FIELD: metallurgy.
SUBSTANCE: invention relates to casting heat-resistant nickel-based alloys used for the manufacture of high-loaded parts of gas turbine engines and plants, namely, working and nozzle blades of gas turbines with a directional columnar and single crystal structure operating at the temperatures of 1000°C and higher. Casting heat-resistant nickel-based alloy contains, wt %: chromium 4.0-9.0; cobalt 9.0-14.0; tungsten 7.0-10.0; molybdenum 1.0-5.0; aluminium 4.0-6.0; tantalum 6.0-10.0; hafnium 0.1-1.0; carbon 0.002-0.1; yttrium 0.001-0.1; lanthanum 0.001-0.1; cerium 0.001-0.1; silicon 0.01-0.2; manganese 0.01-0.3; boron 0.005-0.03; scandium 0.0002-0.01; nickel - the rest.
EFFECT: specific gravity of the alloy decreases while maintaining a high level of heat resistance.
3 tbl, 1 ex
| Title | Year | Author | Number |
|---|---|---|---|
| CAST HEAT-RESISTANT NICKEL ALLOY WITH MONOCRYSTAL STRUCTURE FOR GAS TURBINE ENGINE BLADES | 2024 |
|
RU2821248C1 |
| CAST HEAT-RESISTANT NICKEL ALLOY WITH MONOCRYSTAL STRUCTURE | 2024 |
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| COMPOSITION OF HEAT-RESISTANT NICKEL ALLOY (VERSIONS) | 2007 |
|
RU2353691C2 |
| HEAT-RESISTANT CAST ALLOY ON BASIS OF NICKEL | 2010 |
|
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| HEAT RESISTANT CAST ALLOY ON NICKEL BASE | 2008 |
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| HEAT-RESISTANT NICKEL ALLOY | 2019 |
|
RU2697674C1 |
Authors
Dates
2017-07-21—Published
2015-09-17—Filed