A randomly damaged area of a one-piece composite component (110) of an aircraft (100) is repaired according to a method herein. The damaged area (250) covers skin (210) and underlying stiffening substructure (220) of the component (110). The method includes generating a design of a customized composite replacement panel (310) for replacing the damaged area (250). The design includes replacement skin and underlying co-cured replacement stiffening substructure. The method further includes fabricating the composite replacement panel (310) according to the design. 6327497v1:PRW '-U cc U) (120 UL (0 0 r L) C) c C) C


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    Titel :

    Large area repair of composite aircraft


    Beteiligte:
    MILLER JEFFREY L (Autor:in) / SPENCER SCOTT M (Autor:in) / OAKES GARY D (Autor:in) / DOSTERT STEPHEN J (Autor:in)

    Erscheinungsdatum :

    02.02.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    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 / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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