FIELD: metallurgy.
SUBSTANCE: invention relates to the composition of heat resistant nickel-based corrosion resistant alloy for producing boiler parts and steam turbines (pipes, rotors, discs) operating under ultra-supercritical steam parameters at temperatures up to 760°C by casting methods followed by hot deformation or powder metallurgy methods. Heat-resistant nickel-based alloy for producing boiler parts and steam turbines contains, wt %: carbon 0.015-0.10; chromium 19.0-21.5; cobalt 18.0-20.0; molybdenum 4.1-4.8; aluminium 1.2-1.8; titanium 2.5-3.2; boron 0.003-0.05; zirconium 0.01-0.06; silicon 0.05-0.3; manganese 0.05-0.3; iron ≤0.5; sulfur ≤0.007; phosphorus ≤0.007; tungsten 1.1-1.8; niobium 0.15-0.35; hafnium 0.15-0.30; oxygen ≤20 ppm; copper ≤0.05; vanadium 0.1-0.25; nitrogen ≤30 ppm; scandium 0.002-0.005; barium and/or strontium 0.0001-0.01; the rest is nickel, the total content of titanium and aluminium is about ≤4.4 wt % and ratio of titanium to aluminium content is 1.9-2.1.
EFFECT: alloy is characterized by increased structural stability for service life and high values of long-term strength of the products.
3 cl, 2 tbl
| Title | Year | Author | Number | 
|---|---|---|---|
| HEAT-RESISTANT ALLOY BASED ON NICKEL FOR CASTING OF WORKING BLADES FOR GAS TURBINES | 2018 | 
 | RU2678352C1 | 
| HEAT RESISTANT NICKEL ALLOY FOR PRODUCTION OF ITEMS BY METHOD OF PELLET METALLURGY | 2010 | 
 | RU2428497C1 | 
| HEAT-RESISTANT NICKEL-BASED ALLOY | 1997 | 
 | RU2130088C1 | 
| GRANULATED HIGH-TEMPERATURE NICKEL ALLOY AND PRODUCT MANUFACTURED THEREFROM | 2016 | 
 | RU2623540C1 | 
| HEAT-RESISTANT NICKEL-BASED ALLOY FOR CASTING WITH EQUIAXIAL STRUCTURE INTEGRATED WHEELS AND WORKING BLADES | 2015 | 
 | RU2585148C1 | 
| HEAT-RESISTANT ALLOY BASED ON NICKEL FOR MANUFACTURE OF BLADES OF GAS-TURBINE UNITS | 2014 | 
 | RU2538054C1 | 
| HEAT-RESISTANT NICKEL-BASED ALLOY FOR CASTING GAS TURBINE HOT SECTION PARTS OF PLANTS WITH EQUIAXIAL STRUCTURE | 2015 | 
 | RU2581337C1 | 
| NICKEL-BASE HEAT RESISTANT ALLOY FOR CASTING NOZZLE VANES OF GAS TURBINE PLANTS | 2017 | 
 | RU2636338C1 | 
| SINTERED HEAT-RESISTANT NICKEL ALLOY | 2008 | 
 | RU2368683C1 | 
| HEAT-RESISTANT NICKEL ALLOY | 2019 | 
 | RU2697674C1 | 
Authors
Dates
2017-12-07—Published
2017-03-27—Filed