发明名称 ALUMINUM-BASE ALLOY, METHOD OF PRODUCTION OF SEMIFINISHED PRODUCTS AND ARTICLE FROM THIS ALLOY
摘要 aluminum-base alloys and semifinished products and articles from these alloys. SUBSTANCE: aluminum-base alloy contains, wt.%: magnesium, 0.3-1.2; silicon, 0.3-1.7; manganese, 0.15-1.1; calcium, 0.002-0.1; at least one metal taken from group including copper, zirconium and chromium, 0.02-0.9; aluminum, the balance. It is admissible to have in alloy the following components, wt.%, max.: iron, 1.0; titanium, 0.2; zinc, 0.3. Offered method of production of semifinished products includes preparation of said alloy, casting of ingots, ingot annealing at 350-610 C for 1-20 h, deformation, solid solution heat treatment at 500-550 C for 20-12000 s. Depending on geometrical sizes and surface quality of final semifinished product, it is subjected either to hot deformation, or to hot and cold deformation. Cold-rolled sheet is characterized by equiaxed recrystallization grain sizing 20-30 mcm that provides for its isotropic properties and high technological effectiveness in cold stamping and in condition TI has the following properties in longitudinal direction sigmaV = 335 MPa; sigma0,2 = 275 MPa and delta = 13%. The alloy is used as material for production of various articles, for instance, helicopter rotor blades, fuel tanks, pipelines, vehicle wheels, including articles subject to painting. Parts made of offered alloy are joined by welding, riveting or by bolts. EFFECT: higher efficiency. 13 cl, 3 tbl, 3 ex
申请公布号 RU2163939(C1) 申请公布日期 2001.03.10
申请号 RU19990117622 申请日期 1999.08.09
申请人 O-ISSLEDOVATEL'SKIJ INSTITUT AVIATSIONNYKH MATERIA;LOV;I SKIJ I AVIAT MATERIA O 发明人 GRUSHKO O.E.;EREMINA N.G.;IVANOVA L.A.;SHEVELEVA L.M.
分类号 C22C21/08;C22F1/05;(IPC1-7):C22C21/08 主分类号 C22C21/08
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