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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    Titel :

    Aircraft propulsion system


    Erscheinungsdatum :

    2018-10-17


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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