DE3764383D1 - Brennstoffeinspritzeinrichtung mit axial-centripetaler luftzufuehrung. - Google Patents

Brennstoffeinspritzeinrichtung mit axial-centripetaler luftzufuehrung.

Info

Publication number
DE3764383D1
DE3764383D1 DE8787400532T DE3764383T DE3764383D1 DE 3764383 D1 DE3764383 D1 DE 3764383D1 DE 8787400532 T DE8787400532 T DE 8787400532T DE 3764383 T DE3764383 T DE 3764383T DE 3764383 D1 DE3764383 D1 DE 3764383D1
Authority
DE
Germany
Prior art keywords
axial
fuel injection
air supply
injection device
centripetal air
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
DE8787400532T
Other languages
English (en)
Inventor
Gerard Yves Georges Barbier
Gerard Joseph P Bayle-Labourne
Michel Andre Albert Desaulty
Rodolphe Martinez
Jerome Perigne
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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE3764383D1 publication Critical patent/DE3764383D1/de
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
    • 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
    • F23C7/008—Flow control devices
    • 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
    • F23R3/02—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
    • 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
    • F05B2200/00—Mathematical features
    • F05B2200/30—Mathematical features miscellaneous
    • F05B2200/32—Mathematical features miscellaneous even
    • 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
    • F05B2250/411—Movement of component with one degree of freedom in rotation
    • 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
DE8787400532T 1986-03-20 1987-03-11 Brennstoffeinspritzeinrichtung mit axial-centripetaler luftzufuehrung. Expired - Lifetime DE3764383D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8603971A FR2596102B1 (fr) 1986-03-20 1986-03-20 Dispositif d'injection a vrille axialo-centripete

Publications (1)

Publication Number Publication Date
DE3764383D1 true DE3764383D1 (de) 1990-09-27

Family

ID=9333328

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8787400532T Expired - Lifetime DE3764383D1 (de) 1986-03-20 1987-03-11 Brennstoffeinspritzeinrichtung mit axial-centripetaler luftzufuehrung.

Country Status (5)

Country Link
US (1) US4754600A (de)
EP (1) EP0239462B1 (de)
JP (1) JPS62228630A (de)
DE (1) DE3764383D1 (de)
FR (1) FR2596102B1 (de)

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FR2601115B1 (fr) * 1986-07-03 1988-09-02 Snecma Chambre de combustion annulaire comportant un moyen de commande unique des diaphragmes d'injecteurs
FR2639095B1 (fr) * 1988-11-17 1990-12-21 Snecma Chambre de combustion de turbomachine a bols de prevaporisation montes flottants
FR2661714B1 (fr) * 1990-05-03 1994-06-17 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz.
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
FR2676529B1 (fr) * 1991-05-16 1994-11-25 Snecma Dispositif d'alimentation en comburant d'une turbine a gaz comprenant des diaphragmes de reglage du debit.
US5253478A (en) * 1991-12-30 1993-10-19 General Electric Company Flame holding diverging centerbody cup construction for a dry low NOx combustor
DE4220060C2 (de) * 1992-06-19 1996-10-17 Mtu Muenchen Gmbh Einrichtung zur Betätigung einer den Durchsatz von Verbrennungsluft steuernden Dralleinrichtung eines Brenners für Gasturbinentriebwerke
DE4228817C2 (de) * 1992-08-29 1998-07-30 Mtu Muenchen Gmbh Brennkammer für Gasturbinentriebwerke
DE4228816C2 (de) * 1992-08-29 1998-08-06 Mtu Muenchen Gmbh Brenner für Gasturbinentriebwerke
FR2704305B1 (fr) * 1993-04-21 1995-06-02 Snecma Chambre de combustion comportant un système d'injection à géométrie variable.
US5431019A (en) * 1993-04-22 1995-07-11 Alliedsignal Inc. Combustor for gas turbine engine
US5404711A (en) * 1993-06-10 1995-04-11 Solar Turbines Incorporated Dual fuel injector nozzle for use with a gas turbine engine
DE4339724C1 (de) * 1993-11-22 1995-01-19 Siemens Ag Gasarmatur
US5623827A (en) * 1995-01-26 1997-04-29 General Electric Company Regenerative cooled dome assembly for a gas turbine engine combustor
DE19527269C5 (de) * 1995-07-26 2006-07-27 J. Eberspächer GmbH & Co. KG Ansaugstutzen für die Verbrennungsluft eines Heizgerätes
FR2751731B1 (fr) * 1996-07-25 1998-09-04 Snecma Ensemble bol-deflecteur pour chambre de combustion de turbomachine
FR2752917B1 (fr) * 1996-09-05 1998-10-02 Snecma Systeme d'injection a degre d'homogeneisation avancee
US5899076A (en) * 1996-12-20 1999-05-04 United Technologies Corporation Flame disgorging two stream tangential entry nozzle
US6871501B2 (en) * 2002-12-03 2005-03-29 General Electric Company Method and apparatus to decrease gas turbine engine combustor emissions
US6871488B2 (en) * 2002-12-17 2005-03-29 Pratt & Whitney Canada Corp. Natural gas fuel nozzle for gas turbine engine
US7695275B2 (en) * 2004-06-02 2010-04-13 Fuel Management, Inc. Air:fluid distribution system and method
US7565803B2 (en) * 2005-07-25 2009-07-28 General Electric Company Swirler arrangement for mixer assembly of a gas turbine engine combustor having shaped passages
KR100820233B1 (ko) * 2006-10-31 2008-04-08 한국전력공사 연소기 및 이를 포함하는 멀티 연소기, 그리고 연소방법
US8037689B2 (en) * 2007-08-21 2011-10-18 General Electric Company Turbine fuel delivery apparatus and system
FR2925146B1 (fr) * 2007-12-14 2009-12-25 Snecma Systeme d'injection d'un melange d'air et de carburant dans une chambre de combustion de turbomachine
GB0815761D0 (en) * 2008-09-01 2008-10-08 Rolls Royce Plc Swirler for a fuel injector
DE102009032277A1 (de) * 2009-07-08 2011-01-20 Rolls-Royce Deutschland Ltd & Co Kg Brennkammerkopf einer Gasturbine
US8375548B2 (en) * 2009-10-07 2013-02-19 Pratt & Whitney Canada Corp. Fuel nozzle and method of repair
FR2951245B1 (fr) * 2009-10-13 2013-05-17 Snecma Dispositif d'injection multi-point pour une chambre de combustion de turbomachine
FR2951246B1 (fr) * 2009-10-13 2011-11-11 Snecma Injecteur multi-point pour une chambre de combustion de turbomachine
FR2952166B1 (fr) * 2009-11-05 2012-01-06 Snecma Dispositif melangeur de carburant pour chambre de combustion de turbomachine comprenant des moyens ameliores d'alimentation en air
US20120180486A1 (en) * 2011-01-18 2012-07-19 General Electric Company Gas turbine fuel system for low dynamics
US9764294B2 (en) * 2012-05-21 2017-09-19 Pratt & Whitney Rocketdyne, Inc. Liquid-gas mixer and turbulator therefor
US9395084B2 (en) * 2012-06-06 2016-07-19 General Electric Company Fuel pre-mixer with planar and swirler vanes
US9447974B2 (en) 2012-09-13 2016-09-20 United Technologies Corporation Light weight swirler for gas turbine engine combustor and a method for lightening a swirler for a gas turbine engine
CN105899878B (zh) * 2013-06-18 2018-11-13 伍德沃德有限公司 燃气涡轮燃烧室组件及发动机及相关联的操作方法
JP6191918B2 (ja) * 2014-03-20 2017-09-06 三菱日立パワーシステムズ株式会社 ノズル、バーナ、燃焼器、ガスタービン、ガスタービンシステム
ITUA20163988A1 (it) 2016-05-31 2017-12-01 Nuovo Pignone Tecnologie Srl Ugello carburante per una turbina a gas con swirler radiale e swirler assiale e turbina a gas / fuel nozzle for a gas turbine with radial swirler and axial swirler and gas turbine

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DE386159C (de) * 1923-12-04 Stettin Act Ges Luftzufuehrung bei OElfeuerungen
BE489359A (de) * 1944-10-05
GB644719A (en) * 1947-05-14 1950-10-18 Bataafsche Petroleum Method of and apparatus for temporarily increasing the output of propulsive gases from a combustion chamber
GB663639A (en) * 1948-09-24 1951-12-27 Peabody Engineering Corp Improvements in gas heaters and other heat exchangers
GB672530A (en) * 1950-08-16 1952-05-21 Shell Refining & Marketing Co Improvements in gas turbine combustion chambers
CH323713A (fr) * 1950-08-16 1957-08-15 Shell Refining & Marketing Co Ensemble comprenant une chambre de combustion pour turbine à gaz et un dispositif de guidage d'air de combustion
DE1039785B (de) * 1957-10-12 1958-09-25 Maschf Augsburg Nuernberg Ag Brennkammer mit hoher Waermebelastung, insbesondere fuer Verbrennung heizwertarmer, gasfoermiger Brennstoffe in Gasturbinenanlagen
US3490230A (en) * 1968-03-22 1970-01-20 Us Navy Combustion air control shutter
GB1421399A (en) * 1972-11-13 1976-01-14 Snecma Fuel injectors
FR2206796A5 (de) * 1972-11-13 1974-06-07 Snecma
US3853273A (en) * 1973-10-01 1974-12-10 Gen Electric Axial swirler central injection carburetor
DE2416909A1 (de) * 1974-04-06 1975-10-16 Daimler Benz Ag Betriebsverfahren fuer eine gasturbinenanlage zur abgasverbesserung und entsprechende gasturbinenanlage
FR2270448A1 (en) * 1974-05-10 1975-12-05 Bennes Marrel Gas turbine combustion chamber - has spring loaded bellows controlling annular air flow control membrane
US4563875A (en) * 1974-07-24 1986-01-14 Howald Werner E Combustion apparatus including an air-fuel premixing chamber
US3958413A (en) * 1974-09-03 1976-05-25 General Motors Corporation Combustion method and apparatus
DE2511172A1 (de) * 1975-03-14 1976-09-30 Daimler Benz Ag Filmverdampfungs-brennkammer
DE2522393C2 (de) * 1975-05-21 1984-01-12 Richard Heinze Kunststoff-Spritzgießwerke GmbH & Co, 4900 Herford In einer Aufnahmebohrung verankerbares Beschlagteil
FR2357738A1 (fr) * 1976-07-07 1978-02-03 Snecma Chambre de combustion pour turbomachines
FR2391359A2 (fr) * 1977-05-18 1978-12-15 Snecma Chambre de combustion pour turbomachines
GB1539136A (en) * 1976-07-07 1979-01-24 Snecma Gas turbine combustion chambers
GB1572336A (en) * 1978-05-30 1980-07-30 Lucas Industries Ltd Combustion equipment
US4385490A (en) * 1978-08-14 1983-05-31 Phillips Petroleum Company Combustors and methods of operating same
JPS5535885A (en) * 1978-09-06 1980-03-13 Kobe Steel Ltd Combustion method capable of minimizing production of nitrogen oxide and smoke
US4263780A (en) * 1979-09-28 1981-04-28 General Motors Corporation Lean prechamber outflow combustor with sets of primary air entrances
GB2085146B (en) * 1980-10-01 1985-06-12 Gen Electric Flow modifying device
GB2085147A (en) * 1980-10-01 1982-04-21 Gen Electric Flow modifying device
GB2099978A (en) * 1981-05-11 1982-12-15 Rolls Royce Gas turbine engine combustor
FR2522393B1 (fr) * 1982-02-26 1990-02-02 Chugai Ro Kogyo Kaisha Ltd Bruleur de combustible liquide a reglage par action proportionnelle
GB2134243A (en) * 1983-01-27 1984-08-08 Rolls Royce Combustion equipment for a gas turbine engine
FR2572463B1 (fr) * 1984-10-30 1989-01-20 Snecma Systeme d'injection a geometrie variable.

Also Published As

Publication number Publication date
FR2596102B1 (fr) 1988-05-27
JPS62228630A (ja) 1987-10-07
FR2596102A1 (fr) 1987-09-25
EP0239462A1 (de) 1987-09-30
JPH0476022B2 (de) 1992-12-02
EP0239462B1 (de) 1990-08-22
US4754600A (en) 1988-07-05

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee