A fluxless brazing process has been developed that minimizes degradation of the mechanical properties of Borsic/aluminum composites. The process, which employs 718 aluminum alloy braze, is being used to fabricate full scale Borsic/aluminum-titanium honeycomb-core panels for Mach 3 flight testing on the YF-12 aircraft and ground testing in support of the Supersonic Cruise Aircraft Research (SCAR) Program. The manufacturing development and results of shear tests on full scale panels are presented.


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    Titel :

    Brazed Borsic/aluminum structural panels


    Beteiligte:
    Bales, T. T. (Autor:in) / Wiant, H. R. (Autor:in) / Royster, D. M. (Autor:in)

    Erscheinungsdatum :

    01.03.1977


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Brazed Borsic/Aluminum Structural Panels

    T. T. Bales / H. R. Wiant / D. M. Royster | NTIS | 1977


    Fabrication and evaluation of brazed titanium-clad borsic/aluminum skin-stringer panels

    Bales, T. T. / Royster, D. M. / Mcwithey, R. R. | NTRS | 1980




    Brazed borsic/aluminum structural panels

    Bales, Thomas T. / Wiant, H. Ross / Royster, Dick M. | TIBKAT | 1977