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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    Titel :

    Pitch control device for a ducted tail rotor of a rotorcraft


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

    Erscheinungsdatum :

    19.05.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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    Europäisches Patentamt | 2019

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    PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT

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    PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT

    VOGL JULIUS / KUNTZE-FECHNER GERALD / OTTO VICTORIA | Europäisches Patentamt | 2019

    Freier Zugriff