GB0219461D0 - Fuel injection arrangement - Google Patents
Fuel injection arrangementInfo
- Publication number
- GB0219461D0 GB0219461D0 GBGB0219461.1A GB0219461A GB0219461D0 GB 0219461 D0 GB0219461 D0 GB 0219461D0 GB 0219461 A GB0219461 A GB 0219461A GB 0219461 D0 GB0219461 D0 GB 0219461D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel injection
- injection arrangement
- arrangement
- fuel
- injection
- 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.)
- Ceased
Links
- 239000000446 fuel Substances 0.000 title 1
- 238000002347 injection Methods 0.000 title 1
- 239000007924 injection Substances 0.000 title 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
- F23D11/106—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet
- F23D11/107—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting at the burner outlet at least one of both being subjected to a swirling motion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/38—Nozzles; Cleaning devices therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2210/00—Noise abatement
-
- 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
- F23D2900/11101—Pulverising gas flow impinging on fuel from pre-filming surface, e.g. lip atomizers
-
- 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
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0219461.1A GB0219461D0 (en) | 2002-08-21 | 2002-08-21 | Fuel injection arrangement |
EP03254684A EP1391653A3 (en) | 2002-08-21 | 2003-07-26 | Fuel injection arrangement |
US10/629,795 US20050097889A1 (en) | 2002-08-21 | 2003-07-30 | Fuel injection arrangement |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0219461.1A GB0219461D0 (en) | 2002-08-21 | 2002-08-21 | Fuel injection arrangement |
Publications (1)
Publication Number | Publication Date |
---|---|
GB0219461D0 true GB0219461D0 (en) | 2002-09-25 |
Family
ID=9942709
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB0219461.1A Ceased GB0219461D0 (en) | 2002-08-21 | 2002-08-21 | Fuel injection arrangement |
Country Status (3)
Country | Link |
---|---|
US (1) | US20050097889A1 (en) |
EP (1) | EP1391653A3 (en) |
GB (1) | GB0219461D0 (en) |
Families Citing this family (64)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7779636B2 (en) * | 2005-05-04 | 2010-08-24 | Delavan Inc | Lean direct injection atomizer for gas turbine engines |
US7513098B2 (en) * | 2005-06-29 | 2009-04-07 | Siemens Energy, Inc. | Swirler assembly and combinations of same in gas turbine engine combustors |
DE102005062079A1 (en) * | 2005-12-22 | 2007-07-12 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormic burner with a nebulizer lip |
GB2439097B (en) * | 2006-06-15 | 2008-10-29 | Rolls Royce Plc | Fuel injector |
DE102006032429A1 (en) * | 2006-07-13 | 2008-02-21 | Rolls-Royce Deutschland Ltd & Co Kg | Fuel injection device for an aircraft gas turbine |
US7762072B2 (en) * | 2007-01-16 | 2010-07-27 | Honeywell International Inc. | Combustion systems with rotary fuel slingers |
JP4364911B2 (en) * | 2007-02-15 | 2009-11-18 | 川崎重工業株式会社 | Gas turbine engine combustor |
DE102007043626A1 (en) | 2007-09-13 | 2009-03-19 | Rolls-Royce Deutschland Ltd & Co Kg | Gas turbine lean burn burner with fuel nozzle with controlled fuel inhomogeneity |
DE102007050276A1 (en) * | 2007-10-18 | 2009-04-23 | Rolls-Royce Deutschland Ltd & Co Kg | Lean premix burner for a gas turbine engine |
US8607571B2 (en) * | 2009-09-18 | 2013-12-17 | Delavan Inc | Lean burn injectors having a main fuel circuit and one of multiple pilot fuel circuits with prefiliming air-blast atomizers |
GB0812905D0 (en) * | 2008-07-16 | 2008-08-20 | Rolls Royce Plc | Fuel injection system |
US8959922B2 (en) | 2008-09-29 | 2015-02-24 | Siemens Aktiengesellschaft | Fuel nozzle with flower shaped nozzle tube |
EP2169307A1 (en) * | 2008-09-29 | 2010-03-31 | Siemens Aktiengesellschaft | Fuel nozzle |
GB0820560D0 (en) * | 2008-11-11 | 2008-12-17 | Rolls Royce Plc | Fuel injector |
US8453454B2 (en) * | 2010-04-14 | 2013-06-04 | General Electric Company | Coannular oil injection nozzle |
US9435537B2 (en) * | 2010-11-30 | 2016-09-06 | General Electric Company | System and method for premixer wake and vortex filling for enhanced flame-holding resistance |
DE102011006241A1 (en) * | 2011-03-28 | 2012-10-04 | Rolls-Royce Deutschland Ltd & Co Kg | Device for mixing fuel and air of a jet engine |
JP5772245B2 (en) | 2011-06-03 | 2015-09-02 | 川崎重工業株式会社 | Fuel injection device |
JP5773342B2 (en) * | 2011-06-03 | 2015-09-02 | 川崎重工業株式会社 | Fuel injection device |
US9593851B2 (en) | 2011-06-30 | 2017-03-14 | General Electric Company | Combustor and method of supplying fuel to the combustor |
WO2013002666A1 (en) | 2011-06-30 | 2013-01-03 | General Electric Company | Combustor and method of supplying fuel to the combustor |
GB201112434D0 (en) * | 2011-07-20 | 2011-08-31 | Rolls Royce Plc | A fuel injector |
GB201113421D0 (en) * | 2011-08-04 | 2011-09-21 | Rolls Royce Plc | Fuel injector |
US9423137B2 (en) * | 2011-12-29 | 2016-08-23 | Rolls-Royce Corporation | Fuel injector with first and second converging fuel-air passages |
US9170024B2 (en) | 2012-01-06 | 2015-10-27 | General Electric Company | System and method for supplying a working fluid to a combustor |
US9188337B2 (en) | 2012-01-13 | 2015-11-17 | General Electric Company | System and method for supplying a working fluid to a combustor via a non-uniform distribution manifold |
US9097424B2 (en) | 2012-03-12 | 2015-08-04 | General Electric Company | System for supplying a fuel and working fluid mixture to a combustor |
US9151500B2 (en) * | 2012-03-15 | 2015-10-06 | General Electric Company | System for supplying a fuel and a working fluid through a liner to a combustion chamber |
US9052115B2 (en) | 2012-04-25 | 2015-06-09 | General Electric Company | System and method for supplying a working fluid to a combustor |
US9284888B2 (en) | 2012-04-25 | 2016-03-15 | General Electric Company | System for supplying fuel to late-lean fuel injectors of a combustor |
US8677753B2 (en) | 2012-05-08 | 2014-03-25 | General Electric Company | System for supplying a working fluid to a combustor |
CN102901099A (en) * | 2012-09-14 | 2013-01-30 | 华中科技大学 | Flower petal type combustor |
EP2923150B1 (en) * | 2012-11-21 | 2018-09-05 | General Electric Company | Anti-coking liquid fuel cartridge |
US20140144141A1 (en) * | 2012-11-26 | 2014-05-29 | General Electric Company | Premixer with diluent fluid and fuel tubes having chevron outlets |
US20140144152A1 (en) * | 2012-11-26 | 2014-05-29 | General Electric Company | Premixer With Fuel Tubes Having Chevron Outlets |
US20150285502A1 (en) * | 2014-04-08 | 2015-10-08 | General Electric Company | Fuel nozzle shroud and method of manufacturing the shroud |
US20160061452A1 (en) * | 2014-08-26 | 2016-03-03 | General Electric Company | Corrugated cyclone mixer assembly to facilitate reduced nox emissions and improve operability in a combustor system |
JP6623485B2 (en) * | 2014-09-25 | 2019-12-25 | 三菱日立パワーシステムズ株式会社 | Combustor and gas turbine including the same |
US10317083B2 (en) * | 2014-10-03 | 2019-06-11 | Pratt & Whitney Canada Corp. | Fuel nozzle |
WO2016068922A1 (en) * | 2014-10-30 | 2016-05-06 | Siemens Aktiengesellschaft | Pilot burner and method for stabilizing a pilot flame in a combustor subject to combustion dynamics |
FR3029271B1 (en) * | 2014-11-28 | 2019-06-21 | Safran Aircraft Engines | ANNULAR DEFLECTION WALL FOR TURBOMACHINE COMBUSTION CHAMBER INJECTION SYSTEM PROVIDING EXTENSIVE FUEL ATOMIZATION AREA |
FR3029608B1 (en) * | 2014-12-03 | 2017-01-13 | Snecma | AIR INTAKE CROWN FOR TURBOMACHINE COMBUSTION CHAMBER INJECTION SYSTEM AND FUEL ATOMIZATION METHOD IN INJECTION SYSTEM COMPRISING SAID AIR INTAKE CROWN |
US9863638B2 (en) * | 2015-04-01 | 2018-01-09 | Delavan Inc. | Air shrouds with improved air wiping |
KR101657535B1 (en) * | 2015-05-21 | 2016-09-19 | 두산중공업 주식회사 | Fuel supply nozzle to minimize burning damage. |
GB201512000D0 (en) * | 2015-07-09 | 2015-08-19 | Rolls Royce Plc | Fuel injector |
FR3050806B1 (en) | 2016-04-28 | 2020-02-21 | Safran Aircraft Engines | AIR INTAKE BALL FOR A TURBOMACHINE INJECTION SYSTEM COMPRISING AN AERODYNAMIC DEFLECTOR AT ITS INPUT |
CN106016358B (en) * | 2016-05-30 | 2019-04-30 | 中国科学院工程热物理研究所 | A kind of cyclone having both eddy flow, injection and blending effect |
US10502425B2 (en) * | 2016-06-03 | 2019-12-10 | General Electric Company | Contoured shroud swirling pre-mix fuel injector assembly |
CN106091008B (en) * | 2016-06-13 | 2019-08-02 | 中国科学院工程热物理研究所 | Have both the cyclone and injection apparatus of eddy flow, atomization and blending effect |
PL230047B1 (en) * | 2016-07-06 | 2018-09-28 | Metal Expert Spolka Z Ograniczona Odpowiedzialnoscia Spolka Jawna | High-temperature gas burner |
US20190056108A1 (en) * | 2017-08-21 | 2019-02-21 | General Electric Company | Non-uniform mixer for combustion dynamics attenuation |
GB2568981A (en) * | 2017-12-01 | 2019-06-05 | Rolls Royce Plc | Fuel spray nozzle |
GB201806020D0 (en) * | 2018-02-23 | 2018-05-30 | Rolls Royce | Conduit |
US20200041130A1 (en) | 2018-07-31 | 2020-02-06 | Hotstart, Inc. | Combustor Systems |
USD910717S1 (en) | 2018-07-31 | 2021-02-16 | Hotstart, Inc. | Rotary atomizer |
US10935245B2 (en) | 2018-11-20 | 2021-03-02 | General Electric Company | Annular concentric fuel nozzle assembly with annular depression and radial inlet ports |
US11073114B2 (en) | 2018-12-12 | 2021-07-27 | General Electric Company | Fuel injector assembly for a heat engine |
US11286884B2 (en) | 2018-12-12 | 2022-03-29 | General Electric Company | Combustion section and fuel injector assembly for a heat engine |
GB201820206D0 (en) * | 2018-12-12 | 2019-01-23 | Rolls Royce Plc | A fuel spray nozzle |
US11156360B2 (en) | 2019-02-18 | 2021-10-26 | General Electric Company | Fuel nozzle assembly |
FR3095499B1 (en) * | 2019-04-23 | 2021-06-11 | Safran Helicopter Engines | INJECTOR OF A MIXTURE OF AIR AND FUEL FOR A TURBOMACHINE COMBUSTION CHAMBER |
US11371709B2 (en) | 2020-06-30 | 2022-06-28 | General Electric Company | Combustor air flow path |
CN115711176A (en) * | 2021-08-23 | 2023-02-24 | 通用电气公司 | Dome with integrated trumpet swirler |
DE102022201182A1 (en) | 2022-02-04 | 2023-08-10 | Rolls-Royce Deutschland Ltd & Co Kg | Nozzle assembly with connecting pipe passing through a fuel pipe in a nozzle main body for air flow |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2152057A (en) * | 1938-02-05 | 1939-03-28 | Frank A Kane | Nozzle |
US3153319A (en) * | 1952-07-25 | 1964-10-20 | Young Alec David | Jet noise suppression means |
US2982098A (en) * | 1953-04-22 | 1961-05-02 | Power Jets Res & Dev Ltd | Liquid fuel vaporizing combustion systems |
US3866413A (en) * | 1973-01-22 | 1975-02-18 | Parker Hannifin Corp | Air blast fuel atomizer |
US3974646A (en) * | 1974-06-11 | 1976-08-17 | United Technologies Corporation | Turbofan engine with augmented combustion chamber using vorbix principle |
US4260367A (en) * | 1978-12-11 | 1981-04-07 | United Technologies Corporation | Fuel nozzle for burner construction |
US4284170A (en) * | 1979-10-22 | 1981-08-18 | United Technologies Corporation | Gas turbine noise suppressor |
US4470262A (en) * | 1980-03-07 | 1984-09-11 | Solar Turbines, Incorporated | Combustors |
US4365753A (en) * | 1980-08-22 | 1982-12-28 | Parker-Hannifin Corporation | Boundary layer prefilmer airblast nozzle |
EP0210462B1 (en) * | 1985-07-30 | 1989-03-15 | BBC Brown Boveri AG | Dual combustor |
US5121608A (en) * | 1988-02-06 | 1992-06-16 | Rolls-Royce Plc | Gas turbine engine fuel burner |
FR2692502B1 (en) * | 1992-06-19 | 1995-03-31 | Total Raffinage Distribution | Method and device for spraying a liquid using at least one auxiliary fluid. |
US5251447A (en) * | 1992-10-01 | 1993-10-12 | General Electric Company | Air fuel mixer for gas turbine combustor |
US5505045A (en) * | 1992-11-09 | 1996-04-09 | Fuel Systems Textron, Inc. | Fuel injector assembly with first and second fuel injectors and inner, outer, and intermediate air discharge chambers |
EP0620403B1 (en) * | 1993-04-08 | 1996-12-04 | ABB Management AG | Mixing and flame stabilizing device in a combustion chamber with premixing combustion |
DE59402803D1 (en) * | 1993-04-08 | 1997-06-26 | Asea Brown Boveri | Combustion chamber |
US5487274A (en) * | 1993-05-03 | 1996-01-30 | General Electric Company | Screech suppressor for advanced low emissions gas turbine combustor |
US5676538A (en) * | 1993-06-28 | 1997-10-14 | General Electric Company | Fuel nozzle for low-NOx combustor burners |
US5638682A (en) * | 1994-09-23 | 1997-06-17 | General Electric Company | Air fuel mixer for gas turbine combustor having slots at downstream end of mixing duct |
WO1999006767A1 (en) * | 1997-07-31 | 1999-02-11 | Siemens Aktiengesellschaft | Burner |
JP2002517700A (en) * | 1998-06-04 | 2002-06-18 | シーメンス アクチエンゲゼルシヤフト | Fuel injection nozzle |
WO1999063276A1 (en) * | 1998-06-04 | 1999-12-09 | Siemens Aktiengesellschaft | Fuel jet injector and method for injecting a fuel jet |
WO2000012939A1 (en) * | 1998-08-31 | 2000-03-09 | Siemens Aktiengesellschaft | Burner assembly |
US6161387A (en) * | 1998-10-30 | 2000-12-19 | United Technologies Corporation | Multishear fuel injector |
US6272840B1 (en) * | 2000-01-13 | 2001-08-14 | Cfd Research Corporation | Piloted airblast lean direct fuel injector |
GB0219458D0 (en) * | 2002-08-21 | 2002-09-25 | Rolls Royce Plc | Fuel injection apparatus |
-
2002
- 2002-08-21 GB GBGB0219461.1A patent/GB0219461D0/en not_active Ceased
-
2003
- 2003-07-26 EP EP03254684A patent/EP1391653A3/en not_active Withdrawn
- 2003-07-30 US US10/629,795 patent/US20050097889A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP1391653A2 (en) | 2004-02-25 |
US20050097889A1 (en) | 2005-05-12 |
EP1391653A3 (en) | 2005-05-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |