A landing gear for an aircraft comprising a main strut 8, and inboard and outboard sidestays 24 and 22. The main strut is connected to the aircraft at first end 10a, and the sidestays are connected at attachment points 10c, 10b. The sidestays are connected to the main strut at their first ends, such that they may move up and down along a portion of the main strut. The landing gear may retract into a wing structure 12, by rotating the main strut about an axis parallel to the longitudinal axis of the aircraft. The connection between the sidestays and the main strut may comprise a collar 16. The sidestays may include one or more dampers. Preferably, the attachment points of the strut and sidestays are formed in a straight line.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft landing gear


    Contributors:

    Publication date :

    2017-12-20


    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

    DANDALEIX PIERRE-ETIENNE / HERNANDEZ THIBAULT / MILLS ANDREW | European Patent Office | 2024

    Free access

    Aircraft landing gear

    WILSON FRASER | European Patent Office | 2023

    Free access

    AIRCRAFT LANDING GEAR

    WILSON FRASER | European Patent Office | 2022

    Free access