FR3002287B1 - Procede de melange entre un ecoulement primaire et un ecoulement secondaire dans une turbomachine, dispositif et turbomachine correspondants - Google Patents
Procede de melange entre un ecoulement primaire et un ecoulement secondaire dans une turbomachine, dispositif et turbomachine correspondantsInfo
- Publication number
- FR3002287B1 FR3002287B1 FR1351379A FR1351379A FR3002287B1 FR 3002287 B1 FR3002287 B1 FR 3002287B1 FR 1351379 A FR1351379 A FR 1351379A FR 1351379 A FR1351379 A FR 1351379A FR 3002287 B1 FR3002287 B1 FR 3002287B1
- Authority
- FR
- France
- Prior art keywords
- turbomachine
- flow
- mixing primary
- secondary flow
- primary flow
- 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.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/38—Introducing air inside the jet
- F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
-
- 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
-
- 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
- F05D2260/2212—Improvement of heat transfer by creating turbulence
-
- 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 (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1351379A FR3002287B1 (fr) | 2013-02-18 | 2013-02-18 | Procede de melange entre un ecoulement primaire et un ecoulement secondaire dans une turbomachine, dispositif et turbomachine correspondants |
US14/178,584 US9709002B2 (en) | 2013-02-18 | 2014-02-12 | Method of mixing between a primary flow and a secondary flow in a turbine engine, corresponding device and turbine engine |
GB1402641.3A GB2513949B (en) | 2013-02-18 | 2014-02-14 | Method of mixing between a primary flow and a secondary flow in a turbine engine, corresponding device and turbine engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1351379A FR3002287B1 (fr) | 2013-02-18 | 2013-02-18 | Procede de melange entre un ecoulement primaire et un ecoulement secondaire dans une turbomachine, dispositif et turbomachine correspondants |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3002287A1 FR3002287A1 (fr) | 2014-08-22 |
FR3002287B1 true FR3002287B1 (fr) | 2016-07-01 |
Family
ID=48771578
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1351379A Active FR3002287B1 (fr) | 2013-02-18 | 2013-02-18 | Procede de melange entre un ecoulement primaire et un ecoulement secondaire dans une turbomachine, dispositif et turbomachine correspondants |
Country Status (3)
Country | Link |
---|---|
US (1) | US9709002B2 (fr) |
FR (1) | FR3002287B1 (fr) |
GB (1) | GB2513949B (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3043735B1 (fr) * | 2015-11-17 | 2017-12-29 | Snecma | Conduit d'entree d'air de turbomachine d'aeronef |
CN113847163B (zh) * | 2021-10-25 | 2024-02-23 | 中国航发沈阳发动机研究所 | 一种航空发动机风扇外涵道引射系统 |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2882992A (en) * | 1957-04-15 | 1959-04-21 | United Aircraft Corp | Low-drag exhaust silencer |
US3048376A (en) * | 1958-04-09 | 1962-08-07 | Curtiss Wright Corp | Fluid mixing apparatus |
US3289413A (en) * | 1964-08-19 | 1966-12-06 | Gen Electric | Fluid mixing apparatus for turbofan engines |
FR1525092A (fr) * | 1967-01-23 | 1968-05-17 | Snecma | Turbo-réacteur à flux de gaz chaud et à flux d'air froid |
US4165609A (en) * | 1977-03-02 | 1979-08-28 | The Boeing Company | Gas turbine mixer apparatus |
US4217756A (en) * | 1977-12-27 | 1980-08-19 | Boeing Commercial Airplane Company | Vortex mixers for reducing the noise emitted by jet engines |
US4516660A (en) * | 1980-09-22 | 1985-05-14 | Greenlaw Alfred L | Ejector and method for controlling jet engine noise |
FR2712918A1 (fr) * | 1980-12-06 | 1995-06-02 | Rolls Royce Plc | Perfectionnements à des turbomachines. |
US5771681A (en) * | 1996-09-17 | 1998-06-30 | The Boeing Company | Aircraft turbofan engine mixing apparatus |
US5941065A (en) * | 1996-11-04 | 1999-08-24 | The Boeing Company | Stowable mixer ejection nozzle |
DE10145489B4 (de) * | 2001-09-14 | 2008-11-06 | Mtu Aero Engines Gmbh | Anordnung zum Vermischen von zwei ursprünglich getrennt geführten Fluidströmen in einem Zweikreis-Strahltriebwerk |
US7043898B2 (en) * | 2003-06-23 | 2006-05-16 | Pratt & Whitney Canada Corp. | Combined exhaust duct and mixer for a gas turbine engine |
EP2153051A4 (fr) | 2007-05-22 | 2013-06-19 | Volvo Aero Corp | Agencement de masquage pour moteur à turbine à gaz |
GB2467121B (en) * | 2009-01-21 | 2011-03-30 | Rolls Royce Plc | A gas turbine engine |
-
2013
- 2013-02-18 FR FR1351379A patent/FR3002287B1/fr active Active
-
2014
- 2014-02-12 US US14/178,584 patent/US9709002B2/en active Active
- 2014-02-14 GB GB1402641.3A patent/GB2513949B/en active Active
Also Published As
Publication number | Publication date |
---|---|
US9709002B2 (en) | 2017-07-18 |
FR3002287A1 (fr) | 2014-08-22 |
US20140234074A1 (en) | 2014-08-21 |
GB2513949B (en) | 2020-08-19 |
GB2513949A (en) | 2014-11-12 |
GB201402641D0 (en) | 2014-04-02 |
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Legal Events
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RM | Correction of a material error |
Effective date: 20160404 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
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