FR2774152B1 - Chambre de combustion de turbine a gaz fonctionnant au carburant liquide - Google Patents

Chambre de combustion de turbine a gaz fonctionnant au carburant liquide

Info

Publication number
FR2774152B1
FR2774152B1 FR9800932A FR9800932A FR2774152B1 FR 2774152 B1 FR2774152 B1 FR 2774152B1 FR 9800932 A FR9800932 A FR 9800932A FR 9800932 A FR9800932 A FR 9800932A FR 2774152 B1 FR2774152 B1 FR 2774152B1
Authority
FR
France
Prior art keywords
combustion chamber
gas turbine
liquid fuel
turbine operating
operating
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 - Lifetime
Application number
FR9800932A
Other languages
English (en)
Other versions
FR2774152A1 (fr
Inventor
Gal Jean Herve Le
Patrick Flament
Gerard Martin
Guy Grienche
Gerard Schott
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.)
Safran Helicopter Engines SAS
Original Assignee
IFP Energies Nouvelles IFPEN
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 IFP Energies Nouvelles IFPEN filed Critical IFP Energies Nouvelles IFPEN
Priority to FR9800932A priority Critical patent/FR2774152B1/fr
Priority to EP99400141A priority patent/EP0933594B1/fr
Priority to DE69922559T priority patent/DE69922559T2/de
Priority to US09/238,586 priority patent/US6378310B1/en
Priority to JP11020214A priority patent/JPH11270852A/ja
Publication of FR2774152A1 publication Critical patent/FR2774152A1/fr
Application granted granted Critical
Publication of FR2774152B1 publication Critical patent/FR2774152B1/fr
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
    • F23R3/44—Combustion chambers comprising a single tubular flame tube within a tubular casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
    • 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
    • F23D11/36—Details, e.g. burner cooling means, noise reduction means
    • F23D11/38—Nozzles; Cleaning devices therefor
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • F23R3/58—Cyclone or vortex type combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR9800932A 1998-01-28 1998-01-28 Chambre de combustion de turbine a gaz fonctionnant au carburant liquide Expired - Lifetime FR2774152B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR9800932A FR2774152B1 (fr) 1998-01-28 1998-01-28 Chambre de combustion de turbine a gaz fonctionnant au carburant liquide
EP99400141A EP0933594B1 (fr) 1998-01-28 1999-01-21 Procédé de fonctionnement d'une chambre de combustion de turbine à gaz fonctionnant au carburant liquide
DE69922559T DE69922559T2 (de) 1998-01-28 1999-01-21 Verfahren zum Betreiben einer Gasturbinenbrennkammer für flüssigen Kraftstoff
US09/238,586 US6378310B1 (en) 1998-01-28 1999-01-28 Combustion chamber of a gas turbine working on liquid fuel
JP11020214A JPH11270852A (ja) 1998-01-28 1999-01-28 液体燃料で作動するガスタ―ビンの燃焼室

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9800932A FR2774152B1 (fr) 1998-01-28 1998-01-28 Chambre de combustion de turbine a gaz fonctionnant au carburant liquide

Publications (2)

Publication Number Publication Date
FR2774152A1 FR2774152A1 (fr) 1999-07-30
FR2774152B1 true FR2774152B1 (fr) 2000-03-24

Family

ID=9522281

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9800932A Expired - Lifetime FR2774152B1 (fr) 1998-01-28 1998-01-28 Chambre de combustion de turbine a gaz fonctionnant au carburant liquide

Country Status (5)

Country Link
US (1) US6378310B1 (fr)
EP (1) EP0933594B1 (fr)
JP (1) JPH11270852A (fr)
DE (1) DE69922559T2 (fr)
FR (1) FR2774152B1 (fr)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10040791A1 (de) * 2000-08-21 2002-03-14 Siemens Ag Verfahren und Vorrichtung zur Bestimmung und Kompensation der Verkippung des Spektrums in einer Lichtleitfaser einer Datenübertragungsstrecke
US6543235B1 (en) * 2001-08-08 2003-04-08 Cfd Research Corporation Single-circuit fuel injector for gas turbine combustors
EP1802915B1 (fr) * 2004-10-18 2016-11-30 General Electric Technology GmbH Bruleur pour turbine a gaz
US20060218932A1 (en) * 2004-11-10 2006-10-05 Pfefferle William C Fuel injector
DE102005036889A1 (de) * 2005-08-05 2007-02-15 Gerhard Wohlfarth Verfahren und Vorrichtung zur Einleitung, Förderung und Beschleunigung physikalischer Prozesse bzw. Reaktionen an flüssigen, gasförmigen Stoffen, Stoffgemischen, Lösungen und im besonderen ein Verfahren und Vorrichtung zur Steigerung des Wirkungsgrades bei Verbrennungsvorgängen in Ölfeuerungsanlagen
US8062027B2 (en) * 2005-08-11 2011-11-22 Elster Gmbh Industrial burner and method for operating an industrial burner
US7614211B2 (en) * 2005-12-15 2009-11-10 General Electric Company Swirling flows and swirler to enhance pulse detonation engine operation
FR2903173B1 (fr) * 2006-06-29 2008-08-29 Snecma Sa Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
EP2072899B1 (fr) 2007-12-19 2016-03-30 Alstom Technology Ltd Procédé d'injection de carburant
US9062563B2 (en) * 2008-04-09 2015-06-23 General Electric Company Surface treatments for preventing hydrocarbon thermal degradation deposits on articles
US8683808B2 (en) * 2009-01-07 2014-04-01 General Electric Company Late lean injection control strategy
US8707707B2 (en) * 2009-01-07 2014-04-29 General Electric Company Late lean injection fuel staging configurations
US8701382B2 (en) * 2009-01-07 2014-04-22 General Electric Company Late lean injection with expanded fuel flexibility
US8112216B2 (en) * 2009-01-07 2012-02-07 General Electric Company Late lean injection with adjustable air splits
US8701383B2 (en) * 2009-01-07 2014-04-22 General Electric Company Late lean injection system configuration
US8701418B2 (en) * 2009-01-07 2014-04-22 General Electric Company Late lean injection for fuel flexibility
NL2005381C2 (en) * 2010-09-21 2012-03-28 Micro Turbine Technology B V Combustor with a single limited fuel-air mixing burner and recuperated micro gas turbine.
US20120210717A1 (en) * 2011-02-21 2012-08-23 General Electric Company Apparatus for injecting fluid into a combustion chamber of a combustor
DE102011013950A1 (de) * 2011-03-14 2012-09-20 Air Liquide Deutschland Gmbh Brenner und Verfahren zum Betreiben eines Brenners
US8893500B2 (en) 2011-05-18 2014-11-25 Solar Turbines Inc. Lean direct fuel injector
US8919132B2 (en) 2011-05-18 2014-12-30 Solar Turbines Inc. Method of operating a gas turbine engine
US9182124B2 (en) 2011-12-15 2015-11-10 Solar Turbines Incorporated Gas turbine and fuel injector for the same
US20160053681A1 (en) * 2014-08-20 2016-02-25 General Electric Company Liquid fuel combustor having an oxygen-depleted gas (odg) injection system for a gas turbomachine
CN110397935A (zh) * 2018-04-25 2019-11-01 中国科学院工程热物理研究所 旋风熔融炉及其使用方法

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB387049A (en) * 1930-10-23 1933-02-02 Hubert Jezler Improvements in or relating to the firing of boilers and the like
US2638745A (en) * 1943-04-01 1953-05-19 Power Jets Res & Dev Ltd Gas turbine combustor having tangential air inlets for primary and secondary air
BE560443A (fr) * 1956-09-01
JPS4931059Y1 (fr) * 1970-11-30 1974-08-22
US4006589A (en) * 1975-04-14 1977-02-08 Phillips Petroleum Company Low emission combustor with fuel flow controlled primary air flow and circumferentially directed secondary air flows
US4271675A (en) * 1977-10-21 1981-06-09 Rolls-Royce Limited Combustion apparatus for gas turbine engines
US4222232A (en) * 1978-01-19 1980-09-16 United Technologies Corporation Method and apparatus for reducing nitrous oxide emissions from combustors
EP0124146A1 (fr) * 1983-03-30 1984-11-07 Shell Internationale Researchmaatschappij B.V. Procédé et appareil pour la combustion du combustible avec émission à faible teneur en NOx, de suie et de particules
US4702073A (en) * 1986-03-10 1987-10-27 Melconian Jerry O Variable residence time vortex combustor
US4928481A (en) * 1988-07-13 1990-05-29 Prutech Ii Staged low NOx premix gas turbine combustor
FR2656676B1 (fr) 1989-12-28 1994-07-01 Inst Francais Du Petrole Bruleur industriel a combustible liquide a faible emission d'oxyde d'azote, ledit bruleur generant plusieurs flammes elementaires et son utilisation.
US5628184A (en) * 1993-02-03 1997-05-13 Santos; Rolando R. Apparatus for reducing the production of NOx in a gas turbine
FR2706985B1 (fr) * 1993-06-22 1995-08-25 Pillard Ent Gle Chauffage Indl
US5479781A (en) * 1993-09-02 1996-01-02 General Electric Company Low emission combustor having tangential lean direct injection
US5488829A (en) * 1994-05-25 1996-02-06 Westinghouse Electric Corporation Method and apparatus for reducing noise generated by combustion
US5822992A (en) 1995-10-19 1998-10-20 General Electric Company Low emissions combustor premixer
FR2741424B1 (fr) 1995-11-17 1998-01-02 Schlumberger Services Petrol Bruleur a faible pollution, pour essais de puits petroliers
US5680766A (en) * 1996-01-02 1997-10-28 General Electric Company Dual fuel mixer for gas turbine combustor

Also Published As

Publication number Publication date
US6378310B1 (en) 2002-04-30
FR2774152A1 (fr) 1999-07-30
EP0933594B1 (fr) 2004-12-15
US20020050139A1 (en) 2002-05-02
DE69922559D1 (de) 2005-01-20
JPH11270852A (ja) 1999-10-05
DE69922559T2 (de) 2005-05-12
EP0933594A1 (fr) 1999-08-04

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Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property

Owner name: NUECLETRON HOLDING B.V., NL

Effective date: 20120719

PLFP Fee payment

Year of fee payment: 19

PLFP Fee payment

Year of fee payment: 20

CD Change of name or company name

Owner name: SAFRAN HELICOPTER ENGINES, FR

Effective date: 20170727