FR2774455B1 - Systeme de combustion pour moteur a turbine a gaz et son procede de mise en oeuvre - Google Patents

Systeme de combustion pour moteur a turbine a gaz et son procede de mise en oeuvre

Info

Publication number
FR2774455B1
FR2774455B1 FR9901039A FR9901039A FR2774455B1 FR 2774455 B1 FR2774455 B1 FR 2774455B1 FR 9901039 A FR9901039 A FR 9901039A FR 9901039 A FR9901039 A FR 9901039A FR 2774455 B1 FR2774455 B1 FR 2774455B1
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
implementation method
combustion system
combustion
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 - Lifetime
Application number
FR9901039A
Other languages
English (en)
Other versions
FR2774455A1 (fr
Inventor
Eric Roy Norster
Mahmoud Kowkabi
Pietro Simon De
Hoger Gunter Heinrich Hesse
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.)
Siemens AG
Original Assignee
Alstom Power UK Holdings Ltd
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 Alstom Power UK Holdings Ltd filed Critical Alstom Power UK Holdings Ltd
Publication of FR2774455A1 publication Critical patent/FR2774455A1/fr
Application granted granted Critical
Publication of FR2774455B1 publication Critical patent/FR2774455B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other at least one of the fluids being submitted to a swirling motion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • 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
    • F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/76—Protecting flame and burner parts
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • 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
    • F23R3/36—Supply of different fuels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2202/00—Fluegas recirculation
    • F23C2202/40—Inducing local whirls around flame
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2206/00—Burners for specific applications
    • F23D2206/10—Turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2214/00—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
    • F23D2900/00015—Pilot burners specially adapted for low load or transient conditions, e.g. for increasing stability

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
FR9901039A 1998-01-31 1999-01-29 Systeme de combustion pour moteur a turbine a gaz et son procede de mise en oeuvre Expired - Lifetime FR2774455B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9802021A GB2333832A (en) 1998-01-31 1998-01-31 Multi-fuel gas turbine engine combustor

Publications (2)

Publication Number Publication Date
FR2774455A1 FR2774455A1 (fr) 1999-08-06
FR2774455B1 true FR2774455B1 (fr) 2000-11-24

Family

ID=10826176

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9901039A Expired - Lifetime FR2774455B1 (fr) 1998-01-31 1999-01-29 Systeme de combustion pour moteur a turbine a gaz et son procede de mise en oeuvre

Country Status (6)

Country Link
US (1) US6532726B2 (fr)
JP (2) JPH11257100A (fr)
DE (1) DE19903770B4 (fr)
FR (1) FR2774455B1 (fr)
GB (2) GB2333832A (fr)
IT (1) IT1307122B1 (fr)

Families Citing this family (72)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10064893A1 (de) * 2000-12-23 2002-11-14 Alstom Switzerland Ltd Brenner mit gestufter Brennstoffeindüsung
SE521293C2 (sv) * 2001-02-06 2003-10-21 Volvo Aero Corp Förfarande och anordning för tillförsel av bränsle till en brännkammare
US6427447B1 (en) * 2001-02-06 2002-08-06 United Technologies Corporation Bulkhead for dual fuel industrial and aeroengine gas turbines
FR2824625B1 (fr) * 2001-05-10 2003-08-15 Inst Francais Du Petrole Dispositif et procede d'injection d'un combustible liquide dans un flux d'air pour une chambre de combustion
AU2003225181A1 (en) * 2002-04-26 2003-11-10 Rolls-Royce Corporation Fuel premixing module for gas turbine engine combustor
DE50313028D1 (de) * 2002-05-02 2010-10-14 Alstom Technology Ltd Katalytischer Brenner
GB0230070D0 (en) * 2002-12-23 2003-01-29 Bowman Power Systems Ltd A combustion device
US6935116B2 (en) * 2003-04-28 2005-08-30 Power Systems Mfg., Llc Flamesheet combustor
US6986254B2 (en) * 2003-05-14 2006-01-17 Power Systems Mfg, Llc Method of operating a flamesheet combustor
DE10348604A1 (de) * 2003-10-20 2005-07-28 Rolls-Royce Deutschland Ltd & Co Kg Kraftstoffeinspritzdüse mit filmartiger Kraftstoffplatzierung
WO2007036964A1 (fr) * 2005-09-30 2007-04-05 Ansaldo Energia S.P.A. Procédé d’activation d’une turbine à gaz équipée d’un brûleur à gaz, et dispositif de tourbillonnement axial pour ledit brûleur
GB2432655A (en) * 2005-11-26 2007-05-30 Siemens Ag Combustion apparatus
US7640725B2 (en) * 2006-01-12 2010-01-05 Siemens Energy, Inc. Pilot fuel flow tuning for gas turbine combustors
EP1835231A1 (fr) * 2006-03-13 2007-09-19 Siemens Aktiengesellschaft Brûleur pour une chambre de combustion de turbine à gaz et procédé d'opération du brûleur
EP1835229A1 (fr) 2006-03-13 2007-09-19 Siemens Aktiengesellschaft Chambre de combustion et procédé pour son fonctionnement
US7690203B2 (en) * 2006-03-17 2010-04-06 Siemens Energy, Inc. Removable diffusion stage for gas turbine engine fuel nozzle assemblages
EP1843098A1 (fr) * 2006-04-07 2007-10-10 Siemens Aktiengesellschaft Chambre de combustion pour turbine à gaz
US7631500B2 (en) * 2006-09-29 2009-12-15 General Electric Company Methods and apparatus to facilitate decreasing combustor acoustics
GB2444737B (en) * 2006-12-13 2009-03-04 Siemens Ag Improvements in or relating to burners for a gas turbine engine
EP1970629A1 (fr) * 2007-03-15 2008-09-17 Siemens Aktiengesellschaft Alimentation étagée pour un brûleur
DE102007043626A1 (de) 2007-09-13 2009-03-19 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität
GB2454247A (en) * 2007-11-02 2009-05-06 Siemens Ag A Combustor for a Gas-Turbine Engine Has a Burner Head with Fuel Delivered at a Compound Angle
US7617684B2 (en) * 2007-11-13 2009-11-17 Opra Technologies B.V. Impingement cooled can combustor
GB2455289B (en) * 2007-12-03 2010-04-07 Siemens Ag Improvements in or relating to burners for a gas-turbine engine
US20090165435A1 (en) * 2008-01-02 2009-07-02 Michal Koranek Dual fuel can combustor with automatic liquid fuel purge
US8096132B2 (en) * 2008-02-20 2012-01-17 Flexenergy Energy Systems, Inc. Air-cooled swirlerhead
US20090241547A1 (en) * 2008-03-31 2009-10-01 Andrew Luts Gas turbine fuel injector for lower heating capacity fuels
EP2107313A1 (fr) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Alimentation étagée de combustible dans un brûleur
DE102008019117A1 (de) * 2008-04-16 2009-10-22 Man Turbo Ag Verfahren zum Betreiben eines Vormischbrenners und ein Vormischbrenner zur Durchführung des Verfahrens
EP2112433A1 (fr) * 2008-04-23 2009-10-28 Siemens Aktiengesellschaft Chambre de mélange
EP2169312A1 (fr) * 2008-09-25 2010-03-31 Siemens Aktiengesellschaft Agitateur à gradins pour contrôle dynamique
US8220270B2 (en) * 2008-10-31 2012-07-17 General Electric Company Method and apparatus for affecting a recirculation zone in a cross flow
US8453425B2 (en) * 2009-01-23 2013-06-04 Lockheed Martin Corporation Soot reduction by combustor conditioning
US20100232930A1 (en) * 2009-03-16 2010-09-16 Terry Lynn Gregory Gas turbine engine
EP2239501B1 (fr) * 2009-04-06 2012-01-04 Siemens Aktiengesellschaft Tourbillonnement, chambre à combustion, et turbine à gaz avec tourbillon amélioré
EP2246617B1 (fr) * 2009-04-29 2017-04-19 Siemens Aktiengesellschaft Brûleur pour moteur de turbine à gaz
US8607570B2 (en) * 2009-05-06 2013-12-17 General Electric Company Airblown syngas fuel nozzle with diluent openings
US20100281869A1 (en) * 2009-05-06 2010-11-11 Mark Allan Hadley Airblown Syngas Fuel Nozzle With Diluent Openings
US20100281872A1 (en) * 2009-05-06 2010-11-11 Mark Allan Hadley Airblown Syngas Fuel Nozzle With Diluent Openings
US9297531B2 (en) * 2009-08-13 2016-03-29 Siemens Aktiengesellschaft Gas turbine engine fuel control using gas measurement at the air inlet
EP2327933A1 (fr) * 2009-11-30 2011-06-01 Siemens Aktiengesellschaft Agencement de brûleur
DE102009054669A1 (de) * 2009-12-15 2011-06-16 Man Diesel & Turbo Se Brenner für eine Turbine
US8650851B2 (en) * 2010-01-05 2014-02-18 General Electric Company Systems and methods for controlling fuel flow within a machine
EP2400222A1 (fr) * 2010-06-28 2011-12-28 Siemens Aktiengesellschaft Appareil de combustion
US8511092B2 (en) * 2010-08-13 2013-08-20 General Electric Company Dimpled/grooved face on a fuel injection nozzle body for flame stabilization and related method
EP2489939A1 (fr) * 2011-02-18 2012-08-22 Siemens Aktiengesellschaft Chambre de combustion dotée d'une section de paroi et d'un élément de bord
GB201106116D0 (en) * 2011-04-12 2011-05-25 Rolls Royce Plc Fuel supply arrangement
US20120282558A1 (en) * 2011-05-05 2012-11-08 General Electric Company Combustor nozzle and method for supplying fuel to a combustor
ITMI20111576A1 (it) * 2011-09-02 2013-03-03 Alstom Technology Ltd Metodo per commutare un dispositivo di combustione
US9279370B2 (en) 2011-10-28 2016-03-08 General Electric Company Turbomachine and method of operating a turbomachine to perform a fuel change over at a high load
EP2629008A1 (fr) * 2012-02-15 2013-08-21 Siemens Aktiengesellschaft Injection de carburant inclinée dans une fente de tourbillonnement
JP5924066B2 (ja) * 2012-03-27 2016-05-25 いすゞ自動車株式会社 ディーゼルエンジンの始動装置及び始動方法
WO2013147632A1 (fr) * 2012-03-29 2013-10-03 General Electric Company Capot d'extrémité bidirectionnelle à capacité d'extraction pour dispositif combustor de turbine à gaz
US9212609B2 (en) 2012-11-20 2015-12-15 Solar Turbines Incoporated Combination air assist and pilot gaseous fuel circuit
EP2743581A1 (fr) * 2012-12-11 2014-06-18 Siemens Aktiengesellschaft Injection de carburant à air dirigé
EP2772689A1 (fr) * 2013-02-27 2014-09-03 Siemens Aktiengesellschaft Tir laser supplémentaire pour la stabilité de combustion
DE102013016202A1 (de) * 2013-09-28 2015-04-02 Dürr Systems GmbH "Brennerkopf eines Brenners und Gasturbine mit einem solchen Brenner"
JP6366259B2 (ja) * 2013-11-18 2018-08-01 三菱日立パワーシステムズ株式会社 ２軸ガスタービンの制御装置及び制御方法
EP2905535A1 (fr) * 2014-02-06 2015-08-12 Siemens Aktiengesellschaft Chambre à combustion
US20160348914A1 (en) * 2014-02-11 2016-12-01 Siemens Aktiengesellschaft Swirler for a burner of a gas turbine engine
EP2942563A1 (fr) 2014-05-09 2015-11-11 Siemens Aktiengesellschaft Élément de tourbillonnement d'un brûleur de moteur de turbine à gaz, brûleur de moteur de turbine à gaz et moteur de turbine à gaz
JP6325930B2 (ja) * 2014-07-24 2018-05-16 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
EP3317585B1 (fr) * 2015-06-30 2021-08-04 H2 Ip Uk Limited Ensemble de cartouche de combustible pour une turbine à gaz
EP3184898A1 (fr) * 2015-12-23 2017-06-28 Siemens Aktiengesellschaft Chambre de combustion pour turbine à gaz
US10502425B2 (en) * 2016-06-03 2019-12-10 General Electric Company Contoured shroud swirling pre-mix fuel injector assembly
EP3301374A1 (fr) 2016-09-29 2018-04-04 Siemens Aktiengesellschaft Ensemble de bruleur pilote dote d'une alimentation d'air pilote
JP6779097B2 (ja) * 2016-10-24 2020-11-04 三菱パワー株式会社 ガスタービン燃焼器及びその運転方法
DE102017114362A1 (de) * 2017-06-28 2019-01-03 Man Diesel & Turbo Se Brennkammer einer Gasturbine, Gasturbine und Verfahren zum Betreiben derselben
DE102018112540A1 (de) * 2018-05-25 2019-11-28 Kueppers Solutions Gmbh Brennstoffdüsensystem
US11149941B2 (en) * 2018-12-14 2021-10-19 Delavan Inc. Multipoint fuel injection for radial in-flow swirl premix gas fuel injectors
US20210207541A1 (en) * 2020-01-08 2021-07-08 United Technologies Corporation Method of using a primary fuel to pilot liquid fueled combustors
US11326521B2 (en) * 2020-06-30 2022-05-10 General Electric Company Methods of igniting liquid fuel in a turbomachine

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB217993A (en) * 1923-03-26 1924-06-26 Thomas Crane Improvements in tobacco pipes
CA1178452A (fr) * 1981-07-23 1984-11-27 Robie L. Faulkner Turbines a gaz
DE3241162A1 (de) * 1982-11-08 1984-05-10 Kraftwerk Union AG, 4330 Mülheim Vormischbrenner mit integriertem diffusionsbrenner
GB2175993B (en) * 1985-06-07 1988-12-21 Rolls Royce Improvements in or relating to dual fuel injectors
JP2758301B2 (ja) * 1991-11-29 1998-05-28 株式会社東芝 ガスタービン燃焼器
US5359847B1 (en) * 1993-06-01 1996-04-09 Westinghouse Electric Corp Dual fuel ultra-flow nox combustor
US5404711A (en) * 1993-06-10 1995-04-11 Solar Turbines Incorporated Dual fuel injector nozzle for use with a gas turbine engine
US5450724A (en) * 1993-08-27 1995-09-19 Northern Research & Engineering Corporation Gas turbine apparatus including fuel and air mixer
DE69617290T2 (de) * 1995-01-13 2002-06-13 Europ Gas Turbines Ltd Verbrennungsgerät für Gasturbinenmotor
GB2297151B (en) * 1995-01-13 1998-04-22 Europ Gas Turbines Ltd Fuel injector arrangement for gas-or liquid-fuelled turbine

Also Published As

Publication number Publication date
JP4346724B2 (ja) 2009-10-21
GB2333832A (en) 1999-08-04
GB2336663A (en) 1999-10-27
US20010027637A1 (en) 2001-10-11
DE19903770B4 (de) 2009-11-12
GB9901797D0 (en) 1999-03-17
JPH11270357A (ja) 1999-10-05
US6532726B2 (en) 2003-03-18
DE19903770A1 (de) 1999-09-23
ITTO990062A1 (it) 2000-07-29
IT1307122B1 (it) 2001-10-29
FR2774455A1 (fr) 1999-08-06
GB2336663B (en) 2000-10-04
JPH11257100A (ja) 1999-09-21
GB9802021D0 (en) 1998-03-25

Similar Documents

Publication Publication Date Title
FR2774455B1 (fr) Systeme de combustion pour moteur a turbine a gaz et son procede de mise en oeuvre
FR2741385B1 (fr) Procede de mise en oeuvre d'un moteur diesel
FR2828714B1 (fr) Procede et dispositif de mise en oeuvre d'un moteur a combustion interne
GB2348090B (en) A system and method for controlling an internal combustion engine
GB2339032B (en) Apparatus for controlling a fuel system of an internal combustion engine
FR2777039B1 (fr) Systeme de purification de gaz d'echappement pour moteur a combustion interne
FR2730011B1 (fr) Moteur a combustion interne a plusieurs cylindres a turbocompresseur avec reinjection des gaz d'echappement et procede pour la mise en oeuvre d'un tel moteur a combustion interne
FR2722533B1 (fr) Systeme de recyclage des gaz d'echappement pour un moteur a combustion interne
GB2368144B (en) A control system and method for shutting down an internal combustion engine
FR2830287B1 (fr) Procede et moyens pour la mise en oeuvre d'un moteur a combustion interne
FR2771137B1 (fr) Procede de commande d'un turbocompresseur a gaz d'echappement de suralimentation a geometrie de turbine variable
EP0969190A4 (fr) Procede et appareil de regulation du refroidissement pour moteurs a combustion interne
GB2339307B (en) Method for operating an internal combustion engine
FR2719082B1 (fr) Procédé de refroidissement des gaz d'échappement d'un moteur Diesel, et dispositif pour la mise en Óoeuvre dudit procédé.
FR2752440B1 (fr) Systeme de refroidissement pour un moteur a combustion interne
FR2745033B1 (fr) Systeme de refroidissement pour un moteur a combustion interne
DK111996A (da) Cylindersmøreenhed til en flercylindret forbrændingsmotor, og fremgangsmåde til styring af leveringsmængden fra en cylindersmøreenhed
AU2001296340A1 (en) Computerized system and method for synchronizing engine speed of a plurality of internal combustion engines
FR2771774B1 (fr) Procede de surveillance du systeme d'epuration des gaz d'echappement d'un moteur a combustion interne a allumage exterieur
FR2813100B1 (fr) Procede et dispositif pour la mise en oeuvre d'un moteur a combustion interne
GB9919141D0 (en) Method and apparatus for rejecting waste heat from a system including a combustion engine
FR2744491B1 (fr) Systeme de recyclage de gaz d'echappement pour un moteur a combustion interne
GB2274681B (en) Method for operation of an exhaust system for an internal combustion engine and exhaust system therefor
FR2831923B1 (fr) Systeme et procede de purification de gaz d'echappement destines a un moteur a combustion interne
DE59811055D1 (de) Verfahren zur Synchronisation einer mehrzylindrigen Brennkraftmaschine

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 17

TP Transmission of property

Owner name: SIEMENS AKTIENGESELLSCHAFT, DE

Effective date: 20151130

PLFP Fee payment

Year of fee payment: 18

PLFP Fee payment

Year of fee payment: 19

PLFP Fee payment

Year of fee payment: 20