COMPOSITE STRUCTURAL PANELS AND AIRCRAFT FUSELAGES Structural panel assemblies (10) include first and second composite panels (12, 14) positioned in edgewise alignment, with at least one tab (20) extending from a mating edge (16) of the first panel (12) and including an exterior surface (24) in facing registration with a corresponding portion (34) of an interior surface (32) of the second composite panel (14). The corresponding portion (34) includes a recessed area (36) to interfit with the tab (20) or is otherwise configured to receive the tab (20). The exterior surface of the tab (20) is spaced from the corresponding portion (34), to receive a bonding material (40) therebetween for bonding the composite panels (12, 14). 10 2 42 26 _J~--44 -20 28 2 44 22 20 30 50-- 402 18 34 36 42 124 1 16 Fig.1 g114 74 1 170 142 1416 172 176 142 14 162 170 174 16 Fig. 2


    Access

    Download


    Export, share and cite



    Title :

    Composite structural panels and aircraft fuselages


    Contributors:

    Publication date :

    2016-12-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile



    Composite structural panels and aircraft fuselages

    CARDIN RACHEL | European Patent Office | 2018

    Free access

    COMPOSITE STRUCTURAL PANELS AND AIRCRAFT FUSELAGES

    European Patent Office | 2019

    Free access

    COMPOSITE STRUCTURAL PANELS AND AIRCRAFT FUSELAGES

    CARDIN RACHEL | European Patent Office | 2016

    Free access

    AIRCRAFT FUSELAGES

    DETERT BRUCE RAYMOND | European Patent Office | 2017

    Free access

    Aircraft fuselages

    DETERT BRUCE RAYMOND | European Patent Office | 2015

    Free access