ES2078888T1 - Aparato de camara de combustion y metodo para desarrollar la combustion - Google Patents

Aparato de camara de combustion y metodo para desarrollar la combustion

Info

Publication number
ES2078888T1
ES2078888T1 ES93914042T ES93914042T ES2078888T1 ES 2078888 T1 ES2078888 T1 ES 2078888T1 ES 93914042 T ES93914042 T ES 93914042T ES 93914042 T ES93914042 T ES 93914042T ES 2078888 T1 ES2078888 T1 ES 2078888T1
Authority
ES
Spain
Prior art keywords
combustion chamber
combustion
zone
developing
chamber apparatus
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.)
Granted
Application number
ES93914042T
Other languages
English (en)
Other versions
ES2078888T3 (es
Inventor
Richard L Marshall
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.)
RTX Corp
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 ES2078888T1 publication Critical patent/ES2078888T1/es
Application granted granted Critical
Publication of ES2078888T3 publication Critical patent/ES2078888T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/08—Purpose of the control system to produce clean exhaust gases
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/08—Purpose of the control system to produce clean exhaust gases
    • F05D2270/082—Purpose of the control system to produce clean exhaust gases with as little NOx as possible
    • 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)
  • Auxiliary Devices For And Details Of Packaging Control (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

ES DESCRITA UNA CAMARA DE COMBUSTION (42) PARA UNA MAQUINA (10) GIRATORIA DE FLUJO. VARIOS DETALLES DE CONSTRUCCION SON DESARROLLADOS PARA CONTROLAR LA PRODUCCION DE EMISIONES TALES COMO MONOXIDO DE CARBONO, HIDROCARBONOS NO QUEMADOS Y OXIDOS DE NITROGENO. EN UN CASO, LA CAMARA DE COMBUSTION TIENE UNA ZONA PILOTO (108) QUE SE EXTIENDE AXIALMENTE Y UNA ZONA PRINCIPAL (106) AXIALMENTE ADYACENTE A LA ZONA PILOTO QUE TIENE UNA PARED EXTERNA DIVERGENTE (178) A TRAVES DE LA CUAL LOS GASES QUE SE ARREMOLINAN LOCALMENTE SON INYECTADOS EN LOS GASES ARREMOLINADOS DE LA ZONA PILOTO (108).
ES93914042T 1992-06-12 1993-05-20 Aparato de camara de combustion y metodo para llevar a cabo la combustion. Expired - Lifetime ES2078888T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/898,053 US5406799A (en) 1992-06-12 1992-06-12 Combustion chamber

Publications (2)

Publication Number Publication Date
ES2078888T1 true ES2078888T1 (es) 1996-01-01
ES2078888T3 ES2078888T3 (es) 1997-04-16

Family

ID=25408862

Family Applications (1)

Application Number Title Priority Date Filing Date
ES93914042T Expired - Lifetime ES2078888T3 (es) 1992-06-12 1993-05-20 Aparato de camara de combustion y metodo para llevar a cabo la combustion.

Country Status (8)

Country Link
US (2) US5406799A (es)
EP (1) EP0644994B1 (es)
JP (1) JPH07507862A (es)
AT (1) ATE146872T1 (es)
DE (2) DE69306950T2 (es)
ES (1) ES2078888T3 (es)
GR (1) GR950300068T1 (es)
WO (1) WO1993025851A1 (es)

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FR2727193B1 (fr) * 1994-11-23 1996-12-20 Snecma Chambre de combustion a deux tetes fonctionnant du ralenti au plein gaz
WO1996027766A1 (de) * 1995-03-08 1996-09-12 Bmw Rolls-Royce Gmbh Axial gestufte doppelring-brennkammer einer gasturbine
DE19615910B4 (de) * 1996-04-22 2006-09-14 Alstom Brenneranordnung
JPH11257664A (ja) 1997-12-30 1999-09-21 United Technol Corp <Utc> ガスタ―ビンエンジンの燃料噴射ノズル／ガイドアセンブリ
US6240731B1 (en) 1997-12-31 2001-06-05 United Technologies Corporation Low NOx combustor for gas turbine engine
US6530223B1 (en) * 1998-10-09 2003-03-11 General Electric Company Multi-stage radial axial gas turbine engine combustor
US6412272B1 (en) * 1998-12-29 2002-07-02 United Technologies Corporation Fuel nozzle guide for gas turbine engine and method of assembly/disassembly
DE10020598A1 (de) * 2000-04-27 2002-03-07 Rolls Royce Deutschland Gasturbinenbrennkammer mit Zuleitungsöffnungen
WO2008070210A2 (en) * 2006-06-15 2008-06-12 Indiana University Research And Technology Corporation Pilot fuel injection for a wave rotor engine
US7631500B2 (en) * 2006-09-29 2009-12-15 General Electric Company Methods and apparatus to facilitate decreasing combustor acoustics
CN101688671B (zh) * 2007-07-02 2011-10-12 西门子公司 燃烧器和燃烧器的工作方法
US8176739B2 (en) * 2008-07-17 2012-05-15 General Electric Company Coanda injection system for axially staged low emission combustors
US8220269B2 (en) * 2008-09-30 2012-07-17 Alstom Technology Ltd. Combustor for a gas turbine engine with effusion cooled baffle
US8220271B2 (en) * 2008-09-30 2012-07-17 Alstom Technology Ltd. Fuel lance for a gas turbine engine including outer helical grooves
US8640464B2 (en) * 2009-02-23 2014-02-04 Williams International Co., L.L.C. Combustion system
JP4797079B2 (ja) * 2009-03-13 2011-10-19 川崎重工業株式会社 ガスタービン燃焼器
US20100242483A1 (en) * 2009-03-30 2010-09-30 United Technologies Corporation Combustor for gas turbine engine
RU2534189C2 (ru) * 2010-02-16 2014-11-27 Дженерал Электрик Компани Камера сгорания для газовой турбины(варианты) и способ эксплуатации газовой турбины
EP2434222B1 (en) * 2010-09-24 2019-02-27 Ansaldo Energia IP UK Limited Method for operating a combustion chamber
US9068748B2 (en) * 2011-01-24 2015-06-30 United Technologies Corporation Axial stage combustor for gas turbine engines
US9958162B2 (en) 2011-01-24 2018-05-01 United Technologies Corporation Combustor assembly for a turbine engine
US8479492B2 (en) * 2011-03-25 2013-07-09 Pratt & Whitney Canada Corp. Hybrid slinger combustion system
US9057523B2 (en) 2011-07-29 2015-06-16 United Technologies Corporation Microcircuit cooling for gas turbine engine combustor
WO2013043076A1 (en) * 2011-09-22 2013-03-28 General Electric Company Combustor and method for supplying fuel to a combustor
US9416972B2 (en) 2011-12-07 2016-08-16 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9194586B2 (en) 2011-12-07 2015-11-24 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
US9243802B2 (en) 2011-12-07 2016-01-26 Pratt & Whitney Canada Corp. Two-stage combustor for gas turbine engine
JP6028578B2 (ja) * 2013-01-15 2016-11-16 株式会社Ihi 燃焼器
EP2971649A4 (en) * 2013-03-14 2016-03-16 United Technologies Corp GAS TURBINE ENGINEERING DESIGN WITH NEST OF CONCENTRIC COMBUSTION CHAMBER
US11143407B2 (en) 2013-06-11 2021-10-12 Raytheon Technologies Corporation Combustor with axial staging for a gas turbine engine
US10060631B2 (en) 2013-08-29 2018-08-28 United Technologies Corporation Hybrid diffuser case for a gas turbine engine combustor
US20150107255A1 (en) * 2013-10-18 2015-04-23 General Electric Company Turbomachine combustor having an externally fueled late lean injection (lli) system
RU2561754C1 (ru) 2014-02-12 2015-09-10 Открытое акционерное общество "Газпром" Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации
US9803555B2 (en) * 2014-04-23 2017-10-31 General Electric Company Fuel delivery system with moveably attached fuel tube
US9976743B2 (en) * 2014-07-03 2018-05-22 United Technologies Corporation Dilution hole assembly
US10378773B2 (en) 2014-09-19 2019-08-13 United Technologies Corporation Turbine engine diffuser assembly with airflow mixer
FR3037384B1 (fr) * 2015-06-11 2017-06-23 Turbomeca Module de chambre de combustion cvc de turbomachine comportant une prechambre de combustion
RU2624682C1 (ru) * 2016-07-05 2017-07-05 Новиков Илья Николаевич Кольцевая камера сгорания газотурбинного двигателя и способ осуществления рабочего процесса
US11073286B2 (en) * 2017-09-20 2021-07-27 General Electric Company Trapped vortex combustor and method for operating the same
US10976052B2 (en) * 2017-10-25 2021-04-13 General Electric Company Volute trapped vortex combustor assembly
US10989411B2 (en) * 2019-01-03 2021-04-27 General Electric Company Heat exchanger for turbo machine
GB202019219D0 (en) * 2020-12-07 2021-01-20 Rolls Royce Plc Lean burn combustor
GB202019222D0 (en) 2020-12-07 2021-01-20 Rolls Royce Plc Lean burn combustor
US12516818B2 (en) * 2024-02-14 2026-01-06 General Electric Company Multi-fuel combustion system

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Also Published As

Publication number Publication date
EP0644994A1 (en) 1995-03-29
GR950300068T1 (en) 1996-01-31
WO1993025851A1 (en) 1993-12-23
US5490380A (en) 1996-02-13
DE69306950T2 (de) 1997-05-07
JPH07507862A (ja) 1995-08-31
ES2078888T3 (es) 1997-04-16
ATE146872T1 (de) 1997-01-15
DE69306950D1 (de) 1997-02-06
DE644994T1 (de) 1996-06-27
EP0644994B1 (en) 1996-12-27
US5406799A (en) 1995-04-18

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