A core stiffened panel includes first and second skins having a large cell core and a solid insert joined therebetween. The solid insert has a side surface at least a portion of which is adjacent to the large cell core and may be joined to the large cell core. The first skin, the second skin and the solid insert may be formed from composite materials such as carbon composite materials and preferably have generally matching coefficients of thermal expansion.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Large Cell Core Stiffened Panels with Solid Inserts


    Beteiligte:

    Erscheinungsdatum :

    2017-09-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / B64C AEROPLANES , Flugzeuge



    Stiffened composite panels

    ROSS JOSHUA AMORY / CUDA SHANE FRANK / MCLAUGHLIN MARK RONALD et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Stiffened composite panels

    ROSS JOSHUA AMORY / CUDA SHANE FRANK / MCLAUGHLIN MARK RONALD et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Buckling of Stiffened Panels

    Shama, Mohamed | Springer Verlag | 2013



    Stiffened Carbon/Carbon Compression Panels

    Sawyer, James W. | NTRS | 1992