FR2305596A1 - Systeme de refroidissement pour turbine - Google Patents
Systeme de refroidissement pour turbineInfo
- Publication number
- FR2305596A1 FR2305596A1 FR7608460A FR7608460A FR2305596A1 FR 2305596 A1 FR2305596 A1 FR 2305596A1 FR 7608460 A FR7608460 A FR 7608460A FR 7608460 A FR7608460 A FR 7608460A FR 2305596 A1 FR2305596 A1 FR 2305596A1
- Authority
- FR
- France
- Prior art keywords
- cooling system
- turbine cooling
- turbine
- 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.)
- Granted
Links
- 238000001816 cooling Methods 0.000 title 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/561,713 US3957391A (en) | 1975-03-25 | 1975-03-25 | Turbine cooling |
US05/561,712 US3992126A (en) | 1975-03-25 | 1975-03-25 | Turbine cooling |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2305596A1 true FR2305596A1 (fr) | 1976-10-22 |
FR2305596B1 FR2305596B1 (fr) | 1982-04-09 |
Family
ID=27072720
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7608460A Granted FR2305596A1 (fr) | 1975-03-25 | 1976-03-24 | Systeme de refroidissement pour turbine |
Country Status (6)
Country | Link |
---|---|
JP (1) | JPS51119417A (fr) |
DE (1) | DE2612729A1 (fr) |
FR (1) | FR2305596A1 (fr) |
GB (1) | GB1538614A (fr) |
IL (1) | IL49165A (fr) |
SE (1) | SE411931B (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5127793A (en) * | 1990-05-31 | 1992-07-07 | General Electric Company | Turbine shroud clearance control assembly |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2738949A (en) * | 1950-06-29 | 1956-03-20 | Rolls Royce | Gas-turbine engines and nozzle-guide-vane assemblies therefor |
FR1297645A (fr) * | 1960-08-16 | 1962-06-29 | United Aircraft Corp | Perfectionnements apportés aux turbines à gaz |
US3295824A (en) * | 1966-05-06 | 1967-01-03 | United Aircraft Corp | Turbine vane seal |
US3314648A (en) * | 1961-12-19 | 1967-04-18 | Gen Electric | Stator vane assembly |
FR1519159A (fr) * | 1966-04-18 | 1968-03-29 | Rolls Royce | Perfectionnements aux machines à aubes de guidage pour l'écoulement de fluide |
FR1576055A (fr) * | 1967-07-17 | 1969-07-25 | ||
US3730640A (en) * | 1971-06-28 | 1973-05-01 | United Aircraft Corp | Seal ring for gas turbine |
FR2179455A5 (fr) * | 1972-04-07 | 1973-11-16 | Westinghouse Electric Corp | |
US3807891A (en) * | 1972-09-15 | 1974-04-30 | United Aircraft Corp | Thermal response turbine shroud |
US3836279A (en) * | 1973-02-23 | 1974-09-17 | United Aircraft Corp | Seal means for blade and shroud |
FR2284754A1 (fr) * | 1974-09-13 | 1976-04-09 | Rolls Royce | Element de stator de moteur a turbine a gaz |
-
1976
- 1976-02-27 SE SE7602652A patent/SE411931B/xx unknown
- 1976-03-05 IL IL49165A patent/IL49165A/en unknown
- 1976-03-23 GB GB11614/76A patent/GB1538614A/en not_active Expired
- 1976-03-24 FR FR7608460A patent/FR2305596A1/fr active Granted
- 1976-03-25 JP JP51032053A patent/JPS51119417A/ja active Pending
- 1976-03-25 DE DE19762612729 patent/DE2612729A1/de not_active Withdrawn
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2738949A (en) * | 1950-06-29 | 1956-03-20 | Rolls Royce | Gas-turbine engines and nozzle-guide-vane assemblies therefor |
FR1297645A (fr) * | 1960-08-16 | 1962-06-29 | United Aircraft Corp | Perfectionnements apportés aux turbines à gaz |
US3314648A (en) * | 1961-12-19 | 1967-04-18 | Gen Electric | Stator vane assembly |
FR1519159A (fr) * | 1966-04-18 | 1968-03-29 | Rolls Royce | Perfectionnements aux machines à aubes de guidage pour l'écoulement de fluide |
US3295824A (en) * | 1966-05-06 | 1967-01-03 | United Aircraft Corp | Turbine vane seal |
FR1576055A (fr) * | 1967-07-17 | 1969-07-25 | ||
US3730640A (en) * | 1971-06-28 | 1973-05-01 | United Aircraft Corp | Seal ring for gas turbine |
FR2179455A5 (fr) * | 1972-04-07 | 1973-11-16 | Westinghouse Electric Corp | |
US3807891A (en) * | 1972-09-15 | 1974-04-30 | United Aircraft Corp | Thermal response turbine shroud |
US3836279A (en) * | 1973-02-23 | 1974-09-17 | United Aircraft Corp | Seal means for blade and shroud |
FR2284754A1 (fr) * | 1974-09-13 | 1976-04-09 | Rolls Royce | Element de stator de moteur a turbine a gaz |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5127793A (en) * | 1990-05-31 | 1992-07-07 | General Electric Company | Turbine shroud clearance control assembly |
Also Published As
Publication number | Publication date |
---|---|
DE2612729A1 (de) | 1976-10-14 |
GB1538614A (en) | 1979-01-24 |
FR2305596B1 (fr) | 1982-04-09 |
IL49165A0 (en) | 1976-05-31 |
SE411931B (sv) | 1980-02-11 |
IL49165A (en) | 1977-12-30 |
SE7602652L (sv) | 1976-09-26 |
JPS51119417A (en) | 1976-10-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |