MX173946B - Disposicion de boquilla de combustible para dispositivo de combustion. - Google Patents

Disposicion de boquilla de combustible para dispositivo de combustion.

Info

Publication number
MX173946B
MX173946B MX019115A MX1911590A MX173946B MX 173946 B MX173946 B MX 173946B MX 019115 A MX019115 A MX 019115A MX 1911590 A MX1911590 A MX 1911590A MX 173946 B MX173946 B MX 173946B
Authority
MX
Mexico
Prior art keywords
row
fuel nozzles
air
swirl
radii
Prior art date
Application number
MX019115A
Other languages
English (en)
Inventor
Jim A Clark
James H Shadowen
Thomas L Dubell
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 MX173946B publication Critical patent/MX173946B/es

Links

Classifications

    • 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
    • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • 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
    • F23R3/42—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
    • 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)
  • Spray-Type Burners (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)

Abstract

La presente invención se refiere a un dispositivo anular de combustión para una máquina de turbina de gas, caracterizado porque tiene una pared que se extiende axialmente, anular, externa y una pared que se extiende axialmente, anular, interna, concéntricamente dispuesta en relación a dicha pared externa y definiendo una cámara de combustión; un domo que interconecta a dicha pared interna con dicha pared externa en el extremo delantero para encerrar el extremo delantero de dicha cámara de combustión; una pluralidad de boquillas de combustible que tienen el medio arremolinadores de aire dispuestos en dicho domo, dichas boquillas de combustibe dispuestas en una hilera de radios pequeños y una hilera de radios más grandes, tres boquillas de combustible adyacentes de dicha pluralidad de boquillas de combustible que incluyen dos de dichas boquillas de combustible adyacentes siendo de una de dicha hilera de radios más grandes o dicha hilera de radios más pequeños y una de dichas boquillas de combustible adyacentes, siendo de otra de dicha hilera de radios más grandes o de la hilera de radios más pequeños y dispuestas juntas de tal forma que una línea imaginaria que pasa a través del centro de cada una de dichas tres boquillas de combustible adyacentes, define un triángulo, dichos medios arremolinadores están dispuestos para que la rotación del remolino de aire en cada medio arremolinador de aire de cada hilera está en la misma dirección y la rotación del remolino de cada medio arremolinador de aire en la hilera de radio más grande es opuesto a la rotación del remolino de cada medio arremolinador de aire en la hilera de radio más pequeño, el combustible/aire emitido de cada una de dichas boquillas de combustible interactuando con la descarga de las boquillas de combustible adyacentes para establecer un patrón de remolino e combustible/aire en el extremo frontal de dicho dispositivo anular de combustión para establecer el quemado.
MX019115A 1989-01-12 1990-01-12 Disposicion de boquilla de combustible para dispositivo de combustion. MX173946B (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/296,155 US4991398A (en) 1989-01-12 1989-01-12 Combustor fuel nozzle arrangement

Publications (1)

Publication Number Publication Date
MX173946B true MX173946B (es) 1994-04-11

Family

ID=23140844

Family Applications (1)

Application Number Title Priority Date Filing Date
MX019115A MX173946B (es) 1989-01-12 1990-01-12 Disposicion de boquilla de combustible para dispositivo de combustion.

Country Status (11)

Country Link
US (1) US4991398A (es)
EP (1) EP0378505B1 (es)
JP (1) JP3058887B2 (es)
KR (1) KR960003680B1 (es)
CN (1) CN1024940C (es)
AU (1) AU626626B2 (es)
BR (1) BR9000103A (es)
DE (1) DE69006861T2 (es)
IL (1) IL92977A (es)
MX (1) MX173946B (es)
RU (1) RU1836606C (es)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5284019A (en) * 1990-06-12 1994-02-08 The United States Of America As Represented By The Secretary Of The Air Force Double dome, single anular combustor with daisy mixer
CH684963A5 (de) * 1991-11-13 1995-02-15 Asea Brown Boveri Ringbrennkammer.
FR2694624B1 (fr) * 1992-08-05 1994-09-23 Snecma Chambre de combustion à plusieurs injecteurs de carburant.
US5303542A (en) * 1992-11-16 1994-04-19 General Electric Company Fuel supply control method for a gas turbine engine
US5323604A (en) * 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
US5289685A (en) * 1992-11-16 1994-03-01 General Electric Company Fuel supply system for a gas turbine engine
US5331805A (en) * 1993-04-22 1994-07-26 Alliedsignal Inc. Reduced diameter annular combustor
US5431019A (en) * 1993-04-22 1995-07-11 Alliedsignal Inc. Combustor for gas turbine engine
DE19549143A1 (de) * 1995-12-29 1997-07-03 Abb Research Ltd Gasturbinenringbrennkammer
GB2319078B (en) * 1996-11-08 1999-11-03 Europ Gas Turbines Ltd Combustor arrangement
US5966937A (en) * 1997-10-09 1999-10-19 United Technologies Corporation Radial inlet swirler with twisted vanes for fuel injector
US5987889A (en) * 1997-10-09 1999-11-23 United Technologies Corporation Fuel injector for producing outer shear layer flame for combustion
WO2000049337A1 (de) * 1999-02-16 2000-08-24 Siemens Aktiengesellschaft Brenneranordnung und verfahren zum betrieb einer brenneranordnung
JP2003065537A (ja) * 2001-08-24 2003-03-05 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器
US6625971B2 (en) 2001-09-14 2003-09-30 United Technologies Corporation Fuel nozzle producing skewed spray pattern
KR20030028150A (ko) * 2001-09-27 2003-04-08 한국항공우주연구원 액체추진제 로켓엔진에서의 직교방사형 분사기 배열
US6772583B2 (en) * 2002-09-11 2004-08-10 Siemens Westinghouse Power Corporation Can combustor for a gas turbine engine
US20090217669A1 (en) * 2003-02-05 2009-09-03 Young Kenneth J Fuel nozzles
KR100810310B1 (ko) 2003-08-29 2008-03-07 삼성전자주식회사 조도차가 다른 영상의 재구성 장치 및 방법
US7506511B2 (en) * 2003-12-23 2009-03-24 Honeywell International Inc. Reduced exhaust emissions gas turbine engine combustor
FR2914986B1 (fr) 2007-04-12 2015-04-10 Saint Gobain Isover Bruleur a combustion interne
FR2919672B1 (fr) * 2007-07-30 2014-02-14 Snecma Injecteur de carburant dans une chambre de combustion de turbomachine
GB2454247A (en) * 2007-11-02 2009-05-06 Siemens Ag A Combustor for a Gas-Turbine Engine Has a Burner Head with Fuel Delivered at a Compound Angle
GB2455289B (en) 2007-12-03 2010-04-07 Siemens Ag Improvements in or relating to burners for a gas-turbine engine
US9500368B2 (en) * 2008-09-23 2016-11-22 Siemens Energy, Inc. Alternately swirling mains in lean premixed gas turbine combustors
KR101049359B1 (ko) * 2008-10-31 2011-07-13 한국전력공사 삼중 스월형 가스터빈 연소기
US20100192578A1 (en) * 2009-01-30 2010-08-05 General Electric Company System and method for suppressing combustion instability in a turbomachine
US8763399B2 (en) * 2009-04-03 2014-07-01 Hitachi, Ltd. Combustor having modified spacing of air blowholes in an air blowhole plate
US20100281869A1 (en) * 2009-05-06 2010-11-11 Mark Allan Hadley Airblown Syngas Fuel Nozzle With Diluent Openings
US8904799B2 (en) * 2009-05-25 2014-12-09 Majed Toqan Tangential combustor with vaneless turbine for use on gas turbine engines
US20110072823A1 (en) * 2009-09-30 2011-03-31 Daih-Yeou Chen Gas turbine engine fuel injector
RU2506499C2 (ru) * 2009-11-09 2014-02-10 Дженерал Электрик Компани Топливные форсунки газовой турбины с противоположными направлениями завихрения
US10317081B2 (en) 2011-01-26 2019-06-11 United Technologies Corporation Fuel injector assembly
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
FR2982010B1 (fr) * 2011-10-26 2013-11-08 Snecma Chambre de combustion annulaire dans une turbomachine
RU2561754C1 (ru) 2014-02-12 2015-09-10 Открытое акционерное общество "Газпром" Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации
US10458331B2 (en) * 2016-06-20 2019-10-29 United Technologies Corporation Fuel injector with heat pipe cooling
US20180335214A1 (en) * 2017-05-18 2018-11-22 United Technologies Corporation Fuel air mixer assembly for a gas turbine engine combustor
US11181274B2 (en) 2017-08-21 2021-11-23 General Electric Company Combustion system and method for attenuation of combustion dynamics in a gas turbine engine
US11859819B2 (en) 2021-10-15 2024-01-02 General Electric Company Ceramic composite combustor dome and liners

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2595999A (en) * 1943-11-23 1952-05-06 Westinghouse Electric Corp Power plant combustion apparatus having apertured combustion chamber walls
US2647369A (en) * 1946-09-06 1953-08-04 Leduc Rene Combustion chamber for fluid fuel burning in an air stream of high velocity
GB616635A (en) * 1946-09-13 1949-01-25 Donald Louis Mordell Improvements relating to gas-turbine engines
US3153323A (en) * 1954-03-31 1964-10-20 James R Hamm Internal combustion apparatus
US3000183A (en) * 1957-01-30 1961-09-19 Gen Motors Corp Spiral annular combustion chamber
GB925349A (en) * 1958-12-03 1963-05-08 Lucas Industries Ltd Improvements relating to prime movers incorporating gas turbines
US3720058A (en) * 1970-01-02 1973-03-13 Gen Electric Combustor and fuel injector
DE2223093A1 (de) * 1972-05-12 1973-11-22 Gen Electric Brenner und brennstoffinjektor
JPS4921515A (es) * 1972-05-22 1974-02-26
FR2402068A1 (fr) * 1977-09-02 1979-03-30 Snecma Chambre de combustion anti-pollution
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
GB2036296B (en) * 1978-11-20 1982-12-01 Rolls Royce Gas turbine
EP0193029B1 (de) * 1985-02-26 1988-11-17 BBC Brown Boveri AG Brennkammer für Gasturbinen

Also Published As

Publication number Publication date
JPH02233907A (ja) 1990-09-17
EP0378505B1 (en) 1994-03-02
JP3058887B2 (ja) 2000-07-04
KR960003680B1 (ko) 1996-03-21
BR9000103A (pt) 1991-10-08
AU626626B2 (en) 1992-08-06
EP0378505A1 (en) 1990-07-18
CN1024940C (zh) 1994-06-08
RU1836606C (ru) 1993-08-23
CN1044325A (zh) 1990-08-01
KR900011966A (ko) 1990-08-02
DE69006861T2 (de) 1994-06-09
IL92977A0 (en) 1991-06-10
US4991398A (en) 1991-02-12
AU4774390A (en) 1990-07-19
DE69006861D1 (de) 1994-04-07
IL92977A (en) 1993-07-08

Similar Documents

Publication Publication Date Title
MX173946B (es) Disposicion de boquilla de combustible para dispositivo de combustion.
US11415321B2 (en) Combustor liner for a gas turbine engine and an associated method thereof
CN105473944B (zh) 燃气涡轮燃烧器和具备该燃气涡轮燃烧器的燃气涡轮发动机
ES2123102T3 (es) Alabes de torbellino para camara de combustion de turbina de gas.
JP5678603B2 (ja) 微粉炭バーナ
CN105705866B (zh) 喷嘴、燃烧器以及燃气轮机
US10753283B2 (en) Combustor heat shield cooling hole arrangement
ES2116531T3 (es) Camara de combustion con produccion ultrabaja de nox para dos combustibles.
CA2551539A1 (en) Gas turbine engine combustor with improved cooling
JP2010249136A (ja) 成形した滲み出し冷却孔を持つ燃焼器キャップ
EP2796789A1 (en) Can combustor for a can-annular combustor arrangement in a gas turbine
JP2023504296A (ja) さか火現象を防止することができる水素ガス燃焼装置
US3944142A (en) Split stream burner assembly
CN206176456U (zh) 燃气轮机燃烧室
CN107120652B (zh) 一种分级燃气低氮燃烧器
CN206274175U (zh) 燃气轮机燃烧室
EP2685163B1 (en) Premix burner of the multi-cone type for a gas turbine
CN106439914A (zh) 燃气轮机燃烧室
CN106402934A (zh) 燃气轮机燃烧室及其喷嘴
CN105351930B (zh) 文丘里燃烧器的稳焰器
JP6302886B2 (ja) バーナ装置用の機能付加装置
US3031012A (en) Combustion apparatus
JP2021101152A (ja) 燃焼器及びガスタービン
RU2515909C2 (ru) Кольцевая малоэмиссионная камера сгорания газотурбинного двигателя
CN205447724U (zh) 锅炉