FR2705996B1 - Système de dégivrage des parties avant d'une turbomachine. - Google Patents
Système de dégivrage des parties avant d'une turbomachine.Info
- Publication number
- FR2705996B1 FR2705996B1 FR9306635A FR9306635A FR2705996B1 FR 2705996 B1 FR2705996 B1 FR 2705996B1 FR 9306635 A FR9306635 A FR 9306635A FR 9306635 A FR9306635 A FR 9306635A FR 2705996 B1 FR2705996 B1 FR 2705996B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- front parts
- defrosting system
- defrosting
- parts
- 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 - Fee Related
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
- F02C7/22—Fuel supply systems
- F02C7/224—Heating fuel before feeding to the burner
-
- 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
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- 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
- F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
-
- 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)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9306635A FR2705996B1 (fr) | 1993-06-03 | 1993-06-03 | Système de dégivrage des parties avant d'une turbomachine. |
US08/249,728 US5423174A (en) | 1993-06-03 | 1994-05-26 | Anti-icing system for a gas turbine engine |
GB9410861A GB2278643B (en) | 1993-06-03 | 1994-05-31 | De-icing system for forward parts of a turboshaft engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9306635A FR2705996B1 (fr) | 1993-06-03 | 1993-06-03 | Système de dégivrage des parties avant d'une turbomachine. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2705996A1 FR2705996A1 (fr) | 1994-12-09 |
FR2705996B1 true FR2705996B1 (fr) | 1995-07-07 |
Family
ID=9447709
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9306635A Expired - Fee Related FR2705996B1 (fr) | 1993-06-03 | 1993-06-03 | Système de dégivrage des parties avant d'une turbomachine. |
Country Status (3)
Country | Link |
---|---|
US (1) | US5423174A (fr) |
FR (1) | FR2705996B1 (fr) |
GB (1) | GB2278643B (fr) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2875542B1 (fr) * | 2004-09-21 | 2009-02-13 | Airbus France Sas | Dispositif de protection contre le givrage pour moteurs d'aeronefs et procedes de degivrage associe |
US7230205B2 (en) * | 2005-03-29 | 2007-06-12 | Siemens Power Generation, Inc. | Compressor airfoil surface wetting and icing detection system |
US7328623B2 (en) * | 2006-03-20 | 2008-02-12 | General Electric Company | Temperature and/or pressure sensor assembly |
US20090067993A1 (en) * | 2007-03-22 | 2009-03-12 | Roberge Gary D | Coated variable area fan nozzle |
US7984606B2 (en) * | 2008-11-03 | 2011-07-26 | Propulsion, Gas Turbine, And Energy Evaluations, Llc | Systems and methods for thermal management in a gas turbine powerplant |
US7997062B2 (en) * | 2009-01-29 | 2011-08-16 | Pratt & Whitney Canada Corp. | Dual channel regulated fuel-oil heat exchanger |
US8490403B2 (en) * | 2009-09-09 | 2013-07-23 | General Electric Company | System and method for applying energy externally for fuel gas for dew point heating in gas turbine power plant |
US8429891B2 (en) * | 2009-12-16 | 2013-04-30 | General Electric Company | Anti-icing system using radiant infrared energy from turbine exhaust flues |
US8444093B1 (en) | 2011-04-18 | 2013-05-21 | Eran Epstein | Airplane leading edge de-icing apparatus |
US8844258B2 (en) | 2011-11-23 | 2014-09-30 | General Electric Company | Systems and methods for de-icing a gas turbine engine inlet screen and dehumidifying inlet air filters |
US10502135B2 (en) * | 2012-01-31 | 2019-12-10 | United Technologies Corporation | Buffer system for communicating one or more buffer supply airs throughout a gas turbine engine |
US20130199202A1 (en) * | 2012-02-07 | 2013-08-08 | General Electric Company | System and method for gas turbine inlet air heating |
RU2557878C1 (ru) * | 2013-12-30 | 2015-07-27 | Владимир Леонидович Письменный | Противообледенительная система газотурбинного двигателя |
GB201415078D0 (en) | 2014-08-26 | 2014-10-08 | Rolls Royce Plc | Gas turbine engine anti-icing system |
EP3018304B1 (fr) | 2014-11-06 | 2020-10-14 | United Technologies Corporation | Système de gestion thermique pour moteur à turbine à gaz |
US9567907B2 (en) | 2015-02-24 | 2017-02-14 | General Electrical Company | Imaging assisted gas turbine anti-icing system |
FR3088961A1 (fr) * | 2018-11-22 | 2020-05-29 | Airbus Operations (S.A.S.) | Turbomachine équipée d’un système de dégivrage de l’entrée d’air. |
US11199133B2 (en) * | 2018-12-17 | 2021-12-14 | Hamilton Sundstrand Corporation | Aircraft systems and methods utilizing waste heat in fuel |
JP7192591B2 (ja) * | 2019-03-14 | 2022-12-20 | トヨタ自動車株式会社 | ハイブリッド車両、及び過給機の冷却方法 |
US11384687B2 (en) * | 2019-04-04 | 2022-07-12 | Pratt & Whitney Canada Corp. | Anti-icing system for gas turbine engine |
GB202219390D0 (en) * | 2022-12-21 | 2023-02-01 | Rolls Royce Plc | Gas turbine operation |
US12078103B1 (en) | 2023-08-04 | 2024-09-03 | Rolls-Royce North American Technologies Inc. | Anti-ice mixing unit utilizing bleed air for a gas turbine engine |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB720012A (en) * | 1951-04-23 | 1954-12-08 | Bristol Aeroplane Co Ltd | Improvements in or relating to the cooling of aircraft propulsion plants |
US2925712A (en) * | 1952-12-12 | 1960-02-23 | Rolls Royce | Aircraft fuel system with fuel heating means |
US2970437A (en) * | 1956-02-28 | 1961-02-07 | Thompson Ramo Wooldridge Inc | High temperature pumping system with variable speed pump and refrigeration by-product |
US3123283A (en) * | 1962-12-07 | 1964-03-03 | Anti-icing valve means | |
FR2216175B1 (fr) * | 1973-02-05 | 1975-03-07 | Snecma | |
US3981466A (en) * | 1974-12-23 | 1976-09-21 | The Boeing Company | Integrated thermal anti-icing and environmental control system |
US4041697A (en) * | 1975-07-17 | 1977-08-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Oil cooling system for a gas turbine engine |
GB1559828A (en) * | 1975-09-12 | 1980-01-30 | Rolls Royce | Fuel system for gas turbine engines |
GB2046843B (en) * | 1979-04-17 | 1983-01-26 | Rolls Royce | Gas turbine engines-de-icing-icing |
US4404793A (en) * | 1980-03-20 | 1983-09-20 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Apparatus for improving the fuel efficiency of a gas turbine engine |
IT1166979B (it) * | 1983-10-03 | 1987-05-06 | Nuovo Pignone Spa | Sistema antighiaccio per turbina a gas |
US4782658A (en) * | 1987-05-07 | 1988-11-08 | Rolls-Royce Plc | Deicing of a geared gas turbine engine |
US4783026A (en) * | 1987-05-22 | 1988-11-08 | Avco Corporation | Anti-icing management system |
DE3828834C1 (fr) * | 1988-08-25 | 1989-11-02 | Mtu Muenchen Gmbh |
-
1993
- 1993-06-03 FR FR9306635A patent/FR2705996B1/fr not_active Expired - Fee Related
-
1994
- 1994-05-26 US US08/249,728 patent/US5423174A/en not_active Expired - Fee Related
- 1994-05-31 GB GB9410861A patent/GB2278643B/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
GB2278643A (en) | 1994-12-07 |
US5423174A (en) | 1995-06-13 |
GB9410861D0 (en) | 1994-07-20 |
FR2705996A1 (fr) | 1994-12-09 |
GB2278643B (en) | 1997-01-08 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
TP | Transmission of property | ||
CD | Change of name or company name | ||
ST | Notification of lapse |
Effective date: 20080229 |