FR2695192B1 - Bruleur pour propulseurs a turbines a gaz. - Google Patents

Bruleur pour propulseurs a turbines a gaz.

Info

Publication number
FR2695192B1
FR2695192B1 FR9310306A FR9310306A FR2695192B1 FR 2695192 B1 FR2695192 B1 FR 2695192B1 FR 9310306 A FR9310306 A FR 9310306A FR 9310306 A FR9310306 A FR 9310306A FR 2695192 B1 FR2695192 B1 FR 2695192B1
Authority
FR
France
Prior art keywords
burner
gas turbine
turbine propellers
propellers
gas
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
FR9310306A
Other languages
English (en)
Other versions
FR2695192A1 (fr
Inventor
Nikolaos Zarzalis
Franz Joos
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.)
MTU Aero Engines GmbH
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2695192A1 publication Critical patent/FR2695192A1/fr
Application granted granted Critical
Publication of FR2695192B1 publication Critical patent/FR2695192B1/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
    • F23R3/26—Controlling the air flow
    • 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
    • F23C7/006—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes adjustable
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/40—Movement of component
    • F05B2250/41—Movement of component with one degree of freedom

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR9310306A 1992-08-29 1993-08-27 Bruleur pour propulseurs a turbines a gaz. Expired - Fee Related FR2695192B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4228817A DE4228817C2 (de) 1992-08-29 1992-08-29 Brennkammer für Gasturbinentriebwerke

Publications (2)

Publication Number Publication Date
FR2695192A1 FR2695192A1 (fr) 1994-03-04
FR2695192B1 true FR2695192B1 (fr) 1996-03-22

Family

ID=6466743

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9310306A Expired - Fee Related FR2695192B1 (fr) 1992-08-29 1993-08-27 Bruleur pour propulseurs a turbines a gaz.

Country Status (4)

Country Link
US (1) US5357743A (fr)
DE (1) DE4228817C2 (fr)
FR (1) FR2695192B1 (fr)
GB (1) GB2270973B (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4110507C2 (de) * 1991-03-30 1994-04-07 Mtu Muenchen Gmbh Brenner für Gasturbinentriebwerke mit mindestens einer für die Zufuhr von Verbrennungsluft lastabhängig regulierbaren Dralleinrichtung
DE4444961A1 (de) * 1994-12-16 1996-06-20 Mtu Muenchen Gmbh Einrichtung zur Kühlung insbesondere der Rückwand des Flammrohrs einer Brennkammer für Gasturbinentriebwerke
GB2334087A (en) * 1998-02-03 1999-08-11 Combustion Technology Internat Combustor restrictor
US6272842B1 (en) * 1999-02-16 2001-08-14 General Electric Company Combustor tuning
US6467272B1 (en) * 2001-06-25 2002-10-22 Power Systems Mfg, Llc Means for wear reduction in a gas turbine combustor
DE10164217B4 (de) * 2001-12-31 2004-08-05 Jochen Schanze Brenner für eine Gebäudeheizanlage
US7624576B2 (en) * 2005-07-18 2009-12-01 Pratt & Whitney Canada Corporation Low smoke and emissions fuel nozzle
FR2903170B1 (fr) * 2006-06-29 2011-12-23 Snecma Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
US8196410B2 (en) * 2007-05-18 2012-06-12 Pratt & Whitney Canada Corp. Stress reduction feature to improve fuel nozzle sheath durability
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
DE102014105166B3 (de) * 2014-03-12 2015-08-06 Max Weishaupt Gmbh Drallerzeuger für einen Brenner sowie damit versehene Mischeinrichtung und damit versehener Brenner
FR3116592B1 (fr) * 2020-11-26 2023-06-16 Safran Aircraft Engines Vrille pour dispositif d’injection étagé de turbomachine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2655787A (en) * 1949-11-21 1953-10-20 United Aircraft Corp Gas turbine combustion chamber with variable area primary air inlet
GB826961A (en) * 1956-03-09 1960-01-27 Lucas Industries Ltd Liquid fuel combustion apparatus
DE1039785B (de) * 1957-10-12 1958-09-25 Maschf Augsburg Nuernberg Ag Brennkammer mit hoher Waermebelastung, insbesondere fuer Verbrennung heizwertarmer, gasfoermiger Brennstoffe in Gasturbinenanlagen
CH417224A (de) * 1962-07-24 1966-07-15 Prvni Brnenska Strojirna Einrichtung zur Regelung der Menge der Primärluft bei Brennkammern von Gasturbinen
US3946552A (en) * 1973-09-10 1976-03-30 General Electric Company Fuel injection apparatus
US3853273A (en) * 1973-10-01 1974-12-10 Gen Electric Axial swirler central injection carburetor
US3886728A (en) * 1974-05-01 1975-06-03 Gen Motors Corp Combustor prechamber
US3893296A (en) * 1974-07-01 1975-07-08 Gen Motors Corp Combustion liner
BE819565A (nl) * 1974-08-23 1975-03-05 Werkwijze en inrichting voor het verzamelen van op een vloeistofoppervlak drijvende lichte stof
US4044553A (en) * 1976-08-16 1977-08-30 General Motors Corporation Variable geometry swirler
DE3048461A1 (de) * 1980-12-22 1982-07-22 Central'nyj naučno-issledovatel'skij dizel'nyj institut CNIDI, Leningrad Einrichtung zur regelung des primaerluftverbrauchs fuer brennkammern
US4447010A (en) * 1982-02-26 1984-05-08 Chugai Ro Co., Ltd. Proportional regulation oil burner of low pressure air type
US4542622A (en) * 1982-07-22 1985-09-24 United Technologies Corporation Variable area inlet guide vanes
FR2572463B1 (fr) * 1984-10-30 1989-01-20 Snecma Systeme d'injection a geometrie variable.
FR2596102B1 (fr) * 1986-03-20 1988-05-27 Snecma Dispositif d'injection a vrille axialo-centripete
FR2601115B1 (fr) * 1986-07-03 1988-09-02 Snecma Chambre de combustion annulaire comportant un moyen de commande unique des diaphragmes d'injecteurs
US5197290A (en) * 1990-03-26 1993-03-30 Fuel Systems Textron Inc. Variable area combustor air swirler
DE4110507C2 (de) * 1991-03-30 1994-04-07 Mtu Muenchen Gmbh Brenner für Gasturbinentriebwerke mit mindestens einer für die Zufuhr von Verbrennungsluft lastabhängig regulierbaren Dralleinrichtung

Also Published As

Publication number Publication date
GB2270973B (en) 1995-11-01
DE4228817C2 (de) 1998-07-30
FR2695192A1 (fr) 1994-03-04
DE4228817A1 (de) 1994-03-03
US5357743A (en) 1994-10-25
GB9317835D0 (en) 1993-10-13
GB2270973A (en) 1994-03-30

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20080430