发明名称 ALUMINIUM-BASED ALLOY AND METHOD OF THERMAL TREATMENT THEREOF
摘要 FIELD: metallurgy. SUBSTANCE: alloy, preferably Al-Li-Mg system, comprises, wt %: 1.5-1.9; magnesium, 4.1-6.0; zinc, 0.1-1.5; zirconium, 0.05-0.3; manganese; 0.01-0.8; hydrogen, <EMI ID=0.84 HE=6 WI=36 TI=CHI> and at least one element selected from group consisting of beryllium, 0.001-0.2; yttrium, 0.01-0.5 scandium 0.01-0.3; chromium, 0.01-0.5; and aluminium; the balance. Method comprises hardening, straightening and three-stage aging according to the following procedure: first stage, at 80-90 C for 3- 12 h, second stage, at 110-185 C for 10-48 h, and third stage, at 90-110 C for 8-14 h. EFFECT: higher plasticity of alloy in chemically strong state, high strength and high corrosion resistance, good weldability, high characteristics of viscosity of destruction and thermal stability after healing at 85 C for 1000 h. 3 cl, 1 ex, 3 tbl
申请公布号 RU2133295(C1) 申请公布日期 1999.07.20
申请号 RU19980104394 申请日期 1998.03.05
申请人 O-ISSLEDOVATEL'SKIJ INSTITUT AVIATSIONNYKH MATERIA;I SKIJ I AVIAT MATERIA O;LOV 发明人 FRIDLJANDER I.N.;KOLOBNEV N.I.;KHOKHLATOVA L.B.;KABLOV E.N.;DAVYDOV V.G.;CHERTOVIKOV V.M.;TOLCHENNIKOVA E.G.;GALKIN D.S.;MOZHAROVSKIJ S.M.;VINKLER PETER-JURGEN;LEKHEL'T EHRVIN;PFANNENMJULLER TOMAS
分类号 C22C21/06;C22F1/047;(IPC1-7):C22C21/06 主分类号 C22C21/06
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