The testing of a titanium matrix composite (TMC) F-15 nose gear outer cylinder is discussed. Two cylinders were fabricated. An entire F-15 nose gear was assembled using the first cylinder. This test gear underwent static structural tests to three critical loading conditions and functional evaluations including load-stroke, rebound snubbing, jig drops and strut stroke cycling. The TMC cylinder successfully completed both groups of testing with no signs of structural or functional degradation.


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    Titel :

    Testing of a titanium matrix composite landing gear


    Weitere Titelangaben:

    Erprobung eines Fahrwerks aus Verbundwerkstoff mit Titanmatrix


    Beteiligte:
    Shea, M.A. (Autor:in) / Macy, W.W. (Autor:in) / Morris, D.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1991


    Format / Umfang :

    9 Seiten, 17 Bilder



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Testing of a Titanium Matrix Composite Landing Gear

    Morris, David L. / Shea, Mark A. / Macy, William W. | SAE Technical Papers | 1991


    Titanium Matrix Composite Landing Gear Development

    Morris, David L. / Shea, Mark A. / Macy, William W. | SAE Technical Papers | 1989


    Titanium matrix composite landing gear development

    Macy, W.W. / Shea, M.A. / Morris, D.L. | Tema Archiv | 1989


    ICAS2014_0052: FOD CHARACTERISTICS OF TITANIUM METAL MATRIX COMPOSITE (TMC) TO APPLY AIRCRAFT LANDING GEAR STRUCTURE

    Takahashi, N. / Sato, T. / Fujiwara, K. et al. | British Library Conference Proceedings | 2014


    Structural Testing of Sandwich Composite Main Landing Gear Door

    Dimitroff, Mary / Shah, Aditya K. / Sullivan, Rani W. et al. | AIAA | 2024