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
Application number
FR9306635A
Other languages
English (en)
Other versions
FR2705996A1 (fr
Inventor
Mouton Pierre
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to FR9306635A priority Critical patent/FR2705996B1/fr
Priority to US08/249,728 priority patent/US5423174A/en
Priority to GB9410861A priority patent/GB2278643B/en
Publication of FR2705996A1 publication Critical patent/FR2705996A1/fr
Application granted granted Critical
Publication of FR2705996B1 publication Critical patent/FR2705996B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/22Fuel supply systems
    • F02C7/224Heating fuel before feeding to the burner
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/04Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047Heating to prevent icing
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185Cooling means for reducing the temperature of the cooling air or gas
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
FR9306635A 1993-06-03 1993-06-03 Système de dégivrage des parties avant d'une turbomachine. Expired - Fee Related FR2705996B1 (fr)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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