SU174795A1 - HIGHLY STRONG ALLOY BASED ON TITANIUM - Google Patents
HIGHLY STRONG ALLOY BASED ON TITANIUMInfo
- Publication number
- SU174795A1 SU174795A1 SU903188A SU903188A SU174795A1 SU 174795 A1 SU174795 A1 SU 174795A1 SU 903188 A SU903188 A SU 903188A SU 903188 A SU903188 A SU 903188A SU 174795 A1 SU174795 A1 SU 174795A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- titanium
- alloy based
- highly strong
- strong alloy
- alloy
- Prior art date
Links
Landscapes
- Pressure Welding/Diffusion-Bonding (AREA)
Description
Известны ЁЬ1еокоп.рочные сплавы на о&нове титана, садержащие алю миетий, молибден, ванадий и хром.Known alloys on titanium and new metals are aluminum, molybdenum, vanadium and chromium.
Дл -повышени пластлЧНОсти предлагаетс спла1в следующего химического составаIn order to increase the plasticity, an alloy of the following chemical composition is proposed.
(«%):("%):
.Алюминий2,5-3,5Aluminum 2.5-3.5
Молибден3,2-4,5Molybdenum3,2-4,5
Ванадий6,5-7,5Vanadium6,5-7,5
Хром10-11,3Chrome10-11.3
ТитанОстальноеTitanEmost
Такой сплав при СохраненИи высокой прочнОСти позвол ет получать более высокую пластичность , чем у известных титановых сплавов , «ак на ocHOiBHOM металле, так и в сварном оостоЯ.нии после зака1Л|Ки и упрочи ющей термической обработки, а это обеспечивает повышение .ко«структи,вной прочности изделий из «его.Such an alloy, while maintaining high strength, allows to obtain a higher ductility than that of the known titanium alloys, both on ocHOiBHOM metal and in the welded state after ordering | Ki and reinforcing heat treatment. , arduous strength of products from «it.
После термомеханической обработки сплав обеспечивает следующие механические свойства: .предел прочности 165-175 кгс/мм, относительное удлинение 4,5-6%, угол загиба 10-20°.After thermomechanical treatment, the alloy provides the following mechanical properties:. Strength limit 165-175 kgf / mm, relative elongation 4.5-6%, bend angle 10-20 °.
У сварных образцов предел прочности составл ет 150-160 кгс/мм, угол загиба 15- 25°. Сплав технологичен в виде листа, поковок и щтамповок и может быть использован при изготовлении емкостей высокого давлени . For welded specimens, the tensile strength is 150-160 kgf / mm, the bend angle is 15-25 °. The alloy is technological in the form of sheets, forgings and stampings and can be used in the manufacture of high-pressure tanks.
Предмет и з о б р е т е и н Subject and reference
Высокопрочный сплав на основе титана, содержащий алюминий, молибден, ванадий и хром, отличающийс тем, что, с целью повышени пластичности, он имеет следующий химический состав (в %):A high-strength titanium-based alloy containing aluminum, molybdenum, vanadium, and chromium, characterized in that, in order to increase ductility, it has the following chemical composition (in%):
Алюминий2,5--3,5Aluminum2.5--3.5
Молибден3,2-4,5Molybdenum3,2-4,5
Ванадий6,5-7,5Vanadium6,5-7,5
Хром10-11,3Chrome10-11.3
Титан . .ОстальноеTitan .Rest
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU903188A SU174795A1 (en) | 1964-06-01 | 1964-06-01 | HIGHLY STRONG ALLOY BASED ON TITANIUM |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SU903188A SU174795A1 (en) | 1964-06-01 | 1964-06-01 | HIGHLY STRONG ALLOY BASED ON TITANIUM |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| SU174795A1 true SU174795A1 (en) | 1965-09-07 |
Family
ID=39951681
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU903188A SU174795A1 (en) | 1964-06-01 | 1964-06-01 | HIGHLY STRONG ALLOY BASED ON TITANIUM |
Country Status (1)
| Country | Link |
|---|---|
| SU (1) | SU174795A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2584094A1 (en) * | 1985-06-27 | 1987-01-02 | Mitsubishi Metal Corp | HIGH STRENGTH TITANIUM ALLOY MATERIAL HAVING IMPROVED OUVABILITY AND PROCESS FOR PRODUCING THE SAME |
-
1964
- 1964-06-01 SU SU903188A patent/SU174795A1/en active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2584094A1 (en) * | 1985-06-27 | 1987-01-02 | Mitsubishi Metal Corp | HIGH STRENGTH TITANIUM ALLOY MATERIAL HAVING IMPROVED OUVABILITY AND PROCESS FOR PRODUCING THE SAME |
| US4889170A (en) * | 1985-06-27 | 1989-12-26 | Mitsubishi Kinzoku Kabushiki Kaisha | High strength Ti alloy material having improved workability and process for producing the same |
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