WO2001081026A3 - Method for processing metal and alloy billets - Google Patents
Method for processing metal and alloy billets Download PDFInfo
- Publication number
- WO2001081026A3 WO2001081026A3 PCT/RU2001/000157 RU0100157W WO0181026A3 WO 2001081026 A3 WO2001081026 A3 WO 2001081026A3 RU 0100157 W RU0100157 W RU 0100157W WO 0181026 A3 WO0181026 A3 WO 0181026A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- billets
- processing
- preferential
- stages
- torque load
- Prior art date
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/16—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
- C22F1/18—High-melting or refractory metals or alloys based thereon
- C22F1/183—High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Forging (AREA)
- Junction Field-Effect Transistors (AREA)
Abstract
The invention relates to metallurgy, more precisely to the thermomechanical treatment of billets having a large-grained laminar structure, in particular to titanium and alloys thereof, in order to obtain a defined microstructure for said billets. The aim of the invention is to increase grain reduction, i.e. to obtain a grain size of 5.0 to 10.0 mkm and less for large-sized billets, including billets of 200 kg and more; to provide the billets with a homogeneous or a specified heterogeneous cross section structure; to reduce a specific energy intensity and to increase the size of the processed billet. The invention is also directed at a reduction of the labor coefficient of the process as a whole. The inventive method consists in processing metal and alloy billets by means of inelastic deformation to a degree and at temperature-speed conditions making it possible to reduce the grain size by processing the entire billet or a specified part thereof in one or several stages. In the case of one-stage processing, a torque load is a preferential or exclusive loading component. In the case of several stages, a torque load is a preferential or exclusive loading component used mainly for the first step and tensile and compressive loads are used as preferential or exclusive loading component for the subsequent stages. At least the stage with the torque load is carried out in several processing steps and the loading conditions are selected in such a way that it is possible to transform the microstructure during the deformation and/or during the heat treatment carried out between the stages or steps.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2001250710A AU2001250710A1 (en) | 2000-04-19 | 2001-04-18 | Method for processing metal and alloy billets |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2000109802/02A RU2203975C2 (en) | 2000-04-19 | 2000-04-19 | Method of treatment of blanks made from metals or alloys |
RU2000109802 | 2000-04-19 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2001081026A2 WO2001081026A2 (en) | 2001-11-01 |
WO2001081026A3 true WO2001081026A3 (en) | 2007-11-08 |
Family
ID=20233559
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/RU2001/000157 WO2001081026A2 (en) | 2000-04-19 | 2001-04-18 | Method for processing metal and alloy billets |
Country Status (3)
Country | Link |
---|---|
AU (1) | AU2001250710A1 (en) |
RU (1) | RU2203975C2 (en) |
WO (1) | WO2001081026A2 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2497975C2 (en) * | 2012-02-08 | 2013-11-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Санкт-Петербургский политехнический университет" (ФГБОУ ВПО "СПбГПУ") | Treatment method of flat workpieces from metals and alloys |
RU2528296C2 (en) * | 2012-09-17 | 2014-09-10 | Оскар Акрамович Кайбышев | Method of metals and alloys treatment (versions) and device to this end |
RU2586188C1 (en) * | 2014-12-04 | 2016-06-10 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Санкт-Петербургский государственный университет" (СПбГУ) | Method for intensive plastic deformation by torsion under high pressure with step-by-step heating |
RU2709416C1 (en) * | 2019-10-14 | 2019-12-17 | Федеральное государственное автономное образовательное учреждение высшего образования "Национальный исследовательский технологический университет "МИСиС" | Method of processing technically pure titanium by high plastic deformation |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3519503A (en) * | 1967-12-22 | 1970-07-07 | United Aircraft Corp | Fabrication method for the high temperature alloys |
SU742483A1 (en) * | 1978-01-11 | 1980-06-25 | Калининградский Машиностроительный Завод | Method of thermomechanical treatment of (alpha+beta)-titanium alloys |
SU894015A1 (en) * | 1980-02-25 | 1981-12-30 | Институт физики твердого тела АН СССР | Method of treatment of aluminium and its alloys |
RU2119842C1 (en) * | 1996-06-21 | 1998-10-10 | Институт проблем сверхпластичности металлов РАН | Method for manufacturing axially symmetrical parts and blank making process for performing the same |
RU2134308C1 (en) * | 1996-10-18 | 1999-08-10 | Институт проблем сверхпластичности металлов РАН | Method of treatment of titanium alloys |
-
2000
- 2000-04-19 RU RU2000109802/02A patent/RU2203975C2/en not_active IP Right Cessation
-
2001
- 2001-04-18 AU AU2001250710A patent/AU2001250710A1/en not_active Abandoned
- 2001-04-18 WO PCT/RU2001/000157 patent/WO2001081026A2/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3519503A (en) * | 1967-12-22 | 1970-07-07 | United Aircraft Corp | Fabrication method for the high temperature alloys |
SU742483A1 (en) * | 1978-01-11 | 1980-06-25 | Калининградский Машиностроительный Завод | Method of thermomechanical treatment of (alpha+beta)-titanium alloys |
SU894015A1 (en) * | 1980-02-25 | 1981-12-30 | Институт физики твердого тела АН СССР | Method of treatment of aluminium and its alloys |
RU2119842C1 (en) * | 1996-06-21 | 1998-10-10 | Институт проблем сверхпластичности металлов РАН | Method for manufacturing axially symmetrical parts and blank making process for performing the same |
RU2134308C1 (en) * | 1996-10-18 | 1999-08-10 | Институт проблем сверхпластичности металлов РАН | Method of treatment of titanium alloys |
Also Published As
Publication number | Publication date |
---|---|
AU2001250710A8 (en) | 2008-01-10 |
WO2001081026A2 (en) | 2001-11-01 |
AU2001250710A1 (en) | 2001-11-07 |
RU2203975C2 (en) | 2003-05-10 |
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