DE69412191D1 - Vormischbrennkammer mit konstantem Brennstoff/Luft Verhältnis und einstufiger Verbrennung - Google Patents

Vormischbrennkammer mit konstantem Brennstoff/Luft Verhältnis und einstufiger Verbrennung

Info

Publication number
DE69412191D1
DE69412191D1 DE69412191T DE69412191T DE69412191D1 DE 69412191 D1 DE69412191 D1 DE 69412191D1 DE 69412191 T DE69412191 T DE 69412191T DE 69412191 T DE69412191 T DE 69412191T DE 69412191 D1 DE69412191 D1 DE 69412191D1
Authority
DE
Germany
Prior art keywords
air ratio
constant fuel
combustion chamber
premix
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 - Fee Related
Application number
DE69412191T
Other languages
English (en)
Other versions
DE69412191T2 (de
Inventor
R Jan Mowill
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of DE69412191D1 publication Critical patent/DE69412191D1/de
Application granted granted Critical
Publication of DE69412191T2 publication Critical patent/DE69412191T2/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54—Reverse-flow combustion chambers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/48—Control of fuel supply conjointly with another control of the plant
    • F02C9/50—Control of fuel supply conjointly with another control of the plant with control of working fluid 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air 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
    • F23R3/286—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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • 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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/322—Arrangement of components according to their shape tangential

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
DE69412191T 1993-07-07 1994-06-24 Vormischbrennkammer mit konstantem Brennstoff/Luft Verhältnis und einstufiger Verbrennung Expired - Fee Related DE69412191T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US8688393A 1993-07-07 1993-07-07

Publications (2)

Publication Number Publication Date
DE69412191D1 true DE69412191D1 (de) 1998-09-10
DE69412191T2 DE69412191T2 (de) 1999-01-21

Family

ID=22201519

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69412191T Expired - Fee Related DE69412191T2 (de) 1993-07-07 1994-06-24 Vormischbrennkammer mit konstantem Brennstoff/Luft Verhältnis und einstufiger Verbrennung

Country Status (4)

Country Link
US (3) US5377483A (de)
EP (1) EP0635681B1 (de)
JP (1) JP3527779B2 (de)
DE (1) DE69412191T2 (de)

Families Citing this family (52)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5638674A (en) * 1993-07-07 1997-06-17 Mowill; R. Jan Convectively cooled, single stage, fully premixed controllable fuel/air combustor with tangential admission
US6220034B1 (en) 1993-07-07 2001-04-24 R. Jan Mowill Convectively cooled, single stage, fully premixed controllable fuel/air combustor
US5613357A (en) * 1993-07-07 1997-03-25 Mowill; R. Jan Star-shaped single stage low emission combustor system
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
EP0731316A1 (de) * 1995-02-24 1996-09-11 R. Jan Mowill Sternförmiges, einstufiges, emissionsarmes Verbrennungssystem
US5669218A (en) * 1995-05-31 1997-09-23 Dresser-Rand Company Premix fuel nozzle
US5558069A (en) * 1995-11-09 1996-09-24 Livernois Research & Development Company Method and apparatus for fluid temperature control
US5924276A (en) * 1996-07-17 1999-07-20 Mowill; R. Jan Premixer with dilution air bypass valve assembly
US6250066B1 (en) 1996-11-26 2001-06-26 Honeywell International Inc. Combustor with dilution bypass system and venturi jet deflector
US6070406A (en) 1996-11-26 2000-06-06 Alliedsignal, Inc. Combustor dilution bypass system
US6233915B1 (en) * 1997-04-17 2001-05-22 Allied Signal, Inc. Injection tube for connecting a cold plenum to a hot chamber
WO1999006771A1 (en) 1997-07-31 1999-02-11 Alliedsignal Inc. Rib turbulators for combustor external cooling
US5971026A (en) * 1997-12-09 1999-10-26 Honeywell Inc. Internal geometry shape design for venturi tube-like gas-air mixing valve
EP0936406B1 (de) 1998-02-10 2004-05-06 General Electric Company Brenner mit gleichmässiger Brennstoff/Luft Vormischung zur emissionsarmen Verbrennung
US6925809B2 (en) 1999-02-26 2005-08-09 R. Jan Mowill Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
US6253538B1 (en) 1999-09-27 2001-07-03 Pratt & Whitney Canada Corp. Variable premix-lean burn combustor
WO2001040713A1 (en) 1999-12-03 2001-06-07 Mowill Rolf Jan Cooled premixer exit nozzle for gas turbine combustor and method of operation therefor
US6327860B1 (en) 2000-06-21 2001-12-11 Honeywell International, Inc. Fuel injector for low emissions premixing gas turbine combustor
US6363724B1 (en) 2000-08-31 2002-04-02 General Electric Company Gas only nozzle fuel tip
US6543231B2 (en) * 2001-07-13 2003-04-08 Pratt & Whitney Canada Corp Cyclone combustor
JP2003194338A (ja) 2001-12-14 2003-07-09 R Jan Mowill 可変出口形状を有するガスタービンエンジン用燃料／空気プレミキサ及び出口速度の制御方法
EP3078909B1 (de) * 2002-10-10 2022-05-11 LPP Combustion, LLC Verfahren zum verdampfung von flüssigbrennstoffen zur verbrennung
US6971227B2 (en) * 2003-04-16 2005-12-06 Ingersoll Rand Energy Systems, Inc. System and method to stage primary zone airflow
US7654094B2 (en) 2004-03-09 2010-02-02 Hitachi, Ltd. Radial turbine and method of cooling nozzle of the same
US7162874B2 (en) * 2004-07-30 2007-01-16 Hija Holding B.V. Apparatus and method for gas turbine engine fuel/air premixer exit velocity control
KR101201624B1 (ko) 2004-12-08 2012-11-14 엘피피 컴버션, 엘엘씨 액체 탄화수소 연료의 컨디셔닝을 위한 방법 및 장치
US7540154B2 (en) * 2005-08-11 2009-06-02 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor
US20070107437A1 (en) * 2005-11-15 2007-05-17 Evulet Andrei T Low emission combustion and method of operation
US20070151988A1 (en) * 2005-12-14 2007-07-05 Saucedo Victor M Constant pressure delivery vessel and system
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
US8171716B2 (en) * 2007-08-28 2012-05-08 General Electric Company System and method for fuel and air mixing in a gas turbine
EP2110602A1 (de) * 2008-04-16 2009-10-21 Siemens Aktiengesellschaft Akustiche Teilentkopplung zur Verringerung von selbstinduzierten Flammenschwingungen
US8887390B2 (en) 2008-08-15 2014-11-18 Dresser-Rand Company Method for correcting downstream deflection in gas turbine nozzles
US7712314B1 (en) 2009-01-21 2010-05-11 Gas Turbine Efficiency Sweden Ab Venturi cooling system
EP2299178B1 (de) * 2009-09-17 2015-11-04 Alstom Technology Ltd Verfahren und Gasturbinenverbrennungssystem zum sicheren Mischen von H2-reichen Brennstoffen mit Luft
US8863525B2 (en) 2011-01-03 2014-10-21 General Electric Company Combustor with fuel staggering for flame holding mitigation
WO2012112889A2 (en) * 2011-02-18 2012-08-23 Ethier Jason Fluid flow devices with vertically simple geometry and methods of making the same
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
US8601820B2 (en) 2011-06-06 2013-12-10 General Electric Company Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
US8919137B2 (en) 2011-08-05 2014-12-30 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US9010120B2 (en) 2011-08-05 2015-04-21 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US11015808B2 (en) 2011-12-13 2021-05-25 General Electric Company Aerodynamically enhanced premixer with purge slots for reduced emissions
US9140455B2 (en) 2012-01-04 2015-09-22 General Electric Company Flowsleeve of a turbomachine component
KR101400602B1 (ko) * 2012-04-27 2014-05-27 부경대학교 산학협력단 상온공기 연소기에서 고온공기를 연속으로 공급받는 마일드 연소기
US20140000269A1 (en) * 2012-06-29 2014-01-02 General Electric Company Combustion nozzle and an associated method thereof
JP6327826B2 (ja) * 2013-10-11 2018-05-23 川崎重工業株式会社 ガスタービンの燃料噴射装置
FI127525B (en) * 2014-01-08 2018-08-15 Finno Energy Oy System and method for generating electrical energy
US10030580B2 (en) 2014-04-11 2018-07-24 Dynamo Micropower Corporation Micro gas turbine systems and uses thereof
US20150338101A1 (en) * 2014-05-21 2015-11-26 General Electric Company Turbomachine combustor including a combustor sleeve baffle
GB201414661D0 (en) * 2014-08-19 2014-10-01 Rolls Royce Plc Gas turbine engine and method of operation
RU2656177C1 (ru) * 2014-11-03 2018-05-31 Сименс Акциенгезелльшафт Компоновка горелки

Family Cites Families (85)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2675673A (en) * 1954-04-20 Gas turbine power plant
US1705383A (en) * 1924-04-17 1929-03-12 Mines De Frankenholz Soc D Combustion chamber for use with powdered fuel
US2108822A (en) * 1935-11-11 1938-02-22 Wells A Lippincott Printing plate and formation thereof
US2183836A (en) * 1936-12-18 1939-12-19 Roberts Appliance Corp Gordon Fluid fuel burner
DE748208C (de) * 1938-06-15 1944-10-28 Sulzer Ag Gasturbinenanlage
US2268270A (en) * 1938-12-13 1941-12-30 Sulzer Ag Gas turbine plant
DE872698C (de) * 1942-05-31 1953-04-02 Kloeckner Humboldt Deutz Ag Gasturbine bzw. Strahltriebwerk
US2487514A (en) * 1943-01-16 1949-11-08 Jarvis C Marble Turbine rotor cooling
DE833739C (de) * 1943-09-04 1952-03-10 Maschf Augsburg Nuernberg Ag Gasturbinenanlage
US2608822A (en) * 1944-10-07 1952-09-02 Turbolectric Corp Method of operation and regulation of thermal power plants
US2488969A (en) * 1945-02-27 1949-11-22 Bbc Brown Boveri & Cie Combined gas producer and gas turbine plant
US2489939A (en) * 1945-05-05 1949-11-29 Sulzer Ag Variable load gas turbine system
US2513601A (en) * 1945-12-29 1950-07-04 Sulzer Ag Gas turbine plant
US2621475A (en) * 1946-06-13 1952-12-16 Phillips Petroleum Co Operation of multistage combustion gas turbines
US2469238A (en) * 1947-08-28 1949-05-03 Westinghouse Electric Corp Gas turbine apparatus
GB668834A (en) * 1948-11-02 1952-03-26 Power Jets Res & Dev Ltd Improvements in or relating to gas turbine power plant
CH283198A (de) * 1949-03-25 1952-05-31 Limited Centrax Power Units Gasturbinenanlage.
US2625012A (en) * 1950-04-18 1953-01-13 Gen Engineering And Res Corp Gas turbine power plant, including multiple fluid operated turbines
CH301137A (de) * 1950-11-17 1954-08-31 Power Jets Res & Dev Ltd Verbrennungseinrichtung.
FR1126906A (fr) * 1951-08-08 1956-12-04 Turbine à gaz, plus spécialement pour véhicules
US2663141A (en) * 1952-05-03 1953-12-22 Boeing Co Gas turbine
CH324502A (de) * 1954-12-18 1957-09-30 Bbc Brown Boveri & Cie Selbsttätige Luftregelungseinrichtung bei Brennkammern von Gasturbinenanlagen
US2999359A (en) * 1956-04-25 1961-09-12 Rolls Royce Combustion equipment of gas-turbine engines
US2988884A (en) * 1958-09-23 1961-06-20 Pouit Robert Improvements in gas turbine power plants
US3091080A (en) * 1958-10-27 1963-05-28 United Aircraft Corp Control system for afterburning gas turbine engine
CH363853A (de) * 1959-01-10 1962-08-15 Sulzer Ag Gasturbinenanlage mit zwei Wellen
US3099134A (en) * 1959-12-24 1963-07-30 Havilland Engine Co Ltd Combustion chambers
US3204406A (en) * 1960-04-04 1965-09-07 Ford Motor Co Cooling system for a re-expansion gas turbine engine
US3315467A (en) * 1965-03-11 1967-04-25 Westinghouse Electric Corp Reheat gas turbine power plant with air admission to the primary combustion zone of the reheat combustion chamber structure
FR1590542A (de) * 1968-11-04 1970-04-13
US3899884A (en) * 1970-12-02 1975-08-19 Gen Electric Combustor systems
JPS4923482B1 (de) * 1970-12-27 1974-06-17
FR2189630B1 (de) * 1972-06-23 1980-03-14 Snecma
US3768962A (en) * 1972-10-02 1973-10-30 F Baranowski Gas torch
US3905192A (en) * 1974-08-29 1975-09-16 United Aircraft Corp Combustor having staged premixing tubes
US3958413A (en) * 1974-09-03 1976-05-25 General Motors Corporation Combustion method and apparatus
US3938324A (en) * 1974-12-12 1976-02-17 General Motors Corporation Premix combustor with flow constricting baffle between combustion and dilution zones
US4012904A (en) * 1975-07-17 1977-03-22 Chrysler Corporation Gas turbine burner
US4030288A (en) * 1975-11-10 1977-06-21 Caterpillar Tractor Co. Modular gas turbine engine assembly
US4073137A (en) * 1976-06-02 1978-02-14 United Technologies Corporation Convectively cooled flameholder for premixed burner
DE2629761A1 (de) * 1976-07-02 1978-01-05 Volkswagenwerk Ag Brennkammer fuer gasturbinen
SE404948B (sv) * 1977-03-25 1978-11-06 Stal Laval Turbin Ab Tvaaxlig gasturbinanleggning
US4215535A (en) * 1978-01-19 1980-08-05 United Technologies Corporation Method and apparatus for reducing nitrous oxide emissions from combustors
US4301657A (en) * 1978-05-04 1981-11-24 Caterpillar Tractor Co. Gas turbine combustion chamber
US4255927A (en) * 1978-06-29 1981-03-17 General Electric Company Combustion control system
JPS5545739A (en) * 1978-09-29 1980-03-31 Japan Crown Cork Co Ltd Bonding of polyolefin liner to metallic crown cap
GB2036296B (en) * 1978-11-20 1982-12-01 Rolls Royce Gas turbine
US4260367A (en) * 1978-12-11 1981-04-07 United Technologies Corporation Fuel nozzle for burner construction
US4286430A (en) * 1979-09-17 1981-09-01 Teledyne Industries, Inc. Gas turbine engine
US4297842A (en) * 1980-01-21 1981-11-03 General Electric Company NOx suppressant stationary gas turbine combustor
JPS5741524A (en) * 1980-08-25 1982-03-08 Hitachi Ltd Combustion method of gas turbine and combustor for gas turbine
US4412414A (en) * 1980-09-22 1983-11-01 General Motors Corporation Heavy fuel combustor
US4356698A (en) * 1980-10-02 1982-11-02 United Technologies Corporation Staged combustor having aerodynamically separated combustion zones
GB2161914B (en) * 1980-12-10 1986-06-11 Rolls Royce Combustion equipment for a gas turbine engine
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
US4404806A (en) * 1981-09-04 1983-09-20 General Motors Corporation Gas turbine prechamber and fuel manifold structure
DE3332959A1 (de) * 1983-02-16 1985-03-28 Horst 6208 Bad Schwalbach Dens Einrichtung zur steuerung der verbrennung in sekundaergasstrahlverdichteranlagen fuer gasturbinen
US4807433A (en) * 1983-05-05 1989-02-28 General Electric Company Turbine cooling air modulation
EP0169431B1 (de) * 1984-07-10 1990-04-11 Hitachi, Ltd. Brennkammer für eine Gasturbine
US4700542A (en) * 1984-09-21 1987-10-20 Wang Lin Shu Internal combustion engines and methods of operation
US4641495A (en) * 1985-02-05 1987-02-10 A/S Kongsberg Vapenfabrikk Dual entry radial turbine gas generator
GB2172053B (en) * 1985-03-05 1988-10-05 Rolls Royce Gas turbine engine valve control system
US4747262A (en) * 1985-10-04 1988-05-31 Allied-Signal, Inc. Compressor power unit fuel flow control
JPH0663646B2 (ja) * 1985-10-11 1994-08-22 株式会社日立製作所 ガスタ−ビン用燃焼器
US4994149A (en) 1986-03-06 1991-02-19 Delta Projects Inc. Diluent substitution apparatus
SE453114B (sv) * 1986-04-29 1988-01-11 Asea Stal Ab Sett for drift av ett turbinaggregat
US4838029A (en) * 1986-09-10 1989-06-13 The United States Of America As Represented By The Secretary Of The Air Force Externally vaporizing system for turbine combustor
JP2644745B2 (ja) * 1987-03-06 1997-08-25 株式会社日立製作所 ガスタービン用燃焼器
US4845944A (en) * 1987-05-18 1989-07-11 Sundstrand Corporation Dual mode gas turbine power plant
EP0312620B1 (de) * 1987-10-19 1991-06-12 Hitachi, Ltd. Einrichtung zur Regulierung des Verbrennungsluftdurchsatzes in Gasturbinenbrennkammern
US4966001A (en) * 1987-10-23 1990-10-30 General Electric Company Multiple venturi tube gas fuel injector for catalytic combustor
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
US4928481A (en) * 1988-07-13 1990-05-29 Prutech Ii Staged low NOx premix gas turbine combustor
DE68923413T2 (de) * 1988-09-07 1996-04-04 Hitachi Ltd Kraftstoff-Luftvormischvorrichtung für eine Gasturbine.
DE3838415A1 (de) * 1988-11-09 1990-05-10 Fabeg Gmbh Vorrichtung zum verriegeln von schienenspitzen oder weichenzungen mit zugehoerigen backenschienen
US4944149A (en) * 1988-12-14 1990-07-31 General Electric Company Combustor liner with air staging for NOx control
US5214911A (en) * 1989-12-21 1993-06-01 Sundstrand Corporation Method and apparatus for high altitude starting of gas turbine engine
US5081832A (en) * 1990-03-05 1992-01-21 Rolf Jan Mowill High efficiency, twin spool, radial-high pressure, gas turbine engine
US5070700A (en) * 1990-03-05 1991-12-10 Rolf Jan Mowill Low emissions gas turbine combustor
US5156002A (en) * 1990-03-05 1992-10-20 Rolf J. Mowill Low emissions gas turbine combustor
US5257499A (en) * 1991-09-23 1993-11-02 General Electric Company Air staged premixed dry low NOx combustor with venturi modulated flow split
US5218824A (en) * 1992-06-25 1993-06-15 Solar Turbines Incorporated Low emission combustion nozzle for use with a gas turbine engine
DE9215856U1 (de) * 1992-11-21 1993-01-07 MAN Gutehoffnungshütte AG, 4200 Oberhausen Verdichterluft-Regelung eines Vormischbrenners bei Gasturbinen-Brennkammern

Also Published As

Publication number Publication date
DE69412191T2 (de) 1999-01-21
US5377483A (en) 1995-01-03
EP0635681A1 (de) 1995-01-25
US5481866A (en) 1996-01-09
JPH07180838A (ja) 1995-07-18
JP3527779B2 (ja) 2004-05-17
US5477671A (en) 1995-12-26
EP0635681B1 (de) 1998-08-05

Similar Documents

Publication Publication Date Title
DE69412191D1 (de) Vormischbrennkammer mit konstantem Brennstoff/Luft Verhältnis und einstufiger Verbrennung
DE69407676D1 (de) Luft und Brennstoff/Luft Düsenanordnung mit niedrigem NOx-Gehalt
DE69724031D1 (de) Vormischbrennkammer mit magerer Direkteinspritzung und geringem NOx-Ausstoss
DE59401177D1 (de) Misch- und Flammenstabilisierungseinrichtung in einer Brennkammer mit Vormischverbrennung
DE69224244D1 (de) Gasturbinenbrennkammer mit Einzelwirbel
DE69740148D1 (de) Verbrennungskraftmaschine mit Kompressionszündung und Kraftstoff-Luft Vormischung mit optimaler Verbrennungsregelung
DE59403036D1 (de) Gasturbinen-triebwerk mit lagerkammern und sperrluftkammern
KR100230939B1 (en) Low nox combustion method and its burner
DE69303314D1 (de) Brennkammer mit Vormischerzeuger
DE59508948D1 (de) Injektor zum Einblasen von Luft in den Verbrennungsraum eines Fackelbrenners und Fackelbrenner
DE68915611D1 (de) Brennstoffstrahlbrenner und Verbrennungsverfahren.
MX164478B (es) Mejoras en camara de combustion de turbina de gas con tomas de aire
BR9203444A (pt) Conjunto de combustivel e gas
DE59209209D1 (de) Gasbetriebener Vormischbrenner
DE69509816D1 (de) Gasbrenner mit sehr niedrigen Stickstoffoxidemissionen
DE69517949D1 (de) Verbesserung an Gasbrennersystemen und an mit diesen Systemen ausgerüsteten Geräten
DE59304403D1 (de) Gasturbine mit Abgasgehäuse und Abgaskanal
DE69225555D1 (de) Verbrennungsverfahren mit Rückführung und Pfropfenströmung
IT1308249B1 (it) Carburatore con arricchimento automatico della miscela di carburante e aria.
DE69404566D1 (de) Brennkammer mit Gasabscheider
DE69104335D1 (de) Kombinierte Vebrennungsluftzu- und Abgasabfuhr.
DE69303429D1 (de) Brennkammer mit verstellbaren Primärluftzufuhrbohrungen
DE69227303D1 (de) VORMISCH-GASBRENNER MIT NIEDRIGEM NOx-GEHALT
DE69113686D1 (de) Vormisch-Gasbrenner mit hohem Teillastverhältnis.
AU4984893A (en) Device for whirling diffusion of combustion air for turbo burner

Legal Events

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