An 18 month laboratory test and stress analysis program was conducted to evaluate bonded boron/epoxy doublers for repairing cracks on aluminum aircraft structures. The objective was to obtain a core body of substantiating data which will support approval for use on commercial transports of a technology that is being widely used by the military. The data showed that the doublers had excellent performance.


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    Titel :

    Evaluation of bonded boron/epoxy doublers for commercial aircraft aluminum structures


    Beteiligte:
    Belason, Bruce (Autor:in) / Rutherford, Paul (Autor:in) / Miller, Matthew (Autor:in) / Raj, Shreeram (Autor:in)


    Erscheinungsdatum :

    1994-09-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Evaluation of Bonded Boron/Epoxy Doublers for Large Commercial Transport Aircraft

    Belason, B. / Shahood, T. / Miller, M. et al. | British Library Conference Proceedings | 1993


    Status of Bonded Boron/Epoxy Doublers for Military and Commercial Aircraft Structures

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




    Bonded Boron/Epoxy Composite Doublers for Reinforcement of Metallic Aircraft Structures

    Belason, E. B. / Shahood, T. W. | British Library Online Contents | 1996