IT1058520B - Apparecchio per il raffreddamento di un motore a turbina a gas - Google Patents
Apparecchio per il raffreddamento di un motore a turbina a gasInfo
- Publication number
- IT1058520B IT1058520B IT21541/76A IT2154176A IT1058520B IT 1058520 B IT1058520 B IT 1058520B IT 21541/76 A IT21541/76 A IT 21541/76A IT 2154176 A IT2154176 A IT 2154176A IT 1058520 B IT1058520 B IT 1058520B
- Authority
- IT
- Italy
- Prior art keywords
- cooling
- gas turbine
- turbine engine
- engine
- gas
- Prior art date
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
- 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 (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/561,713 US3957391A (en) | 1975-03-25 | 1975-03-25 | Turbine cooling |
Publications (1)
Publication Number | Publication Date |
---|---|
IT1058520B true IT1058520B (it) | 1982-05-10 |
Family
ID=24243114
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT21541/76A IT1058520B (it) | 1975-03-25 | 1976-03-24 | Apparecchio per il raffreddamento di un motore a turbina a gas |
Country Status (2)
Country | Link |
---|---|
US (1) | US3957391A (it) |
IT (1) | IT1058520B (it) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4069662A (en) * | 1975-12-05 | 1978-01-24 | United Technologies Corporation | Clearance control for gas turbine engine |
US4314792A (en) * | 1978-12-20 | 1982-02-09 | United Technologies Corporation | Turbine seal and vane damper |
US4279123A (en) * | 1978-12-20 | 1981-07-21 | United Technologies Corporation | External gas turbine engine cooling for clearance control |
US4513567A (en) * | 1981-11-02 | 1985-04-30 | United Technologies Corporation | Gas turbine engine active clearance control |
GB2245314B (en) * | 1983-05-26 | 1992-04-22 | Rolls Royce | Cooling of gas turbine engine shroud rings |
US4566851A (en) * | 1984-05-11 | 1986-01-28 | United Technologies Corporation | First stage turbine vane support structure |
US4655682A (en) * | 1985-09-30 | 1987-04-07 | United Technologies Corporation | Compressor stator assembly having a composite inner diameter shroud |
DE3606597C1 (de) * | 1986-02-28 | 1987-02-19 | Mtu Muenchen Gmbh | Schaufel- und Dichtspaltoptimierungseinrichtung fuer Verdichter von Gasturbinentriebwerken |
US4721434A (en) * | 1986-12-03 | 1988-01-26 | United Technologies Corporation | Damping means for a stator |
EP3011140B1 (en) | 2013-06-17 | 2021-05-26 | Raytheon Technologies Corporation | Gas turbine engine component with rib support |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2427244A (en) * | 1944-03-07 | 1947-09-09 | Gen Electric | Gas turbine |
GB641144A (en) * | 1948-07-16 | 1950-08-02 | Bristol Aeroplane Co Ltd | Improvements in or relating to blade-fixing means for compressors, fans, turbines orthe like |
DE1213423B (de) * | 1960-06-04 | 1966-03-31 | Maschf Augsburg Nuernberg Ag | Befestigung der Schaufeln eines Leitschaufel-kranzes einer Stroemungsmaschine am Leitschaufeltraeger mittels gummielastischer Elemente |
US3423071A (en) * | 1967-07-17 | 1969-01-21 | United Aircraft Corp | Turbine vane retention |
US3781125A (en) * | 1972-04-07 | 1973-12-25 | Westinghouse Electric Corp | Gas turbine nozzle vane structure |
US3836279A (en) * | 1973-02-23 | 1974-09-17 | United Aircraft Corp | Seal means for blade and shroud |
-
1975
- 1975-03-25 US US05/561,713 patent/US3957391A/en not_active Expired - Lifetime
-
1976
- 1976-03-24 IT IT21541/76A patent/IT1058520B/it active
Also Published As
Publication number | Publication date |
---|---|
US3957391A (en) | 1976-05-18 |
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