Metal-matrix composites of aluminum, titanium, nickel and their alloys reinforced by continuous filaments of boron or silicon carbide are considered. The aluminum-boron system provides advantages at temperatures to 600 F for general application; the titanium-silicon carbide system shows promise for high-temperature applications;but the nickel-silicon carbide system presents problems in compatibility between the two materials at high temperatures. Selection of matrix alloys depends on filament loading, thermal history imposed by fabrication and usage requirements, the composite reinforcement geometry, and the nature of-stress distribution resulting from external loadings.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Metal-Matrix Composites Behavior and Aerospace Applications


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Webb, B. A. (Autor:in) / Shimizu, H. (Autor:in) / Dolowy, J. F. (Autor:in) / Taylor, R. J. (Autor:in)

    Kongress:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1967



    Erscheinungsdatum :

    01.02.1967




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch






    DEVELOPING METAL MATRIX COMPOSITES FOR ORDNANCE AND AEROSPACE APPLICATIONS

    Gordon, B. L. / Society of Allied Weight Engineers | British Library Conference Proceedings | 2002



    Ceramic Matrix Composites (CMCs) for Aerospace Applications

    Eswara Prasad, N. / Anil Kumar / Subramanyam, J. | Springer Verlag | 2016