GB761369A - Cobalt-base alloy and its manufacturing process - Google Patents
Cobalt-base alloy and its manufacturing processInfo
- Publication number
- GB761369A GB761369A GB25500/53A GB2550053A GB761369A GB 761369 A GB761369 A GB 761369A GB 25500/53 A GB25500/53 A GB 25500/53A GB 2550053 A GB2550053 A GB 2550053A GB 761369 A GB761369 A GB 761369A
- Authority
- GB
- United Kingdom
- Prior art keywords
- per cent
- alloy
- temperature
- forms
- cobalt
- 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
- C22C19/07—Alloys based on nickel or cobalt based on cobalt
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Powder Metallurgy (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
A cast alloy for use at high temperatures consists of: Co at least 39 per cent, Cr 20-35 per cent, Mo 5-20 per cent, W 0-10 per cent, Ni 3-15 per cent, C 0.3-1.2 per cent, Ti 0-0.5 per cent, Zr 0.05-0.3 per cent. Si 0.5-2 per cent, Mn 0.5-1.2 per cent (the total less than 3 per cent). Fe less than 6 per cent., the cobalt-base solid solution being present simultaneously in two allotropic forms, viz. the a and b forms, and the relative proportions of the two forms being stable at the temperature of use. The proportions of the a -promoting elements Ni, Fe and C and the b -promoting elements Cr and Mo are preferably such that the a and b forms are present in the alloy in substantially equal amounts, i.e. the atomic proportions of Co, the a -promoters and the b -promoters are preferably 9:1.5-2:7 respectively. The relative proportion of the allotropic forms is rendered constant at the temperature of use by casting the alloy into preheated moulds and maintaining the alloy in the moulds at a temperature in the region of the future working temperature for at least 24 hours. The alloy may be subsequently subjected to a mechanical strain at a temperature equal to or greater than the working temperature.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR761369X | 1952-09-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB761369A true GB761369A (en) | 1956-11-14 |
Family
ID=9172818
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB25500/53A Expired GB761369A (en) | 1952-09-16 | 1953-09-15 | Cobalt-base alloy and its manufacturing process |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB761369A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3312505A1 (en) * | 1982-04-07 | 1983-10-20 | Mitsubishi Kinzoku K.K., Tokyo | COBALT ALLOY FOR BUILD-UP WELDING WITH IMPROVED RESISTANCE TO WELDING CRACKS |
-
1953
- 1953-09-15 GB GB25500/53A patent/GB761369A/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3312505A1 (en) * | 1982-04-07 | 1983-10-20 | Mitsubishi Kinzoku K.K., Tokyo | COBALT ALLOY FOR BUILD-UP WELDING WITH IMPROVED RESISTANCE TO WELDING CRACKS |
GB2120276A (en) * | 1982-04-07 | 1983-11-30 | Mitsubishi Metal Corp | Cobalt alloy for build-up welding having improved resistance to weld crack |
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