GB1141409A - Heat treatment and working of titanium alloys - Google Patents
Heat treatment and working of titanium alloysInfo
- Publication number
- GB1141409A GB1141409A GB339067A GB339067A GB1141409A GB 1141409 A GB1141409 A GB 1141409A GB 339067 A GB339067 A GB 339067A GB 339067 A GB339067 A GB 339067A GB 1141409 A GB1141409 A GB 1141409A
- Authority
- GB
- United Kingdom
- Prior art keywords
- beta
- alpha
- transus
- working
- temperature
- 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)
- Heat Treatment Of Steel (AREA)
Abstract
1,141,409. Improving physical properties; working at specified temperatures. CONTINENTAL TITANIUM METALS CORP. G.m.b.H. 23 Jan., 1967 [24 Jan., 1966], No. 3390/67. Heading B3V. [Also in Division C7] Titanium alloys containing in the annealed condition up to 25% of the beta phase at room temperature are heated to above the beta transus to achieve substantially complete transformation, quenched to partially transform the beta phase to alpha or to a martensitic phase which transforms to alpha on subsequent heating, and worked at a temperature sufficiently below the beta transus to effect spheroidization of the alpha grains. The initial heating, during which working may be effected, may be to a temperature between 50‹ and 100‹ F. above the transus, while quenching should be to at least 30‹ F. below the transus, and is preferably to ambient temperature. At least 50% deformation should then be effected, at a temperature not more than 400‹ F. below the beta transus, and this may be followed by a stress relief anneal at 1350‹ F. for 2 hours in the case of alpha-beta alloys, or at 1650-1675‹ F. for 1 hour followed by 1050-1100‹ F. for 8 hours and air-cooling in the case of alpha or lean beta alloys. Particular alloys referred to are Ti/ 2À5% Sn/5% Al, Ti/5% Al/5% Sn/5% 'Zr, Ti/ 7% Al/12% Zr, Ti/6% Al/4% V, Ti/8% Al/1% Mo/1% V, Ti/5% Al/5% Sn/5% Zr/1% Mo/1% V, while hot-working temperatures were in the range 1750-1875‹ F.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US52280066A | 1966-01-24 | 1966-01-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1141409A true GB1141409A (en) | 1969-01-29 |
Family
ID=24082407
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB339067A Expired GB1141409A (en) | 1966-01-24 | 1967-01-23 | Heat treatment and working of titanium alloys |
Country Status (3)
Country | Link |
---|---|
BE (1) | BE693096A (en) |
GB (1) | GB1141409A (en) |
SE (1) | SE342850B (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1076104A1 (en) * | 1999-08-12 | 2001-02-14 | The Boeing Company | Titanium alloy having enhanced notch toughness and method of producing same |
WO2010089256A1 (en) | 2009-02-05 | 2010-08-12 | Otto Fuchs Kg | Method for the beta annealing of a workpiece produced from a ti alloy |
CN111889598A (en) * | 2020-08-07 | 2020-11-06 | 攀钢集团攀枝花钛材有限公司江油分公司 | TC4 titanium alloy forged material and preparation method thereof |
-
1967
- 1967-01-17 SE SE67567A patent/SE342850B/xx unknown
- 1967-01-23 GB GB339067A patent/GB1141409A/en not_active Expired
- 1967-01-24 BE BE693096D patent/BE693096A/xx unknown
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1076104A1 (en) * | 1999-08-12 | 2001-02-14 | The Boeing Company | Titanium alloy having enhanced notch toughness and method of producing same |
EP2172576A1 (en) * | 1999-08-12 | 2010-04-07 | The Boeing Company | Titanium alloy having enhanced notch toughness and method of producing same |
WO2010089256A1 (en) | 2009-02-05 | 2010-08-12 | Otto Fuchs Kg | Method for the beta annealing of a workpiece produced from a ti alloy |
DE102009003430A1 (en) * | 2009-02-05 | 2010-09-23 | Otto Fuchs Kg | A method of heat treating a Ti alloy workpiece |
US8388776B2 (en) | 2009-02-05 | 2013-03-05 | Otto Fuchs Kg | Method for the β annealing of a work piece produced from a Ti alloy |
CN111889598A (en) * | 2020-08-07 | 2020-11-06 | 攀钢集团攀枝花钛材有限公司江油分公司 | TC4 titanium alloy forged material and preparation method thereof |
Also Published As
Publication number | Publication date |
---|---|
SE342850B (en) | 1972-02-21 |
BE693096A (en) | 1967-07-03 |
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