FIELD: metallurgy.
SUBSTANCE: metal-matrix composites based on a high-entropy alloy. Invention can be used for structural applications in aircraft and power engineering, including at high temperatures. Metal-matrix composite Al5Nb24Ti40V5Zr26/TiB2 obtained by vacuum-arc remelting in pure argon of aluminium, niobium, titanium, vanadium, zirconium with the addition of TiB2 with an average particle size of 4 mcm, contains a matrix of high-entropy alloy Al5Nb24Ti40V5Zr26 and a reinforcing component TiB2, while the matrix alloy contains: 5 at.% of aluminium, 24 at.% of niobium, 40 at.% of titanium, 5 at.% of vanadium and 26 at.% of zirconium, and the metal matrix composite contains 1% by weight of TiB2.
EFFECT: invention is aimed at obtaining a metal-matrix composite with high tensile strength, yield strength and tensile plasticity at room temperature.
1 cl, 2 dwg, 1 tbl, 2 ex
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Authors
Dates
2023-04-04—Published
2022-07-11—Filed