FR2674317B1 - Chambre de combustion de turbomachine comportant un reglage du debit de comburant. - Google Patents

Chambre de combustion de turbomachine comportant un reglage du debit de comburant.

Info

Publication number
FR2674317B1
FR2674317B1 FR9103374A FR9103374A FR2674317B1 FR 2674317 B1 FR2674317 B1 FR 2674317B1 FR 9103374 A FR9103374 A FR 9103374A FR 9103374 A FR9103374 A FR 9103374A FR 2674317 B1 FR2674317 B1 FR 2674317B1
Authority
FR
France
Prior art keywords
turbomachine
adjustment
combustion chamber
fuel flow
fuel
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
FR9103374A
Other languages
English (en)
Other versions
FR2674317A1 (fr
Inventor
Barbier Gerard
Yves
Georges
Bardey Xavier
Marie
Henri
Desaulty Michel
Andre
Albert
Meunier Serge
Marcel
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 Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR9103374A priority Critical patent/FR2674317B1/fr
Priority to US07/851,167 priority patent/US5235805A/en
Priority to DE69200735T priority patent/DE69200735T2/de
Priority to EP92400715A priority patent/EP0506516B1/fr
Publication of FR2674317A1 publication Critical patent/FR2674317A1/fr
Application granted granted Critical
Publication of FR2674317B1 publication Critical patent/FR2674317B1/fr
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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/045—Air inlet arrangements using pipes
    • 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
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR9103374A 1991-03-20 1991-03-20 Chambre de combustion de turbomachine comportant un reglage du debit de comburant. Expired - Fee Related FR2674317B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR9103374A FR2674317B1 (fr) 1991-03-20 1991-03-20 Chambre de combustion de turbomachine comportant un reglage du debit de comburant.
US07/851,167 US5235805A (en) 1991-03-20 1992-03-12 Gas turbine engine combustion chamber with oxidizer intake flow control
DE69200735T DE69200735T2 (de) 1991-03-20 1992-03-18 Verbrennungsluftzufuhreinrichtung für eine Brennkammer einer Turbomaschine.
EP92400715A EP0506516B1 (fr) 1991-03-20 1992-03-18 Chambre de combustion de turbomachine comportant un réglage du débit de comburant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9103374A FR2674317B1 (fr) 1991-03-20 1991-03-20 Chambre de combustion de turbomachine comportant un reglage du debit de comburant.

Publications (2)

Publication Number Publication Date
FR2674317A1 FR2674317A1 (fr) 1992-09-25
FR2674317B1 true FR2674317B1 (fr) 1993-05-28

Family

ID=9410929

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9103374A Expired - Fee Related FR2674317B1 (fr) 1991-03-20 1991-03-20 Chambre de combustion de turbomachine comportant un reglage du debit de comburant.

Country Status (4)

Country Link
US (1) US5235805A (fr)
EP (1) EP0506516B1 (fr)
DE (1) DE69200735T2 (fr)
FR (1) FR2674317B1 (fr)

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DE19520291A1 (de) * 1995-06-02 1996-12-05 Abb Management Ag Brennkammer
GB9919981D0 (en) * 1999-08-24 1999-10-27 Rolls Royce Plc Combustion apparatus
US6351949B1 (en) * 1999-09-03 2002-03-05 Allison Advanced Development Company Interchangeable combustor chute
US6499993B2 (en) 2000-05-25 2002-12-31 General Electric Company External dilution air tuning for dry low NOX combustors and methods therefor
US6331110B1 (en) * 2000-05-25 2001-12-18 General Electric Company External dilution air tuning for dry low NOx combustors and methods therefor
GB2379499B (en) 2001-09-11 2004-01-28 Rolls Royce Plc Gas turbine engine combustor
US7000396B1 (en) * 2004-09-02 2006-02-21 General Electric Company Concentric fixed dilution and variable bypass air injection for a combustor
EP1907685A1 (fr) * 2005-07-05 2008-04-09 Stéphane Véronneau Configurations de foyers
US20090260340A1 (en) * 2008-04-17 2009-10-22 General Electric Company Combustor of a Turbine, a Method of Retro-Fitting a Combustor of a Turbine and a Method of Building a Combustor of a Turbine
US8590313B2 (en) * 2008-07-30 2013-11-26 Rolls-Royce Corporation Precision counter-swirl combustor
US9010123B2 (en) * 2010-07-26 2015-04-21 Honeywell International Inc. Combustors with quench inserts
DE102011012414A1 (de) * 2011-02-25 2012-08-30 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer
US9062884B2 (en) * 2011-05-26 2015-06-23 Honeywell International Inc. Combustors with quench inserts
US20130283806A1 (en) * 2012-04-26 2013-10-31 General Electric Company Combustor and a method for repairing the combustor
US20130305729A1 (en) * 2012-05-21 2013-11-21 General Electric Company Turbomachine combustor and method for adjusting combustion dynamics in the same
DE102012022259A1 (de) * 2012-11-13 2014-05-28 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerschindel einer Gasturbine sowie Verfahren zu deren Herstellung
EP2735796B1 (fr) * 2012-11-23 2020-01-01 Ansaldo Energia IP UK Limited Paroi située sur la trajectoire des gaz chauds d'une turbine à gaz et procédé pour améliorer le comportement de fonctionnment d'une turbine à gaz
US9228747B2 (en) * 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
WO2015147938A2 (fr) * 2014-01-03 2015-10-01 United Technologies Corporation Passe-fil refroidi pour un ensemble paroi de chambre de combustion
EP2957833B1 (fr) 2014-06-17 2018-10-24 Rolls-Royce Corporation Ensemble chambre de combustion avec des goulottes
FR3022613B1 (fr) * 2014-06-24 2019-04-19 Safran Helicopter Engines Bossage pour chambre de combustion.
DE112015003440T5 (de) * 2014-07-25 2017-04-13 Mitsubishi Hitachi Power Systems, Ltd. Zylinder für Brennkammer, Brennkammer und Gasturbine
US9909549B2 (en) 2014-10-01 2018-03-06 National Technology & Engineering Solutions Of Sandia, Llc Ducted fuel injection
US10788212B2 (en) * 2015-01-12 2020-09-29 General Electric Company System and method for an oxidant passageway in a gas turbine system with exhaust gas recirculation
US20160209035A1 (en) * 2015-01-16 2016-07-21 Solar Turbines Incorporated Combustion hole insert with integrated film restarter
KR101843961B1 (ko) * 2015-05-27 2018-03-30 두산중공업 주식회사 회전가능한 공기유도캡이 마련된 연소기 챔버.
US10138855B2 (en) 2015-07-01 2018-11-27 National Technology & Engineering Solutions Of Sandia, Llc Ducted fuel injection with ignition assist
US10161626B2 (en) 2015-07-01 2018-12-25 National Technology & Engineering Solutions Of Sandia, Llc Ducted fuel injection
CN108463628A (zh) * 2016-01-13 2018-08-28 桑迪亚国家技术与工程解决方案有限公司 导管式燃料喷射
RU167336U1 (ru) * 2016-04-06 2017-01-10 Публичное акционерное общество "Научно-производственное объединение "Сатурн" Жаровая труба камеры сгорания газотурбинного двигателя
US11187415B2 (en) * 2017-12-11 2021-11-30 General Electric Company Fuel injection assemblies for axial fuel staging in gas turbine combustors
US11137144B2 (en) 2017-12-11 2021-10-05 General Electric Company Axial fuel staging system for gas turbine combustors
US11255543B2 (en) * 2018-08-07 2022-02-22 General Electric Company Dilution structure for gas turbine engine combustor
US11248789B2 (en) 2018-12-07 2022-02-15 Raytheon Technologies Corporation Gas turbine engine with integral combustion liner and turbine nozzle
US11572835B2 (en) * 2021-05-11 2023-02-07 General Electric Company Combustor dilution hole
US11959643B2 (en) * 2021-06-07 2024-04-16 General Electric Company Combustor for a gas turbine engine
CN114484497A (zh) * 2021-11-30 2022-05-13 北京动力机械研究所 一种紧凑一体化设计的冷却掺混斗
US20240255146A1 (en) * 2023-02-01 2024-08-01 Rtx Corporation Dilution passages for combustor of a gas turbine engine

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Publication number Priority date Publication date Assignee Title
US3099134A (en) * 1959-12-24 1963-07-30 Havilland Engine Co Ltd Combustion chambers
CH411464A (de) * 1962-07-24 1966-04-15 Prvni Brnenska Strojirna Brennkammer für Gasturbinen
FR1340751A (fr) * 1962-12-11 1963-10-18 Cem Comp Electro Mec Perfectionnement aux turbines à combustion
US3608310A (en) * 1966-06-27 1971-09-28 Gen Motors Corp Turbine stator-combustor structure
US3490230A (en) * 1968-03-22 1970-01-20 Us Navy Combustion air control shutter
GB1278590A (en) * 1968-09-20 1972-06-21 Lucas Industries Ltd Combustion chambers for gas turbine engines
US3958413A (en) * 1974-09-03 1976-05-25 General Motors Corporation Combustion method and apparatus
JPS5129726A (fr) * 1974-09-06 1976-03-13 Mitsubishi Heavy Ind Ltd
US4050240A (en) * 1976-08-26 1977-09-27 General Motors Corporation Variable air admission device for a combustor assembly
FR2572463B1 (fr) * 1984-10-30 1989-01-20 Snecma Systeme d'injection a geometrie variable.
FR2599821B1 (fr) * 1986-06-04 1988-09-02 Snecma Chambre de combustion pour turbomachines a orifices de melange assurant le positionnement de la paroi chaude sur la paroi froide
JPH07113329B2 (ja) * 1986-12-15 1995-12-06 三井造船株式会社 ガスタ−ビン

Also Published As

Publication number Publication date
EP0506516B1 (fr) 1994-11-30
EP0506516A1 (fr) 1992-09-30
US5235805A (en) 1993-08-17
DE69200735D1 (de) 1995-01-12
DE69200735T2 (de) 1995-04-27
FR2674317A1 (fr) 1992-09-25

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