GB940057A - Production of structurally useful titanium metal products - Google Patents
Production of structurally useful titanium metal productsInfo
- Publication number
- GB940057A GB940057A GB1536162A GB1536162A GB940057A GB 940057 A GB940057 A GB 940057A GB 1536162 A GB1536162 A GB 1536162A GB 1536162 A GB1536162 A GB 1536162A GB 940057 A GB940057 A GB 940057A
- Authority
- GB
- United Kingdom
- Prior art keywords
- temperature
- mesh
- compact
- extrusion
- titanium metal
- 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
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/04—Making non-ferrous alloys by powder metallurgy
- C22C1/045—Alloys based on refractory metals
- C22C1/0458—Alloys based on titanium, zirconium or hafnium
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Lubricants (AREA)
- Extrusion Of Metal (AREA)
Abstract
In a process of fabricating titanium metal powder, ductile a titanium powder (99.5% purity) is compacted at a temperature below the a -b transition temperature (885 DEG C.) and the compact is then extruded at a reduction ratio of at least 10:1 at a temperature below said transformation temperature. The a titanium powder minus 14 mesh and preferably 30 mesh to 200 mesh is compacted either hydrostatically or mechanically at 10-75 t.s.i. to produce a compact of at least 80% theoretical density. The temperature of pressing may vary front room temperature to 90 DEG C. The green compact is coated with a lubricant such as colloidal graphite in oil, or other inorganic or organic lubricants and preferably heated to 400 DEG C.-600 DEG C. in argon prior to insertion in the heated extrusion die assembly. Extrusion is effected at 200 DEG C.-750 DEG C. at a reduction ratio of 10:1 to 50:1 at a maximum speed of 350 inches per minute. Either tubes or rods are produced by the extrusion. The green compact may be machined to the correct size of the container of the extrusion die before coating with the lubricant. U.S.A. Specifications 2,835,568, 2,847,297 and Canadian Specifications 591,701 and 591,785 are referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11252761A | 1961-05-25 | 1961-05-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB940057A true GB940057A (en) | 1963-10-23 |
Family
ID=22344373
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1536162A Expired GB940057A (en) | 1961-05-25 | 1962-04-19 | Production of structurally useful titanium metal products |
Country Status (2)
Country | Link |
---|---|
BE (1) | BE618147A (en) |
GB (1) | GB940057A (en) |
-
1962
- 1962-04-19 GB GB1536162A patent/GB940057A/en not_active Expired
- 1962-05-25 BE BE618147A patent/BE618147A/en unknown
Also Published As
Publication number | Publication date |
---|---|
BE618147A (en) | 1962-11-26 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1378216A (en) | Method of manufacturing a blade having a plurality of internal cooling channels | |
GB1380381A (en) | Method of manufacturing composite articles | |
GB1509675A (en) | Production of high density powdered metal parts | |
ES397558A1 (en) | Production of reflective metal flake pigments | |
GB1451168A (en) | Method for producing superconducting wire | |
GB1346439A (en) | Composite metal article | |
GB1317340A (en) | Production of tubing | |
GB1381037A (en) | Production of bevel gears | |
GB940057A (en) | Production of structurally useful titanium metal products | |
GB1095798A (en) | A method of producing bimetallic tubular bodies | |
GB847690A (en) | Method of manufacturing metallic articles of openwork honeycomb structure | |
GB1313370A (en) | Hot expanding of hollow metal billets | |
GB1373190A (en) | Zinc forging alloy and its heat treatment | |
GB909319A (en) | Solderable composite aluminium wire | |
WO1996021958A3 (en) | Non-vaporising getter and method of obtaining the same | |
FR2076088A7 (en) | Carbon fibre reinforced metal wire | |
SE8603563L (en) | PROCEDURE FOR THE PREPARATION OF POWDER METAL SURGICAL FORM | |
GB1400118A (en) | Method for the production of hollow powder metal articles | |
ES8600986A1 (en) | Process for manufacturing tubes by powder metallurgy and tubular work pieces obtained thereby (semi-products). | |
JPS56151890A (en) | Manufacture of internally stepped double heat pipe | |
GB879590A (en) | Improvements relating to the forming of sintered articles | |
GB1473341A (en) | Manufacturing superconductors | |
GB598423A (en) | Improvements in a method of compacting metal powder into complicated shapes | |
GB2016523A (en) | Producing a forging from porous metal pellets | |
GB868528A (en) | Thermoplastic connecting members for pipes and method of preparing them |