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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    Title :

    Evaluation of Bonded Boron/Epoxy Doublers for Commercial Aircraft Aluminum Structures


    Contributors:
    B. Belason (author) / P. Rutherford (author) / M. Miller (author) / S. Raj (author)

    Publication date :

    1994


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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

    Belason, Bruce / Rutherford, Paul / Miller, Matthew et al. | NTRS | 1994


    Evaluation of Bonded Boron/Epoxy Doublers for Commercial Aircraft Aluminum Structures

    Belason, B. / Rutherford, P. / Miller, M. et al. | British Library Conference Proceedings | 1994


    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


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

    Belason, E. B. / SAE | British Library Conference Proceedings | 1995