FIELD: metallurgy.
SUBSTANCE: refractory nickel based alloy for casting of nozzle vanes with an equiaxial structure of gas turbine plants comprises the following components in wt %: carbon 0.07-0.10; chrome 21.0-21.7; cobalt 10.3-10.8; tungsten 3.6-4.0; titanium 3.6-3.9; aluminium 2.5-2.8; niobium 0.15-0.3; boron 0.010-0.020; zirconium ≤ 0.03; yttrium ≤ 0.03; molybdenum 0.7-1.0; manganese ≤ 0.03, silicon ≤ 0.3; lanthanum ≤ 0.02; iron ≤ 0.5; copper ≤ 0.05; sulphur ≤ 0.005; phosphorous ≤ 0.008; nitrogen ≤ 15 ppm; oxygen ≤ 20 ppm, and nickel - the rest. The total content of aluminium and titanium is 6.1-6.7 wt %, and the ratio Ti:Al is 1.3-1.4.
EFFECT: alloy is characterised by an increased long-term strength at work temperatures of 700-900 degrees in a combination with high oxidation resistance and corrosion strength, increased structural stability for the service life and improved process characteristics.
2 tbl
| Title | Year | Author | Number | 
|---|---|---|---|
| NICKEL-BASE HEAT RESISTANT ALLOY FOR CASTING NOZZLE VANES OF GAS TURBINE PLANTS | 2017 | 
 | RU2636338C1 | 
| REFRACTORY ALLOY ON NICKEL BASE FOR CASTING OF NOZZLE VANES WITH EQUIAXIAL STRUCTURE OF GAS TURBINE PLANTS | 2014 | 
 | RU2542195C1 | 
| HEAT-RESISTANT NICKEL-BASED ALLOY FOR CASTING GAS TURBINE HOT SECTION PARTS OF PLANTS WITH EQUIAXIAL STRUCTURE | 2015 | 
 | RU2581337C1 | 
| HEAT AND CORROSION RESISTANT NICKEL-BASED ALLOY FOR CASTING OF LARGE-SIZED WORKING AND NOZZLE BLADES OF GAS-TURBINE UNITS | 2018 | 
 | RU2678353C1 | 
| BLADE OF GAS-TURBINE UNIT MADE OF HEAT-RESISTANT NICKEL-BASED ALLOY AND MANUFACTURING METHOD THEREOF | 2014 | 
 | RU2581339C1 | 
| HEAT-RESISTANT ALLOY BASED ON NICKEL FOR CASTING OF BLADES OF GAS-TURBINE UNITS | 2014 | 
 | RU2570130C1 | 
| COMPOSITION OF NICKEL-BASED HEAT-RESISTANT ALLOY CHARGE OF EQUIAXIAL STRUCTURE FOR GAS TURBINE WORKING BLADE CASTING | 2014 | 
 | RU2562202C1 | 
| HEAT-RESISTANT ALLOY BASED ON NICKEL FOR MANUFACTURE OF BLADES OF GAS-TURBINE UNITS AND METHOD OF ITS HEAT TREATMENT | 2014 | 
 | RU2539643C1 | 
| REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2014 | 
 | RU2542194C1 | 
| REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2013 | 
 | RU2524515C1 | 
Authors
Dates
2016-02-27—Published
2014-12-19—Filed