A randomly damaged area of a one-piece composite component of an aircraft is repaired according to a method herein. The damaged area covers skin and underlying stiffening substructure of the component. The method includes generating a design of a customized composite replacement panel for replacing the damaged area. The design includes replacement skin and underlying co-cured replacement stiffening substructure. The method further includes fabricating the composite replacement panel according to the design.


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    Titel :

    Large area repair of composite aircraft


    Weitere Titelangaben:

    Reparatur eines großen Bereichs eines Verbundstoffflugzeugs
    Réparation de grande surface d'avion composite


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

    Erscheinungsdatum :

    2020-09-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Large area repair of composite aircraft

    MILLER JEFFREY L / SPENCER SCOTT M / OAKES GARY D et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    LARGE AREA REPAIR OF COMPOSITE AIRCRAFT

    MILLER JEFFREY L / SPENCER SCOTT M / OAKES GARY D et al. | Europäisches Patentamt | 2015

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    Rapid Repair of Large Area Damage to Contoured Aircraft Structures

    Frailey, J. A. / Carter, D. W. / Advisory Group for Aerospace Research and Development; Structures and Materials Panel | British Library Conference Proceedings | 1995


    Repair Dock for Large Aircraft

    V. I. Mavrin / N. I. Prozorov | NTIS | 1975