GB782148A - Improvements in and relating to the heat treatment of titanium alloys - Google Patents
Improvements in and relating to the heat treatment of titanium alloysInfo
- Publication number
- GB782148A GB782148A GB30840/55A GB3084055A GB782148A GB 782148 A GB782148 A GB 782148A GB 30840/55 A GB30840/55 A GB 30840/55A GB 3084055 A GB3084055 A GB 3084055A GB 782148 A GB782148 A GB 782148A
- Authority
- GB
- United Kingdom
- Prior art keywords
- temperature
- hours
- etching
- relating
- coarsening
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
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)
- ing And Chemical Polishing (AREA)
Abstract
Titanium base alloys having compositions within one of the following ranges in per cent by weight. Al 2.0-8.0, Si 0.1-1.5, V 2.0-6.0 or Mo 1.0-6.0 or Mo and V 1.0-6.0; Al 4.0-6.0, Si 0.3-0.5, V 3.0-5.0; Al 4.0-6.0, Si 0.3-0.5, Mo 3.0-4.0; Al 2.0-8.0, Mo 1.0-6.0 the remainder in each case being Ti together with impurities O up to 0.2, N up to 0.1, C up to 0.25 and H up to 0.02, the Al content being at least as great as that of Mo or V or the combination thereof, are heated to a temperature high in the polyphase field to coarsen the microstructure and to form a continuous alpha phase, then quickly cooled and aged at a temperature below the coarsening temperature till the beta phase is dark etching. The final condition of the beta phase is determined by etching with a solution of 60 cc. glycerine, 20 cc. concentrated nitric acid and 20 cc. precipitated hydrofluoric acid. The coarsening treatment may be at 1500-1650 DEG F. for 4-24 hours, the alloy being rapidly cooled in inert atmosphere or air or by quenching to room temperature or to the ageing temperature of 1000-1200 DEG F. at which it is held e.g. for 4-48 hours.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US782148XA | 1954-10-27 | 1954-10-27 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB782148A true GB782148A (en) | 1957-09-04 |
Family
ID=22142661
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30840/55A Expired GB782148A (en) | 1954-10-27 | 1955-10-27 | Improvements in and relating to the heat treatment of titanium alloys |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB782148A (en) |
Cited By (4)
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 |
GB2203755A (en) * | 1987-04-22 | 1988-10-26 | Nippon Kokan Kk | Corrosion resistant titanium alloy |
GB2498408A (en) * | 2012-01-12 | 2013-07-17 | Titanium Metals Corp | A titanium alloy comprising aluminium, vanadium, molybdenum, silicon and oxygen |
US12104239B2 (en) | 2014-05-15 | 2024-10-01 | General Electric Company | Titanium alloys and their methods of production |
-
1955
- 1955-10-27 GB GB30840/55A patent/GB782148A/en not_active Expired
Cited By (9)
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 |
GB2178758A (en) * | 1985-06-27 | 1987-02-18 | Mitsubishi Metal Corp | Titanium base alloy |
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 |
GB2203755A (en) * | 1987-04-22 | 1988-10-26 | Nippon Kokan Kk | Corrosion resistant titanium alloy |
GB2203755B (en) * | 1987-04-22 | 1991-08-14 | Nippon Kokan Kk | High strength and corrosion resistant titanium alloy having excellent corrosion-wear properties |
GB2498408A (en) * | 2012-01-12 | 2013-07-17 | Titanium Metals Corp | A titanium alloy comprising aluminium, vanadium, molybdenum, silicon and oxygen |
GB2498408B (en) * | 2012-01-12 | 2013-12-18 | Titanium Metals Corp | Titanium alloy with improved properties |
US10119178B2 (en) | 2012-01-12 | 2018-11-06 | Titanium Metals Corporation | Titanium alloy with improved properties |
US12104239B2 (en) | 2014-05-15 | 2024-10-01 | General Electric Company | Titanium alloys and their methods of production |
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