A shock strut is disclosed. The shock strut may have multiple pistons and multiple chambers. In this manner, the shock strut may compress different lengths for different applied forces at different points during its stroke.


    Access

    Download


    Export, share and cite



    Title :

    Two-stage secondary piston for landing gear


    Contributors:

    Publication date :

    2016-08-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



    TWO-STAGE SECONDARY PISTON FOR LANDING GEAR

    KALLIO JEREMY DANIEL | European Patent Office | 2015

    Free access

    Drone Piston Landing Gear

    KIM JI SUNG | European Patent Office | 2020

    Free access

    SWING-ARM PISTON LANDING GEAR SYSTEMS AND METHODS

    SCHUSTER EWALD / WHITLOCK JENNIFER / LONG JOSHUA B et al. | European Patent Office | 2024

    Free access

    SWING-ARM PIVOT PISTON LANDING GEAR SYSTEMS AND METHODS

    SCHUSTER EWALD / WHITLOCK JENNIFER / LONG JOSHUA et al. | European Patent Office | 2020

    Free access

    SWING-ARM PIVOT PISTON LANDING GEAR SYSTEMS AND METHODS

    SCHUSTER EWALD / WHITLOCK JENNIFER / LONG JOSHUA B et al. | European Patent Office | 2020

    Free access