An electrical power system for an aircraft includes a DC:AC power electronics converter and a transverse flux electrical machine. The transverse flux electrical machine includes a rotor that is coupleable to a rotating shaft of a propulsor of the aircraft, wherein the rotor includes a plurality of permanent magnets defining a number, NP, of evenly distributed rotor poles. The transverse flux electrical machine further includes a stator arranged to interact with the rotor, such that a torque is produced. The stator includes a plurality of coils.


    Access

    Download


    Export, share and cite



    Title :

    Electrical machines for aircraft power and propulsion systems


    Contributors:

    Publication date :

    2023-11-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    ELECTRICAL MACHINES FOR AIRCRAFT POWER AND PROPULSION SYSTEMS

    CHONG ELLIS F H / REEH ANDREAS / BAUER JOHANNES GABRIEL et al. | European Patent Office | 2024

    Free access

    Electrical machines for aircraft power and propulsion systems

    ELLIS F H CHONG / ANDREAS REEH / JOHANNES GABRIEL BAUER et al. | European Patent Office | 2024

    Free access

    Electrical machines for aircraft power and propulsion systems

    CHONG ELLIS F H / REEH ANDREAS / BAUER JOHANNES GABRIEL et al. | European Patent Office | 2025

    Free access

    Electrical machines for aircraft power and propulsion systems

    ELLIS F H CHONG / ANDREAS REEH / JOHANNES GABRIEL BAUER et al. | European Patent Office | 2024

    Free access

    Electrical machines for aircraft power and propulsion systems

    CHONG ELLIS F H / REEH ANDREAS / BAUER JOHANNES GABRIEL et al. | European Patent Office | 2023

    Free access