A technique is directed to operating an unmanned aerial vehicle (UAV) having a fuselage defining a flight direction of the UAV and wing-plate assemblies that propel the UAV in the flight direction defined by the fuselage. The technique involves providing, while the flight direction defined by fuselage of the UAV points vertically from a takeoff location on the ground, thrust from propulsion units of the wing-plate assemblies to fly the UAV along a vertical takeoff path. The technique further involves maneuvering, after the UAV flies along the vertical takeoff path, the UAV to align the flight direction along a horizontal flight path that is perpendicular to the vertical takeoff path. The technique further involves providing, after the UAV flies along the horizontal flight path, thrust from the propulsion units of the wing-plate assemblies to land the UAV along a vertical landing path that is perpendicular to the horizontal flight path.


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    Title :

    UAV WITH WING-PLATE ASSEMBLIES PROVIDING EFFICIENT VERTICAL TAKEOFF AND LANDING CAPABILITY


    Additional title:

    UNBEMANNTES LUFTFAHRZEUG MIT FLÜGELPLATTENANORDNUNGEN ZUM EFFIZIENTEN VERTIKALEN STARTEN UND LANDEN
    AÉRONEF SANS PILOTE DOTÉ D'ASSEMBLAGES DE PLAQUES D'AILE QUI ASSURENT UNE CAPACITÉ À DÉCOLLAGE ET D'ATTERRISSAGE VERTICAUX EFFICACES


    Contributors:

    Publication date :

    2020-08-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge







    AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING CAPABILITY

    SAUER SEBASTIAN / KURZ CARLO / ZLATKOV BRANISLAV et al. | European Patent Office | 2022

    Free access