GB1482692A - Manufacture of fluid-cooled gas turbine buckets - Google Patents
Manufacture of fluid-cooled gas turbine bucketsInfo
- Publication number
- GB1482692A GB1482692A GB41272/74A GB4127274A GB1482692A GB 1482692 A GB1482692 A GB 1482692A GB 41272/74 A GB41272/74 A GB 41272/74A GB 4127274 A GB4127274 A GB 4127274A GB 1482692 A GB1482692 A GB 1482692A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- cooled gas
- fluid
- manufacture
- skin
- 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
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
-
- 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
- C23C24/00—Coating starting from inorganic powder
- C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
- C23C24/10—Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
-
- 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/18—After-treatment
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/182—Transpiration cooling
- F01D5/183—Blade walls being porous
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
- F01D5/187—Convection cooling
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1482692 Cooled gas turbine rotor blades GENERAL ELECTRIC CO 23 Sept 1974 [24 Sept 1973] 41272/74 Addition to 1402391 Heading F1T [Also in Division B3] A fluid-cooled gas turbine rotor blade 10 comprises a blade core 12 having a plurality of grooves 13 and a skin 11 in accordance with Specification 1402391 the material selected for temporarily occupying the grooves during manufacture does not actively alloy with the material selected for the skin and the core material, and the core surface is covered by at least one rigid layer of material selected for the skin.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00400137A US3848307A (en) | 1972-04-03 | 1973-09-24 | Manufacture of fluid-cooled gas turbine airfoils |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1482692A true GB1482692A (en) | 1977-08-10 |
Family
ID=23582371
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB41272/74A Expired GB1482692A (en) | 1973-09-24 | 1974-09-23 | Manufacture of fluid-cooled gas turbine buckets |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS5076422A (en) |
FR (1) | FR2244908B2 (en) |
GB (1) | GB1482692A (en) |
IT (1) | IT1022212B (en) |
NL (1) | NL7412547A (en) |
NO (1) | NO743382L (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4623087A (en) * | 1983-05-26 | 1986-11-18 | Rolls-Royce Limited | Application of coatings to articles |
GB2246174A (en) * | 1982-06-29 | 1992-01-22 | Rolls Royce | Cooled aerofoil for a gas turbine engine |
-
1974
- 1974-09-19 NO NO743382A patent/NO743382L/no unknown
- 1974-09-23 GB GB41272/74A patent/GB1482692A/en not_active Expired
- 1974-09-23 NL NL7412547A patent/NL7412547A/en not_active Application Discontinuation
- 1974-09-23 IT IT27584/74A patent/IT1022212B/en active
- 1974-09-24 FR FR7432219A patent/FR2244908B2/fr not_active Expired
- 1974-09-24 JP JP49109861A patent/JPS5076422A/ja active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2246174A (en) * | 1982-06-29 | 1992-01-22 | Rolls Royce | Cooled aerofoil for a gas turbine engine |
GB2246174B (en) * | 1982-06-29 | 1992-04-15 | Rolls Royce | A cooled aerofoil for a gas turbine engine |
US4623087A (en) * | 1983-05-26 | 1986-11-18 | Rolls-Royce Limited | Application of coatings to articles |
Also Published As
Publication number | Publication date |
---|---|
FR2244908A2 (en) | 1975-04-18 |
NO743382L (en) | 1975-04-21 |
IT1022212B (en) | 1978-03-20 |
FR2244908B2 (en) | 1978-06-09 |
NL7412547A (en) | 1975-03-26 |
JPS5076422A (en) | 1975-06-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |