FR897709A - Process for cooling gas turbine blades - Google Patents
Process for cooling gas turbine bladesInfo
- Publication number
- FR897709A FR897709A FR897709DA FR897709A FR 897709 A FR897709 A FR 897709A FR 897709D A FR897709D A FR 897709DA FR 897709 A FR897709 A FR 897709A
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- cooling gas
- turbine blades
- blades
- cooling
- 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
-
- 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
- F01D5/185—Liquid cooling
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE897709X | 1942-06-09 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR897709A true FR897709A (en) | 1945-03-29 |
Family
ID=6848808
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR897709D Expired FR897709A (en) | 1942-06-09 | 1943-06-22 | Process for cooling gas turbine blades |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR897709A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2746671A (en) * | 1950-04-14 | 1956-05-22 | United Aircraft Corp | Compressor deicing and thrust balancing arrangement |
US2847185A (en) * | 1953-04-13 | 1958-08-12 | Rolls Royce | Hollow blading with means to supply fluid thereinto for turbines or compressors |
US2866618A (en) * | 1953-02-13 | 1958-12-30 | Thomas W Jackson | Reverse flow air cooled turbine blade |
US2868500A (en) * | 1949-02-15 | 1959-01-13 | Boulet George | Cooling of blades in machines where blading is employed |
US2920866A (en) * | 1954-12-20 | 1960-01-12 | A V Roe Canada Ltd | Hollow air cooled sheet metal turbine blade |
US3051439A (en) * | 1958-06-18 | 1962-08-28 | Rolls Royce | Blades for gas turbine engines |
FR2358546A1 (en) * | 1976-07-12 | 1978-02-10 | Gen Electric | BLADE END STRUCTURE FOR OPEN CIRCUIT LIQUID-COOLED TURBINE |
FR2476744A1 (en) * | 1980-02-22 | 1981-08-28 | Gen Electric | MOBILE TURBINE GAS TURBINE COOLED BY LIQUID AND CONTRE-CURRENT STEAM |
-
1943
- 1943-06-22 FR FR897709D patent/FR897709A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2868500A (en) * | 1949-02-15 | 1959-01-13 | Boulet George | Cooling of blades in machines where blading is employed |
US2746671A (en) * | 1950-04-14 | 1956-05-22 | United Aircraft Corp | Compressor deicing and thrust balancing arrangement |
US2866618A (en) * | 1953-02-13 | 1958-12-30 | Thomas W Jackson | Reverse flow air cooled turbine blade |
US2847185A (en) * | 1953-04-13 | 1958-08-12 | Rolls Royce | Hollow blading with means to supply fluid thereinto for turbines or compressors |
US2920866A (en) * | 1954-12-20 | 1960-01-12 | A V Roe Canada Ltd | Hollow air cooled sheet metal turbine blade |
US3051439A (en) * | 1958-06-18 | 1962-08-28 | Rolls Royce | Blades for gas turbine engines |
FR2358546A1 (en) * | 1976-07-12 | 1978-02-10 | Gen Electric | BLADE END STRUCTURE FOR OPEN CIRCUIT LIQUID-COOLED TURBINE |
FR2476744A1 (en) * | 1980-02-22 | 1981-08-28 | Gen Electric | MOBILE TURBINE GAS TURBINE COOLED BY LIQUID AND CONTRE-CURRENT STEAM |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR918158A (en) | Improvements to gas turbines | |
FR897709A (en) | Process for cooling gas turbine blades | |
FR895652A (en) | Installation of gas turbines | |
FR896166A (en) | Guide vane support for steam and gas turbines, especially for high pressures and high temperatures | |
FR896203A (en) | Guide vane supports for steam or gas turbines | |
FR897716A (en) | Cooled gas turbine | |
FR897710A (en) | Gas turbine cooled rotor | |
FR912791A (en) | Sealed box for steam and gas turbines working at high temperatures | |
FR870124A (en) | Turbine rotor of ceramic materials, in particular for gas turbines | |
FR905735A (en) | Method and apparatus for manufacturing turbo-machine blades | |
FR903268A (en) | Rotor of ceramic materials, in particular for gas turbines | |
FR881104A (en) | Method of using gas turbines | |
FR895583A (en) | Drive wheel or rotor for cooled gas turbines | |
FR977824A (en) | Starting device for gas turbine powertrains | |
FR977692A (en) | Improvements to gas turbine heat engines | |
FR902328A (en) | Stator for exhaust gas turbine | |
FR51723E (en) | Rotor vane for exhaust gas turbines | |
FR903215A (en) | Moderator for gas and air lines | |
FR892504A (en) | Turbine blade, in particular for gas turbines | |
FR892691A (en) | Cantilever turbine, especially for hot gases | |
FR847942A (en) | Full blade cooling device for exhaust gas turbines | |
FR897352A (en) | Inverter shutdown process | |
FR911454A (en) | Fireplace for gas turbine installations | |
FR838088A (en) | Operating process for gas turbines and gas turbines for carrying out this process | |
FR897024A (en) | Eyepiece for gas masks |