Al-Li alloys can provide reduced weight and increased stiffness as replacements for conventional aluminum alloy aircraft components. A study was conducted to compare the performance of 2090 Al-Li and 7075 Al alloys in-service on Navy aircraft, during shipboard exposure and in laboratory accelerated tests. Results from this investigation indicated that no additional maintenance was required during in-service exposure and that the corrosion behavior of the two alloys in laboratory tests and during shipboard exposure was comparable.


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    Titel :

    In-Service Evaluation of 2090 Aluminum-Lithium Alloy on F/A-18 Aircraft


    Beteiligte:
    J. Kozol (Autor:in) / E. S. Tankins (Autor:in) / J. J. Thompson (Autor:in) / C. E. Neu (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    31 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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