GB0622550D0 - Low emission combustor and method of operation - Google Patents

Low emission combustor and method of operation

Info

Publication number
GB0622550D0
GB0622550D0 GBGB0622550.2A GB0622550A GB0622550D0 GB 0622550 D0 GB0622550 D0 GB 0622550D0 GB 0622550 A GB0622550 A GB 0622550A GB 0622550 D0 GB0622550 D0 GB 0622550D0
Authority
GB
United Kingdom
Prior art keywords
low emission
emission combustor
combustor
low
emission
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Withdrawn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
GBGB0622550.2A
Other versions
GB2432206A (en
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB0622550D0 publication Critical patent/GB0622550D0/en
Publication of GB2432206A publication Critical patent/GB2432206A/en
Withdrawn legal-status Critical Current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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • 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
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • 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
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/58—Cyclone or vortex type combustion chambers
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
GB0622550A 2005-11-15 2006-11-13 Low emission combustor and method of operation Withdrawn GB2432206A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/280,664 US20070107437A1 (en) 2005-11-15 2005-11-15 Low emission combustion and method of operation

Publications (2)

Publication Number Publication Date
GB0622550D0 true GB0622550D0 (en) 2006-12-20
GB2432206A GB2432206A (en) 2007-05-16

Family

ID=37594788

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0622550A Withdrawn GB2432206A (en) 2005-11-15 2006-11-13 Low emission combustor and method of operation

Country Status (5)

Country Link
US (1) US20070107437A1 (en)
JP (1) JP2007139411A (en)
CN (1) CN1975259A (en)
DE (1) DE102006053679A1 (en)
GB (1) GB2432206A (en)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5473934B2 (en) * 2007-11-27 2014-04-16 アルストム テクノロジー リミテッド Apparatus and method for operating gas turbine equipment using second hydrogen-rich fuel
US8220271B2 (en) * 2008-09-30 2012-07-17 Alstom Technology Ltd. Fuel lance for a gas turbine engine including outer helical grooves
US8220269B2 (en) * 2008-09-30 2012-07-17 Alstom Technology Ltd. Combustor for a gas turbine engine with effusion cooled baffle
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
US8607570B2 (en) * 2009-05-06 2013-12-17 General Electric Company Airblown syngas fuel nozzle with diluent openings
US8776525B2 (en) * 2009-12-29 2014-07-15 Rolls-Royce North American Technologies, Inc. Gas turbine engine and combustor
WO2012141982A1 (en) * 2011-04-13 2012-10-18 The Regents Of The University Of California Natural draft low swirl burner
US8919132B2 (en) 2011-05-18 2014-12-30 Solar Turbines Inc. Method of operating a gas turbine engine
US8893500B2 (en) 2011-05-18 2014-11-25 Solar Turbines Inc. Lean direct fuel injector
KR101774093B1 (en) * 2011-08-22 2017-09-12 마제드 토칸 Can-annular combustor with staged and tangential fuel-air nozzles for use on gas turbine engines
WO2013028169A1 (en) 2011-08-22 2013-02-28 Majed Toqan Can-annular combustor with premixed tangential fuel-air nozzles for use on gas turbine engines
KR101774630B1 (en) * 2011-08-22 2017-09-19 마제드 토칸 Tangential annular combustor with premixed fuel and air for use on gas turbine engines
RU2618785C2 (en) * 2011-08-22 2017-05-11 Маджед ТОКАН Tangential and flameless annular combustion chamber for gas turbine engines
US20130081407A1 (en) * 2011-10-04 2013-04-04 David J. Wiebe Aero-derivative gas turbine engine with an advanced transition duct combustion assembly
US9182124B2 (en) 2011-12-15 2015-11-10 Solar Turbines Incorporated Gas turbine and fuel injector for the same
EP2808611B1 (en) 2013-05-31 2015-12-02 Siemens Aktiengesellschaft Injector for introducing a fuel-air mixture into a combustion chamber
EP2808612A1 (en) 2013-05-31 2014-12-03 Siemens Aktiengesellschaft Gas turbine combustion chamber with tangential late lean injection
EP2808610A1 (en) 2013-05-31 2014-12-03 Siemens Aktiengesellschaft Gas turbine combustion chamber with tangential late lean injection
WO2014201135A1 (en) 2013-06-11 2014-12-18 United Technologies Corporation Combustor with axial staging for a gas turbine engine
US20150345794A1 (en) * 2014-05-28 2015-12-03 General Electric Company Systems and methods for coherence reduction in combustion system
US9845732B2 (en) * 2014-05-28 2017-12-19 General Electric Company Systems and methods for variation of injectors for coherence reduction in combustion system
CN108036358B (en) * 2017-11-09 2019-05-28 清华大学 A kind of gas-turbine combustion chamber and its application method
EP3643970A1 (en) 2018-10-23 2020-04-29 Robert Staudacher Continuously operating and fluid-respiring fluid energy machine and method for operating same
US11415058B2 (en) * 2020-12-23 2022-08-16 Collins Engine Nozzles, Inc. Torch ignitors with tangential injection
US11415059B2 (en) * 2020-12-23 2022-08-16 Collins Engine Nozzles, Inc. Tangentially mounted torch ignitors
US20220333783A1 (en) * 2021-03-07 2022-10-20 CPS-Holding Limited Hydrogen-Fueled Combustor for Gas Turbines
DE102022208339A1 (en) * 2022-08-10 2024-02-15 Rolls-Royce Deutschland Ltd & Co Kg Combustion chamber arrangement for operation with liquid and/or gaseous fuel, gas turbine arrangement and method

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB824306A (en) * 1956-04-25 1959-11-25 Rolls Royce Improvements in or relating to combustion equipment of gas-turbine engines
US4420929A (en) * 1979-01-12 1983-12-20 General Electric Company Dual stage-dual mode low emission gas turbine combustion system
JPH0670376B2 (en) * 1986-09-01 1994-09-07 株式会社日立製作所 Catalytic combustion device
US4928481A (en) * 1988-07-13 1990-05-29 Prutech Ii Staged low NOx premix gas turbine combustor
US4910957A (en) * 1988-07-13 1990-03-27 Prutech Ii Staged lean premix low nox hot wall gas turbine combustor with improved turndown capability
US5195315A (en) * 1991-01-14 1993-03-23 United Technologies Corporation Double dome combustor with counter rotating toroidal vortices and dual radial fuel injection
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US5479781A (en) * 1993-09-02 1996-01-02 General Electric Company Low emission combustor having tangential lean direct injection
US5680765A (en) * 1996-01-05 1997-10-28 Choi; Kyung J. Lean direct wall fuel injection method and devices
US20010049932A1 (en) * 1996-05-02 2001-12-13 Beebe Kenneth W. Premixing dry low NOx emissions combustor with lean direct injection of gas fuel
US6220035B1 (en) * 1997-09-15 2001-04-24 Alliedsignal Inc. Annular combustor tangential injection flame stabilizer
GB2337102A (en) * 1998-05-09 1999-11-10 Europ Gas Turbines Ltd Gas-turbine engine combustor
GB9911867D0 (en) * 1999-05-22 1999-07-21 Rolls Royce Plc A combustion chamber assembly and a method of operating a combustion chamber assembly

Also Published As

Publication number Publication date
GB2432206A (en) 2007-05-16
US20070107437A1 (en) 2007-05-17
JP2007139411A (en) 2007-06-07
DE102006053679A1 (en) 2007-05-24
CN1975259A (en) 2007-06-06

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)