An aircraft provided with a rotor that is provided with blades and a set of swashplates. The set of swashplates comprises both a rotary swashplate and also a non-rotary swashplate, a lower scissors linkage being hinged to the non-rotary swashplate and being hinged to a member that is stationary in rotation about the axis of rotation, the rotor comprising a plurality of servo-controls each provided with a top hinge hinged to a top attachment fitting of the non-rotary swashplate and with a bottom hinge hinged to a bottom attachment fitting that is stationary in a reference frame of the aircraft. For at least one servo-control referred to as the “inclined servo-control”, the bottom hinge is offset in azimuth about the axis of rotation relative to the top hinge.


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    Title :

    AÉRONEF MUNI D'UN ENSEMBLE DE PLATEAUX CYCLIQUES ET D'AU MOINS UNE SERVOCOMMANDE INCLINÉE


    Additional title:

    AN AIRCRAFT PROVIDED WITH A SWASHPLATE ARRANGEMENT AND WITH AT LEAST ONE SERVO-CONTROL THAT IS INCLINED
    LUFTFAHRZEUG, DAS MIT EINER TAUMELSCHEIBENANORDNUNG UND MINDESTENS EINEM GENEIGTEN SERVOANTRIEB AUSGESTATTET IST


    Contributors:

    Publication date :

    2019-01-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge





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