A shock strut is disclosed. The shock strut may include a shock strut cylinder, a shock strut piston that is slidably disposed within the shock strut cylinder, a metering pin, and a percolation seal configured to restrict a flow of liquid between the shock strut cylinder and the shock strut piston.


    Access

    Download


    Export, share and cite



    Title :

    Landing gear percolation


    Contributors:

    Publication date :

    2023-11-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



    LANDING GEAR PERCOLATION

    BODKI BASAVARAJ / NAGARAJA HEMANTH / HEALEY STEVE | European Patent Office | 2022

    Free access

    LANDING GEAR PERCOLATION

    BODKI BASAVARAJ / NAGARAJA HEMANTH / HEALEY STEVE | European Patent Office | 2022

    Free access

    LANDING GEAR

    WILSON FRAZER / BRIANCOURT STEPHEN / IQBAL KAMRAN et al. | European Patent Office | 2018

    Free access

    LANDING GEAR

    SAKOTA NEBOJSA / WIJKER NORMAN | European Patent Office | 2018

    Free access

    Landing Gear

    Dreier, Mark E. | AIAA | 2007