FIELD: metallurgy.
SUBSTANCE: thermomechanical processing of structural high-strength pseudo-β-titanium alloys, and can be used for load-bearing structures in shipbuilding, aviation and space technology, power plants. A method for manufacturing deformed semi-finished products from high-strength pseudo-β-titanium alloys includes production of an ingot and its thermomechanical processing by ten heatings, deformations, and coolings. First, heating is carried out to a temperature from (Tpt+250)°C to (Tpt+350)°C followed by three stages of deformation with a degree of deformation of 30-60% with alternating upset and drawing. Then heating is carried out to a temperature (Tpt-30)°C followed by two stages of deformation with a degree of deformation of 10-25% at each stage. Next, recrystallization treatment is carried out with heating to a temperature (Tpt+120)°C and subsequent deformation with a degree of deformation of 15-35% with cooling to room temperature, then heating to a temperature (Tpt-30)°C followed by two stages of deformation with a degree of deformation of 10-25% in each stage. Further, additional recrystallization treatment is carried out with heating to a temperature (Tpt+100)°C followed by deformation with a degree of deformation of 15-35% with cooling to the ambient temperature. Next, heating is carried out to a temperature (Tpt-30)°C followed by three stages of deformation with a degree of deformation of 10-25% at each stage, then heating is carried out to a temperature (Tpt-30)°C followed by four stages of deformation with a degree of deformation of 15-30% with alternating upset and drawing. Next, heating is carried out to a temperature (TpT-30)°C followed by four stages of deformation with a degree of deformation of 10-25% at each stage, then heating is carried out to a temperature (Tpt-30)°C followed by three stages of deformation with a degree of deformation of 10-25% at each stage, then heating is carried out to a temperature (Tpt-30)°C followed by three stages of deformation with a degree of deformation of 10-25% at each stage, where Tpt is the polymorphic transformation temperature.
EFFECT: semi-finished products with a thickness of 180 mm and above are characterized by high mechanical properties.
2 cl, 2 tbl, 1 ex
Title | Year | Author | Number |
---|---|---|---|
METHOD OF THERMOMECHANICAL PROCESSING OF HIGH-ALLOYED PSEUDO- (TITANIUM ALLOYS ALLOYED BY RARE AND RARE-EARTH METALS | 2016 |
|
RU2635650C1 |
METHOD OF PRODUCING DEFORMED PARTS FROM PSEUDO-BETA-TITANIUM ALLOYS | 2010 |
|
RU2441097C1 |
METHOD OF THE THERMOMECHANICAL PROCESSING OF THE ARTICLES MADE OUT OF THE TITANIUM ALLOYS | 2006 |
|
RU2318074C1 |
METHOD OF THE THERMOMECHANICAL PROCESSING OF THE ARTICLES MADE OUT OF THE TITANIUM ALLOYS | 2006 |
|
RU2318075C1 |
METHOD OF THERMOMECHANICAL TREATMENT OF PRODUCTS MADE OF TITANIUM ALLOYS | 2009 |
|
RU2384647C1 |
METHOD OF THERMOMECHANICAL TREATMENT OF ITEMS FROM TITANIUM ALLOYS | 2011 |
|
RU2457273C1 |
METHOD OF THERMO-MECHANICAL TREATMENT OF TITANIUM ALLOYS | 2007 |
|
RU2369661C2 |
METHOD OF THERMOMECHANICAL PROCESSING OF TITANIUM ALLOYS | 2007 |
|
RU2368698C2 |
METHOD OF THERMO-MECHANICAL TREATMENT OF TITANIUM ALLOYS | 2007 |
|
RU2369662C2 |
METHOD OF THERMOMECHANICAL TREATMENT OF TITANIUM ALLOYS | 2007 |
|
RU2368697C2 |
Authors
Dates
2023-12-04—Published
2022-10-24—Filed