFT POWER AND PROPULSION SYSTEMS


    Beteiligte:
    CHONG ELLIS F H (Autor:in) / REEH ANDREAS (Autor:in) / BAUER JOHANNES GABRIEL (Autor:in) / RUDENKO ANTON (Autor:in)

    Erscheinungsdatum :

    2024-07-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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