EP1526332A3 - Fuel injection nozzle - Google Patents

Fuel injection nozzle Download PDF

Info

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Withdrawn
Application number
EP20040023823
Other languages
German (de)
French (fr)
Other versions
EP1526332A2 (en
Inventor
Leif Rackwitz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
Rolls Royce Deutschland Ltd and Co KG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rolls Royce Deutschland Ltd and Co KG filed Critical Rolls Royce Deutschland Ltd and Co KG
Publication of EP1526332A2 publication Critical patent/EP1526332A2/en
Publication of EP1526332A3 publication Critical patent/EP1526332A3/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners 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
    • F23D11/106Burners 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D11/00Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10Burners 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
    • F23D11/106Burners 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
    • F23D11/107Burners 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23DBURNERS
    • F23D2900/00Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/11101Pulverising 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.

Figure imgaf001
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.
Figure imgaf001

EP20040023823 2003-10-20 2004-10-06 Fuel injection nozzle Withdrawn EP1526332A3 (en)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
EP1526332A3 (en) Fuel injection nozzle
EP1607580A3 (en) Platform cooling of vanes in a gas turbine
EP1881161A3 (en) Aeroengine bleed valve
EP1832733A3 (en) Inlet cone made of a fibre composite for a gas turbine plant and method for its manufacture
EP2261463A3 (en) Turbomachine with a group of bladed stages
EP2273196A3 (en) Gas turbine combustion chamber head
EP1832812A3 (en) Gas turbine combustion chamber wall with absorption of combustion chamber vibrations
EP2003398A3 (en) Fuel nozzle providing shaped fuel spray
EP1512912A3 (en) Homogeneous mixture formation by swirled injection of the fuel
CH699759B8 (en) Pre-mixing device with protection device for a turbine engine and method for producing the premixing device.
EP1892399A3 (en) Aero engine bleed valve
EP1830042A3 (en) Static mixer and exhaust after treatment system
EP2275743A3 (en) Gas turbine combustion chamber with starter film for cooling the combustion chamber wall
AT500458B1 (en) INTERNAL COMBUSTION ENGINE, IN PARTICULAR OTTO INTERNAL COMBUSTION ENGINE
EP1843099A3 (en) Gas turbine combustor and operating method
DE20117873U1 (en) Open filter body with improved flow properties
EP2589751A3 (en) Turbine last stage flow path
EP1605204A3 (en) Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same
EP2014987A3 (en) Method of producing effusion holes
EP1645802A3 (en) Premix Burner
DE112014002109T5 (en) Exhaust diffuser for a gas turbine engine exhaust system
EP1251314A3 (en) Catalytic burner
EP2423597A3 (en) Premix burner for a gas turbine
RU2007134591A (en) FUEL INJECTOR WITH DISTRIBUTED CHANNELS
EP1598106A3 (en) Nozzle unit

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

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

AX Request for extension of the european patent

Extension state: AL HR LT LV MK

RIN1 Information on inventor provided before grant (corrected)

Inventor name: RACKWITZ, LEIF

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

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

AX Request for extension of the european patent

Extension state: AL HR LT LV MK

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

18D Application deemed to be withdrawn

Effective date: 20160310