GB990022A - Improvements in alloys with a nickel-chromium base - Google Patents
Improvements in alloys with a nickel-chromium baseInfo
- Publication number
- GB990022A GB990022A GB353361A GB353361A GB990022A GB 990022 A GB990022 A GB 990022A GB 353361 A GB353361 A GB 353361A GB 353361 A GB353361 A GB 353361A GB 990022 A GB990022 A GB 990022A
- Authority
- GB
- United Kingdom
- Prior art keywords
- alloys
- nickel
- contents
- minutes
- hours
- 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
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Manufacture And Refinement Of Metals (AREA)
Abstract
A creep-resistant alloy contains in percentage by weight <FORM:0990022/C6-C7/1> the Ti and Al contents being such that Ti:Al lies within the range of 0.7:1, and (Ti+Al) is between the limits defined by Mo (0.15 Cr-2.7) + (25.6-0.9 Cr) and Mo (0.15 Cr-2.7) + (23.5-0.9 Cr), the Ti and Al contents being furthermore so controlled that Mo+2Al+4Ti is not less than 22. The molten alloy may be refined by holding under high vacuum for at least 5 minutes; exemplified is treatment for 90 minutes at 1500 DEG C. under a pressure not exceeding 200 microns. A heat treatment sequence referred to consists of 1 1/2 hours at 1200 DEG C. air cooling, 6 hours at 1050 DEG C. and again air cooling. The alloy may be used for turbine parts.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB353361A GB990022A (en) | 1961-01-30 | 1961-01-30 | Improvements in alloys with a nickel-chromium base |
DE1962J0021225 DE1231907B (en) | 1961-01-30 | 1962-01-29 | Use of a kneaded and aged nickel-chromium-cobalt alloy for objects with high impact strength |
CH111962A CH450734A (en) | 1961-01-30 | 1962-01-30 | Heat resistant alloy, nickel-chromium-cobalt-molybdenum |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB353361A GB990022A (en) | 1961-01-30 | 1961-01-30 | Improvements in alloys with a nickel-chromium base |
Publications (1)
Publication Number | Publication Date |
---|---|
GB990022A true GB990022A (en) | 1965-04-22 |
Family
ID=9760121
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB353361A Expired GB990022A (en) | 1961-01-30 | 1961-01-30 | Improvements in alloys with a nickel-chromium base |
Country Status (3)
Country | Link |
---|---|
CH (1) | CH450734A (en) |
DE (1) | DE1231907B (en) |
GB (1) | GB990022A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3042973A1 (en) * | 2015-01-07 | 2016-07-13 | Rolls-Royce plc | A nickel alloy |
US10266919B2 (en) | 2015-07-03 | 2019-04-23 | Rolls-Royce Plc | Nickel-base superalloy |
US10309229B2 (en) | 2014-01-09 | 2019-06-04 | Rolls-Royce Plc | Nickel based alloy composition |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB715140A (en) * | 1951-12-05 | 1954-09-08 | Mond Nickel Co Ltd | Improvements relating to heat-resisting alloys and articles and parts made therefrom |
GB733489A (en) * | 1952-07-09 | 1955-07-13 | Mond Nickel Co Ltd | Improvements relating to nickel-chromium-cobalt alloys |
GB814029A (en) * | 1956-10-29 | 1959-05-27 | Mond Nickel Co Ltd | Improvements in nickel-chromium-cobalt alloys |
-
1961
- 1961-01-30 GB GB353361A patent/GB990022A/en not_active Expired
-
1962
- 1962-01-29 DE DE1962J0021225 patent/DE1231907B/en active Pending
- 1962-01-30 CH CH111962A patent/CH450734A/en unknown
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10309229B2 (en) | 2014-01-09 | 2019-06-04 | Rolls-Royce Plc | Nickel based alloy composition |
EP3042973A1 (en) * | 2015-01-07 | 2016-07-13 | Rolls-Royce plc | A nickel alloy |
US10138534B2 (en) | 2015-01-07 | 2018-11-27 | Rolls-Royce Plc | Nickel alloy |
US10266919B2 (en) | 2015-07-03 | 2019-04-23 | Rolls-Royce Plc | Nickel-base superalloy |
US10422024B2 (en) | 2015-07-03 | 2019-09-24 | Rolls-Royce Plc | Nickel-base superalloy |
Also Published As
Publication number | Publication date |
---|---|
DE1231907B (en) | 1967-01-05 |
CH450734A (en) | 1968-01-31 |
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