FR2889254B1 - Turboreacteur pour aeronef, ensemble propulseur comportant un tel turboreacteur, et aeronef comportant au moins un tel ensemble propulseur - Google Patents

Turboreacteur pour aeronef, ensemble propulseur comportant un tel turboreacteur, et aeronef comportant au moins un tel ensemble propulseur

Info

Publication number
FR2889254B1
FR2889254B1 FR0552343A FR0552343A FR2889254B1 FR 2889254 B1 FR2889254 B1 FR 2889254B1 FR 0552343 A FR0552343 A FR 0552343A FR 0552343 A FR0552343 A FR 0552343A FR 2889254 B1 FR2889254 B1 FR 2889254B1
Authority
FR
France
Prior art keywords
aircraft
propeller assembly
turboreactor
turbojet engine
propeller
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
FR0552343A
Other languages
English (en)
Other versions
FR2889254A1 (fr
Inventor
Herve Marche
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0552343A priority Critical patent/FR2889254B1/fr
Priority to US11/490,195 priority patent/US7997061B2/en
Publication of FR2889254A1 publication Critical patent/FR2889254A1/fr
Application granted granted Critical
Publication of FR2889254B1 publication Critical patent/FR2889254B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • 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
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
    • Y10T137/0645—With condition responsive control means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0552343A 2005-07-28 2005-07-28 Turboreacteur pour aeronef, ensemble propulseur comportant un tel turboreacteur, et aeronef comportant au moins un tel ensemble propulseur Expired - Fee Related FR2889254B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0552343A FR2889254B1 (fr) 2005-07-28 2005-07-28 Turboreacteur pour aeronef, ensemble propulseur comportant un tel turboreacteur, et aeronef comportant au moins un tel ensemble propulseur
US11/490,195 US7997061B2 (en) 2005-07-28 2006-07-20 Turbojet engine for aircraft, propulsion unit comprising such a turbojet engine and aircraft comprising such a propulsion unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0552343A FR2889254B1 (fr) 2005-07-28 2005-07-28 Turboreacteur pour aeronef, ensemble propulseur comportant un tel turboreacteur, et aeronef comportant au moins un tel ensemble propulseur

Publications (2)

Publication Number Publication Date
FR2889254A1 FR2889254A1 (fr) 2007-02-02
FR2889254B1 true FR2889254B1 (fr) 2011-05-06

Family

ID=36120911

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0552343A Expired - Fee Related FR2889254B1 (fr) 2005-07-28 2005-07-28 Turboreacteur pour aeronef, ensemble propulseur comportant un tel turboreacteur, et aeronef comportant au moins un tel ensemble propulseur

Country Status (2)

Country Link
US (1) US7997061B2 (fr)
FR (1) FR2889254B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008045093A1 (fr) * 2006-10-12 2008-04-17 United Technologies Corporation Bifurcation de moteur à turbine à gaz dans une tuyère à zone variable de soufflante
US9885313B2 (en) 2009-03-17 2018-02-06 United Technologes Corporation Gas turbine engine bifurcation located fan variable area nozzle
CA2936633C (fr) 2015-08-12 2021-12-28 Rolls-Royce North American Technologies, Inc. Echangeur de chaleur pour un systeme de propulsion de moteur de turbine a gaz
US11174816B2 (en) 2019-02-25 2021-11-16 Rolls-Royce Corporation Bypass duct conformal heat exchanger array

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2153929A1 (de) * 1971-10-29 1973-05-10 Motoren Turbinen Union Einrichtung zur luftentnahme fuer flugzeuge mit strahltriebwerken
GB2194592B (en) * 1986-08-27 1990-07-04 Rolls Royce Plc Fluid outlet duct
US5123242A (en) * 1990-07-30 1992-06-23 General Electric Company Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine
US5203163A (en) * 1990-08-01 1993-04-20 General Electric Company Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air
CA2046797A1 (fr) * 1990-08-01 1992-02-02 Franklin D. Parsons Montage d'echangeur de chaleur dans un canal de flux d'une turbine a gaz pour refroidir l'air chaud de prelevement
GB9027782D0 (en) * 1990-12-21 1991-02-13 Rolls Royce Plc Heat exchanger apparatus
FR2734319B1 (fr) * 1995-05-15 1997-07-18 Aerospatiale Dispositif pour prelever et refroidir de l'air chaud au niveau d'un moteur d'aeronef
FR2734320B1 (fr) * 1995-05-15 1997-07-18 Aerospatiale Dispositif pour prelever et refroidir de l'air chaud au niveau d'un moteur d'aeronef
DE19524733A1 (de) * 1995-07-07 1997-01-09 Bmw Rolls Royce Gmbh Fluggasturbinen-Triebwerk mit einem Flüssigkeits-Luft-Wärmetauscher
GB2319307B (en) * 1996-11-12 2000-11-08 Rolls Royce Plc Gas turbine engine cooling air flow control
US6415595B1 (en) * 2000-08-22 2002-07-09 Hamilton Sundstrand Corporation Integrated thermal management and coolant system for an aircraft
US7607308B2 (en) * 2005-12-08 2009-10-27 General Electric Company Shrouded turbofan bleed duct
US7765788B2 (en) * 2006-07-06 2010-08-03 United Technologies Corporation Cooling exchanger duct

Also Published As

Publication number Publication date
US20100237200A1 (en) 2010-09-23
FR2889254A1 (fr) 2007-02-02
US7997061B2 (en) 2011-08-16

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Legal Events

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Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

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Year of fee payment: 12

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Effective date: 20210305