FIELD: metallurgy; inter- metallic compounds on base of Ni3Al; articles produced by precision casting. SUBSTANCE: proposed alloy is intended for castings of gas-turbine engines working at high thermal and power loads, mainly for working blades of aircraft and rocket gas turbines. Proposed alloy on base of Ni3Al, contains aluminum, chromium, molybdenum, tungsten, titanium, carbon at additional inclusion of cobalt, rhenium, tantalum and lanthanum at the following relationship, mass-%: Al, 7.7-8.7; Cr, 5.0-6.0; W, 2.5- 3.5; Mo, 4.5-5.5; Ti, 0.3-0.8; C, 0.005-0.01; Co, 3.5-4.5; Re, 1.2-1.8; Ta, 0.1-1.0; La, 0.015-0.025; the remainder being Ni and article made from it. EFFECT: enhanced reliability; increased service life of articles. 2 cl, 2 tbl, 1 ex
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Authors
Dates
2004-01-20—Published
2002-11-11—Filed