FIELD: metallurgy.
SUBSTANCE: invention relates to metallurgy, specifically to titanium-based alloys, and is intended for use in steam-turbine plants and heavy-duty welded structures operated at high temperature. Titanium-based alloy contains, wt%: aluminium 4.3-6.3; molybdenum 1.5-2.5; carbon 0.05-0.14; zirconium 0.2-1.0; oxygen 0.06-0.14; silicon 0.02-0.12; iron 0.05-0.25; niobium 0.03-1.20; hafnium 0.01-0.5; titanium - balance.
EFFECT: alloy has high creep strength at 500°C and preset residual deformation of 2/10 % while maintaining high mechanical properties and corrosion resistance of welded structures.
1 cl, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
TITANIUM-BASED ALLOY | 2013 |
|
RU2506336C1 |
HIGH-TEMPERATURE TITANIUM ALLOYS | 2019 |
|
RU2772375C2 |
HEAT AND CORROSION RESISTANT NICKEL-BASED ALLOY FOR CASTING OF LARGE-SIZED WORKING AND NOZZLE BLADES OF GAS-TURBINE UNITS | 2018 |
|
RU2678353C1 |
HIGH-TENSILE DEFORMED ALLOY ON BASE OF ALUMINIUM AND ITEM OUT OF THIS ALLOY | 2008 |
|
RU2394113C1 |
HEAT RESISTANT ALLOY | 2021 |
|
RU2765806C1 |
FABRICABLE, HIGH STRENGTH, OXIDATION RESISTANT Ni-Cr-Co-Mo-Al ALLOYS | 2014 |
|
RU2650659C2 |
HEAT-RESISTANT ALLOY | 2019 |
|
RU2700347C1 |
TITANIUM-BASE ALLOY | 1991 |
|
RU2030474C1 |
REFRACTORY POWDER NICKEL-BASED ALLOY | 2009 |
|
RU2410457C1 |
NICKEL-BASE HEAT RESISTANT ALLOY FOR CASTING NOZZLE VANES OF GAS TURBINE PLANTS | 2017 |
|
RU2636338C1 |
Authors
Dates
2016-05-10—Published
2014-12-17—Filed