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.)
Prevention of corrosion in duralumin airplane structures
West. Flying
Western Flying ; 5 , n 2
1929
Aufsatz (Zeitschrift)
Englisch
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Prevention of Corrosion in Duralumin Airplane Structures
SAE Technical Papers | 1929
|Duralumin All-Metal Airplane Construction
SAE Technical Papers | 1928
|Corrosion embrittlement of duralumin
SLUB | 1928
|Corrosion embrittlement of duralumin
SLUB | 1928
|Corrosion embrittlement of duralumin
SLUB | 1928
|