A rotor assembly including a rotor mast, a rotor hub coupled to the rotor mast, a plurality of rotor blades coupled to the rotor hub, a control tube extending through the rotor mast, a crosshead coupled to the control tube, and a mechanism configured to drive the rotor mast in rotation. Wherein the mechanism is longitudinally positioned between a top portion and a bottom portion of the control tube and translation of the control tube relative to the rotor mast causes rotation of the rotor blades about their pitch-change axes. While the crosshead is installed, the crosshead is prevented from angular rotation about the mast axis. A pin of a rotor blade assembly is captured between opposing tabs of the crosshead and movable relative to the opposing tabs in response to translation of the crosshead along the mast axis


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ROTOR ASSEMBLY


    Beteiligte:

    Erscheinungsdatum :

    2021-05-13


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    ROTOR ASSEMBLY AND AIRCRAFT WITH ROTOR ASSEMBLY

    THOMPSON GEORGE MATTHEW / SHERRILL PAUL / KNOLL JONATHAN | Europäisches Patentamt | 2023

    Freier Zugriff

    ROTOR ASSEMBLY

    MARSHALL BRYAN / LOOS ERIC | Europäisches Patentamt | 2023

    Freier Zugriff

    ROTOR ASSEMBLY

    THOMPSON GEORGE MATTHEW / SPELLER CHARLES HUBERT / KNOLL JONATHAN | Europäisches Patentamt | 2023

    Freier Zugriff

    Rotor assembly

    THOMPSON GEORGE MATTHEW / SPELLER CHARLES HUBERT / KNOLL JONATHAN | Europäisches Patentamt | 2022

    Freier Zugriff

    Rotor assembly

    Europäisches Patentamt | 2020

    Freier Zugriff