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


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    Title :

    Pitch control device for a ducted tail rotor of a rotorcraft


    Contributors:

    Publication date :

    2020-05-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT

    European Patent Office | 2019

    Free access

    PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT

    VOGL JULIUS / KUNTZE-FECHNER GERALD / OTTO VICTORIA | European Patent Office | 2019

    Free access

    PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT

    VOGL JULIUS / KUNTZE-FECHNER GERALD / OTTO VICTORIA | European Patent Office | 2018

    Free access

    PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT

    GERALD KUNTZE FECHNER / JULIUS VOGL / VICTORIA OTTO | European Patent Office | 2018

    Free access

    PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT

    VOGL JULIUS / KUNTZE-FECHNER GERALD / OTTO VICTORIA | European Patent Office | 2019

    Free access