A propulsion system for an aircraft comprises at least first and second propulsors, each propulsor being independently driven by a respective electric motor. The first and second propulsors each comprise respective rotors comprising a plurality of blades. The rotor of the first propulsor (30a) comprises a different number of blades to the rotor of the second propulsor, and the rotors of the first and second propulsors each have a blade pitch varying mechanism.


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    Titel :

    MULTI-PROPULSOR ELECTRIC AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    26.01.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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