An aerodyne comprises a fuselage, a fixed wing , a thruster for cruising flight, and a rotary wing for stages of vertical flight and held stationary during cruising flight. The rotary wing includes at least two contrarotating single-blades disposed at the top of the fuselage and hinged about respective axes perpendicular to the rotor axes of rotation. A maneuvering procedure for maneuvering the aerodyne includes a transition stage between a stage of vertical flight and a stage of cruising flight, wherein in the transition stage, when the speed of each single-blade is less than a threshold speed of rotation, the pitch of each single-blade is such that it no longer provides any lift force and the transverse hinge of the single-blade to its rotor axis is held locked in a position such that the single-blade is perpendicular to the rotor shaft.


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    Titel :

    VEHICULE AERIEN COMPRENANT AU MOINS DEUX VOILURES TOURNANTES ALIGNEES SELON SON AXE DE ROULIS


    Weitere Titelangaben:

    AERIAL VEHICLE COMPRISING AT LEAST TWO ROTARY WINGS ALIGNED ALONG ITS ROLL AXIS
    LUFTFAHRZEUG MIT MINDESTENS ZWEI ENTLANG SEINER WALZENACHSE AUSGERICHTETEN DREHFLÜGELN


    Beteiligte:

    Erscheinungsdatum :

    20.01.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    VEHICULE AERIEN COMPRENANT AU MOINS DEUX VOILURES TOURNANTES ALIGNEES SELON SON AXE DE ROULIS

    SIMON JEAN-MICHEL | Europäisches Patentamt | 2019

    Freier Zugriff




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    Lacaine, J. | Engineering Index Backfile | 1932