An aircraft landing gear assembly (10) includes a main strut and an axle (18b) on which wheel and brake assemblies (20b, 22b) are mounted. An adaptor member (30) is mounted on a mounting pin and arranged to define a brake rod anchor point (28). The adaptor member is coupled to a part of the landing gear assembly so as to react brake torque and can be formed from a different material than a portion of the main strut.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft landing gear assembly


    Additional title:

    Flugzeugfahrwerkanordnung
    Ensemble de train d'atterrissage d'avion


    Contributors:

    Publication date :

    2017-03-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Aircraft landing gear assembly

    THOMPSON ROBERT IAN | European Patent Office | 2024

    Free access

    AIRCRAFT LANDING GEAR ASSEMBLY

    BENNETT IAN | European Patent Office | 2024

    Free access

    AIRCRAFT LANDING GEAR ASSEMBLY

    BERTHOUD MARCELO / GUIMARAES MAIA LEANDRO / JUESAS PORTOLES JORGE | European Patent Office | 2023

    Free access

    AIRCRAFT LANDING GEAR ASSEMBLY

    BERTHOUD MARCELO / GUIMARAES MAIA LEANDRO / JUESAS PORTOLES JORGE | European Patent Office | 2023

    Free access

    AIRCRAFT LANDING GEAR ASSEMBLY

    BARSALI GUILHERME | European Patent Office | 2023

    Free access