CS57291A3 - Burner of a gas turbine with low emissions - Google Patents

Burner of a gas turbine with low emissions

Info

Publication number
CS57291A3
CS57291A3 CS91572A CS57291A CS57291A3 CS 57291 A3 CS57291 A3 CS 57291A3 CS 91572 A CS91572 A CS 91572A CS 57291 A CS57291 A CS 57291A CS 57291 A3 CS57291 A3 CS 57291A3
Authority
CS
Czechoslovakia
Prior art keywords
burner
gas turbine
low emissions
emissions
low
Prior art date
Application number
CS91572A
Other languages
English (en)
Inventor
Rolf Jan Mowill
Original Assignee
Rolf Jan Mowill
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
Priority claimed from US07/488,136 external-priority patent/US5070700A/en
Application filed by Rolf Jan Mowill filed Critical Rolf Jan Mowill
Publication of CS57291A3 publication Critical patent/CS57291A3/cs

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
    • F23R3/34—Feeding into different combustion zones
    • 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
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
CS91572A 1990-03-05 1991-03-05 Burner of a gas turbine with low emissions CS57291A3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/488,136 US5070700A (en) 1990-03-05 1990-03-05 Low emissions gas turbine combustor
US07/658,858 US5156002A (en) 1990-03-05 1991-02-21 Low emissions gas turbine combustor

Publications (1)

Publication Number Publication Date
CS57291A3 true CS57291A3 (en) 1992-02-19

Family

ID=27049234

Family Applications (1)

Application Number Title Priority Date Filing Date
CS91572A CS57291A3 (en) 1990-03-05 1991-03-05 Burner of a gas turbine with low emissions

Country Status (4)

Country Link
US (1) US5156002A (cs)
EP (1) EP0445652A1 (cs)
JP (1) JP3150367B2 (cs)
CS (1) CS57291A3 (cs)

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US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
US5628182A (en) * 1993-07-07 1997-05-13 Mowill; R. Jan Star combustor with dilution ports in can portions
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor
US5377483A (en) * 1993-07-07 1995-01-03 Mowill; R. Jan Process for single stage premixed constant fuel/air ratio combustion
US5572862A (en) * 1993-07-07 1996-11-12 Mowill Rolf Jan Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
US5638674A (en) * 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
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DE19615910B4 (de) * 1996-04-22 2006-09-14 Alstom Brenneranordnung
US5924276A (en) * 1996-07-17 1999-07-20 Mowill; R. Jan Premixer with dilution air bypass valve assembly
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WO2001040713A1 (en) * 1999-12-03 2001-06-07 Mowill Rolf Jan Cooled premixer exit nozzle for gas turbine combustor and method of operation therefor
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US6508061B2 (en) * 2001-04-25 2003-01-21 Pratt & Whitney Canada Corp Diffuser combustor
CA2453532C (en) 2001-07-10 2009-05-26 Mitsubishi Heavy Industries, Ltd. Premixing nozzle, combustor,and gas turbine
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
EP3078909B1 (en) * 2002-10-10 2022-05-11 LPP Combustion, LLC Method for vaporization of liquid fuels for combustion
CN101187477B (zh) * 2002-10-10 2011-03-30 Lpp燃烧有限责任公司 汽化燃烧用液体燃料的系统及其使用方法
US6931853B2 (en) * 2002-11-19 2005-08-23 Siemens Westinghouse Power Corporation Gas turbine combustor having staged burners with dissimilar mixing passage geometries
US6857271B2 (en) * 2002-12-16 2005-02-22 Power Systems Mfg., Llc Secondary fuel nozzle with readily customizable pilot fuel flow rate
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US8387390B2 (en) 2006-01-03 2013-03-05 General Electric Company Gas turbine combustor having counterflow injection mechanism
US8529646B2 (en) 2006-05-01 2013-09-10 Lpp Combustion Llc Integrated system and method for production and vaporization of liquid hydrocarbon fuels for combustion
US10422534B2 (en) * 2006-06-26 2019-09-24 Joseph Michael Teets Fuel air premix chamber for a gas turbine engine
CA2667047C (en) * 2006-10-20 2012-07-24 Ihi Corporation Gas turbine combustor
JP2008185254A (ja) * 2007-01-30 2008-08-14 General Electric Co <Ge> 同軸燃料−空気通路を有する逆流噴射機構
JP5296320B2 (ja) * 2007-01-30 2013-09-25 ゼネラル・エレクトリック・カンパニイ 逆流噴射機構を有するシステム及び燃料及び空気を噴射する方法
US8707704B2 (en) * 2007-05-31 2014-04-29 General Electric Company Method and apparatus for assembling turbine engines
US8689559B2 (en) * 2009-03-30 2014-04-08 General Electric Company Secondary combustion system for reducing the level of emissions generated by a turbomachine
US8365534B2 (en) 2011-03-15 2013-02-05 General Electric Company Gas turbine combustor having a fuel nozzle for flame anchoring
RU2011115528A (ru) 2011-04-21 2012-10-27 Дженерал Электрик Компани (US) Топливная форсунка, камера сгорания и способ работы камеры сгорания
US9010082B2 (en) * 2012-01-03 2015-04-21 General Electric Company Turbine engine and method for flowing air in a turbine engine
FR3013805B1 (fr) * 2013-11-26 2018-01-26 Safran Helicopter Engines Ensemble de combustion a acces facilite des cannes de prevaporisation.
US9863346B2 (en) * 2014-10-03 2018-01-09 GM Global Technology Operations LLC Method and apparatus for estimating nitrogen oxides out of an engine
JP6870966B2 (ja) * 2016-11-30 2021-05-12 三菱重工業株式会社 燃焼器ノズル、及びガスタービン
CN115031260B (zh) * 2022-05-30 2023-08-22 中国人民解放军空军工程大学 一种旋转爆震燃烧室出口喉道位置固定的可调喷管
EP4528164A3 (en) * 2023-09-25 2025-04-09 General Electric Company Combustion section with a primary combustor and a set of secondary combustors

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US4389848A (en) * 1981-01-12 1983-06-28 United Technologies Corporation Burner construction for gas turbines
DE3113416A1 (de) * 1981-04-03 1982-10-21 Ruhrgas Ag, 4300 Essen Verfahren zum betrieb eines einem luftstrom ausgesetzten gasbrenners sowie brenner zur durchfuehrung des verfahrens
US4845952A (en) * 1987-10-23 1989-07-11 General Electric Company Multiple venturi tube gas fuel injector for catalytic combustor
US4974415A (en) * 1987-11-20 1990-12-04 Sundstrand Corporation Staged, coaxial multiple point fuel injection in a hot gas generator
JP6135448B2 (ja) 2013-10-17 2017-05-31 アイシン・エィ・ダブリュ株式会社 情報提供システム、情報提供方法、及び情報提供プログラム

Also Published As

Publication number Publication date
EP0445652A1 (en) 1991-09-11
US5156002A (en) 1992-10-20
JPH06265146A (ja) 1994-09-20
JP3150367B2 (ja) 2001-03-26

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