A method of servicing a shock absorber of an aircraft landing gear shock absorbing strut, the shock absorber including a sealed, variable volume chamber containing a liquid and a gas in fluid communication with one another, the method comprising: using a mixer to mix the liquid and the gas within the chamber until the liquid is uniformly saturated with the gas; and subsequently performing one or more servicing actions.


    Access

    Download


    Export, share and cite



    Title :

    Method of servicing an aircraft landing gear shock absorbing strut


    Contributors:
    BROWN ADAM (author) / SMITH JON (author)

    Publication date :

    2022-10-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



    METHOD OF SERVICING AN AIRCRAFT LANDING GEAR SHOCK ABSORBING STRUT

    BROWN ADAM / SMITH JON | European Patent Office | 2019

    Free access

    METHOD OF SERVICING AN AIRCRAFT LANDING GEAR SHOCK ABSORBING STRUT

    BROWN ADAM / SMITH JOHN | European Patent Office | 2024

    Free access

    METHOD OF SERVICING AN AIRCRAFT LANDING GEAR SHOCK ABSORBING STRUT

    BROWN ADAM / SMITH JON | European Patent Office | 2022

    Free access

    Aircraft landing gear shock absorbing strut

    URBINATI SIMONE / HILLIARD MATT / SMITH JON | European Patent Office | 2020

    Free access

    AIRCRAFT LANDING GEAR SHOCK ABSORBING STRUT

    URBINATI SIMONE / HILLIARD MATT / SMITH JON | European Patent Office | 2018

    Free access