A lift rotor or ‘thrust’ system or assembly for a VTOL aircraft, comprising first and second lifting thrusters or rotors contained within a housing, the housing containing a leading edge, a trailing edge, a upper surface and a lower surface; wherein the housing includes one or more airflow manipulation devices provided on or associated with the housing configured to manage the airflow into or through at least one of the first and second rotors. In other aspects, the invention embraces an aircraft wing including a lift thruster system as defined above, and also an aircraft comprising such a lift thruster system.


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    Titel :

    VERTICAL TAKE-OFF AND LANDING AIRCRAFT


    Weitere Titelangaben:

    VERTIKAL STARTENDES UND LANDENDES FLUGZEUG
    AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX


    Beteiligte:
    MORGAN BRIAN (Autor:in)

    Erscheinungsdatum :

    2019-09-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge