FR2632014B1 - Injecteur de carburant pour moteur a turbine a gaz - Google Patents

Injecteur de carburant pour moteur a turbine a gaz

Info

Publication number
FR2632014B1
FR2632014B1 FR8906658A FR8906658A FR2632014B1 FR 2632014 B1 FR2632014 B1 FR 2632014B1 FR 8906658 A FR8906658 A FR 8906658A FR 8906658 A FR8906658 A FR 8906658A FR 2632014 B1 FR2632014 B1 FR 2632014B1
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
fuel injector
injector
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
FR8906658A
Other languages
English (en)
Other versions
FR2632014A1 (fr
Inventor
Bryan Leslie Belcher
David William Wrightham
Kenneth George Page
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of FR2632014A1 publication Critical patent/FR2632014A1/fr
Application granted granted Critical
Publication of FR2632014B1 publication Critical patent/FR2632014B1/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
    • F23D—BURNERS
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • 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
    • F23D11/10—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour
    • F23D11/12—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space the spraying being induced by a gaseous medium, e.g. water vapour characterised by the shape or arrangement of the outlets from the nozzle
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
    • F23L7/002—Supplying water
    • F23L7/005—Evaporated water; Steam

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Spray-Type Burners (AREA)
FR8906658A 1988-05-27 1989-05-22 Injecteur de carburant pour moteur a turbine a gaz Expired - Fee Related FR2632014B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8812589A GB2219070B (en) 1988-05-27 1988-05-27 Fuel injector

Publications (2)

Publication Number Publication Date
FR2632014A1 FR2632014A1 (fr) 1989-12-01
FR2632014B1 true FR2632014B1 (fr) 1994-05-27

Family

ID=10637642

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8906658A Expired - Fee Related FR2632014B1 (fr) 1988-05-27 1989-05-22 Injecteur de carburant pour moteur a turbine a gaz

Country Status (5)

Country Link
US (1) US4948055A (fr)
JP (1) JPH02146228A (fr)
DE (1) DE3916413A1 (fr)
FR (1) FR2632014B1 (fr)
GB (1) GB2219070B (fr)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2231651B (en) * 1989-05-18 1991-10-16 Rolls Royce Plc Injector
GB9025778D0 (en) * 1990-11-27 1991-01-09 Rolls Royce Plc Improvements in or relating to gas generators
DE4206665A1 (de) * 1992-03-03 1993-09-16 Edgar Rathsburg Modifiziertes thermisches turbinen-strahltriebwerk mit zusaetzlichem wasserdampfbetrieb
US5218824A (en) * 1992-06-25 1993-06-15 Solar Turbines Incorporated Low emission combustion nozzle for use with a gas turbine engine
US5309709A (en) * 1992-06-25 1994-05-10 Solar Turbines Incorporated Low emission combustion system for a gas turbine engine
IT1263683B (it) * 1992-08-21 1996-08-27 Westinghouse Electric Corp Complesso di ugello per combustibile per una turbina a gas
DE4301887A1 (de) * 1993-01-14 1994-07-21 Struck Wilfried Gas- Dampf- Verfahren
US5404711A (en) * 1993-06-10 1995-04-11 Solar Turbines Incorporated Dual fuel injector nozzle for use with a gas turbine engine
US5423173A (en) * 1993-07-29 1995-06-13 United Technologies Corporation Fuel injector and method of operating the fuel injector
DE4339094A1 (de) * 1993-11-16 1995-05-18 Abb Management Ag Verfahren zur Dämpfung von thermoakustischen Schwingungen sowie Vorrichtung zur Durchführung des Verfahrens
US5564269A (en) * 1994-04-08 1996-10-15 Westinghouse Electric Corporation Steam injected gas turbine system with topping steam turbine
DE4422532A1 (de) * 1994-06-28 1996-01-04 Abb Management Ag Brennstoffdüse
DE4424599A1 (de) * 1994-07-13 1996-01-18 Abb Research Ltd Verfahren und Vorrichtung zum Betreiben eines kombinierten Brenners für flüssige und gasförmige Brennstoffe
US5617716A (en) * 1994-09-16 1997-04-08 Electric Power Research Institute Method for supplying vaporized fuel oil to a gas turbine combustor and system for same
US6170264B1 (en) 1997-09-22 2001-01-09 Clean Energy Systems, Inc. Hydrocarbon combustion power generation system with CO2 sequestration
US6367239B1 (en) * 1998-12-09 2002-04-09 General Electric Company Fuel delivery systems and method
US6247316B1 (en) 2000-03-22 2001-06-19 Clean Energy Systems, Inc. Clean air engines for transportation and other power applications
US6983605B1 (en) * 2000-04-07 2006-01-10 General Electric Company Methods and apparatus for reducing gas turbine engine emissions
US6637183B2 (en) 2000-05-12 2003-10-28 Clean Energy Systems, Inc. Semi-closed brayton cycle gas turbine power systems
JP4635324B2 (ja) * 2000-10-25 2011-02-23 株式会社Ｉｈｉ 二流体サイクル用の低ＮＯｘ燃焼器とその運転方法
US6530222B2 (en) * 2001-07-13 2003-03-11 Pratt & Whitney Canada Corp. Swirled diffusion dump combustor
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
US6983603B2 (en) 2002-10-24 2006-01-10 Pratt & Whitney Canada Corp. Detection of gas turbine engine hot section condition
US20050241311A1 (en) 2004-04-16 2005-11-03 Pronske Keith L Zero emissions closed rankine cycle power system
US20100089020A1 (en) * 2008-10-14 2010-04-15 General Electric Company Metering of diluent flow in combustor
US8567199B2 (en) * 2008-10-14 2013-10-29 General Electric Company Method and apparatus of introducing diluent flow into a combustor
US20100089022A1 (en) * 2008-10-14 2010-04-15 General Electric Company Method and apparatus of fuel nozzle diluent introduction
US9121609B2 (en) * 2008-10-14 2015-09-01 General Electric Company Method and apparatus for introducing diluent flow into a combustor
JP6037858B2 (ja) * 2013-01-30 2016-12-07 三菱日立パワーシステムズ株式会社 燃焼器
US10731861B2 (en) 2013-11-18 2020-08-04 Raytheon Technologies Corporation Dual fuel nozzle with concentric fuel passages for a gas turbine engine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3309866A (en) * 1965-03-11 1967-03-21 Gen Electric Combustion process and apparatus
US3785146A (en) * 1972-05-01 1974-01-15 Gen Electric Self compensating flow divider for a gas turbine steam injection system
US4041699A (en) * 1975-12-29 1977-08-16 The Garrett Corporation High temperature gas turbine
GB2035540B (en) * 1978-11-23 1983-02-09 Rolls Royce Gas turbine engine fuel injector
US4327547A (en) * 1978-11-23 1982-05-04 Rolls-Royce Limited Fuel injectors
GB2050592B (en) * 1979-06-06 1983-03-16 Rolls Royce Gas turbine
GB2055186B (en) * 1979-08-01 1983-05-25 Rolls Royce Gas turbine engine dual fuel injector
EP0193838B1 (fr) * 1985-03-04 1989-05-03 Siemens Aktiengesellschaft Disposition de brûleur pour installations de combustion, en particulier pour chambres de combustion d'installations de turbines à gaz ainsi que procédé de sa mise en oeuvre

Also Published As

Publication number Publication date
DE3916413A1 (de) 1989-11-30
GB8812589D0 (en) 1988-06-29
GB2219070A (en) 1989-11-29
JPH02146228A (ja) 1990-06-05
US4948055A (en) 1990-08-14
GB2219070B (en) 1992-03-25
FR2632014A1 (fr) 1989-12-01

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Legal Events

Date Code Title Description
ST Notification of lapse