FIELD: metallurgy.
SUBSTANCE: proposed refractory nickel based alloy comprises the following components in wt %: carbon 0.02-0.13; chrome 15.6-16.2; cobalt 8.2-8.8; tungsten 2.4-2.8; molybdenum 1.5-2.0; aluminium 3.3-3.7; titanium 3.3-3.7; niobium 0.6-1.1; boron 0.005-0.015; tantalum 1.5-2.0, hafnium 0.00-0.2; zirconium 0.03-0.08; calcium 0.00-0.02; manganese ≤0.02; copper 0.00-0.05; sulphur ≤0.005; phosphorus ≤0.005; nitrogen 10-20 ppm; oxygen 10-15 ppm, at least two elements chosen from the following group: silicon ≤0.25; magnesium 0.00-0.02; iron ≤0.2; nickel - rest.
EFFECT: alloy is characterised by high characteristics of long-term strength in combination with high oxidation ands corrosion resistance, improved structural homogeneity.
2 tbl
Title | Year | Author | Number |
---|---|---|---|
COMPOSITION OF NICKEL-BASED HEAT-RESISTANT ALLOY CHARGE OF EQUIAXIAL STRUCTURE FOR GAS TURBINE WORKING BLADE CASTING | 2014 |
|
RU2562202C1 |
NICKEL-BASE HEAT RESISTANT ALLOY FOR CASTING NOZZLE VANES OF GAS TURBINE PLANTS | 2017 |
|
RU2636338C1 |
REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2013 |
|
RU2524515C1 |
HEAT-RESISTANT ALLOY BASED ON NICKEL FOR CASTING OF WORKING BLADES FOR GAS TURBINES | 2018 |
|
RU2678352C1 |
REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2014 |
|
RU2542194C1 |
HEAT AND CORROSION RESISTANT NICKEL-BASED ALLOY FOR CASTING OF LARGE-SIZED WORKING AND NOZZLE BLADES OF GAS-TURBINE UNITS | 2018 |
|
RU2678353C1 |
REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2013 |
|
RU2525883C1 |
BLADE OF GAS-TURBINE UNIT MADE OF HEAT-RESISTANT NICKEL-BASED ALLOY AND MANUFACTURING METHOD THEREOF | 2014 |
|
RU2581339C1 |
HEAT-RESISTANT NICKEL-BASED CAST ALLOY AND AN ARTICLE MADE THEREFROM | 2018 |
|
RU2672463C1 |
HEAT-RESISTANT ALLOY BASED ON NICKEL FOR MANUFACTURE OF BLADES OF GAS-TURBINE UNITS AND METHOD OF ITS HEAT TREATMENT | 2014 |
|
RU2539643C1 |
Authors
Dates
2015-12-10—Published
2014-06-11—Filed