CA1133366A - Method of selective grain growth in nickel-base superalloys by controlled boron diffusion - Google Patents
Method of selective grain growth in nickel-base superalloys by controlled boron diffusionInfo
- Publication number
- CA1133366A CA1133366A CA341,220A CA341220A CA1133366A CA 1133366 A CA1133366 A CA 1133366A CA 341220 A CA341220 A CA 341220A CA 1133366 A CA1133366 A CA 1133366A
- Authority
- CA
- Canada
- Prior art keywords
- boron
- article
- carbon
- grain growth
- nickel
- 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
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C8/00—Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
- C23C8/04—Treatment of selected surface areas, e.g. using masks
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/005—Selecting particular materials
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Crystallography & Structural Chemistry (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Powder Metallurgy (AREA)
- Heat Treatment Of Nonferrous Metals Or Alloys (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US97004778A | 1978-12-15 | 1978-12-15 | |
US970,047 | 1978-12-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1133366A true CA1133366A (en) | 1982-10-12 |
Family
ID=25516358
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA341,220A Expired CA1133366A (en) | 1978-12-15 | 1979-12-04 | Method of selective grain growth in nickel-base superalloys by controlled boron diffusion |
Country Status (9)
Country | Link |
---|---|
JP (1) | JPS5582757A (enrdf_load_stackoverflow) |
BE (1) | BE880645A (enrdf_load_stackoverflow) |
CA (1) | CA1133366A (enrdf_load_stackoverflow) |
CH (1) | CH648866A5 (enrdf_load_stackoverflow) |
DE (1) | DE2949673A1 (enrdf_load_stackoverflow) |
FR (1) | FR2444086A1 (enrdf_load_stackoverflow) |
GB (1) | GB2043116A (enrdf_load_stackoverflow) |
IT (1) | IT1126062B (enrdf_load_stackoverflow) |
NL (1) | NL7908902A (enrdf_load_stackoverflow) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0196447B1 (de) * | 1985-03-15 | 1989-08-09 | BBC Brown Boveri AG | Verfahren zur Erhöhung des Oxydations- und Korrosionswiderstandes eines Bauteils aus einer dispersionsgehärteten Superlegierung durch eine Oberflächenbehandlung |
EP0214080A3 (en) * | 1985-08-16 | 1987-11-25 | United Technologies Corporation | Reduction of twinning in directional recrystallization of nickel base superalloys |
JP6685800B2 (ja) | 2016-03-31 | 2020-04-22 | 三菱重工業株式会社 | タービン翼の設計方法、タービン翼の製造方法及びタービン翼 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1127157A (en) * | 1966-06-13 | 1968-09-11 | Orenda Ltd | Method for improving the fatigue resistance of turbine blades |
FR1528328A (fr) * | 1966-06-21 | 1968-06-07 | Int Nickel Ltd | Affinage du grain de métaux |
US3597286A (en) * | 1968-02-23 | 1971-08-03 | Westinghouse Electric Corp | Method of treating a high strength high ductility iron-cobalt alloy |
US3741821A (en) * | 1971-05-10 | 1973-06-26 | United Aircraft Corp | Processing for integral gas turbine disc/blade component |
US4078951A (en) * | 1976-03-31 | 1978-03-14 | University Patents, Inc. | Method of improving fatigue life of cast nickel based superalloys and composition |
US4093476A (en) * | 1976-12-22 | 1978-06-06 | Special Metals Corporation | Nickel base alloy |
-
1979
- 1979-12-04 CA CA341,220A patent/CA1133366A/en not_active Expired
- 1979-12-04 GB GB7941819A patent/GB2043116A/en not_active Withdrawn
- 1979-12-11 NL NL7908902A patent/NL7908902A/nl not_active Application Discontinuation
- 1979-12-11 DE DE19792949673 patent/DE2949673A1/de active Granted
- 1979-12-14 JP JP16170579A patent/JPS5582757A/ja active Granted
- 1979-12-14 IT IT41681/79A patent/IT1126062B/it active
- 1979-12-14 FR FR7930742A patent/FR2444086A1/fr not_active Withdrawn
- 1979-12-14 BE BE0/198587A patent/BE880645A/fr not_active IP Right Cessation
- 1979-12-14 CH CH11125/79A patent/CH648866A5/de not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
IT7941681A0 (it) | 1979-12-14 |
GB2043116A (en) | 1980-10-01 |
DE2949673C2 (enrdf_load_stackoverflow) | 1989-06-22 |
BE880645A (fr) | 1980-06-16 |
CH648866A5 (de) | 1985-04-15 |
FR2444086A1 (fr) | 1980-07-11 |
IT1126062B (it) | 1986-05-14 |
JPS6344816B2 (enrdf_load_stackoverflow) | 1988-09-07 |
NL7908902A (nl) | 1980-06-17 |
JPS5582757A (en) | 1980-06-21 |
DE2949673A1 (de) | 1980-06-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MKEX | Expiry |