FIELD: metallurgy.
SUBSTANCE: invention relates to powder metallurgy, particularly to heat-resistant nickel alloys. It can be used in gas turbine engine for manufacturing of heavy duty components, operating at increased temperatures. Heat-resistant sintered nickel alloy, contains, wt %: carbon 0.07-0.12; chrome 10.0-12.0; cobalt 13.0-15.0; tungsten 4.6-5.6; molybdenum 2.7-3.5; titanium 2.5-3.5; aluminium 3.7-4.4; niobium 3.1- 3.8; hafnium 0.05-0.2; boron 0.005-0.05; zirconium 0.001-0.05; magnesium 0.001-0.05; cerium 0.001-0.05; iron 0.01-1.0; manganese 0.001-0.5; silicon 0.001-0.5; nickel - the rest.
EFFECT: obtaining allot, which allows high strength, high-temperature strength, resistance to "MTsU" at reduction of rate of fatigue crack propagation at operating temperatures.
1 tbl, 1 ex
Title | Year | Author | Number |
---|---|---|---|
SINTERED HEAT-RESISTANT NICKEL ALLOY | 2008 |
|
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RU2410457C1 |
TEMPERATURE-RESISTANT NICKEL ALLOY FOR RECEIVING OF PRODUCTS BY METHOD OF GRANULES METALLURGY | 2008 |
|
RU2359053C1 |
POWDER HEAT RESISTANT ALLOY ON BASE OF NICKEL | 2010 |
|
RU2428498C1 |
DEFORMABLE NICKEL-BASED HEAT-RESISTANT ALLOY | 2019 |
|
RU2695097C1 |
HEAT-RESISTANT NICKEL ALLOY | 2019 |
|
RU2697674C1 |
Authors
Dates
2009-10-27—Published
2008-06-20—Filed