An aircraft propulsion system comprises a vertical lift propulsor (22) mounted within a wing (13) of the aircraft (10). The vertical propulsor (22) comprises an electric motor (30) comprising a rotor (28) mounted to a plurality of propulsor blades (24), the motor (30) further comprising a stator (32). The rotor (28) is provided radially outwardly of the stator.


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    Title :

    AIRCRAFT PROPULSION SYSTEM


    Additional title:

    FLUGZEUGANTRIEBSSYSTEM
    SYSTÈME DE PROPULSION D'AVION


    Contributors:

    Publication date :

    2022-06-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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