GB889243A - Improvements in or relating to austenitic alloys - Google Patents
Improvements in or relating to austenitic alloysInfo
- Publication number
- GB889243A GB889243A GB6352/59A GB635259A GB889243A GB 889243 A GB889243 A GB 889243A GB 6352/59 A GB6352/59 A GB 6352/59A GB 635259 A GB635259 A GB 635259A GB 889243 A GB889243 A GB 889243A
- Authority
- GB
- United Kingdom
- Prior art keywords
- range
- hours
- alloy
- service
- followed
- 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
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
An alloy for service at elevated temperatures contains:- .C.\sO 0,15% .Si.\sO 1,5% .Mn.\sO 1,5% .Cr.10-20% .Al.0,5-4% Al+Ti lying within the range 2,5-7% .Ti.1,0-4,5% Al+Ti lying within the range 2,5-7% .Mo.1-8% .W.2-15% .V.\sO 1,5% .B.0,006-0,06% .Ni.30-55% .Fe.22-45% .Impurities (e.g. N2, P, S, Co, Cu).\sO 1,5% It is solution treated for 1/2 to 2 hours in the range 1750-2150 DEG F. and quenched in water, oil or air. For service at temperatures of about 1200 DEG F. the alloy is then given a double precipitation treatment consisting of 1/2 to 24 hours in the range 1450-1650 DEG F. followed by air cooling and then 1/2 to 24 hours in the range 1200-1400 DEG F., again followed by air cooling. For service at temperatures around 1500 DEG F., optimum stress rupture properties are developed by a single stage precipitation treatment of 1/2 to 24 hours in the range 1250-1450 DEG F. followed by air cooling. Use of the alloy for turbine parts is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US889243XA | 1958-02-24 | 1958-02-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB889243A true GB889243A (en) | 1962-02-14 |
Family
ID=22214304
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6352/59A Expired GB889243A (en) | 1958-02-24 | 1959-02-24 | Improvements in or relating to austenitic alloys |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB889243A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0040901A1 (en) * | 1980-05-28 | 1981-12-02 | Westinghouse Electric Corporation | Alloys |
EP0136998A1 (en) * | 1983-08-10 | 1985-04-10 | Voest-Alpine Stahl Aktiengesellschaft | Wrought nickel-base alloy and process for its thermal treatment |
-
1959
- 1959-02-24 GB GB6352/59A patent/GB889243A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0040901A1 (en) * | 1980-05-28 | 1981-12-02 | Westinghouse Electric Corporation | Alloys |
EP0136998A1 (en) * | 1983-08-10 | 1985-04-10 | Voest-Alpine Stahl Aktiengesellschaft | Wrought nickel-base alloy and process for its thermal treatment |
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