FIELD: nonferrous metal alloys. SUBSTANCE: invention, in particular, relates to refractory nickel-based alloys used for manufacturing heavy-duty parts, e. g. gas turbine blades operated at temperatures up to 1000 C, by directional crystallization and monocrystallic casting methods. Proposed alloy contains, wt %: chromium 1.0- 4.0, aluminum 5.0-7.0, titanium <2.0, molybdenum ≤ 4.0, tungsten 12.0- 16.0, tantalum 4.0-10.0, cobalt 10.0-14.0, niobium ≤ 2.0, yttrium 0.003- 0.1, lanthanum 0.001-0.1, cerium 0.003-0.1, and nickel - to 100%, provided that 18,0≤W+Ta≤24,0, and summary content of chromium, tungsten, tantalum, molybdenum, and niobium does not exceed 26.0%. EFFECT: reduced cost due to exclusion of expensive rhenium and balanced content of other alloying components. 2 tbl
| Title | Year | Author | Number | 
|---|---|---|---|
| HEAT-RESISTANT CAST ALLOY ON BASIS OF NICKEL | 2010 | 
 | RU2439185C1 | 
| CONTENT OF HEAT-RESISTANT NICKEL ALLOY FOR SINGLE-CRYSTAL CASTING (VERSIONS) | 2007 | 
 | RU2348725C2 | 
| COMPOSITION OF HEAT-RESISTANT NICKEL ALLOY (VERSIONS) | 2007 | 
 | RU2353691C2 | 
| REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2013 | 
 | RU2525883C1 | 
| CASTING HEAT RESISTANT NICKEL-BASED ALLOY | 2015 | 
 | RU2626118C2 | 
| REFRACTORY NICKEL ALLOY FOR SINGLE-CRYSTAL CASTING AND PRODUCT MADE FROM THIS ALLOY | 2000 | 
 | RU2186144C1 | 
| CASTING NICKEL ALLOY WITH INCREASED HEAT STRENGTH AND RESISTANCE TO SULFIDE CORROSION | 2015 | 
 | RU2623940C2 | 
| REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2013 | 
 | RU2524515C1 | 
| REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE HOT SECTION PARTS | 2013 | 
 | RU2519075C1 | 
| HEAT-RESISTANT GRANULAR NICKEL-BASED ALLOY | 2008 | 
 | RU2386714C1 | 
Authors
Dates
2003-12-20—Published
2002-08-29—Filed