A former for an aircraft fuselage is disclosed. An example former has a first face and a second face. Each of the faces is shaped as a component of the aircraft fuselage. The example former has a cellular structure between the first face and the second face. The cellular structure has a low density of wall material relative to density of a solid former, and can withstand high out-of-plane compression and out-of-plane shear forces. An adhesive attaches the first face to a first side of the cellular structure, and the second face to a second side of the cellular structure. The edge of the former may support a skin of the aircraft fuselage.


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    Titel :

    FORMERS FOR AIRCRAFT FUSELAGE


    Beteiligte:
    MILLER TED J (Autor:in)

    Erscheinungsdatum :

    13.09.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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