Closure devices and methods are provided for closing a stringer penetration space defined between a stringer and a wing rib of an aircraft wing section. According to certain embodiments, the closure devices will integrally include a forward face plate positioned in covering relationship to at least a portion of the stringer penetration space, and a rearwardly projecting attachment arm rigidly adapted for rigid attachment to the stringer so as to positionally fix the forward face plate relative to the stringer penetration space.


    Access

    Download


    Export, share and cite



    Title :

    DEVICES AND METHODS TO STRUCTURALLY CLOSE AND SEAL OPENINGS IN AN AIRCRAFT WING FUEL TANK



    Publication date :

    2020-10-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Devices and methods to structurally close and seal openings in an aircraft wing fuel tank

    VILAS BOAS ALBERTO VILAR / DA SILVA DANIEL GONÇALVES / MARTINS GUSTAVO DEDDING et al. | European Patent Office | 2023

    Free access

    Wing fuel tank and aircraft

    REN KERONG / WANG WENWEN / QING HUA et al. | European Patent Office | 2024

    Free access

    Fuel tank for fixed-wing aircraft

    JI BAOFENG / WANG ZHIYONG / WANG FEI et al. | European Patent Office | 2020

    Free access

    Structurally integrated fuel tank

    MUPPAVARAPU RAJKIRAN / KALIVARATHAN VENGADASSALAM / SHARMA NIKHIL et al. | European Patent Office | 2024

    Free access

    AIRCRAFT WING WITH FUEL TANK AND FUEL CELL

    TULLOCH WILLIAM | European Patent Office | 2024

    Free access