The invention is related to a pitch control device (14) for a ducted tail rotor of a rotorcraft. The pitch control device (14) comprises a control input member (16) with a disc-shaped central component (16a) and at least two connecting arms (16b) that extend radially from the disc-shaped central component (16a), wherein the disc-shaped central component (16a) is provided for being mounted to an associated pitch control shaft of the ducted tail rotor, and a control transfer member (15) with a ring-shaped connector (15a) and at leas two push rods (15b) that extend axially from the ring-shaped connector (15a), wherein each one of the at least two push rods (15b) is provided for being coupled to an associated pitch lever of a rotor blade of the ducted tail rotor.


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    Titel :

    PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT


    Weitere Titelangaben:

    ANSTELLWINKELSTEUERUNGSVORRICHTUNG FÜR EINEN HECKROTOR EINES DREHFLÜGLERS
    DISPOSITIF DE COMMANDE DE PAS POUR UN FENESTRON D'UN GIRAVION


    Beteiligte:
    VOGL JULIUS (Autor:in) / KUNTZE-FECHNER GERALD (Autor:in) / OTTO VICTORIA (Autor:in)

    Erscheinungsdatum :

    17.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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