This disclosure is directed to a method for assembling an aircraft fuselage (400, 500), comprising: providing (502) a mid-fuselage section (404, 414, 424) having a first end and a second end; providing (504) a boron reinforced keel (400, 410, 420); securing (506) the boron reinforced keel (400, 410, 420) to the mid-fuselage section (404, 414, 424, 502) such that a first portion of the boron reinforced keel (400, 410, 420) extends beyond the mid-fuselage section (404) first end; providing (510) a second fuselage section; securing (512) the first portion of the boron reinforced keel (400, 410, 420) to the second fuselage section; and splicing the second fuselage section to the mid-fuselage section (404, 414, 424, 502).


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    Title :

    Boron fiber reinforced structural components


    Additional title:

    Borfaserverstärkte Strukturkomponenten
    Composants structurels renforcés de fibres de bore


    Contributors:

    Publication date :

    2018-08-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / 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 / 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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