FIELD: metallurgy.
SUBSTANCE: invention relates to metallurgy, specifically to nickel-based alloys intended for production of parts and assemblies, having high wear and corrosion resistance, antifriction properties, used in aircraft industry. Nickel-based alloy contains, in wt%: copper 29.5-32.5; iron 1.6-2.9; silicon 4.7-5.1; manganese 0.5-1.8; molybdenum 0.1-0.3; tungsten 0.8-1.2; titanium 0.1-0.3; carbon 0.05-0.35; magnesium 0.03-0.30; dysprosium 0.035; calcium 0.02; cerium 0.07; nickel - balance. Alloy is characterised by high values of ductility, ultimate strength and hardness.
EFFECT: longer service life and higher reliability of articles made from alloy.
2 cl, 2 tbl, 3 ex
Title | Year | Author | Number |
---|---|---|---|
HIGH-STRENGTH BERYLLIUM-CONTAINING STEEL | 2015 |
|
RU2600467C1 |
HEAT RESISTANT NICKEL-BASED ALLOY FOR PRODUCING BOILER PARTS AND STEAM TURBINES OPERATING UNDER ULTRA-SUPERCRITICAL STEAM PARAMETERS | 2017 |
|
RU2637844C1 |
HEAT-RESISTANT ALLOY BASED ON NICKEL FOR MANUFACTURE OF BLADES OF GAS-TURBINE UNITS | 2014 |
|
RU2538054C1 |
HEAT-RESISTANT NICKEL-BASED CAST ALLOY AND AN ARTICLE MADE THEREFROM | 2018 |
|
RU2672463C1 |
HEAT-RESISTANT CAST NICKEL-BASED ALLOY AND ARTICLE MADE THEREFROM | 2017 |
|
RU2656908C1 |
HEAT-RESISTANT NICKEL-BASED CAST ALLOY AND AN ARTICLE MADE THEREFROM | 2018 |
|
RU2674274C1 |
REFRACTORY ALLOY ON NICKEL BASE FOR CASTING OF NOZZLE VANES WITH EQUIAXIAL STRUCTURE OF GAS TURBINE PLANTS | 2014 |
|
RU2576290C1 |
NICKEL-BASE CAST HIGH-TEMPERATURE ALLOY | 1996 |
|
RU2112069C1 |
HEAT-RESISTANT DEFORMABLE NICKEL-BASED ALLOY WITH LOW TEMPERATURE COEFFICIENT OF LINEAR EXPANSION AND ARTICLE MADE FROM IT | 2019 |
|
RU2721261C1 |
HEATPROOF POWDERY NICKEL ALLOY | 2008 |
|
RU2371495C1 |
Authors
Dates
2016-10-27—Published
2015-06-25—Filed