FIELD: responsible components of gas turbine engines. SUBSTANCE: the alloy comprises the following components (wt %): 0.005-0.12 carbon; 0.005-0.015 boron; 9.5-11.4 chromium; 5.2-6.8 cobalt; 0.5-1.5 molybdenum; 7.5-9.8 tungsten; 3.8-4.4 aluminium; 4.0-4.6 titanium; 0.5-1.5 niobium; 0.3-0.8 manganese; 0.005-0.02 calcium; 0.01-0.03 yttrium; 0.005-0.03 zirconium; and nickel, the base. EFFECT: improved properties of the highly heat resistant alloy. 2 cl, 2 tbl
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Authors
Dates
1994-09-30—Published
1991-11-21—Filed