DE69203729D1 - Gasbrenner mit niedrigem nox-gehalt. - Google Patents

Gasbrenner mit niedrigem nox-gehalt.

Info

Publication number
DE69203729D1
DE69203729D1 DE69203729T DE69203729T DE69203729D1 DE 69203729 D1 DE69203729 D1 DE 69203729D1 DE 69203729 T DE69203729 T DE 69203729T DE 69203729 T DE69203729 T DE 69203729T DE 69203729 D1 DE69203729 D1 DE 69203729D1
Authority
DE
Germany
Prior art keywords
gas burner
low nox
nox content
content
low
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
Application number
DE69203729T
Other languages
English (en)
Other versions
DE69203729T2 (de
Inventor
John Mcvey
Thomas Rosfjord
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69203729D1 publication Critical patent/DE69203729D1/de
Application granted granted Critical
Publication of DE69203729T2 publication Critical patent/DE69203729T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • 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
    • F23R3/34—Feeding into different combustion zones
    • 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
    • F23D2900/00008—Burner assemblies with diffusion and premix modes, i.e. dual mode burners

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
DE69203729T 1991-12-16 1992-10-19 Gasbrenner mit niedrigem nox-gehalt. Expired - Fee Related DE69203729T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/807,483 US5263325A (en) 1991-12-16 1991-12-16 Low NOx combustion
PCT/US1992/008932 WO1993012388A1 (en) 1991-12-16 1992-10-19 LOW NOx COMBUSTION

Publications (2)

Publication Number Publication Date
DE69203729D1 true DE69203729D1 (de) 1995-08-31
DE69203729T2 DE69203729T2 (de) 1996-04-11

Family

ID=25196485

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69203729T Expired - Fee Related DE69203729T2 (de) 1991-12-16 1992-10-19 Gasbrenner mit niedrigem nox-gehalt.

Country Status (5)

Country Link
US (1) US5263325A (de)
EP (1) EP0617780B1 (de)
JP (1) JP3312152B2 (de)
DE (1) DE69203729T2 (de)
WO (1) WO1993012388A1 (de)

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DE4417536A1 (de) * 1994-05-19 1995-11-23 Abb Management Ag Verfahren zum Betrieb einer Brennkammer
US5617716A (en) * 1994-09-16 1997-04-08 Electric Power Research Institute Method for supplying vaporized fuel oil to a gas turbine combustor and system for same
US5813232A (en) * 1995-06-05 1998-09-29 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
EP0747635B1 (de) * 1995-06-05 2003-01-15 Rolls-Royce Corporation Magervormischbrenner mit niedrigem NOx-Ausstoss für industrielle Gasturbinen
US5675971A (en) * 1996-01-02 1997-10-14 General Electric Company Dual fuel mixer for gas turbine combustor
EP0926325A3 (de) 1997-12-23 2001-04-25 United Technologies Corporation Einrichtung für einen mit flüssigem Brennstoff betriebene Brennkammer
JPH11257664A (ja) 1997-12-30 1999-09-21 United Technol Corp <Utc> ガスタ―ビンエンジンの燃料噴射ノズル／ガイドアセンブリ
US6240731B1 (en) 1997-12-31 2001-06-05 United Technologies Corporation Low NOx combustor for gas turbine engine
DE19812834B4 (de) * 1998-03-24 2004-12-16 Alstom Verfahren zum Zünden der Brenner von Brennkammern in Gasturbinenanlagen
US6560967B1 (en) 1998-05-29 2003-05-13 Jeffrey Mark Cohen Method and apparatus for use with a gas fueled combustor
US6158957A (en) * 1998-12-23 2000-12-12 United Technologies Corporation Thermal barrier removal process
US6412272B1 (en) 1998-12-29 2002-07-02 United Technologies Corporation Fuel nozzle guide for gas turbine engine and method of assembly/disassembly
US6298667B1 (en) * 2000-06-22 2001-10-09 General Electric Company Modular combustor dome
US7121097B2 (en) 2001-01-16 2006-10-17 Catalytica Energy Systems, Inc. Control strategy for flexible catalytic combustion system
US6718772B2 (en) 2000-10-27 2004-04-13 Catalytica Energy Systems, Inc. Method of thermal NOx reduction in catalytic combustion systems
US6796129B2 (en) 2001-08-29 2004-09-28 Catalytica Energy Systems, Inc. Design and control strategy for catalytic combustion system with a wide operating range
US6966186B2 (en) * 2002-05-01 2005-11-22 Siemens Westinghouse Power Corporation Non-catalytic combustor for reducing NOx emissions
US6772583B2 (en) * 2002-09-11 2004-08-10 Siemens Westinghouse Power Corporation Can combustor for a gas turbine engine
US20040255588A1 (en) * 2002-12-11 2004-12-23 Kare Lundberg Catalytic preburner and associated methods of operation
WO2004065777A2 (en) * 2003-01-17 2004-08-05 Catalytica Energy Systems, Inc. Dynamic control system and method for multi-combustor catalytic gas turbine engine
WO2005026675A2 (en) * 2003-09-05 2005-03-24 Catalytica Energy Systems, Inc. Catalyst module overheating detection and methods of response
US20060283181A1 (en) * 2005-06-15 2006-12-21 Arvin Technologies, Inc. Swirl-stabilized burner for thermal management of exhaust system and associated method
SE529333C2 (sv) * 2005-11-23 2007-07-10 Norsk Hydro As Förbränningsinstallation
US20080020333A1 (en) * 2006-06-14 2008-01-24 Smaling Rudolf M Dual reaction zone fuel reformer and associated method
US8006482B2 (en) * 2007-03-02 2011-08-30 Caterpillar Inc. Method of purging fluid injector by heating
US7958721B2 (en) * 2007-06-29 2011-06-14 Caterpillar Inc. Regeneration system having integral purge and ignition device
US8147121B2 (en) * 2008-07-09 2012-04-03 General Electric Company Pre-mixing apparatus for a turbine engine
US8112999B2 (en) * 2008-08-05 2012-02-14 General Electric Company Turbomachine injection nozzle including a coolant delivery system
US7886991B2 (en) * 2008-10-03 2011-02-15 General Electric Company Premixed direct injection nozzle
US8209986B2 (en) * 2008-10-29 2012-07-03 General Electric Company Multi-tube thermal fuse for nozzle protection from a flame holding or flashback event
US8297059B2 (en) * 2009-01-22 2012-10-30 General Electric Company Nozzle for a turbomachine
US9140454B2 (en) * 2009-01-23 2015-09-22 General Electric Company Bundled multi-tube nozzle for a turbomachine
US8539773B2 (en) * 2009-02-04 2013-09-24 General Electric Company Premixed direct injection nozzle for highly reactive fuels
US8157189B2 (en) * 2009-04-03 2012-04-17 General Electric Company Premixing direct injector
US8607568B2 (en) * 2009-05-14 2013-12-17 General Electric Company Dry low NOx combustion system with pre-mixed direct-injection secondary fuel nozzle
US8794545B2 (en) * 2009-09-25 2014-08-05 General Electric Company Internal baffling for fuel injector
US8276385B2 (en) * 2009-10-08 2012-10-02 General Electric Company Staged multi-tube premixing injector
US8613197B2 (en) * 2010-08-05 2013-12-24 General Electric Company Turbine combustor with fuel nozzles having inner and outer fuel circuits
US20120180487A1 (en) * 2011-01-19 2012-07-19 General Electric Company System for flow control in multi-tube fuel nozzle
US8875516B2 (en) 2011-02-04 2014-11-04 General Electric Company Turbine combustor configured for high-frequency dynamics mitigation and related method
US20130036743A1 (en) * 2011-08-08 2013-02-14 General Electric Company Turbomachine combustor assembly
US9033699B2 (en) * 2011-11-11 2015-05-19 General Electric Company Combustor
US20130122437A1 (en) * 2011-11-11 2013-05-16 General Electric Company Combustor and method for supplying fuel to a combustor
US9134031B2 (en) * 2012-01-04 2015-09-15 General Electric Company Combustor of a turbomachine including multiple tubular radial pathways arranged at multiple circumferential and axial locations
US9134023B2 (en) * 2012-01-06 2015-09-15 General Electric Company Combustor and method for distributing fuel in the combustor
US9052112B2 (en) * 2012-02-27 2015-06-09 General Electric Company Combustor and method for purging a combustor
US8511086B1 (en) * 2012-03-01 2013-08-20 General Electric Company System and method for reducing combustion dynamics in a combustor
US9267690B2 (en) 2012-05-29 2016-02-23 General Electric Company Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same
US20130327050A1 (en) * 2012-06-07 2013-12-12 General Electric Company Controlling flame stability of a gas turbine generator
CN102721057B (zh) * 2012-06-25 2014-08-13 潘育坛 一种工业用燃气燃烧器
US20140000269A1 (en) * 2012-06-29 2014-01-02 General Electric Company Combustion nozzle and an associated method thereof
US9291103B2 (en) * 2012-12-05 2016-03-22 General Electric Company Fuel nozzle for a combustor of a gas turbine engine
US9303873B2 (en) * 2013-03-15 2016-04-05 General Electric Company System having a multi-tube fuel nozzle with a fuel nozzle housing
FR3004239B1 (fr) * 2013-04-05 2020-10-23 Fives Pillard Bruleur gaz a premelange bas nox
CN105452774B (zh) * 2013-10-18 2017-07-14 三菱重工业株式会社 燃料喷射器、燃烧器以及燃气轮机
US9435540B2 (en) 2013-12-11 2016-09-06 General Electric Company Fuel injector with premix pilot nozzle
US10107499B2 (en) * 2014-07-31 2018-10-23 General Electric Company Fuel plenum for a fuel nozzle and method of making same
CN105509069A (zh) * 2014-09-23 2016-04-20 苏州宝联重工股份有限公司 一种新型常明灯稳燃器装置
US9714767B2 (en) 2014-11-26 2017-07-25 General Electric Company Premix fuel nozzle assembly
US10030869B2 (en) 2014-11-26 2018-07-24 General Electric Company Premix fuel nozzle assembly
US9982892B2 (en) 2015-04-16 2018-05-29 General Electric Company Fuel nozzle assembly including a pilot nozzle
US9803867B2 (en) 2015-04-21 2017-10-31 General Electric Company Premix pilot nozzle
US20180313540A1 (en) * 2017-05-01 2018-11-01 General Electric Company Acoustic Damper for Gas Turbine Engine Combustors
US10890329B2 (en) 2018-03-01 2021-01-12 General Electric Company Fuel injector assembly for gas turbine engine
EP3861255A2 (de) * 2018-10-05 2021-08-11 Fives Pillard Brenner und verbrennungsverfahren für einen brenner
US10935245B2 (en) 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports
US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
US11073114B2 (en) 2018-12-12 2021-07-27 General Electric Company Fuel injector assembly for a heat engine
US11156360B2 (en) 2019-02-18 2021-10-26 General Electric Company Fuel nozzle assembly

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH303030A (de) * 1952-08-15 1954-11-15 Bbc Brown Boveri & Cie Gasbrenner, vorzugsweise für Brennkammern von Gasturbinenanlagen.
US2935128A (en) * 1957-06-06 1960-05-03 Nat Airoil Burner Company Inc High pressure gas burners
US3685950A (en) * 1969-06-23 1972-08-22 Mitsubishi Electric Corp Combustion apparatus for mixing fuel and air in divided portions
GB1465785A (en) * 1973-03-12 1977-03-02 Tokyo Gas Co Ltd Burner and method of combustion-
JPS5271737A (en) * 1975-12-11 1977-06-15 Daido Steel Co Ltd Burner
US4100733A (en) * 1976-10-04 1978-07-18 United Technologies Corporation Premix combustor
US4618323A (en) * 1980-02-19 1986-10-21 Southers California Edison Method and burner tip for suppressing emissions of nitrogen oxides
EP0095788B1 (de) * 1982-05-28 1985-12-18 BBC Aktiengesellschaft Brown, Boveri & Cie. Brennkammer einer Gasturbine und Verfahren zu deren Betrieb
US5121608A (en) * 1988-02-06 1992-06-16 Rolls-Royce Plc Gas turbine engine fuel burner
JPH02147610U (de) * 1989-05-11 1990-12-14

Also Published As

Publication number Publication date
EP0617780B1 (de) 1995-07-26
EP0617780A1 (de) 1994-10-05
DE69203729T2 (de) 1996-04-11
US5263325A (en) 1993-11-23
JP3312152B2 (ja) 2002-08-05
WO1993012388A1 (en) 1993-06-24
JPH07501876A (ja) 1995-02-23

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee