GB749909A - Improvements in or relating to the hot working of nickel chromium alloy materials - Google Patents
Improvements in or relating to the hot working of nickel chromium alloy materialsInfo
- Publication number
- GB749909A GB749909A GB191953A GB191953A GB749909A GB 749909 A GB749909 A GB 749909A GB 191953 A GB191953 A GB 191953A GB 191953 A GB191953 A GB 191953A GB 749909 A GB749909 A GB 749909A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blank
- nickel
- extrusion
- forging
- working
- 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
- C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt 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)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
- Electroplating Methods And Accessories (AREA)
Abstract
749,909. Forging; extruding. ROLLSROYCE, Ltd. Feb. 9, 1954 [Jan. 22, 1953], No. 1919/53. Classes 83 (2) and 83 (4). In the hot working of a blank formed from a nickel-chrome alloy, the blank is thinly coated with nickel prior to heating. The hot working may comprise extruding or forging and the nickel coating acts as a lubricant between the blank and the forming dies and protects the surface of the blank from oxidation, thus preventing scale formation and enabling higher working temperatures to be used. The coating is preferably applied by electrodeposition. Making turbine blades.-In the manufacture of a gas turbine blade, a blank of nickel-chrome alloy containing titanium and aluminium, is produced by upsetting, swaging or extrusion and is then machined in a lathe or grinder to provide a good surface finish. The blank is then plated to a depth of 0.001-0.003 inch, heated and forged to shape. The forging may be repeated with reheating. Where the blank is produced by extrusion the metal slug may be coated with nickel prior to extrusion. The nickel coating is subsequently removed by mechanical polishing or by electro-polishing. Working at specifced temperatures.-The hot extrusion or forging operation is performed at a temperature of 1120-1200‹ C. Specification 734,210 is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB191953A GB749909A (en) | 1953-01-22 | 1953-01-22 | Improvements in or relating to the hot working of nickel chromium alloy materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB191953A GB749909A (en) | 1953-01-22 | 1953-01-22 | Improvements in or relating to the hot working of nickel chromium alloy materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB749909A true GB749909A (en) | 1956-06-06 |
Family
ID=9730322
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB191953A Expired GB749909A (en) | 1953-01-22 | 1953-01-22 | Improvements in or relating to the hot working of nickel chromium alloy materials |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB749909A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1078520B (en) * | 1956-04-25 | 1960-03-31 | Comptoir Ind Etirage | Process for lubrication during hot extrusion of metals or metal alloys that are difficult to compress |
| US2947076A (en) * | 1956-12-21 | 1960-08-02 | Rolls Royce | Manufacture of turbine blades |
| EP0248757A1 (en) * | 1986-06-02 | 1987-12-09 | United Technologies Corporation | Nickel base superalloy articles and method for making |
| WO2015088859A3 (en) * | 2013-12-10 | 2015-12-10 | Lei Chen | Electrodeposited nickel-chromium alloy |
| US10378118B2 (en) | 2013-12-11 | 2019-08-13 | United Technologies Corporation | Electroformed nickel-chromium alloy |
| US10669851B2 (en) | 2013-12-10 | 2020-06-02 | Raytheon Technologies Corporation | Nickel-chromium-aluminum composite by electrodeposition |
-
1953
- 1953-01-22 GB GB191953A patent/GB749909A/en not_active Expired
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1078520B (en) * | 1956-04-25 | 1960-03-31 | Comptoir Ind Etirage | Process for lubrication during hot extrusion of metals or metal alloys that are difficult to compress |
| US2947076A (en) * | 1956-12-21 | 1960-08-02 | Rolls Royce | Manufacture of turbine blades |
| EP0248757A1 (en) * | 1986-06-02 | 1987-12-09 | United Technologies Corporation | Nickel base superalloy articles and method for making |
| WO2015088859A3 (en) * | 2013-12-10 | 2015-12-10 | Lei Chen | Electrodeposited nickel-chromium alloy |
| US10669851B2 (en) | 2013-12-10 | 2020-06-02 | Raytheon Technologies Corporation | Nickel-chromium-aluminum composite by electrodeposition |
| US10669867B2 (en) | 2013-12-10 | 2020-06-02 | Raytheon Technologies Corporation | Electrodeposited nickel-chromium alloy |
| US10378118B2 (en) | 2013-12-11 | 2019-08-13 | United Technologies Corporation | Electroformed nickel-chromium alloy |
| US11732372B2 (en) | 2013-12-11 | 2023-08-22 | Raytheon Technologies Corporation | Electroformed nickel-chromium alloy |
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