GB1193774A - Nickel-Chromium-Cobalt-Aluminium Alloy - Google Patents
Nickel-Chromium-Cobalt-Aluminium AlloyInfo
- Publication number
- GB1193774A GB1193774A GB1648868A GB1648868A GB1193774A GB 1193774 A GB1193774 A GB 1193774A GB 1648868 A GB1648868 A GB 1648868A GB 1648868 A GB1648868 A GB 1648868A GB 1193774 A GB1193774 A GB 1193774A
- Authority
- GB
- United Kingdom
- Prior art keywords
- nickel
- cobalt
- chromium
- aluminium alloy
- april
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B01—PHYSICAL OR CHEMICAL PROCESSES OR APPARATUS IN GENERAL
- B01D—SEPARATION
- B01D19/00—Degasification of liquids
- B01D19/02—Foam dispersion or prevention
-
- 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
- C22C19/058—Alloys based on nickel or cobalt based on nickel with chromium without Mo and W
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01M—LUBRICATING OF MACHINES OR ENGINES IN GENERAL; LUBRICATING INTERNAL COMBUSTION ENGINES; CRANKCASE VENTILATING
- F01M11/00—Component parts, details or accessories, not provided for in, or of interest apart from, groups F01M1/00 - F01M9/00
- F01M11/08—Separating lubricant from air or fuel-air mixture before entry into cylinder
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Dispersion Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1,193,774. Nickel base alloys. ROLLSROYCE Ltd. April 2, 1969 [April 5, 1968], No. 16488/68. Heading C7A. A nickel base alloy, especially suitable for blades or vanes in gas turbine engines, comprises:- the balance, apart from impurities and residual deoxidizers, being Ni, and is so proportioned that the "F" factor Cr + Co/3 = 17À5-20% and Al + Ti +Nb + Ta is in the range 12À25 - 0À15F to 13À275- 0À15F.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1648868A GB1193774A (en) | 1968-04-05 | 1968-04-05 | Nickel-Chromium-Cobalt-Aluminium Alloy |
FR6909108A FR2005594A1 (en) | 1968-04-05 | 1969-03-27 | Nickel chromium cobalt aluminium alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1648868A GB1193774A (en) | 1968-04-05 | 1968-04-05 | Nickel-Chromium-Cobalt-Aluminium Alloy |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1193774A true GB1193774A (en) | 1970-06-03 |
Family
ID=10078255
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1648868A Expired GB1193774A (en) | 1968-04-05 | 1968-04-05 | Nickel-Chromium-Cobalt-Aluminium Alloy |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2005594A1 (en) |
GB (1) | GB1193774A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2457907A1 (en) * | 1979-05-29 | 1980-12-26 | Howmet Turbine Components | COATING COMPOSITION FOR PROTECTION AGAINST HIGH TEMPERATURE OXIDATION OF SUPER-ALLOYS AND COMPONENTS OF SUPER-ALLOYS THUS COATED |
-
1968
- 1968-04-05 GB GB1648868A patent/GB1193774A/en not_active Expired
-
1969
- 1969-03-27 FR FR6909108A patent/FR2005594A1/en not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2457907A1 (en) * | 1979-05-29 | 1980-12-26 | Howmet Turbine Components | COATING COMPOSITION FOR PROTECTION AGAINST HIGH TEMPERATURE OXIDATION OF SUPER-ALLOYS AND COMPONENTS OF SUPER-ALLOYS THUS COATED |
Also Published As
Publication number | Publication date |
---|---|
FR2005594A1 (en) | 1969-12-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PLE | Entries relating assignments, transmissions, licences in the register of patents | ||
PLNP | Patent lapsed through nonpayment of renewal fees |