FR2586453B1 - Carburateur pour moteur a turbine a gaz - Google Patents

Carburateur pour moteur a turbine a gaz

Info

Publication number
FR2586453B1
FR2586453B1 FR8612018A FR8612018A FR2586453B1 FR 2586453 B1 FR2586453 B1 FR 2586453B1 FR 8612018 A FR8612018 A FR 8612018A FR 8612018 A FR8612018 A FR 8612018A FR 2586453 B1 FR2586453 B1 FR 2586453B1
Authority
FR
France
Prior art keywords
carburetor
gas turbine
turbine engine
engine
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 - Lifetime
Application number
FR8612018A
Other languages
English (en)
Other versions
FR2586453A1 (fr
Inventor
John William Vinson
Pamela Chi-Ping Kwong
Paul Edward Sabla
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
Publication of FR2586453A1 publication Critical patent/FR2586453A1/fr
Application granted granted Critical
Publication of FR2586453B1 publication Critical patent/FR2586453B1/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
    • F23R3/28—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
    • 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
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • F23D14/22—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other
    • F23D14/24—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone with separate air and gas feed ducts, e.g. with ducts running parallel or crossing each other 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
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
    • 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
    • Y02T50/678—Aviation using fuels of non-fossil origin

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
FR8612018A 1985-08-23 1986-08-25 Carburateur pour moteur a turbine a gaz Expired - Lifetime FR2586453B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/768,600 US4653278A (en) 1985-08-23 1985-08-23 Gas turbine engine carburetor

Publications (2)

Publication Number Publication Date
FR2586453A1 FR2586453A1 (fr) 1987-02-27
FR2586453B1 true FR2586453B1 (fr) 1992-11-06

Family

ID=25082953

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8612018A Expired - Lifetime FR2586453B1 (fr) 1985-08-23 1986-08-25 Carburateur pour moteur a turbine a gaz

Country Status (8)

Country Link
US (1) US4653278A (fr)
JP (1) JPS6270629A (fr)
CA (1) CA1250439A (fr)
CH (1) CH682002A5 (fr)
DE (1) DE3626545A1 (fr)
FR (1) FR2586453B1 (fr)
GB (2) GB2179435B (fr)
IT (1) IT1197110B (fr)

Families Citing this family (115)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2150277B (en) * 1983-11-26 1987-01-28 Rolls Royce Combustion apparatus for a gas turbine engine
FR2602271B1 (fr) * 1986-07-30 1990-07-27 Snecma Dispositif d'injection, pour turbomachines, a vrille de turbulence a calage variable
US4955201A (en) * 1987-12-14 1990-09-11 Sundstrand Corporation Fuel injectors for turbine engines
US5040371A (en) * 1988-12-12 1991-08-20 Sundstrand Corporation Fuel injectors for use with combustors
US5167116A (en) * 1989-07-07 1992-12-01 Fuel Systems Textron Inc. Small airblast fuel nozzle with high efficiency inner air swirler
US5144804A (en) * 1989-07-07 1992-09-08 Fuel Systems Textron Inc. Small airblast fuel nozzle with high efficiency inner air swirler
US5097657A (en) * 1989-12-07 1992-03-24 Sundstrand Corporation Method of fabricating a fuel injector
FR2665729B1 (fr) * 1990-08-08 1994-09-23 Snecma Dispositif d'injection de carburant pour une chambre de combustion de turbomachine.
US5117624A (en) * 1990-09-17 1992-06-02 General Electric Company Fuel injector nozzle support
US5165241A (en) * 1991-02-22 1992-11-24 General Electric Company Air fuel mixer for gas turbine combustor
FR2673705A1 (fr) * 1991-03-06 1992-09-11 Snecma Chambre de combustion de turbomachine munie d'un dispositif anti-cokefaction du fond de ladite chambre.
US5239832A (en) * 1991-12-26 1993-08-31 General Electric Company Birdstrike resistant swirler support for combustion chamber dome
US5307634A (en) * 1992-02-26 1994-05-03 United Technologies Corporation Premix gas nozzle
US5274995A (en) * 1992-04-27 1994-01-04 General Electric Company Apparatus and method for atomizing water in a combustor dome assembly
US5256352A (en) * 1992-09-02 1993-10-26 United Technologies Corporation Air-liquid mixer
US5251447A (en) * 1992-10-01 1993-10-12 General Electric Company Air fuel mixer for gas turbine combustor
US5394688A (en) * 1993-10-27 1995-03-07 Westinghouse Electric Corporation Gas turbine combustor swirl vane arrangement
US5444982A (en) * 1994-01-12 1995-08-29 General Electric Company Cyclonic prechamber with a centerbody
US5461865A (en) * 1994-02-24 1995-10-31 United Technologies Corporation Tangential entry fuel nozzle
DE19549140A1 (de) * 1995-12-29 1997-07-03 Asea Brown Boveri Verfahren zum Betrieb einer Gasturbogruppe mit niederkalorischem Brennstoff
FR2751054B1 (fr) * 1996-07-11 1998-09-18 Snecma Chambre de combustion anti-nox a injection de carburant de type annulaire
FR2753779B1 (fr) * 1996-09-26 1998-10-16 Systeme d'injection aerodynamique d'un melange air carburant
US5966937A (en) * 1997-10-09 1999-10-19 United Technologies Corporation Radial inlet swirler with twisted vanes for fuel injector
US6550251B1 (en) 1997-12-18 2003-04-22 General Electric Company Venturiless swirl cup
US6547163B1 (en) 1999-10-01 2003-04-15 Parker-Hannifin Corporation Hybrid atomizing fuel nozzle
US6374615B1 (en) 2000-01-28 2002-04-23 Alliedsignal, Inc Low cost, low emissions natural gas combustor
DE10205573B4 (de) * 2002-02-11 2005-10-06 J. Eberspächer GmbH & Co. KG Zerstäuberdüse für einen Brenner
DE10207311B4 (de) * 2002-02-21 2005-06-09 J. Eberspächer GmbH & Co. KG Zerstäuberdüse für einen Brenner, insbesondere für ein an einem Fahrzeug einsetzbares Heizgerät
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
US8015821B2 (en) * 2008-01-11 2011-09-13 Spytek Aerospace Corporation Apparatus and method for a gas turbine entrainment system
MY153097A (en) * 2008-03-28 2014-12-31 Exxonmobil Upstream Res Co Low emission power generation and hydrocarbon recovery systems and methods
AU2009228283B2 (en) 2008-03-28 2015-02-05 Exxonmobil Upstream Research Company Low emission power generation and hydrocarbon recovery systems and methods
US8056343B2 (en) * 2008-10-01 2011-11-15 General Electric Company Off center combustor liner
US8215116B2 (en) * 2008-10-02 2012-07-10 General Electric Company System and method for air-fuel mixing in gas turbines
AU2009303735B2 (en) 2008-10-14 2014-06-26 Exxonmobil Upstream Research Company Methods and systems for controlling the products of combustion
US20100170253A1 (en) * 2009-01-07 2010-07-08 General Electric Company Method and apparatus for fuel injection in a turbine engine
US20110072823A1 (en) * 2009-09-30 2011-03-31 Daih-Yeou Chen Gas turbine engine fuel injector
US20110107767A1 (en) * 2009-11-06 2011-05-12 General Electric Company Secondary fuel nozzle venturi
CN102597418A (zh) 2009-11-12 2012-07-18 埃克森美孚上游研究公司 低排放发电和烃采收***及方法
US8850819B2 (en) * 2010-06-25 2014-10-07 United Technologies Corporation Swirler, fuel and air assembly and combustor
JP5759543B2 (ja) 2010-07-02 2015-08-05 エクソンモービル アップストリーム リサーチ カンパニー 排ガス再循環方式及び直接接触型冷却器による化学量論的燃焼
CN102971508B (zh) 2010-07-02 2016-06-01 埃克森美孚上游研究公司 Co2分离***和分离co2的方法
SG10201505280WA (en) 2010-07-02 2015-08-28 Exxonmobil Upstream Res Co Stoichiometric combustion of enriched air with exhaust gas recirculation
AU2011271633B2 (en) 2010-07-02 2015-06-11 Exxonmobil Upstream Research Company Low emission triple-cycle power generation systems and methods
TWI564474B (zh) 2011-03-22 2017-01-01 艾克頌美孚上游研究公司 於渦輪系統中控制化學計量燃燒的整合系統和使用彼之產生動力的方法
TWI563165B (en) 2011-03-22 2016-12-21 Exxonmobil Upstream Res Co Power generation system and method for generating power
TWI593872B (zh) 2011-03-22 2017-08-01 艾克頌美孚上游研究公司 整合系統及產生動力之方法
TWI563166B (en) 2011-03-22 2016-12-21 Exxonmobil Upstream Res Co Integrated generation systems and methods for generating power
TWI435978B (zh) * 2011-10-31 2014-05-01 Atomic Energy Council 富氫氣體燃燒器
US9188063B2 (en) 2011-11-03 2015-11-17 Delavan Inc. Injectors for multipoint injection
CN104428490B (zh) 2011-12-20 2018-06-05 埃克森美孚上游研究公司 提高的煤层甲烷生产
US9423137B2 (en) * 2011-12-29 2016-08-23 Rolls-Royce Corporation Fuel injector with first and second converging fuel-air passages
US9353682B2 (en) 2012-04-12 2016-05-31 General Electric Company Methods, systems and apparatus relating to combustion turbine power plants with exhaust gas recirculation
US10273880B2 (en) 2012-04-26 2019-04-30 General Electric Company System and method of recirculating exhaust gas for use in a plurality of flow paths in a gas turbine engine
US9784185B2 (en) 2012-04-26 2017-10-10 General Electric Company System and method for cooling a gas turbine with an exhaust gas provided by the gas turbine
US10107495B2 (en) 2012-11-02 2018-10-23 General Electric Company Gas turbine combustor control system for stoichiometric combustion in the presence of a diluent
US9869279B2 (en) 2012-11-02 2018-01-16 General Electric Company System and method for a multi-wall turbine combustor
US9708977B2 (en) 2012-12-28 2017-07-18 General Electric Company System and method for reheat in gas turbine with exhaust gas recirculation
US9631815B2 (en) 2012-12-28 2017-04-25 General Electric Company System and method for a turbine combustor
US9611756B2 (en) 2012-11-02 2017-04-04 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
US10215412B2 (en) 2012-11-02 2019-02-26 General Electric Company System and method for load control with diffusion combustion in a stoichiometric exhaust gas recirculation gas turbine system
US9803865B2 (en) 2012-12-28 2017-10-31 General Electric Company System and method for a turbine combustor
US9599070B2 (en) 2012-11-02 2017-03-21 General Electric Company System and method for oxidant compression in a stoichiometric exhaust gas recirculation gas turbine system
US10161312B2 (en) 2012-11-02 2018-12-25 General Electric Company System and method for diffusion combustion with fuel-diluent mixing in a stoichiometric exhaust gas recirculation gas turbine system
US9574496B2 (en) 2012-12-28 2017-02-21 General Electric Company System and method for a turbine combustor
US10208677B2 (en) 2012-12-31 2019-02-19 General Electric Company Gas turbine load control system
US9581081B2 (en) 2013-01-13 2017-02-28 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
US9512759B2 (en) 2013-02-06 2016-12-06 General Electric Company System and method for catalyst heat utilization for gas turbine with exhaust gas recirculation
US9938861B2 (en) 2013-02-21 2018-04-10 Exxonmobil Upstream Research Company Fuel combusting method
TW201502356A (zh) 2013-02-21 2015-01-16 Exxonmobil Upstream Res Co 氣渦輪機排氣中氧之減少
US10221762B2 (en) 2013-02-28 2019-03-05 General Electric Company System and method for a turbine combustor
TW201500635A (zh) 2013-03-08 2015-01-01 Exxonmobil Upstream Res Co 處理廢氣以供用於提高油回收
US9784182B2 (en) 2013-03-08 2017-10-10 Exxonmobil Upstream Research Company Power generation and methane recovery from methane hydrates
US9618261B2 (en) 2013-03-08 2017-04-11 Exxonmobil Upstream Research Company Power generation and LNG production
US20140250945A1 (en) 2013-03-08 2014-09-11 Richard A. Huntington Carbon Dioxide Recovery
US9631542B2 (en) 2013-06-28 2017-04-25 General Electric Company System and method for exhausting combustion gases from gas turbine engines
US9835089B2 (en) 2013-06-28 2017-12-05 General Electric Company System and method for a fuel nozzle
US9617914B2 (en) 2013-06-28 2017-04-11 General Electric Company Systems and methods for monitoring gas turbine systems having exhaust gas recirculation
TWI654368B (zh) 2013-06-28 2019-03-21 美商艾克頌美孚上游研究公司 用於控制在廢氣再循環氣渦輪機系統中的廢氣流之系統、方法與媒體
US9587510B2 (en) 2013-07-30 2017-03-07 General Electric Company System and method for a gas turbine engine sensor
US9903588B2 (en) 2013-07-30 2018-02-27 General Electric Company System and method for barrier in passage of combustor of gas turbine engine with exhaust gas recirculation
US9951658B2 (en) 2013-07-31 2018-04-24 General Electric Company System and method for an oxidant heating system
US10030588B2 (en) 2013-12-04 2018-07-24 General Electric Company Gas turbine combustor diagnostic system and method
US9752458B2 (en) 2013-12-04 2017-09-05 General Electric Company System and method for a gas turbine engine
FR3015638B1 (fr) * 2013-12-23 2019-05-31 Safran Aircraft Engines Segment d'obturation de traversee coulissante de systeme d'injection pour turbomachine
US10227920B2 (en) 2014-01-15 2019-03-12 General Electric Company Gas turbine oxidant separation system
US9915200B2 (en) 2014-01-21 2018-03-13 General Electric Company System and method for controlling the combustion process in a gas turbine operating with exhaust gas recirculation
US9863267B2 (en) 2014-01-21 2018-01-09 General Electric Company System and method of control for a gas turbine engine
US10079564B2 (en) 2014-01-27 2018-09-18 General Electric Company System and method for a stoichiometric exhaust gas recirculation gas turbine system
RU2548525C1 (ru) * 2014-02-12 2015-04-20 Открытое акционерное общество "Газпром" Способ сжигания предварительно подготовленной "бедной" топливовоздушной смеси в двухконтурной малоэмиссионной горелке с применением диффузионного стабилизирующего факела
US10047633B2 (en) 2014-05-16 2018-08-14 General Electric Company Bearing housing
US10060359B2 (en) 2014-06-30 2018-08-28 General Electric Company Method and system for combustion control for gas turbine system with exhaust gas recirculation
US10655542B2 (en) 2014-06-30 2020-05-19 General Electric Company Method and system for startup of gas turbine system drive trains with exhaust gas recirculation
US9885290B2 (en) 2014-06-30 2018-02-06 General Electric Company Erosion suppression system and method in an exhaust gas recirculation gas turbine system
US9851105B2 (en) 2014-07-03 2017-12-26 United Technologies Corporation Self-cooled orifice structure
US9869247B2 (en) 2014-12-31 2018-01-16 General Electric Company Systems and methods of estimating a combustion equivalence ratio in a gas turbine with exhaust gas recirculation
US9819292B2 (en) 2014-12-31 2017-11-14 General Electric Company Systems and methods to respond to grid overfrequency events for a stoichiometric exhaust recirculation gas turbine
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
US10094566B2 (en) 2015-02-04 2018-10-09 General Electric Company Systems and methods for high volumetric oxidant flow in gas turbine engine with exhaust gas recirculation
US10316746B2 (en) 2015-02-04 2019-06-11 General Electric Company Turbine system with exhaust gas recirculation, separation and extraction
US10253690B2 (en) 2015-02-04 2019-04-09 General Electric Company Turbine system with exhaust gas recirculation, separation and extraction
US10267270B2 (en) 2015-02-06 2019-04-23 General Electric Company Systems and methods for carbon black production with a gas turbine engine having exhaust gas recirculation
US10145269B2 (en) 2015-03-04 2018-12-04 General Electric Company System and method for cooling discharge flow
US10480792B2 (en) 2015-03-06 2019-11-19 General Electric Company Fuel staging in a gas turbine engine
US10385809B2 (en) 2015-03-31 2019-08-20 Delavan Inc. Fuel nozzles
US9897321B2 (en) 2015-03-31 2018-02-20 Delavan Inc. Fuel nozzles
US10876477B2 (en) 2016-09-16 2020-12-29 Delavan Inc Nozzles with internal manifolding
KR102119879B1 (ko) * 2018-03-07 2020-06-08 두산중공업 주식회사 파일럿 연료 분사 장치, 이를 구비한 연료 노즐 및 가스 터빈
CN109282307B (zh) * 2018-08-09 2020-04-21 中国航发沈阳发动机研究所 一种用于火焰筒头部的驻涡腔旋流雾化装置
US10895384B2 (en) 2018-11-29 2021-01-19 General Electric Company Premixed fuel nozzle
US11226100B2 (en) * 2019-07-22 2022-01-18 Delavan Inc. Fuel manifolds
US11378275B2 (en) * 2019-12-06 2022-07-05 Raytheon Technologies Corporation High shear swirler with recessed fuel filmer for a gas turbine engine
US11598526B2 (en) * 2021-04-16 2023-03-07 General Electric Company Combustor swirl vane apparatus
US11802693B2 (en) * 2021-04-16 2023-10-31 General Electric Company Combustor swirl vane apparatus

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB562062A (en) * 1942-12-09 1944-06-16 Wellman Smith Owen Eng Co Ltd Improvements in or relating to gas burners and the like
US2618928A (en) * 1944-05-19 1952-11-25 Power Jets Res & Dev Ltd Combustion apparatus with vaned fuel injector means
GB650608A (en) * 1948-11-26 1951-02-28 Lucas Ltd Joseph Improvements relating to internal combustion engine systems
US2625788A (en) * 1948-12-15 1953-01-20 Mcdonnell Aircraft Corp Flame holder and fuel nozzle supporting mechanism for ram jet engines
CH303030A (de) * 1952-08-15 1954-11-15 Bbc Brown Boveri & Cie Gasbrenner, vorzugsweise für Brennkammern von Gasturbinenanlagen.
US2982099A (en) * 1956-10-09 1961-05-02 Rolls Royce Fuel injection arrangement in combustion equipment for gas turbine engines
US2974488A (en) * 1956-11-27 1961-03-14 Snecma Combustion devices for continuous-flow internal combustion machines
US3366373A (en) * 1965-06-21 1968-01-30 Zink Co John Apparatus for adding heat to gas turbine exhaust
GB1165163A (en) * 1966-04-30 1969-09-24 Nat Res Dev Improvements in and relating to Fuel Burning Equipment
US3739576A (en) * 1969-08-11 1973-06-19 United Aircraft Corp Combustion system
JPS4931059Y1 (fr) * 1970-11-30 1974-08-22
GB1337121A (en) * 1970-11-30 1973-11-14 Airoil Burner Fuel burner assemblies
US3851462A (en) * 1973-06-29 1974-12-03 United Aircraft Corp Method for reducing turbine inlet guide vane temperatures
US3853273A (en) * 1973-10-01 1974-12-10 Gen Electric Axial swirler central injection carburetor
CH577627A5 (fr) * 1974-04-03 1976-07-15 Bbc Sulzer Turbomaschinen
US4198815A (en) * 1975-12-24 1980-04-22 General Electric Company Central injection fuel carburetor
DE2641605C2 (de) * 1975-12-24 1986-06-19 General Electric Co., Schenectady, N.Y. Vorrichtung zur Zufuhr von Luft und Brennstoff
US4070826A (en) * 1975-12-24 1978-01-31 General Electric Company Low pressure fuel injection system
DE2710618C2 (de) * 1977-03-11 1982-11-11 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Brennstoffeinspritzdüse für Gasturbinentriebwerke
US4152108A (en) * 1977-07-15 1979-05-01 John Zink Company Steam injection to zone of onset of combustion in fuel burner
US4180974A (en) * 1977-10-31 1980-01-01 General Electric Company Combustor dome sleeve
GB2055187B (en) * 1979-08-01 1983-12-14 Rolls Royce Gaseous fuel injector for a gas turbine engine
US4584834A (en) * 1982-07-06 1986-04-29 General Electric Company Gas turbine engine carburetor

Also Published As

Publication number Publication date
US4653278A (en) 1987-03-31
GB8613546D0 (en) 1986-07-09
IT8621513A1 (it) 1988-02-22
FR2586453A1 (fr) 1987-02-27
DE3626545A1 (de) 1987-02-26
GB8902546D0 (en) 1989-03-22
GB2179435B (en) 1990-02-21
GB2211596B (en) 1990-03-07
CA1250439A (fr) 1989-02-28
GB2211596A (en) 1989-07-05
CH682002A5 (fr) 1993-06-30
IT8621513A0 (it) 1986-08-22
IT1197110B (it) 1988-11-25
GB2179435A (en) 1987-03-04
JPS6270629A (ja) 1987-04-01

Similar Documents

Publication Publication Date Title
FR2586453B1 (fr) Carburateur pour moteur a turbine a gaz
FR2592092B1 (fr) Turbine a aubes refroidies notamment pour moteur a turbine a gaz
FR2617907B1 (fr) Moteur a turbine a gaz
FR2588312B1 (fr) Inverseur de poussee pour moteur a turbine a gaz
DE3665627D1 (en) Combustion liner for a gas turbine engine
FR2557212B1 (fr) Structure de stator pour un moteur a turbine a gaz
FR2575221B1 (fr) Stator refroidissable pour un moteur a turbine a gaz
FR2580725B1 (fr) Module propulsif pour un moteur a turbine a gaz aeronautique
IT1178620B (it) Complesso di combustione per motore a turbina a gas
FR2594886B1 (fr) Module propulsif pour un moteur aeronautique a turbine a gaz
FR2619161B1 (fr) Chassis assemble pour moteur a turbine a gaz
IT1168267B (it) Carburatore per turbomotore a gas
FR2590933B1 (fr) Aube refrigeree pour moteur a turbine a gaz
FR2573130B1 (fr) Joint d'etancheite refroidissable pour un moteur a turbine a gaz.
FR2589427B1 (fr) Module d'helice pour un moteur a turbine a gaz aeronautique
FR2632015B1 (fr) Syste me d'injecteurs pour moteur a turbine a gaz
GB2150277B (en) Combustion apparatus for a gas turbine engine
FR2557202B1 (fr) Turbocompresseur a gaz d'echappement pour moteur a combustion interne
FR2583459B1 (fr) Dispositif de regulation de carburant pour un moteur a turbine a gaz.
FR2586755B1 (fr) Systeme de carburant pour un moteur a turbine a gaz
FR2592438B1 (fr) Compresseur de gaz pour moteur a reaction iet ce moteur
FR2632014B1 (fr) Injecteur de carburant pour moteur a turbine a gaz
FR2624954B1 (fr) Structure de chambre de combustion pour moteur a turbine a gaz
FR2510665B1 (fr) Injecteur mixte de carburant pour moteur a turbine a gaz
FR2527268B1 (fr) Prediffuseur pour un moteur a turbine a gaz