AU2001236532A1 - Low cost, low emissions natural gas combustor - Google Patents

Low cost, low emissions natural gas combustor

Info

Publication number
AU2001236532A1
AU2001236532A1 AU2001236532A AU3653201A AU2001236532A1 AU 2001236532 A1 AU2001236532 A1 AU 2001236532A1 AU 2001236532 A AU2001236532 A AU 2001236532A AU 3653201 A AU3653201 A AU 3653201A AU 2001236532 A1 AU2001236532 A1 AU 2001236532A1
Authority
AU
Australia
Prior art keywords
low
natural gas
gas combustor
low cost
emissions natural
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.)
Abandoned
Application number
AU2001236532A
Inventor
Rudolph Dudebout
John J Lipinski
Ram Srinivasan
Frank J. Zupanc
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.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
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 Honeywell International Inc filed Critical Honeywell International Inc
Publication of AU2001236532A1 publication Critical patent/AU2001236532A1/en
Abandoned 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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
AU2001236532A 2000-01-28 2001-01-25 Low cost, low emissions natural gas combustor Abandoned AU2001236532A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/493,646 US6374615B1 (en) 2000-01-28 2000-01-28 Low cost, low emissions natural gas combustor
US09493646 2000-01-28
PCT/US2001/002404 WO2001055646A1 (en) 2000-01-28 2001-01-25 Low cost, low emissions natural gas combustor

Publications (1)

Publication Number Publication Date
AU2001236532A1 true AU2001236532A1 (en) 2001-08-07

Family

ID=23961126

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2001236532A Abandoned AU2001236532A1 (en) 2000-01-28 2001-01-25 Low cost, low emissions natural gas combustor

Country Status (3)

Country Link
US (1) US6374615B1 (en)
AU (1) AU2001236532A1 (en)
WO (1) WO2001055646A1 (en)

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US7603841B2 (en) * 2001-07-23 2009-10-20 Ramgen Power Systems, Llc Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
US6694743B2 (en) 2001-07-23 2004-02-24 Ramgen Power Systems, Inc. Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
US7003961B2 (en) * 2001-07-23 2006-02-28 Ramgen Power Systems, Inc. Trapped vortex combustor
US6820411B2 (en) * 2002-09-13 2004-11-23 The Boeing Company Compact, lightweight high-performance lift thruster incorporating swirl-augmented oxidizer/fuel injection, mixing and combustion
US6935116B2 (en) * 2003-04-28 2005-08-30 Power Systems Mfg., Llc Flamesheet combustor
US7065972B2 (en) * 2004-05-21 2006-06-27 Honeywell International, Inc. Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions
US20070028595A1 (en) * 2005-07-25 2007-02-08 Mongia Hukam C High pressure gas turbine engine having reduced emissions
CN100483029C (en) * 2006-01-12 2009-04-29 中国科学院工程热物理研究所 Combustion chamber of miniature gas turbine with double premixed channel using natural gas
EP1835229A1 (en) * 2006-03-13 2007-09-19 Siemens Aktiengesellschaft Combustor and method of operating a combustor
US8166763B2 (en) * 2006-09-14 2012-05-01 Solar Turbines Inc. Gas turbine fuel injector with a removable pilot assembly
US7841167B2 (en) * 2006-11-17 2010-11-30 General Electric Company Pulse detonation engine bypass and cooling flow with downstream mixing volume
US7762077B2 (en) * 2006-12-05 2010-07-27 Pratt & Whitney Rocketdyne, Inc. Single-stage hypersonic vehicle featuring advanced swirl combustion
US20080128547A1 (en) * 2006-12-05 2008-06-05 Pratt & Whitney Rocketdyne, Inc. Two-stage hypersonic vehicle featuring advanced swirl combustion
ITTO20070193A1 (en) 2007-03-14 2008-09-15 Ansaldo Ricerche S P A PREMIX BURNER OF A GAS TURBINE, IN PARTICULAR FOR A MICROTURBINE
US7762058B2 (en) * 2007-04-17 2010-07-27 Pratt & Whitney Rocketdyne, Inc. Ultra-compact, high performance aerovortical rocket thruster
US7690192B2 (en) * 2007-04-17 2010-04-06 Pratt & Whitney Rocketdyne, Inc. Compact, high performance swirl combustion rocket engine
US8286433B2 (en) 2007-10-26 2012-10-16 Solar Turbines Inc. Gas turbine fuel injector with removable pilot liquid tube
US8096132B2 (en) * 2008-02-20 2012-01-17 Flexenergy Energy Systems, Inc. Air-cooled swirlerhead
EP2107313A1 (en) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Fuel staging in a burner
US8454350B2 (en) * 2008-10-29 2013-06-04 General Electric Company Diluent shroud for combustor
US20120266602A1 (en) * 2011-04-22 2012-10-25 General Electric Company Aerodynamic Fuel Nozzle
US8893500B2 (en) 2011-05-18 2014-11-25 Solar Turbines Inc. Lean direct fuel injector
US8919132B2 (en) 2011-05-18 2014-12-30 Solar Turbines Inc. Method of operating a gas turbine engine
US9182124B2 (en) 2011-12-15 2015-11-10 Solar Turbines Incorporated Gas turbine and fuel injector for the same
CN102878580B (en) * 2012-09-12 2015-04-22 中国科学院工程热物理研究所 Lean premixed combustion chamber for gas turbine
EP2923150B1 (en) * 2012-11-21 2018-09-05 General Electric Company Anti-coking liquid fuel cartridge
WO2014123850A1 (en) 2013-02-06 2014-08-14 United Technologies Corporation Gas turbine engine component with upstream-directed cooling film holes
EP2954261B1 (en) 2013-02-08 2020-03-04 United Technologies Corporation Gas turbine engine combustor
WO2014160299A1 (en) 2013-03-14 2014-10-02 United Technologies Corporation Combustor panel with increased durability
WO2017002074A1 (en) * 2015-06-30 2017-01-05 Ansaldo Energia Ip Uk Limited Gas turbine fuel components
US10344981B2 (en) * 2016-12-16 2019-07-09 Delavan Inc. Staged dual fuel radial nozzle with radial liquid fuel distributor
US10634355B2 (en) * 2016-12-16 2020-04-28 Delavan Inc. Dual fuel radial flow nozzles
US10527286B2 (en) * 2016-12-16 2020-01-07 Delavan, Inc Staged radial air swirler with radial liquid fuel distributor
US11519334B2 (en) * 2017-07-31 2022-12-06 General Electric Company Torch igniter for a combustor
US11326521B2 (en) 2020-06-30 2022-05-10 General Electric Company Methods of igniting liquid fuel in a turbomachine
JP2022150960A (en) * 2021-03-26 2022-10-07 本田技研工業株式会社 Fuel nozzle device for gas turbine
DE102022202937A1 (en) * 2022-03-24 2023-09-28 Rolls-Royce Deutschland Ltd & Co Kg Nozzle assembly with central fuel supply and at least two air channels

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US4301657A (en) 1978-05-04 1981-11-24 Caterpillar Tractor Co. Gas turbine combustion chamber
US4260367A (en) 1978-12-11 1981-04-07 United Technologies Corporation Fuel nozzle for burner construction
US4845940A (en) 1981-02-27 1989-07-11 Westinghouse Electric Corp. Low NOx rich-lean combustor especially useful in gas turbines
EP0169431B1 (en) 1984-07-10 1990-04-11 Hitachi, Ltd. Gas turbine combustor
ATE42821T1 (en) 1985-03-04 1989-05-15 Siemens Ag BURNER ARRANGEMENT FOR COMBUSTION PLANTS, IN PARTICULAR FOR COMBUSTION CHAMBERS OF GAS TURBINE PLANTS, AND METHOD FOR THEIR OPERATION.
US4653278A (en) 1985-08-23 1987-03-31 General Electric Company Gas turbine engine carburetor
JPH0663646B2 (en) 1985-10-11 1994-08-22 株式会社日立製作所 Combustor for gas turbine
JP2644745B2 (en) 1987-03-06 1997-08-25 株式会社日立製作所 Gas turbine combustor
US4928481A (en) 1988-07-13 1990-05-29 Prutech Ii Staged low NOx premix gas turbine combustor
US5163287A (en) * 1989-12-22 1992-11-17 Sundstrand Corporation Stored energy combustor with fuel injector containing igniter means for accommodating thermal expansion
GB9023004D0 (en) 1990-10-23 1990-12-05 Rolls Royce Plc A gas turbine engine combustion chamber and a method of operating a gas turbine engine combustion chamber
US5372008A (en) 1992-11-10 1994-12-13 Solar Turbines Incorporated Lean premix combustor system
US5321947A (en) 1992-11-10 1994-06-21 Solar Turbines Incorporated Lean premix combustion system having reduced combustion pressure oscillation
US5361586A (en) 1993-04-15 1994-11-08 Westinghouse Electric Corporation Gas turbine ultra low NOx combustor
US5623826A (en) 1993-07-30 1997-04-29 Hitachi, Ltd. Combustor having a premix chamber with a blade-like structural member and method of operating the combustor
EP0776444B1 (en) 1994-07-13 2001-10-04 Volvo Aero Corporation Low-emission combustion chamber for gas turbine engines
US5638682A (en) 1994-09-23 1997-06-17 General Electric Company Air fuel mixer for gas turbine combustor having slots at downstream end of mixing duct
US5590529A (en) 1994-09-26 1997-01-07 General Electric Company Air fuel mixer for gas turbine combustor
US5613363A (en) 1994-09-26 1997-03-25 General Electric Company Air fuel mixer for gas turbine combustor
GB2297151B (en) 1995-01-13 1998-04-22 Europ Gas Turbines Ltd Fuel injector arrangement for gas-or liquid-fuelled turbine
EP0728989B1 (en) 1995-01-13 2001-11-28 European Gas Turbines Limited Gas turbine engine combustor
US5813232A (en) 1995-06-05 1998-09-29 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
US5685139A (en) 1996-03-29 1997-11-11 General Electric Company Diffusion-premix nozzle for a gas turbine combustor and related method

Also Published As

Publication number Publication date
WO2001055646A1 (en) 2001-08-02
US6374615B1 (en) 2002-04-23

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