FR2917714B1 - Turboreacteur pour aeronef - Google Patents
Turboreacteur pour aeronefInfo
- Publication number
- FR2917714B1 FR2917714B1 FR0755988A FR0755988A FR2917714B1 FR 2917714 B1 FR2917714 B1 FR 2917714B1 FR 0755988 A FR0755988 A FR 0755988A FR 0755988 A FR0755988 A FR 0755988A FR 2917714 B1 FR2917714 B1 FR 2917714B1
- Authority
- FR
- France
- Prior art keywords
- turboreactor
- aircraft
- 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
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/14—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines with external combustion, e.g. scram-jet engines
-
- 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
- F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
-
- 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
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/32—Arrangement of components according to their shape
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/221—Improvement of heat transfer
- F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
-
- 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
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0755988A FR2917714B1 (fr) | 2007-06-25 | 2007-06-25 | Turboreacteur pour aeronef |
EP08806024A EP2167798A2 (fr) | 2007-06-25 | 2008-06-18 | Turboreacteur pour aeronef |
BRPI0812818-9A2A BRPI0812818A2 (pt) | 2007-06-25 | 2008-06-18 | Turbo-reator para aeronave |
CA2690601A CA2690601A1 (fr) | 2007-06-25 | 2008-06-18 | Turbojet engine for aircraft |
JP2010514052A JP2010531408A (ja) | 2007-06-25 | 2008-06-18 | 航空機用ターボジェットエンジン |
PCT/FR2008/051089 WO2009007564A2 (fr) | 2007-06-25 | 2008-06-18 | Turboreacteur pour aeronef |
US12/665,790 US20100300066A1 (en) | 2007-06-25 | 2008-06-18 | Turbojet engine for aircraft |
RU2010102057/11A RU2471682C2 (ru) | 2007-06-25 | 2008-06-18 | Турбореактивный двигатель для летательного аппарата |
CN200880021702A CN101730791A (zh) | 2007-06-25 | 2008-06-18 | 用于飞行器的涡轮喷气发动机 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0755988A FR2917714B1 (fr) | 2007-06-25 | 2007-06-25 | Turboreacteur pour aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2917714A1 FR2917714A1 (fr) | 2008-12-26 |
FR2917714B1 true FR2917714B1 (fr) | 2009-11-27 |
Family
ID=39137037
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0755988A Expired - Fee Related FR2917714B1 (fr) | 2007-06-25 | 2007-06-25 | Turboreacteur pour aeronef |
Country Status (9)
Country | Link |
---|---|
US (1) | US20100300066A1 (fr) |
EP (1) | EP2167798A2 (fr) |
JP (1) | JP2010531408A (fr) |
CN (1) | CN101730791A (fr) |
BR (1) | BRPI0812818A2 (fr) |
CA (1) | CA2690601A1 (fr) |
FR (1) | FR2917714B1 (fr) |
RU (1) | RU2471682C2 (fr) |
WO (1) | WO2009007564A2 (fr) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2955617B1 (fr) * | 2010-01-26 | 2012-10-26 | Airbus Operations Sas | Propulseur a turbomachine pour aeronef |
GB201007215D0 (en) * | 2010-04-30 | 2010-06-16 | Rolls Royce Plc | Gas turbine engine |
FR2989110B1 (fr) * | 2012-04-05 | 2016-09-09 | Snecma | Aube de stator formee par un ensemble de parties d'aube |
US10145253B2 (en) | 2012-04-05 | 2018-12-04 | Safran Aircraft Engines | Stator vane formed by a set of vane parts |
US9168716B2 (en) | 2012-09-14 | 2015-10-27 | The Boeing Company | Metallic sandwich structure having small bend radius |
US10385777B2 (en) * | 2012-10-01 | 2019-08-20 | United Technologies Corporation | Bifurcated inlet scoop for gas turbine engine |
FR3006996B1 (fr) * | 2013-06-14 | 2016-12-09 | European Aeronautic Defence & Space Co Eads France | Ensemble de propulsion electrique pour aeronef |
FR3018858B1 (fr) * | 2014-03-19 | 2019-04-05 | Airbus Operations (S.A.S.) | Ensemble propulsif d'aeronef comprenant un systeme de refroidissement |
CN103982302B (zh) * | 2014-05-23 | 2016-02-17 | 中国航空动力机械研究所 | 用于燃气轮机发电机组的冷却机构及燃气轮机发电机组 |
FR3024495B1 (fr) * | 2014-07-31 | 2019-07-12 | Safran Aircraft Engines | Dispositif de circulation d'air a debit ajustable pour turbomachine |
DE102015110615A1 (de) * | 2015-07-01 | 2017-01-19 | Rolls-Royce Deutschland Ltd & Co Kg | Leitschaufel eines Gasturbinentriebwerks, insbesondere eines Flugtriebwerks |
US10036318B2 (en) | 2015-12-22 | 2018-07-31 | Snecma | Air circulation device for turbomachine |
FR3047270B1 (fr) * | 2016-01-29 | 2019-03-29 | Safran Aircraft Engines | Echangeur thermique surfacique et traitement acoustique |
CN107054698B (zh) * | 2017-03-07 | 2021-04-06 | 沈武云 | 航天器外表面除热装置 |
CN110159358B (zh) * | 2018-02-14 | 2022-02-08 | 中国航发商用航空发动机有限责任公司 | 级间机匣 |
GB201817153D0 (en) * | 2018-10-22 | 2018-12-05 | Rolls Royce Plc | Gas turbine engine |
FR3093540B1 (fr) * | 2019-03-07 | 2021-04-23 | Safran Aircraft Engines | Turbomachine double flux a gaz a bras echangeur thermique |
WO2020249599A1 (fr) | 2019-06-14 | 2020-12-17 | Rolls-Royce Deutschland Ltd & Co Kg | Turbine à gaz et système de gestion de chaleur destiné au refroidissement d'huile dans un système d'huile d'une turbine à gaz |
GB202017401D0 (en) * | 2020-11-03 | 2020-12-16 | Rolls Royce Plc | Gas turbine engine with cabin blower system |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3842597A (en) * | 1973-03-16 | 1974-10-22 | Gen Electric | Gas turbine engine with means for reducing the formation and emission of nitrogen oxides |
US4254618A (en) * | 1977-08-18 | 1981-03-10 | General Electric Company | Cooling air cooler for a gas turbofan engine |
US4914904A (en) * | 1988-11-09 | 1990-04-10 | Avco Corporation | Oil cooler for fan jet engines |
GB2234805A (en) * | 1989-08-04 | 1991-02-13 | Rolls Royce Plc | A heat exchanger arrangement for a gas turbine engine |
US5123242A (en) * | 1990-07-30 | 1992-06-23 | General Electric Company | Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
SU1804042A1 (ru) * | 1991-03-28 | 1994-01-15 | Киевский механический завод им.О.К.Антонова | Система охлаждения теплообменника двигателя |
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 |
GB0315894D0 (en) * | 2003-07-08 | 2003-08-13 | Rolls Royce Plc | Aircraft engine arrangement |
US7377098B2 (en) * | 2004-08-26 | 2008-05-27 | United Technologies Corporation | Gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger |
US7377100B2 (en) * | 2004-08-27 | 2008-05-27 | Pratt & Whitney Canada Corp. | Bypass duct fluid cooler |
GB0607771D0 (en) * | 2006-04-20 | 2006-05-31 | Rolls Royce Plc | A heat exchanger arrangement |
FR2902830B1 (fr) * | 2006-06-27 | 2008-08-08 | Airbus France Sas | Turboreacteur pour aeronef |
US7658060B2 (en) * | 2006-07-19 | 2010-02-09 | United Technologies Corporation | Lubricant cooling exchanger dual intake duct |
-
2007
- 2007-06-25 FR FR0755988A patent/FR2917714B1/fr not_active Expired - Fee Related
-
2008
- 2008-06-18 CA CA2690601A patent/CA2690601A1/fr not_active Abandoned
- 2008-06-18 JP JP2010514052A patent/JP2010531408A/ja active Pending
- 2008-06-18 WO PCT/FR2008/051089 patent/WO2009007564A2/fr active Application Filing
- 2008-06-18 RU RU2010102057/11A patent/RU2471682C2/ru not_active IP Right Cessation
- 2008-06-18 BR BRPI0812818-9A2A patent/BRPI0812818A2/pt not_active IP Right Cessation
- 2008-06-18 US US12/665,790 patent/US20100300066A1/en not_active Abandoned
- 2008-06-18 EP EP08806024A patent/EP2167798A2/fr not_active Withdrawn
- 2008-06-18 CN CN200880021702A patent/CN101730791A/zh active Pending
Also Published As
Publication number | Publication date |
---|---|
US20100300066A1 (en) | 2010-12-02 |
RU2010102057A (ru) | 2011-07-27 |
CA2690601A1 (fr) | 2009-01-15 |
FR2917714A1 (fr) | 2008-12-26 |
RU2471682C2 (ru) | 2013-01-10 |
WO2009007564A3 (fr) | 2009-04-30 |
JP2010531408A (ja) | 2010-09-24 |
EP2167798A2 (fr) | 2010-03-31 |
CN101730791A (zh) | 2010-06-09 |
WO2009007564A2 (fr) | 2009-01-15 |
BRPI0812818A2 (pt) | 2014-12-09 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address |
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 |
|
ST | Notification of lapse |
Effective date: 20150227 |