CA1027380A - Injecteur de combustible pour chambre de combustion de turbine - Google Patents

Injecteur de combustible pour chambre de combustion de turbine

Info

Publication number
CA1027380A
CA1027380A CA205,301A CA205301A CA1027380A CA 1027380 A CA1027380 A CA 1027380A CA 205301 A CA205301 A CA 205301A CA 1027380 A CA1027380 A CA 1027380A
Authority
CA
Canada
Prior art keywords
fuel injection
gas turbine
turbine combustor
injection arrangement
arrangement
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
Application number
CA205,301A
Other languages
English (en)
Other versions
CA205301S (en
Inventor
Barry Weinstein
Edward D. Riley
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of CA1027380A publication Critical patent/CA1027380A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/101—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet
    • F23D11/105—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour medium and fuel meeting before the burner outlet at least one of the fluids being submitted to a swirling motion
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
CA205,301A 1973-09-10 1974-07-22 Injecteur de combustible pour chambre de combustion de turbine Expired CA1027380A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/395,605 US3946552A (en) 1973-09-10 1973-09-10 Fuel injection apparatus

Publications (1)

Publication Number Publication Date
CA1027380A true CA1027380A (fr) 1978-03-07

Family

ID=23563723

Family Applications (1)

Application Number Title Priority Date Filing Date
CA205,301A Expired CA1027380A (fr) 1973-09-10 1974-07-22 Injecteur de combustible pour chambre de combustion de turbine

Country Status (8)

Country Link
US (1) US3946552A (fr)
JP (1) JPS5922129B2 (fr)
BE (1) BE819722A (fr)
CA (1) CA1027380A (fr)
DE (1) DE2442895C2 (fr)
FR (1) FR2243332B1 (fr)
GB (1) GB1478395A (fr)
IT (1) IT1021212B (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111678128A (zh) * 2020-06-30 2020-09-18 安徽工业大学 一种基于高精度控制获取高稳定火焰的液体燃烧系统及燃烧方法

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EP0895024B1 (fr) * 1993-07-30 2003-01-02 United Technologies Corporation Mélangeur à tourbillon pour une chambre de combustion
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DE4444961A1 (de) * 1994-12-16 1996-06-20 Mtu Muenchen Gmbh Einrichtung zur Kühlung insbesondere der Rückwand des Flammrohrs einer Brennkammer für Gasturbinentriebwerke
US5623827A (en) * 1995-01-26 1997-04-29 General Electric Company Regenerative cooled dome assembly for a gas turbine engine combustor
US5697553A (en) * 1995-03-03 1997-12-16 Parker-Hannifin Corporation Streaked spray nozzle for enhanced air/fuel mixing
US5813232A (en) * 1995-06-05 1998-09-29 Allison Engine Company, Inc. Dry low emission combustor for gas turbine engines
DE19604347A1 (de) * 1996-02-07 1997-08-14 Koerting Ag Brenner für flüssigen oder gasförmigen Brennstoff, insbesondere für Öl
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US7013649B2 (en) * 2004-05-25 2006-03-21 General Electric Company Gas turbine engine combustor mixer
DE102004027702A1 (de) * 2004-06-07 2006-01-05 Alstom Technology Ltd Injektor für Flüssigbrennstoff sowie gestufter Vormischbrenner mit diesem Injektor
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US7316117B2 (en) * 2005-02-04 2008-01-08 Siemens Power Generation, Inc. Can-annular turbine combustors comprising swirler assembly and base plate arrangements, and combinations
US7513098B2 (en) 2005-06-29 2009-04-07 Siemens Energy, Inc. Swirler assembly and combinations of same in gas turbine engine combustors
US7681569B2 (en) * 2006-01-23 2010-03-23 Lytesyde, Llc Medical liquid processor apparatus and method
US7717096B2 (en) * 2006-01-23 2010-05-18 Lytesyde, Llc Fuel processor apparatus and method
US20070264602A1 (en) * 2006-01-26 2007-11-15 Frenette Henry E Vapor fuel combustion system
JP5023526B2 (ja) * 2006-03-23 2012-09-12 株式会社Ｉｈｉ 燃焼器用バーナ及び燃焼方法
US7870737B2 (en) * 2007-04-05 2011-01-18 United Technologies Corporation Hooded air/fuel swirler for a gas turbine engine
US8028674B2 (en) * 2007-08-07 2011-10-04 Lytesyde, Llc Fuel processor apparatus and method
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US8281597B2 (en) * 2008-12-31 2012-10-09 General Electric Company Cooled flameholder swirl cup
US8850819B2 (en) * 2010-06-25 2014-10-07 United Technologies Corporation Swirler, fuel and air assembly and combustor
US10317081B2 (en) * 2011-01-26 2019-06-11 United Technologies Corporation Fuel injector assembly
US9920932B2 (en) 2011-01-26 2018-03-20 United Technologies Corporation Mixer assembly for a gas turbine engine
US8973368B2 (en) 2011-01-26 2015-03-10 United Technologies Corporation Mixer assembly for a gas turbine engine
RU2451878C1 (ru) * 2011-02-07 2012-05-27 Открытое акционерное общество "Газпром" Способ предварительной подготовки и сжигания "бедной" топливовоздушной смеси в малоэмиссионной горелке
US9134023B2 (en) * 2012-01-06 2015-09-15 General Electric Company Combustor and method for distributing fuel in the combustor
US9657938B2 (en) 2014-02-07 2017-05-23 Eugene R. Frenette Fuel combustion system
RU2564746C2 (ru) * 2014-02-12 2015-10-10 Публичное акционерное общество "Газпром" Способ сжигания предварительно подготовленной "бедной" топливовоздушной смеси в двухконтурной малоэмиссионной горелке с регулировкой расхода пилотного топлива
RU2564474C2 (ru) * 2014-02-12 2015-10-10 Публичное акционерное общество "Газпром" Способ сжигания предварительно подготовленной "бедной" топливовоздушной смеси в двухконтурной малоэмиссионной горелке с повышенной устойчивостью сжигания пилотного топлива
WO2016160037A1 (fr) 2015-04-03 2016-10-06 Frenette Eugene R Système de combustion de combustible
JP6664825B2 (ja) * 2015-05-08 2020-03-13 三菱日立パワーシステムズインダストリー株式会社 低カロリーガスバーナ装置及びボイラ
FR3050806B1 (fr) * 2016-04-28 2020-02-21 Safran Aircraft Engines Vrille d'admission d'air pour systeme d'injection de turbomachine comprenant un deflecteur aerodynamique a son entree
US10801726B2 (en) 2017-09-21 2020-10-13 General Electric Company Combustor mixer purge cooling structure
US10890329B2 (en) 2018-03-01 2021-01-12 General Electric Company Fuel injector assembly for gas turbine engine
US10935245B2 (en) 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports
US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
US11073114B2 (en) 2018-12-12 2021-07-27 General Electric Company Fuel injector assembly for a heat engine
US11226101B2 (en) * 2019-02-01 2022-01-18 General Electric Company Combustor swirler
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FR3122720B1 (fr) * 2021-05-04 2024-05-03 Safran Aircraft Engines Cône de diffusion pour partie arrière de turboréacteur intégrant un système d'injection d'air et de carburant

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111678128A (zh) * 2020-06-30 2020-09-18 安徽工业大学 一种基于高精度控制获取高稳定火焰的液体燃烧系统及燃烧方法

Also Published As

Publication number Publication date
DE2442895A1 (de) 1975-03-13
US3946552A (en) 1976-03-30
JPS5076424A (fr) 1975-06-23
BE819722A (fr) 1974-12-31
FR2243332A1 (fr) 1975-04-04
IT1021212B (it) 1978-01-30
FR2243332B1 (fr) 1978-06-09
JPS5922129B2 (ja) 1984-05-24
DE2442895C2 (de) 1986-07-03
GB1478395A (en) 1977-06-29

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