FIELD: wrought not thermally hardened alloys used as structural materials in shipbuilding; aerospace engineering; oil-and-gas extraction industry.
SUBSTANCE: proposed alloy contains the following components, mass-%: magnesium, 5.5-6.5; scandium, 0.10-0.20; manganese, 0.5-1.0; chromium, 0.10-0.25; zirconium, 0.05-0.20; titanium, 0.02-0.15; zinc, 0.1-1.0; boron, 0.003-0.015; beryllium, 0.0002-0.005; the remainder being aluminum.
EFFECT: high ductility of alloy with strength characteristics at prototype level.
2 tbl, 1 ex
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Authors
Dates
2006-01-20—Published
2004-05-20—Filed