A system (401) for use with a tripod landing gear assembly of an aircraft may comprise: a tension strut assembly (450) having a tension strut (452) extending from an upper end to a lower end; a drag brace assembly (402) having an upper brace and a lower brace, the upper brace pivotably coupled to the lower brace at a center point, the lower brace rotatably coupled to the lower end of the tension strut; and a jury linkage (414) pivotally coupled to the drag brace assembly at the center point rotatably coupled to a middle portion of the tension strut, the middle portion between the upper end and the lower end.


    Access

    Download


    Export, share and cite



    Title :

    TRIPOD LANDING GEAR ASSEMBLY


    Additional title:

    DREIBEINIGE FAHRWERKSANORDNUNG
    ENSEMBLE TRÉPIED DE TRAIN D'ATTERRISSAGE


    Contributors:

    Publication date :

    2021-10-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    TRIPOD LANDING GEAR ASSEMBLY

    MARTIN DENNIS W | European Patent Office | 2021

    Free access

    Tripod landing gear assembly

    MARTIN DENNIS W | European Patent Office | 2023

    Free access

    TRIPOD LANDING GEAR ASSEMBLY

    MARTIN DENNIS W | European Patent Office | 2021

    Free access

    LANDING GEAR ASSEMBLY

    BENNETT IAN ROBERT | European Patent Office | 2024

    Free access

    LANDING GEAR ASSEMBLY

    PERKINS CHRISTOPHER JAMES / BOSCOLO MARCO / WHITE NICHOLAS et al. | European Patent Office | 2022

    Free access