FIELD: metallurgy.
SUBSTANCE: invention refers to heat-resistant cast alloys on the basis of nickel, which is used for manufacture of high-loaded parts, and namely blades of gas turbines with directed column and monocrystalline structure, which operate at temperatures above 1000°C and higher. Heat-resistant alloy contains the following components, wt %: chrome 5.0-8.0, cobalt 9.0-12.0, tungsten 14.0-16.0, aluminium 4.0-6.0, tantalum 6.0-10.0, carbon 0.002-0.1, yttrium 0.001-0.1, lanthanum 0.001-0.1, cerium 0.001-0.1, silicon 0.01-0.3, magnesium 0.01-0.15, manganese 0.01-0.3, nickel is the rest. Total content of tungsten and tantalum is within the range, wt %, 21.9≤(W+Ta)≤23.5, and total content of chrome and cobalt is within the range, wt %, 17.2≤(Cr+Co)≤18.8.
EFFECT: increasing high-temperature strength of alloy at simultaneous sufficient reduction of its cost and deficiency.
2 tbl
| Title | Year | Author | Number | 
|---|---|---|---|
| CAST HEAT-RESISTANT NICKEL ALLOY WITH MONOCRYSTALLINE STRUCTURE | 2021 | 
 | RU2768946C1 | 
| COMPOSITION OF HEAT-RESISTANT NICKEL ALLOY (VERSIONS) | 2007 | 
 | RU2353691C2 | 
| CAST HEAT-RESISTANT NICKEL ALLOY WITH MONOCRYSTALLINE STRUCTURE | 2021 | 
 | RU2769330C1 | 
| CASTING HEAT RESISTANT NICKEL-BASED ALLOY | 2015 | 
 | RU2626118C2 | 
| HEAT-RESISTANT NICKEL ALLOY | 2019 | 
 | RU2697674C1 | 
| CAST HEAT-RESISTANT NICKEL ALLOY WITH MONOCRYSTAL STRUCTURE | 2024 | 
 | RU2828002C1 | 
| CAST HEAT-RESISTANT NICKEL ALLOY WITH MONOCRYSTAL STRUCTURE FOR GAS TURBINE ENGINE BLADES | 2024 | 
 | RU2821248C1 | 
| HEAT-RESISTANT NICKEL ALLOY FOR CASTING PARTS WITH MONOCRYSTALLINE STRUCTURE | 2021 | 
 | RU2768947C1 | 
| REFRACTORY NICKEL ALLOY FOR SINGLE-CRYSTAL CASTING AND PRODUCT MADE FROM THIS ALLOY | 2000 | 
 | RU2186144C1 | 
| HEAT-RESISTANT ALLOY ON BASE OF NICKEL FOR MONO-CRYSTAL CASTING AND ITEM MADE OUT OF THIS ALLOY | 2008 | 
 | RU2369652C1 | 
Authors
Dates
2012-01-10—Published
2010-12-21—Filed