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.
AÉRONEF MUNI D'UN ENSEMBLE DE PLATEAUX CYCLIQUES ET D'AU MOINS UNE SERVOCOMMANDE INCLINÉE
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
2019-01-02
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
AERONEF MUNI D'UN ENSEMBLE DE PLATEAUX CYCLIQUE ET D'AU MOINS UNE SERVOCOMMANDE INCLINEE
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