EP1526332A3 - Fuel injection nozzle - Google Patents
Fuel injection nozzle Download PDFInfo
- Publication number
- EP1526332A3 EP1526332A3 EP20040023823 EP04023823A EP1526332A3 EP 1526332 A3 EP1526332 A3 EP 1526332A3 EP 20040023823 EP20040023823 EP 20040023823 EP 04023823 A EP04023823 A EP 04023823A EP 1526332 A3 EP1526332 A3 EP 1526332A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- injection nozzle
- fuel injection
- fuel
- fuel openings
- openings
- 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.)
- Withdrawn
Links
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
-
- 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
- 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
- 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
Abstract
Die Erfindung bezieht sich auf eine Kraftstoffeinspritzdüse für eine Gasturbinenbrennkammer, mit einem Filmleger 1, in dem mehrere Kraftstofföffnungen 2 ausgebildet sind. Die Erfindung zeichnet sich dadurch aus, dass die Mittelachsen 5 der Kraftstofföffnungen 2 durch den Filmleger 1 bezüglich ihrer radialen Ausrichtung im Wesentlichen parallel zur Hauptströmungsrichtung 6 der Luft angeordnet sind. The invention relates to a fuel injection nozzle for a gas turbine combustor, with a film former 1, in which a plurality of fuel openings 2 are formed. The invention is characterized in that the center axes 5 of the fuel openings 2 are arranged by the film feeder 1 with respect to their radial orientation substantially parallel to the main flow direction 6 of the air.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE2003148604 DE10348604A1 (en) | 2003-10-20 | 2003-10-20 | Fuel injector with filmy fuel placement |
DE10348604 | 2003-10-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1526332A2 EP1526332A2 (en) | 2005-04-27 |
EP1526332A3 true EP1526332A3 (en) | 2012-02-15 |
Family
ID=34384376
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP20040023823 Withdrawn EP1526332A3 (en) | 2003-10-20 | 2004-10-06 | Fuel injection nozzle |
Country Status (3)
Country | Link |
---|---|
US (1) | US9033263B2 (en) |
EP (1) | EP1526332A3 (en) |
DE (1) | DE10348604A1 (en) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060283181A1 (en) * | 2005-06-15 | 2006-12-21 | Arvin Technologies, Inc. | Swirl-stabilized burner for thermal management of exhaust system and associated method |
EP2236932A1 (en) | 2009-03-17 | 2010-10-06 | Siemens Aktiengesellschaft | Burner and method for operating a burner, in particular for a gas turbine |
US8453454B2 (en) * | 2010-04-14 | 2013-06-04 | General Electric Company | Coannular oil injection nozzle |
US9188063B2 (en) | 2011-11-03 | 2015-11-17 | Delavan Inc. | Injectors for multipoint injection |
EP3087323B1 (en) * | 2014-04-03 | 2019-08-21 | Siemens Aktiengesellschaft | Fuel nozzle, burner having such a fuel nozzle, and gas turbine having such a burner |
US10508812B2 (en) | 2014-05-12 | 2019-12-17 | General Electric Company | Pre-film liquid fuel cartridge |
US10385809B2 (en) | 2015-03-31 | 2019-08-20 | Delavan Inc. | Fuel nozzles |
US9897321B2 (en) | 2015-03-31 | 2018-02-20 | Delavan Inc. | Fuel nozzles |
US10132500B2 (en) | 2015-10-16 | 2018-11-20 | Delavan Inc. | Airblast injectors |
US20180058696A1 (en) * | 2016-08-23 | 2018-03-01 | General Electric Company | Fuel-air mixer assembly for use in a combustor of a turbine engine |
US10876477B2 (en) | 2016-09-16 | 2020-12-29 | Delavan Inc | Nozzles with internal manifolding |
US10344981B2 (en) | 2016-12-16 | 2019-07-09 | Delavan Inc. | Staged dual fuel radial nozzle with radial liquid fuel distributor |
US20180335214A1 (en) * | 2017-05-18 | 2018-11-22 | United Technologies Corporation | Fuel air mixer assembly for a gas turbine engine combustor |
US11149948B2 (en) | 2017-08-21 | 2021-10-19 | General Electric Company | Fuel nozzle with angled main injection ports and radial main injection ports |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3819898A1 (en) * | 1988-06-11 | 1989-12-14 | Daimler Benz Ag | Combustion chamber for a thermal turbo-engine |
DE19532264A1 (en) * | 1995-09-01 | 1997-03-06 | Mtu Muenchen Gmbh | Device for the preparation of a mixture of fuel and air in combustion chambers for gas turbine engines |
EP1331441A1 (en) * | 2002-01-21 | 2003-07-30 | National Aerospace Laboratory of Japan | Liquid atomizing nozzle |
Family Cites Families (49)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3955361A (en) * | 1971-12-15 | 1976-05-11 | Phillips Petroleum Company | Gas turbine combustor with controlled fuel mixing |
SE371685B (en) | 1972-04-21 | 1974-11-25 | Stal Laval Turbin Ab | |
GB1421399A (en) | 1972-11-13 | 1976-01-14 | Snecma | Fuel injectors |
US3866413A (en) * | 1973-01-22 | 1975-02-18 | Parker Hannifin Corp | Air blast fuel atomizer |
US3930369A (en) * | 1974-02-04 | 1976-01-06 | General Motors Corporation | Lean prechamber outflow combustor with two sets of primary air entrances |
US3980233A (en) * | 1974-10-07 | 1976-09-14 | Parker-Hannifin Corporation | Air-atomizing fuel nozzle |
US4170108A (en) * | 1975-04-25 | 1979-10-09 | Rolls-Royce Limited | Fuel injectors for gas turbine engines |
US4141213A (en) * | 1977-06-23 | 1979-02-27 | General Motors Corporation | Pilot flame tube |
US4218020A (en) * | 1979-02-23 | 1980-08-19 | General Motors Corporation | Elliptical airblast nozzle |
US4425755A (en) | 1980-09-16 | 1984-01-17 | Rolls-Royce Limited | Gas turbine dual fuel burners |
CH670296A5 (en) | 1986-02-24 | 1989-05-31 | Bbc Brown Boveri & Cie | Gas turbine fuel nozzle - has externally-supported premixing chamber for liq. fuel and air |
CA1306873C (en) * | 1987-04-27 | 1992-09-01 | Jack R. Taylor | Low coke fuel injector for a gas turbine engine |
FR2673705A1 (en) * | 1991-03-06 | 1992-09-11 | Snecma | Combustion chamber of a turbine engine equipped with an anti-coking device for the bottom of said chamber |
DE4228816C2 (en) * | 1992-08-29 | 1998-08-06 | Mtu Muenchen Gmbh | Burners for gas turbine engines |
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 |
FR2698157B1 (en) * | 1992-11-18 | 1994-12-16 | Snecma | Aerodynamic combustion chamber injection system. |
US5303554A (en) | 1992-11-27 | 1994-04-19 | Solar Turbines Incorporated | Low NOx injector with central air swirling and angled fuel inlets |
DE4316474A1 (en) | 1993-05-17 | 1994-11-24 | Abb Management Ag | Premix burner for operating an internal combustion engine, a combustion chamber of a gas turbine group or a combustion system |
US5479781A (en) | 1993-09-02 | 1996-01-02 | General Electric Company | Low emission combustor having tangential lean direct injection |
US5351477A (en) * | 1993-12-21 | 1994-10-04 | General Electric Company | Dual fuel mixer for gas turbine combustor |
DE4424597B4 (en) | 1994-07-13 | 2006-03-23 | Alstom | incinerator |
US5701732A (en) | 1995-01-24 | 1997-12-30 | Delavan Inc. | Method and apparatus for purging of gas turbine injectors |
US5778676A (en) * | 1996-01-02 | 1998-07-14 | General Electric Company | Dual fuel mixer for gas turbine combustor |
US5680766A (en) * | 1996-01-02 | 1997-10-28 | General Electric Company | Dual fuel mixer for gas turbine combustor |
GB2319078B (en) * | 1996-11-08 | 1999-11-03 | Europ Gas Turbines Ltd | Combustor arrangement |
JP3619626B2 (en) * | 1996-11-29 | 2005-02-09 | 株式会社東芝 | Operation method of gas turbine combustor |
US5816049A (en) * | 1997-01-02 | 1998-10-06 | General Electric Company | Dual fuel mixer for gas turbine combustor |
DE19729246C2 (en) | 1997-07-09 | 2001-06-28 | Deutsch Zentr Luft & Raumfahrt | Atomizer nozzle for atomizing fuel in burners |
US5966937A (en) * | 1997-10-09 | 1999-10-19 | United Technologies Corporation | Radial inlet swirler with twisted vanes for fuel injector |
GB9726697D0 (en) | 1997-12-18 | 1998-02-18 | Secr Defence | Fuel injector |
GB2333832A (en) * | 1998-01-31 | 1999-08-04 | Europ Gas Turbines Ltd | Multi-fuel gas turbine engine combustor |
DE19803879C1 (en) * | 1998-01-31 | 1999-08-26 | Mtu Muenchen Gmbh | Dual fuel burner |
US6119459A (en) * | 1998-08-18 | 2000-09-19 | Alliedsignal Inc. | Elliptical axial combustor swirler |
DE59810284D1 (en) | 1998-10-14 | 2004-01-08 | Alstom Switzerland Ltd | Burner for operating a heat generator |
IT1313547B1 (en) * | 1999-09-23 | 2002-07-24 | Nuovo Pignone Spa | PRE-MIXING CHAMBER FOR GAS TURBINES |
EP1096201A1 (en) * | 1999-10-29 | 2001-05-02 | Siemens Aktiengesellschaft | Burner |
US6272840B1 (en) | 2000-01-13 | 2001-08-14 | Cfd Research Corporation | Piloted airblast lean direct fuel injector |
US6474071B1 (en) * | 2000-09-29 | 2002-11-05 | General Electric Company | Multiple injector combustor |
US6363726B1 (en) * | 2000-09-29 | 2002-04-02 | General Electric Company | Mixer having multiple swirlers |
DE10056243A1 (en) * | 2000-11-14 | 2002-05-23 | Alstom Switzerland Ltd | Combustion chamber and method for operating this combustion chamber |
FR2836986B1 (en) * | 2002-03-07 | 2004-11-19 | Snecma Moteurs | MULTI-MODEL INJECTION SYSTEM FOR AN AIR / FUEL MIXTURE IN A COMBUSTION CHAMBER |
EP1499800B1 (en) * | 2002-04-26 | 2011-06-29 | Rolls-Royce Corporation | Fuel premixing module for gas turbine engine combustor |
DE10219354A1 (en) * | 2002-04-30 | 2003-11-13 | Rolls Royce Deutschland | Gas turbine combustion chamber with targeted fuel introduction to improve the homogeneity of the fuel-air mixture |
US6986255B2 (en) * | 2002-10-24 | 2006-01-17 | Rolls-Royce Plc | Piloted airblast lean direct fuel injector with modified air splitter |
JP4065947B2 (en) * | 2003-08-05 | 2008-03-26 | 独立行政法人 宇宙航空研究開発機構 | Fuel / air premixer for gas turbine combustor |
DE10340826A1 (en) * | 2003-09-04 | 2005-03-31 | Rolls-Royce Deutschland Ltd & Co Kg | Homogeneous mixture formation by twisted injection of the fuel |
US6968255B1 (en) * | 2004-10-22 | 2005-11-22 | Pulse Microsystems, Ltd. | Method and system for automatically deriving stippling stitch designs in embroidery patterns |
JP2006300448A (en) * | 2005-04-22 | 2006-11-02 | Mitsubishi Heavy Ind Ltd | Combustor for gas turbine |
-
2003
- 2003-10-20 DE DE2003148604 patent/DE10348604A1/en not_active Withdrawn
-
2004
- 2004-10-06 EP EP20040023823 patent/EP1526332A3/en not_active Withdrawn
- 2004-10-19 US US10/967,320 patent/US9033263B2/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3819898A1 (en) * | 1988-06-11 | 1989-12-14 | Daimler Benz Ag | Combustion chamber for a thermal turbo-engine |
DE19532264A1 (en) * | 1995-09-01 | 1997-03-06 | Mtu Muenchen Gmbh | Device for the preparation of a mixture of fuel and air in combustion chambers for gas turbine engines |
EP1331441A1 (en) * | 2002-01-21 | 2003-07-30 | National Aerospace Laboratory of Japan | Liquid atomizing nozzle |
Also Published As
Publication number | Publication date |
---|---|
US20050133642A1 (en) | 2005-06-23 |
US9033263B2 (en) | 2015-05-19 |
EP1526332A2 (en) | 2005-04-27 |
DE10348604A1 (en) | 2005-07-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
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AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR |
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AX | Request for extension of the european patent |
Extension state: AL HR LT LV MK |
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RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: RACKWITZ, LEIF |
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PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
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AX | Request for extension of the european patent |
Extension state: AL HR LT LV MK |
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RIC1 | Information provided on ipc code assigned before grant |
Ipc: F23R 3/28 20060101ALI20120112BHEP Ipc: F23D 11/10 20060101AFI20120112BHEP |
|
17P | Request for examination filed |
Effective date: 20120814 |
|
AKX | Designation fees paid |
Designated state(s): DE FR GB |
|
17Q | First examination report despatched |
Effective date: 20130618 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
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18D | Application deemed to be withdrawn |
Effective date: 20160310 |