During the 70's, the availability of unniderectional boron biber fabric at Dassault Aviation did allow reinforcement of metallic structures by direct ply lay up on the mental. To be able to apply these reinforcement on airplanes, it was necessary to define a resin system inducing low thermal stresses in the metal during its cure, and with acceptable mechanical properties after aging. Validation was done by simple tests on samples, by application of test repairs on the major fatigue test of the Mercure airplane. Reinforcements of the type are in service for almost 20 years on the Mercure airliner.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Reparations Composites de Structures Metalliques: Vingt Ans d'Experience (Composite Repair of Metallic Airframe; Twenty Years of Experience)


    Publication date :

    1995


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Composite Repair of Metallic Airframe: Twenty Years of Experience

    Druet, M. / Advisory Group for Aerospace Research and Development; Structures and Materials Panel | British Library Conference Proceedings | 1995


    Composite material repairs to metallic airframe components

    CHRISTIAN, T. F. / HAMMOND, D. O. / COCHRAN, J. B. | AIAA | 1992


    Composite material repairs to metallic airframe components

    CHRISTIAN, JR., T. / HAMMOND, D. / COCHRAN, J. | AIAA | 1989


    Damage tolerance investigations of innovative metallic airframe structures

    Häusler, Sascha Marc | GWLB - Gottfried Wilhelm Leibniz Bibliothek | 2011