The invention is related to a rotor assembly 1 for a rotorcraft, comprising a rotor shaft 8, a torque transmission unit 4 that is non-rotatably mounted to the rotor shaft, a rotor hub 7 that is rotatably mounted to the rotor shaft 8 via an associated angular displacement enabling component 9, and at least two rotor blades 2b, 2d that are connected to the rotor hub 7, wherein the torque transmission unit 4 is coupled to the at least two rotor blades on a rotor assembly outflow side via a pitch control unit 10, wherein the pitch control unit transmits to the at least two rotor blades 2b, 2d torque that is applied from the rotor shaft 8 to the torque transmission unit 4, and wherein the pitch control unit 10 increases a respective pitch angle of the at least two rotor blades 2b, 2d if the torque is increased.


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    Titel :

    A ROTOR ASSEMBLY FOR A ROTORCRAFT WITH TORQUE CONTROLLED COLLECTIVE PITCH


    Weitere Titelangaben:

    ROTORANORDNUNG FÜR EIN ROTORFLUGZEUG MIT DREHMOMENTGESTEUERTER KOLLEKTIVER STEIGUNG
    ENSEMBLE ROTOR POUR UN GIRAVION COMPORTANT UN PAS COLLECTIF CONTRÔLÉ PAR UN COUPLE


    Beteiligte:
    BUESING MORITZ (Autor:in)

    Erscheinungsdatum :

    27.11.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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