FR2902831B1 - Turboreacteur pour aeronef - Google Patents

Turboreacteur pour aeronef

Info

Publication number: FR2902831B1
Authority: FR; France
Prior art keywords: turboreactor; aircraft
Prior art date: 2006-06-27
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

FR0652654A

Other languages

English (en)

Other versions

FR2902831A1 (fr

Inventor

Guillaume Bulin

Patrick Oberle

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.)

2006-06-27

Filing date

2006-06-27

Publication date

2010-10-22

2006-06-27 Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS

2006-06-27 Priority to FR0652654A priority Critical patent/FR2902831B1/fr

2007-06-21 Priority to US11/766,286 priority patent/US8235657B2/en

2007-12-28 Publication of FR2902831A1 publication Critical patent/FR2902831A1/fr

2010-10-22 Application granted granted Critical

2010-10-22 Publication of FR2902831B1 publication Critical patent/FR2902831B1/fr

Status Expired - Fee Related legal-status Critical Current

2026-06-27 Anticipated expiration legal-status Critical

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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/08—Cooling; Heating; Heat-insulation
- F01D25/12—Cooling
- 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
- 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
- F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
- 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
- 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
- F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
- F02K3/105—Heating the by-pass flow
- F02K3/115—Heating the by-pass flow by means of indirect heat exchange
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/0021—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics
- 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)
Physics & Mathematics (AREA)
Fluid Mechanics (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)
Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

FR0652654A 2006-06-27 2006-06-27 Turboreacteur pour aeronef Expired - Fee Related FR2902831B1 (fr)

Priority Applications (2)

Application Number	Priority Date	Filing Date	Title
FR0652654A FR2902831B1 (fr)	2006-06-27	2006-06-27	Turboreacteur pour aeronef
US11/766,286 US8235657B2 (en)	2006-06-27	2007-06-21	Turbojet for aircraft

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
FR0652654A FR2902831B1 (fr)	2006-06-27	2006-06-27	Turboreacteur pour aeronef

Publications (2)

Publication Number	Publication Date
FR2902831A1 FR2902831A1 (fr)	2007-12-28
FR2902831B1 true FR2902831B1 (fr)	2010-10-22

Family

ID=37668174

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
FR0652654A Expired - Fee Related FR2902831B1 (fr)	2006-06-27	2006-06-27	Turboreacteur pour aeronef

Country Status (2)

Country	Link
US (1)	US8235657B2 (fr)
FR (1)	FR2902831B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2946089B1 (fr) *	2009-05-27	2012-05-04	Airbus France	Dispositif de refroidissement de fluides pour propulseur a turbomachine
FR3029240B1 (fr) *	2014-11-27	2016-11-18	Snecma	Agencements a entree d'air et piege de corps etrangers dans un ensemble propulsif d'aeronef
DE102015203218A1 (de)	2015-02-23	2016-08-25	Rolls-Royce Deutschland Ltd & Co Kg	Gasturbinentriebwerk mit Ölkühler in der Triebwerksverkleidung
US10697371B2 (en) *	2015-12-28	2020-06-30	General Electric Company	Method and system for a combined air-oil cooler and fuel-oil cooler heat exchanger
US11125160B2 (en) *	2015-12-28	2021-09-21	General Electric Company	Method and system for combination heat exchanger
US10125684B2 (en) *	2015-12-29	2018-11-13	Pratt & Whitney Canada Corp.	Surface cooler for aero engine
US10648361B2 (en) *	2016-07-26	2020-05-12	United Technologies Corporation	Oil debris monitor with sequential coil system and associated algorithms for particle confirmation
US11035295B2 (en) *	2018-04-18	2021-06-15	Lockheed Martin Corporation	Engine nacelle heat exchanger
US20250236408A1 (en) *	2024-01-22	2025-07-24	Rtx Corporation	Framed heat exchanger for aircraft propulsion system

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US1533284A (en) *	1921-02-17	1925-04-14	Alfred V Verville	Annular radiator mounting for airplanes
US2171817A (en) *	1936-12-22	1939-09-05	Messerschmitt Boelkow Blohm	Radiator for aviation engines
US2423175A (en) *	1943-11-15	1947-07-01	Churchill John Adrian	Heat exchange apparatus
US2487842A (en) *	1948-03-09	1949-11-15	Westinghouse Electric Corp	Aircraft power plant apparatus
US2731239A (en) *	1951-06-15	1956-01-17	Garrett Corp	Oil cooler cooled by air and fuel
US3693554A (en) *	1970-05-11	1972-09-26	Acf Ind Inc	Flat car having a plurality of fixed intermediate bulkheads
US3693354A (en) *	1971-01-22	1972-09-26	Gen Electric	Aircraft engine fan duct burner system
US4120150A (en) *	1977-05-17	1978-10-17	The United States Of America As Represented By The Secretary Of The Air Force	Compact fuel-to-air heat exchanger for jet engine application
US5020318A (en) *	1987-11-05	1991-06-04	General Electric Company	Aircraft engine frame construction
US4887664A (en) *	1987-12-07	1989-12-19	Westinghouse Electric Corp.	Heat exchanger system having adjustable heat transfer capacity
US5123242A (en) *	1990-07-30	1992-06-23	General Electric Company	Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine
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
US5269135A (en) *	1991-10-28	1993-12-14	General Electric Company	Gas turbine engine fan cooled heat exchanger
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
US6058696A (en) *	1997-12-22	2000-05-09	United Technologies Corporation	Inlet and outlet module for a heat exchanger for a flowpath for working medium gases
JP3823584B2 (ja) *	1999-02-15	2006-09-20	日産自動車株式会社	熱交換器
GB2364770A (en) *	2000-07-11	2002-02-06	Delphi Tech Inc	Heat exchanger and fluid pipe therefor
US20040182559A1 (en) *	2001-03-22	2004-09-23	Kent Scott Edward	Heat exchanger tube
DE50311194D1 (de) *	2002-06-11	2009-04-02	Erbsloeh Aluminium Gmbh	Hohlkammerprofil aus metall, insbesondere für wärmetauscher
FR2858999B1 (fr) *	2003-08-18	2005-11-11	Snecma Moteurs	Turbomachine pour aeronef a emissions de bruit reduites
KR100518856B1 (ko) *	2003-09-04	2005-09-30	엘지전자 주식회사	플랫 튜브 열 교환기

2006
- 2006-06-27 FR FR0652654A patent/FR2902831B1/fr not_active Expired - Fee Related
2007
- 2007-06-21 US US11/766,286 patent/US8235657B2/en not_active Expired - Fee Related

Also Published As

Publication number	Publication date
US8235657B2 (en)	2012-08-07
US20100028139A1 (en)	2010-02-04
FR2902831A1 (fr)	2007-12-28

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FR2911114B1 (fr)	2009-02-27	Cockpit securise pour aeronef
DE112007003147A5 (de)	2009-09-24	Rohr-Biegevorrichtung
FR2903733B1 (fr)	2011-03-04	Turbomoteur pour aeronef.
DE602006016174D1 (de)	2010-09-23	Blisterverpackungsverfahren
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DE602006013286D1 (de)	2010-05-12	Sicherheitseinrictung

Legal Events

Date	Code	Title	Description
2011-10-21	CA	Change of address	Effective date: 20110916
2011-10-21	CD	Change of name or company name	Owner name: AIRBUS HOLDING, FR Effective date: 20110916
2011-10-21	CJ	Change in legal form	Effective date: 20110916
2011-10-21	TP	Transmission of property	Owner name: AIRBUS HOLDING, FR Effective date: 20110913
2016-06-27	PLFP	Fee payment	Year of fee payment: 11
2017-06-21	PLFP	Fee payment	Year of fee payment: 12
2018-06-20	PLFP	Fee payment	Year of fee payment: 13
2019-06-19	PLFP	Fee payment	Year of fee payment: 14
2021-03-12	ST	Notification of lapse	Effective date: 20210206