FIELD: metallurgy. SUBSTANCE: invention relates to deformable thermally non-hardened aluminum alloys designated for usage in the form of deformed semiproducts as structural materials used in ship building, aerospace technique and transport machine engineering. The proposed alloy comprises the following components, wt.-%: magnesium, 5.3-6.5; manganese, 0.6-1.2; chrome, 0.01-0.25; zirconium, 0.02-0.17; titanium, 0.01-0.15; beryllium, 0.0001-0.005; aluminum, the balance being the total content of manganese, chrome and zirconium is 1.5%, not above. Invention provides the creation of alloy with guaranteed high strength properties, ductility and technological effectiveness in hot and cold deformation. EFFECT: valuable properties of alloy. 2 tbl, 3 ex
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Authors
Dates
2003-09-20—Published
2001-07-06—Filed