Aluminum alloys found extremely susceptible to both surface corrosion and intercrystalline corrosion; contact of duralumin with brass or steel hastens corrosion; protective paint coverings dissolved by dope where fabric surfaces meet metal parts; all-duralumin structures not suitable for sea-going aircraft unless joints and seams are of watertight construction; few manufacturers awake to corrosion; service precautions recommended; frequency of overhaul of seaplanes. (See also Soc. Automotive Engrs. -- Jl., vol. 24, no. 1, Jan. 1929, pp. 24-27 and (discussion) 27-29; and Italian translation in Notiziario Tecnico di Aeronautica, vol. 7, no. 6, June 1929, pp. 57-62.)


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    Titel :

    Prevention of corrosion in duralumin airplane structures


    Weitere Titelangaben:

    West. Flying


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1929


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Prevention of Corrosion in Duralumin Airplane Structures

    RICHARDSON, L. B. | SAE Technical Papers | 1929


    Duralumin All-Metal Airplane Construction

    STOUT, W. B. | SAE Technical Papers | 1928


    Corrosion embrittlement of duralumin

    Rawdon, Henry S. | SLUB | 1928


    Corrosion embrittlement of duralumin

    Rawdon, Henry S. | SLUB | 1928


    Corrosion embrittlement of duralumin

    Rawdon, Henry S. | SLUB | 1928