The invention is related to a rotorcraft (1) with a fuselage (4) and at least one main rotor (2), said at least one main rotor (2) being drivable for controlling an associated pitch attitude of said rotorcraft (1) in operation, and said fuselage (4) being equipped with at least one passive wing-type aerodynamic device (6) that is adapted for generating independently of said associated pitch attitude a lift force (14a) acting on said fuselage (4), said lift force (14a) being oriented perpendicular to an air flow (12) that is directed in operation of said rotorcraft (1) against said passive wing-type aerodynamic device (6).


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    Title :

    Rotorcraft with a fuselage and at least one main rotor


    Additional title:

    Hubschrauber mit einem Rumpf und mindestens einem Hauptrotor
    Hélicoptère comprenenat un fuselage et au moins un rotor principal


    Contributors:

    Publication date :

    2019-01-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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