FR2967239B1 - Jets auto-oscillants d'injection de combustible - Google Patents
Jets auto-oscillants d'injection de combustible Download PDFInfo
- Publication number
- FR2967239B1 FR2967239B1 FR1160093A FR1160093A FR2967239B1 FR 2967239 B1 FR2967239 B1 FR 2967239B1 FR 1160093 A FR1160093 A FR 1160093A FR 1160093 A FR1160093 A FR 1160093A FR 2967239 B1 FR2967239 B1 FR 2967239B1
- Authority
- FR
- France
- Prior art keywords
- self
- fuel injection
- injection jets
- swing
- swing fuel
- 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
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
- F23D14/46—Details, e.g. noise reduction means
- F23D14/48—Nozzles
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
-
- 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
- F05D2250/20—Three-dimensional
- F05D2250/24—Three-dimensional ellipsoidal
- F05D2250/241—Three-dimensional ellipsoidal spherical
-
- 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
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/14—Special features of gas burners
- F23D2900/14482—Burner nozzles incorporating a fluidic oscillator
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
- F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators
-
- 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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/941,340 US8572981B2 (en) | 2010-11-08 | 2010-11-08 | Self-oscillating fuel injection jets |
US12/941.340 | 2010-11-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2967239A1 FR2967239A1 (fr) | 2012-05-11 |
FR2967239B1 true FR2967239B1 (fr) | 2018-04-27 |
Family
ID=45971288
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1160093A Expired - Fee Related FR2967239B1 (fr) | 2010-11-08 | 2011-11-07 | Jets auto-oscillants d'injection de combustible |
Country Status (5)
Country | Link |
---|---|
US (1) | US8572981B2 (fr) |
JP (1) | JP5925464B2 (fr) |
CN (1) | CN102538012B (fr) |
DE (1) | DE102011055053A1 (fr) |
FR (1) | FR2967239B1 (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3076081A1 (fr) * | 2015-04-01 | 2016-10-05 | Siemens Aktiengesellschaft | Générateur de turbulence, brûleur et chambre de combustion d'un moteur à turbine à gaz |
KR101884694B1 (ko) * | 2015-05-27 | 2018-08-02 | 두산중공업 주식회사 | 연료 분출구를 가진 노즐허브 |
US10392947B2 (en) | 2015-07-13 | 2019-08-27 | General Electric Company | Compositions and methods of attachment of thick environmental barrier coatings on CMC components |
US10378444B2 (en) | 2015-08-19 | 2019-08-13 | General Electric Company | Engine component for a gas turbine engine |
US10197278B2 (en) | 2015-09-02 | 2019-02-05 | General Electric Company | Combustor assembly for a turbine engine |
US10168051B2 (en) | 2015-09-02 | 2019-01-01 | General Electric Company | Combustor assembly for a turbine engine |
US9976746B2 (en) | 2015-09-02 | 2018-05-22 | General Electric Company | Combustor assembly for a turbine engine |
US11149646B2 (en) | 2015-09-02 | 2021-10-19 | General Electric Company | Piston ring assembly for a turbine engine |
US10161266B2 (en) | 2015-09-23 | 2018-12-25 | General Electric Company | Nozzle and nozzle assembly for gas turbine engine |
US10563867B2 (en) | 2015-09-30 | 2020-02-18 | General Electric Company | CMC articles having small complex features for advanced film cooling |
CN108019774B (zh) * | 2016-11-01 | 2019-12-06 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | 用于燃气轮机的预混合燃料喷嘴和燃烧室 |
KR102024542B1 (ko) * | 2017-07-14 | 2019-09-24 | 두산중공업 주식회사 | 연소기용 노즐 및 이를 구비하는 가스터빈 |
US11402097B2 (en) | 2018-01-03 | 2022-08-02 | General Electric Company | Combustor assembly for a turbine engine |
Family Cites Families (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1139004A (en) * | 1966-02-28 | 1969-01-08 | Mini Of Technology | Improvements in or relating to combustion devices |
US3510239A (en) * | 1966-04-18 | 1970-05-05 | Maurice Partiot | Directional radiant heaters |
US3748852A (en) * | 1969-12-05 | 1973-07-31 | L Cole | Self-stabilizing pressure compensated injector |
CA969088A (en) * | 1971-12-21 | 1975-06-10 | Firma Schwank G.M.B.H. | Burner-plate for infra-red radiators |
US4052002A (en) * | 1974-09-30 | 1977-10-04 | Bowles Fluidics Corporation | Controlled fluid dispersal techniques |
US5857339A (en) * | 1995-05-23 | 1999-01-12 | The United States Of America As Represented By The Secretary Of The Air Force | Combustor flame stabilizing structure |
US5822992A (en) * | 1995-10-19 | 1998-10-20 | General Electric Company | Low emissions combustor premixer |
US6383602B1 (en) * | 1996-12-23 | 2002-05-07 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream which flows through a substrate, and related articles of manufacture |
GB2337102A (en) * | 1998-05-09 | 1999-11-10 | Europ Gas Turbines Ltd | Gas-turbine engine combustor |
DE19934612A1 (de) * | 1999-07-23 | 2001-01-25 | Abb Alstom Power Ch Ag | Verfahren zur aktiven Unterdrückung von strömungsmechanischen Instabilitäten in einem Verbrennungssystem sowie Verbrennungssystem zur Durchführung des Verfahrens |
IT1313547B1 (it) * | 1999-09-23 | 2002-07-24 | Nuovo Pignone Spa | Camera di premiscelamento per turbine a gas |
US6481209B1 (en) * | 2000-06-28 | 2002-11-19 | General Electric Company | Methods and apparatus for decreasing combustor emissions with swirl stabilized mixer |
DE10040869A1 (de) | 2000-08-21 | 2002-03-07 | Alstom Power Nv | Verfahren und Vorrichtung zur Unterdrückung von Strömungswirbeln innerhalb einer Strömungskraftmaschine |
GB2368386A (en) * | 2000-10-23 | 2002-05-01 | Alstom Power Nv | Gas turbine engine combustion system |
US6715983B2 (en) | 2001-09-27 | 2004-04-06 | General Electric Company | Method and apparatus for reducing distortion losses induced to gas turbine engine airflow |
US6675581B1 (en) * | 2002-07-15 | 2004-01-13 | Power Systems Mfg, Llc | Fully premixed secondary fuel nozzle |
US7057326B2 (en) * | 2003-05-29 | 2006-06-06 | General Electric Company | Rotor body containment shell with reduced windage losses |
ITTO20031013A1 (it) | 2003-12-16 | 2005-06-17 | Ansaldo Energia Spa | Sistema di smorzamento di instabilita' termoacustiche in un dispositivo combustore per una turbina a gas. |
US8449171B2 (en) | 2005-04-08 | 2013-05-28 | Commonwealth Scientific And Industrial Research Organisation | Method for microfluidic mixing and mixing device |
JP4476177B2 (ja) * | 2005-06-06 | 2010-06-09 | 三菱重工業株式会社 | ガスタービンの燃焼バーナー |
GB2435508B (en) * | 2006-02-22 | 2011-08-03 | Siemens Ag | A swirler for use in a burner of a gas turbine engine |
EP1890083A1 (fr) * | 2006-08-16 | 2008-02-20 | Siemens Aktiengesellschaft | Injecteur de carburant pour une turbine à gaz |
US20080104961A1 (en) * | 2006-11-08 | 2008-05-08 | Ronald Scott Bunker | Method and apparatus for enhanced mixing in premixing devices |
JP4296519B2 (ja) | 2006-12-19 | 2009-07-15 | 株式会社日立製作所 | 燃料噴射弁 |
JP2008248733A (ja) * | 2007-03-29 | 2008-10-16 | Mitsubishi Heavy Ind Ltd | ガスタービン用高温部材 |
EP2085698A1 (fr) * | 2008-02-01 | 2009-08-05 | Siemens Aktiengesellschaft | Pilotage d'un brûleur à jets à grande vitesse à l'aide d'un pilote par écoulement à vortex guidé |
US20100011770A1 (en) * | 2008-07-21 | 2010-01-21 | Ronald James Chila | Gas Turbine Premixer with Cratered Fuel Injection Sites |
EP2169304A1 (fr) * | 2008-09-25 | 2010-03-31 | Siemens Aktiengesellschaft | Aube de turbulence |
US8851402B2 (en) * | 2009-02-12 | 2014-10-07 | General Electric Company | Fuel injection for gas turbine combustors |
RU2548521C2 (ru) * | 2009-05-05 | 2015-04-20 | Сименс Акциенгезелльшафт | Завихритель, камера сгорания и газовая турбина с улучшенным перемешиванием |
US20110023494A1 (en) * | 2009-07-28 | 2011-02-03 | General Electric Company | Gas turbine burner |
-
2010
- 2010-11-08 US US12/941,340 patent/US8572981B2/en active Active
-
2011
- 2011-11-04 DE DE102011055053A patent/DE102011055053A1/de not_active Withdrawn
- 2011-11-04 CN CN201110372734.9A patent/CN102538012B/zh not_active Expired - Fee Related
- 2011-11-07 JP JP2011243085A patent/JP5925464B2/ja not_active Expired - Fee Related
- 2011-11-07 FR FR1160093A patent/FR2967239B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN102538012B (zh) | 2015-08-12 |
DE102011055053A1 (de) | 2012-05-10 |
US20120111015A1 (en) | 2012-05-10 |
FR2967239A1 (fr) | 2012-05-11 |
JP2012102995A (ja) | 2012-05-31 |
JP5925464B2 (ja) | 2016-05-25 |
CN102538012A (zh) | 2012-07-04 |
US8572981B2 (en) | 2013-11-05 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 5 |
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Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
|
ST | Notification of lapse |
Effective date: 20230705 |