A forward part of an aircraft comprising a fuselage and a landing gear well housing a forward landing gear comprising a breaker strut designed to adopt an extended configuration when the landing gear is extended, configuration in which said breaker strut lies in a strut plane parallel to the transverse direction of the forward part. The forward part comprises a transverse beam resisting strut reactions located above the landing gear well and mounted on the fuselage at its two ends, the beam having a globally rectangular cross-section, in which the median plane parallel to the length of the rectangle is coincident with said strut plane.


    Access

    Download


    Export, share and cite



    Title :

    Front landing-gear well


    Contributors:

    Publication date :

    2016-11-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LANDING GEAR WELL ROOF

    BELLET DANIEL / GALLANT GUILLAUME / LOYANT FRANÇOIS et al. | European Patent Office | 2016

    Free access

    Landing gear well roof

    BELLET DANIEL / GALLANT GUILLAUME / LOYANT FRANÇOIS et al. | European Patent Office | 2019

    Free access

    FRONT LANDING GEAR MODULE FOR AIRCRAFT

    BERNADET PHILIPPE | European Patent Office | 2020

    Free access

    Front landing gear module for aircraft

    BERNADET PHILIPPE | European Patent Office | 2022

    Free access

    Front landing gear of unmanned aerial vehicle

    ZHOU WUHAO / HAN SIYUAN / HU RENFEI et al. | European Patent Office | 2015

    Free access