Design and fabrication of a titanium matrix composite (TMC) F-15 nose landing gear (NLG) outer cylinder is discussed. Results of a field experience survey examining landing gear (LG) operations are also discussed. Weight, supportabilty and cost benefits are summarized for this component and projected for production applications of the material.


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    Titel :

    Titanium Matrix Composite Landing Gear Development


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Morris, David L. (Autor:in) / Shea, Mark A. (Autor:in) / Macy, William W. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1989



    Erscheinungsdatum :

    1989-09-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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