FIELD: metallurgy.
SUBSTANCE: invention can be used for manufacture of parts of aerospace equipment, which operate at temperatures of up to 1600°C. Heat-resistant disperse strengthened alloy based on niobium and methods for its obtaining are described. Alloy contains niobium matrix inside which there located are disperse escapes of Al2O3 with diameter of up to 10 mcm at the following component ratio, wt %: Al - 0.1-20, O2 - 0.05-10, Fe, Cr, Cu, Ni, Ti, Cr, Mn - not more than 2.5 in total, Nb - the rest. Method for obtaining heat-resistant alloy based on niobium as per it. 1, which involves crushing of powder mixture, contains the following, wt %: Al - 0.1-20, Fe, Cr, Cu, Ni, Ti, Cr, Mn not more than 2.5 in total and niobium is the rest; first, in dry condition during 14-16 hours, and then in presence of acetone during 4-6 hours at ratio of weight of powders to weight of grinding balls of 1 : (8.5-11.5) till supersaturated solid solution Nb(Al) is formed; after that, the obtained mixture is compacted and sintered at temperature of 1650-1750°C during 20-60 minutes. Besides, sintering can be carried out in vacuum of 0.13-0.01 Pa or at pressure of 13.33-1.33 Pa in CO environment.
EFFECT: increasing ductility from room temperature to high temperatures and manufacturability of the material.
6 cl, 6 dwg, 6 ex
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Authors
Dates
2012-10-20—Published
2011-05-24—Filed