A landing gear is disclosed having a main strut connected at one end to an aircraft via a main joint is disclosed. The landing gear further includes an inboard sidestay assembly connected to the main strut. The inboard sidestay assembly includes a forward stay connected at one end to the aircraft, a rear stay connected at one end to the fuselage, and a shear web extending between the forward stay and the rear stay and configured to resist movement of the forward stay relative to the rear stay. The landing gear is arranged such that when the landing gear is extended substantially all the landing gear loads are transferred from the landing gear to the aircraft via one or more of the main joint, the forward stay and the rear stay.


    Access

    Download


    Export, share and cite



    Title :

    LANDING GEAR


    Contributors:

    Publication date :

    2018-12-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Landing gear

    SUVEREN SERCAN / AKGUN BURAK | European Patent Office | 2025

    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


    Landing gear

    European Patent Office | 2016

    Free access