FIELD: metallurgy.
SUBSTANCE: invention relates to metallurgy. Cast work blade with monocrystal structure contains body, lock flange and lock part, and comprises two fragments connected by fusion zone. Fusion zone of two fragments with height 5-30 mm is located between lock flange and blade lock part. One fragment - lock part - is made out of alloy with increased short-term strength, another fragment - blade body and lock flange - are made out of alloy with increased heat resistance. Difference of temperatures of complete dissolution of strengthening γ'- phase of two heat resistant alloys TSOLγ' is maximum 20°C, and difference of alloy densities is ~8%. The heat resistant alloy on nickel base to manufacture lock part of the work blade under invention contains wt %: carbon 0.001-0.12; chrome 6.5-9.8; cobalt 4.0-7.2; molybdenum 1.6-3.7; tungsten 2.0-4.2; titanium 3.0-4.5; aluminium 4.8-6.2; niobium 0.08-0.22; manganese 0.002 - 0.12; silicon 0.005 - 0.2; nickel - the rest. Method of heat treatment of cast blade includes homogenizing annealing at 1250±10°C for 2-3 hours with further cooling with rate 25-40°C/min to 690-710°C, further heating to ageing temperature, holding for 16-24 hours, and cooling with rate 20-40°C/min to 500°C, holding for 5-30 minutes, and air cooling.
EFFECT: increased strength of blade, and operation reliability of turbine.
5 cl, 1 dwg, 2 tbl
Title | Year | Author | Number |
---|---|---|---|
REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2014 |
|
RU2542194C1 |
REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2013 |
|
RU2524515C1 |
REFRACTORY NICKEL-BASED ALLOY FOR CASTING GAS TURBINE WORKING BLADES | 2013 |
|
RU2525883C1 |
HEAT-RESISTANT ALLOY ON BASE OF NICKEL FOR MONO-CRYSTAL CASTING AND ITEM MADE OUT OF THIS ALLOY | 2008 |
|
RU2369652C1 |
HEAT-RESISTANT ALLOY BASED ON NICKEL FOR CASTING OF BLADES OF GAS-TURBINE UNITS | 2014 |
|
RU2570130C1 |
HEAT-RESISTANT ALLOY BASED ON NICKEL FOR CASTING OF WORKING BLADES FOR GAS TURBINES | 2018 |
|
RU2678352C1 |
BLADE OF GAS-TURBINE UNIT MADE OF HEAT-RESISTANT NICKEL-BASED ALLOY AND MANUFACTURING METHOD THEREOF | 2014 |
|
RU2581339C1 |
HEAT AND CORROSION RESISTANT NICKEL-BASED ALLOY FOR CASTING OF LARGE-SIZED WORKING AND NOZZLE BLADES OF GAS-TURBINE UNITS | 2018 |
|
RU2678353C1 |
CAST HEAT-RESISTANT NICKEL-BASED ALLOY AND PRODUCT MADE THEREOF | 2016 |
|
RU2633679C1 |
NICKEL-BASE HEAT-RESISTANT ALLOY | 1998 |
|
RU2131944C1 |
Authors
Dates
2015-10-27—Published
2014-08-28—Filed