FIELD: metallurgy of alloys, more particularly, manufacture of heat resistant nickel-based alloys by directed crystallization and monocrystalline casting of components, namely gas turbine vanes operating at high temperatures (1000-1100). SUBSTANCE: alloy comprises, wt.%: carbon, 0.05-0.12; chrome, 5.0-6.0; cobalt, 8.0-10.0; tungsten, 6.5-7.5; molybdenum, 0.8-1.5; aluminium 5.5-6.0; cobalt, 8.0-10.0; tantalum, 4.4-5.4, rhenium, 3.8-4.6; boron, 0.001-0.02; niobium, 0.6-1.0; cerium, 0.005-0.10; yttrium, 0.0001- 0.002; lanthanum, 0.001-0.05; neodymium, 0.0005-0.01; and nickel, the balance, provided that the following condition is observed: 9,5≤(1/2W+1/2Re+1/2Ta+Mo+Nb)≤10,5. EFFECT: improved technological and heat resistance characteristics of the alloy. 1 ex, 2 tbl
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Authors
Dates
2000-04-27—Published
1999-01-18—Filed