FIELD: metallurgy.
SUBSTANCE: deformed not thermally hardenable alloy on base of aluminium is used in form of deformed semi-finished products as structure material, mainly for soldered units of airspace engineering produced by methods of high temperature soldering. Here is disclosed the said alloy containing wt %: manganese 0.9-1.4, magnesium 0.5-0.7, scandium 0.17-0.35, zirconium 0.05-0.12, titanium 0.01-0.05, iron 0.4-0.6, cerium 0.0001-0.0009, aluminium - the rest.
EFFECT: increased strength of alloy after high temperature solder operation facilitating reduction of weight and dimension of soldered unit of aircraft.
1 tbl, 1 ex
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Authors
Dates
2011-04-20—Published
2010-04-20—Filed