FR2295238A1 - Systeme et methode pour le refroidissement des aubes d'une turbine - Google Patents
Systeme et methode pour le refroidissement des aubes d'une turbineInfo
- Publication number
- FR2295238A1 FR2295238A1 FR7538265A FR7538265A FR2295238A1 FR 2295238 A1 FR2295238 A1 FR 2295238A1 FR 7538265 A FR7538265 A FR 7538265A FR 7538265 A FR7538265 A FR 7538265A FR 2295238 A1 FR2295238 A1 FR 2295238A1
- Authority
- FR
- France
- Prior art keywords
- turbine
- 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.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
- F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
-
- 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
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/534,620 US3936215A (en) | 1974-12-20 | 1974-12-20 | Turbine vane cooling |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2295238A1 true FR2295238A1 (fr) | 1976-07-16 |
Family
ID=24130851
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7538265A Withdrawn FR2295238A1 (fr) | 1974-12-20 | 1975-12-15 | Systeme et methode pour le refroidissement des aubes d'une turbine |
Country Status (7)
Country | Link |
---|---|
US (1) | US3936215A (fr) |
BE (1) | BE836802A (fr) |
CA (1) | CA1045040A (fr) |
DE (1) | DE2554010A1 (fr) |
FR (1) | FR2295238A1 (fr) |
GB (1) | GB1534000A (fr) |
SE (1) | SE7513778L (fr) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3310529A1 (de) * | 1982-03-23 | 1996-10-31 | Snecma | Vorrichtung zum Kühlen des Rotors einer Gasturbine |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3980411A (en) * | 1975-10-20 | 1976-09-14 | United Technologies Corporation | Aerodynamic seal for a rotary machine |
FR2370171A1 (fr) * | 1976-11-05 | 1978-06-02 | Snecma | Procede et dispositif pour la diminution du bruit des turbomachines |
GB1561229A (en) * | 1977-02-18 | 1980-02-13 | Rolls Royce | Gas turbine engine cooling system |
US4236869A (en) * | 1977-12-27 | 1980-12-02 | United Technologies Corporation | Gas turbine engine having bleed apparatus with dynamic pressure recovery |
GB2075123B (en) * | 1980-05-01 | 1983-11-16 | Gen Electric | Turbine cooling air deswirler |
US4416111A (en) * | 1981-02-25 | 1983-11-22 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Air modulation apparatus |
US4435123A (en) * | 1982-04-19 | 1984-03-06 | United Technologies Corporation | Cooling system for turbines |
US4708588A (en) * | 1984-12-14 | 1987-11-24 | United Technologies Corporation | Turbine cooling air supply system |
US4674955A (en) * | 1984-12-21 | 1987-06-23 | The Garrett Corporation | Radial inboard preswirl system |
US4759688A (en) * | 1986-12-16 | 1988-07-26 | Allied-Signal Inc. | Cooling flow side entry for cooled turbine blading |
US4822244A (en) * | 1987-10-15 | 1989-04-18 | United Technologies Corporation | Tobi |
US5232335A (en) * | 1991-10-30 | 1993-08-03 | General Electric Company | Interstage thermal shield retention system |
EP0928364A1 (fr) | 1996-09-26 | 1999-07-14 | Siemens Aktiengesellschaft | Compensation de la perte de pression d'une conduite d'air de refroidissement dans une installation de turbine a gaz |
US6185924B1 (en) | 1997-10-17 | 2001-02-13 | Hitachi, Ltd. | Gas turbine with turbine blade cooling |
DE50106969D1 (de) * | 2001-03-30 | 2005-09-08 | Siemens Ag | Gekühlte Gasturbinenschaufel |
GB2382847A (en) | 2001-12-06 | 2003-06-11 | Alstom | Gas turbine wet compression |
GB2382848A (en) | 2001-12-06 | 2003-06-11 | Alstom | Gas turbine wet compression |
DE10256193A1 (de) * | 2002-12-02 | 2004-06-09 | Alstom Technology Ltd | Verfahren zur Steuerung der Flüssigkeitseinspritzung in einen Zuströmkanal einer Kraft- oder Arbeitsmaschine |
US7244104B2 (en) * | 2005-05-31 | 2007-07-17 | Pratt & Whitney Canada Corp. | Deflectors for controlling entry of fluid leakage into the working fluid flowpath of a gas turbine engine |
US7189055B2 (en) * | 2005-05-31 | 2007-03-13 | Pratt & Whitney Canada Corp. | Coverplate deflectors for redirecting a fluid flow |
US7189056B2 (en) * | 2005-05-31 | 2007-03-13 | Pratt & Whitney Canada Corp. | Blade and disk radial pre-swirlers |
US7685823B2 (en) * | 2005-10-28 | 2010-03-30 | Power Systems Mfg., Llc | Airflow distribution to a low emissions combustor |
US7669425B2 (en) * | 2006-10-25 | 2010-03-02 | Siemens Energy, Inc. | Closed loop turbine cooling fluid reuse system for a turbine engine |
JP4981709B2 (ja) * | 2008-02-28 | 2012-07-25 | 三菱重工業株式会社 | ガスタービン及びディスク並びにディスクの径方向通路形成方法 |
US8277170B2 (en) * | 2008-05-16 | 2012-10-02 | General Electric Company | Cooling circuit for use in turbine bucket cooling |
US8353669B2 (en) * | 2009-08-18 | 2013-01-15 | United Technologies Corporation | Turbine vane platform leading edge cooling holes |
US8578720B2 (en) | 2010-04-12 | 2013-11-12 | Siemens Energy, Inc. | Particle separator in a gas turbine engine |
US8677766B2 (en) | 2010-04-12 | 2014-03-25 | Siemens Energy, Inc. | Radial pre-swirl assembly and cooling fluid metering structure for a gas turbine engine |
US8613199B2 (en) | 2010-04-12 | 2013-12-24 | Siemens Energy, Inc. | Cooling fluid metering structure in a gas turbine engine |
US8584469B2 (en) | 2010-04-12 | 2013-11-19 | Siemens Energy, Inc. | Cooling fluid pre-swirl assembly for a gas turbine engine |
US8935926B2 (en) | 2010-10-28 | 2015-01-20 | United Technologies Corporation | Centrifugal compressor with bleed flow splitter for a gas turbine engine |
GB201103890D0 (en) * | 2011-03-08 | 2011-04-20 | Rolls Royce Plc | Gas turbine engine swirled cooling air |
US20130170979A1 (en) * | 2012-01-04 | 2013-07-04 | General Electric Company | Double ended brush seal assembly for a compressor |
US8939711B2 (en) * | 2013-02-15 | 2015-01-27 | Siemens Aktiengesellschaft | Outer rim seal assembly in a turbine engine |
US9359902B2 (en) | 2013-06-28 | 2016-06-07 | Siemens Energy, Inc. | Turbine airfoil with ambient cooling system |
WO2015030926A1 (fr) | 2013-08-30 | 2015-03-05 | United Technologies Corporation | Déflecteur pour aube de moteur à turbine à gaz |
GB201420966D0 (en) * | 2014-11-26 | 2015-01-07 | Rolls Royce Plc | Compressor cooling |
US10030582B2 (en) * | 2015-02-09 | 2018-07-24 | United Technologies Corporation | Orientation feature for swirler tube |
JP6647952B2 (ja) | 2016-04-25 | 2020-02-14 | 三菱重工業株式会社 | ガスタービン |
JP7096058B2 (ja) * | 2018-04-18 | 2022-07-05 | 三菱重工業株式会社 | ガスタービンシステム |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3663118A (en) * | 1970-06-01 | 1972-05-16 | Gen Motors Corp | Turbine cooling control |
US3768921A (en) * | 1972-02-24 | 1973-10-30 | Aircraft Corp | Chamber pressure control using free vortex flow |
-
1974
- 1974-12-20 US US05/534,620 patent/US3936215A/en not_active Expired - Lifetime
-
1975
- 1975-11-07 CA CA239,355A patent/CA1045040A/fr not_active Expired
- 1975-12-01 DE DE19752554010 patent/DE2554010A1/de not_active Withdrawn
- 1975-12-08 SE SE7513778A patent/SE7513778L/xx unknown
- 1975-12-15 FR FR7538265A patent/FR2295238A1/fr not_active Withdrawn
- 1975-12-18 BE BE162876A patent/BE836802A/fr unknown
- 1975-12-19 GB GB52155/75A patent/GB1534000A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3310529A1 (de) * | 1982-03-23 | 1996-10-31 | Snecma | Vorrichtung zum Kühlen des Rotors einer Gasturbine |
US5700130A (en) * | 1982-03-23 | 1997-12-23 | Societe National D'etude Et De Construction De Moterus D'aviation S.N.E.C.M.A. | Device for cooling and gas turbine rotor |
DE3310529C2 (de) * | 1982-03-23 | 1998-10-08 | Snecma | Vorrichtung zum Kühlen des Rotors einer Gasturbine |
Also Published As
Publication number | Publication date |
---|---|
CA1045040A (fr) | 1978-12-26 |
BE836802A (fr) | 1976-04-16 |
GB1534000A (en) | 1978-11-29 |
SE7513778L (sv) | 1976-06-21 |
US3936215A (en) | 1976-02-03 |
DE2554010A1 (de) | 1976-07-01 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |