The fabrication of UH-1 helicopter tail rotor drive shafts from graphite/epoxy composite materials is discussed. Procedures for eliminating wrinkles caused by lack of precure compaction are described. The development of the adhesive bond between aluminum end couplings and the composite tube is analyzed. Performance tests to validate the superiority of the composite materials are reported.


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    Titel :

    Cooperative program for design, fabrication, and testing of graphite/epoxy composite helicopter shafting


    Beteiligte:
    Wright, C. C. (Autor:in) / Baker, D. J. (Autor:in) / Corvelli, N. (Autor:in) / Thurston, L. (Autor:in) / Clary, R. (Autor:in) / Illg, W. (Autor:in)

    Erscheinungsdatum :

    1971-10-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




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