An aircraft landing gear is disclosed having a first oleo strut include a sleeve portion and a slider portion, the slider portion being slidable within a hydraulic fluid chamber of the sleeve portion, and a second, similar oleo strut. The landing gear also includes a hydraulic fluid balancer having a balance chamber separated into first and second end sections, wherein the hydraulic fluid chamber of the sleeve portion of the first oleo strut is fluidly connected to the first section of the balance chamber and the hydraulic fluid chamber of the sleeve portion of the second oleo strut is fluidly connected to the second section of the balance chamber of the hydraulic fluid balancer.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT LANDING GEAR


    Additional title:

    FLUGZEUGFAHRWERK
    TRAIN D'ATTERRISSAGE D'AÉRONEF


    Contributors:

    Publication date :

    2024-01-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR OF AIRCRAFT AND AIRCRAFT COMPRISING LANDING GEAR

    SAKAMOTO FUMINOBU / KUROSE TOYOTOSHI | European Patent Office | 2018

    Free access

    Landing gear of aircraft and aircraft comprising landing gear

    SAKAMOTO FUMINOBU / KUROSE TOYOTOSHI | European Patent Office | 2021

    Free access

    Aircraft landing gear

    FRASER WILSON / BENJAMIN BISHOP | European Patent Office | 2023

    Free access

    AIRCRAFT LANDING GEAR

    THOMPSON ROBERT IAN | European Patent Office | 2021

    Free access

    AIRCRAFT LANDING GEAR

    WILSON FRASER | European Patent Office | 2019

    Free access