IN170055B - - Google Patents

Info

Publication number
IN170055B
IN170055B IN700/CAL/88A IN700CA1988A IN170055B IN 170055 B IN170055 B IN 170055B IN 700CA1988 A IN700CA1988 A IN 700CA1988A IN 170055 B IN170055 B IN 170055B
Authority
IN
India
Application number
IN700/CAL/88A
Other languages
English (en)
Inventor
John William Vinson
Stephen John Howell
Elias Harry Lampes
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IN170055B publication Critical patent/IN170055B/en

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
    • 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
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • 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

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)
IN700/CAL/88A 1988-01-14 1988-08-22 IN170055B (el)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/143,792 US4854127A (en) 1988-01-14 1988-01-14 Bimodal swirler injector for a gas turbine combustor

Publications (1)

Publication Number Publication Date
IN170055B true IN170055B (el) 1992-02-01

Family

ID=22505662

Family Applications (1)

Application Number Title Priority Date Filing Date
IN700/CAL/88A IN170055B (el) 1988-01-14 1988-08-22

Country Status (11)

Country Link
US (1) US4854127A (el)
JP (1) JPH01182530A (el)
CN (1) CN1018384B (el)
CA (1) CA1289756C (el)
DE (1) DE3830185A1 (el)
FR (1) FR2626043B1 (el)
GB (1) GB2214630B (el)
IN (1) IN170055B (el)
IT (1) IT1227060B (el)
SE (1) SE466710B (el)
SG (1) SG15892G (el)

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US5101634A (en) * 1989-12-20 1992-04-07 Sundstrand Corporation Fuel injector for a turbine engine
CA2076102C (en) * 1991-09-23 2001-12-18 Stephen John Howell Aero-slinger combustor
US5265425A (en) * 1991-09-23 1993-11-30 General Electric Company Aero-slinger combustor
US5274995A (en) * 1992-04-27 1994-01-04 General Electric Company Apparatus and method for atomizing water in a combustor dome assembly
US5309709A (en) * 1992-06-25 1994-05-10 Solar Turbines Incorporated Low emission combustion system for a gas turbine engine
US5218824A (en) * 1992-06-25 1993-06-15 Solar Turbines Incorporated Low emission combustion nozzle for use with a gas turbine engine
FR2695713B1 (fr) * 1992-09-17 1994-10-21 Snecma Système d'injection aérodynamique à prémélange.
US5505045A (en) * 1992-11-09 1996-04-09 Fuel Systems Textron, Inc. Fuel injector assembly with first and second fuel injectors and inner, outer, and intermediate air discharge chambers
WO1994028351A1 (en) * 1993-06-01 1994-12-08 Pratt & Whitney Canada, Inc. Radially mounted air blast fuel injector
US5404711A (en) * 1993-06-10 1995-04-11 Solar Turbines Incorporated Dual fuel injector nozzle for use with a gas turbine engine
GB9326367D0 (en) * 1993-12-23 1994-02-23 Rolls Royce Plc Fuel injection apparatus
US5444982A (en) * 1994-01-12 1995-08-29 General Electric Company Cyclonic prechamber with a centerbody
US5408830A (en) * 1994-02-10 1995-04-25 General Electric Company Multi-stage fuel nozzle for reducing combustion instabilities in low NOX gas turbines
US5564271A (en) * 1994-06-24 1996-10-15 United Technologies Corporation Pressure vessel fuel nozzle support for an industrial gas turbine engine
FR2727192B1 (fr) 1994-11-23 1996-12-20 Snecma Systeme d'injection d'une chambre de combustion a deux tetes
US5761907A (en) * 1995-12-11 1998-06-09 Parker-Hannifin Corporation Thermal gradient dispersing heatshield assembly
FR2753779B1 (fr) * 1996-09-26 1998-10-16 Systeme d'injection aerodynamique d'un melange air carburant
US6021635A (en) * 1996-12-23 2000-02-08 Parker-Hannifin Corporation Dual orifice liquid fuel and aqueous flow atomizing nozzle having an internal mixing chamber
GB2332509B (en) * 1997-12-19 2002-06-19 Europ Gas Turbines Ltd Fuel/air mixing arrangement for combustion apparatus
US6141967A (en) * 1998-01-09 2000-11-07 General Electric Company Air fuel mixer for gas turbine combustor
GB2337102A (en) * 1998-05-09 1999-11-10 Europ Gas Turbines Ltd Gas-turbine engine combustor
US6082113A (en) * 1998-05-22 2000-07-04 Pratt & Whitney Canada Corp. Gas turbine fuel injector
US6289676B1 (en) 1998-06-26 2001-09-18 Pratt & Whitney Canada Corp. Simplex and duplex injector having primary and secondary annular lud channels and primary and secondary lud nozzles
GB9818160D0 (en) 1998-08-21 1998-10-14 Rolls Royce Plc A combustion chamber
US6357237B1 (en) * 1998-10-09 2002-03-19 General Electric Company Fuel injection assembly for gas turbine engine combustor
DE19905996A1 (de) 1999-02-15 2000-08-17 Abb Alstom Power Ch Ag Brennstofflanze zum Eindüsen von flüssigen und/oder gasförmigen Brennstoffen in eine Brennkammer
US6460344B1 (en) 1999-05-07 2002-10-08 Parker-Hannifin Corporation Fuel atomization method for turbine combustion engines having aerodynamic turning vanes
US6883332B2 (en) * 1999-05-07 2005-04-26 Parker-Hannifin Corporation Fuel nozzle for turbine combustion engines having aerodynamic turning vanes
US6547163B1 (en) 1999-10-01 2003-04-15 Parker-Hannifin Corporation Hybrid atomizing fuel nozzle
US6256995B1 (en) 1999-11-29 2001-07-10 Pratt & Whitney Canada Corp. Simple low cost fuel nozzle support
DE10051221A1 (de) * 2000-10-16 2002-07-11 Alstom Switzerland Ltd Brenner mit gestufter Brennstoff-Eindüsung
US6487861B1 (en) * 2001-06-05 2002-12-03 General Electric Company Combustor for gas turbine engines with low air flow swirlers
US6543235B1 (en) 2001-08-08 2003-04-08 Cfd Research Corporation Single-circuit fuel injector for gas turbine combustors
US6523350B1 (en) * 2001-10-09 2003-02-25 General Electric Company Fuel injector fuel conduits with multiple laminated fuel strips
DE10219354A1 (de) * 2002-04-30 2003-11-13 Rolls Royce Deutschland Gasturbinenbrennkammer mit gezielter Kraftstoffeinbringung zur Verbesserung der Homogenität des Kraftstoff-Luft-Gemisches
US7065955B2 (en) * 2003-06-18 2006-06-27 General Electric Company Methods and apparatus for injecting cleaning fluids into combustors
CN1302201C (zh) * 2003-07-16 2007-02-28 沈阳黎明航空发动机(集团)有限责任公司 一种重型燃气轮机
JP4476176B2 (ja) * 2005-06-06 2010-06-09 三菱重工業株式会社 ガスタービンの予混合燃焼バーナー
JP4486549B2 (ja) * 2005-06-06 2010-06-23 三菱重工業株式会社 ガスタービンの燃焼器
US7536862B2 (en) * 2005-09-01 2009-05-26 General Electric Company Fuel nozzle for gas turbine engines
US7788927B2 (en) * 2005-11-30 2010-09-07 General Electric Company Turbine engine fuel nozzles and methods of assembling the same
GB2434437B (en) * 2006-01-19 2011-01-26 Siemens Ag Improvements in or relating to combustion apparatus
FR2899314B1 (fr) * 2006-03-30 2008-05-09 Snecma Sa Dispositif d'injection d'un melange d'air et de carburant, chambre de combustion et turbomachine munies d'un tel dispositif
GB2444737B (en) * 2006-12-13 2009-03-04 Siemens Ag Improvements in or relating to burners for a gas turbine engine
CA2686702C (en) * 2007-04-30 2016-08-16 Nuovo Pignone, S.P.A. Method and system for turbine blade characterization
DE102007043626A1 (de) 2007-09-13 2009-03-19 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität
US8402744B2 (en) * 2008-03-22 2013-03-26 Pratt & Whitney Rocketdyne, Inc. Valve system for a gas turbine engine
US8286416B2 (en) * 2008-04-02 2012-10-16 Pratt & Whitney Rocketdyne, Inc. Valve system for a gas turbine engine
US8578716B2 (en) * 2008-03-22 2013-11-12 United Technologies Corporation Valve system for a gas turbine engine
US8240126B2 (en) * 2008-03-22 2012-08-14 Pratt & Whitney Rocketdyne, Inc. Valve system for a gas turbine engine
GB0811647D0 (en) * 2008-06-26 2008-07-30 Rolls Royce Plc A fuel control arrangement
RU2477425C2 (ru) * 2008-12-10 2013-03-10 АйЭйчАй КОРПОРЕЙШН Камера сгорания
BRPI0923233A2 (pt) * 2008-12-10 2016-01-26 Ihi Corp combustor
US8099940B2 (en) * 2008-12-18 2012-01-24 Solar Turbines Inc. Low cross-talk gas turbine fuel injector
US8104286B2 (en) * 2009-01-07 2012-01-31 General Electric Company Methods and systems to enhance flame holding in a gas turbine engine
US20110072823A1 (en) * 2009-09-30 2011-03-31 Daih-Yeou Chen Gas turbine engine fuel injector
IN2012DN01786A (el) * 2009-10-09 2015-06-05 Siemens Ag
FR2955375B1 (fr) * 2010-01-18 2012-06-15 Turbomeca Dispositif d'injection et chambre de combustion de turbomachine equipee d'un tel dispositif d'injection
RU2447304C2 (ru) * 2010-03-19 2012-04-10 Общество с ограниченной ответственностью Финансово-промышленная компания "Космос-Нефть-Газ" Газотурбинная установка
US8671691B2 (en) * 2010-05-26 2014-03-18 General Electric Company Hybrid prefilming airblast, prevaporizing, lean-premixing dual-fuel nozzle for gas turbine combustor
US8919132B2 (en) 2011-05-18 2014-12-30 Solar Turbines Inc. Method of operating a gas turbine engine
US8893500B2 (en) 2011-05-18 2014-11-25 Solar Turbines Inc. Lean direct fuel injector
JP6037338B2 (ja) * 2011-06-02 2016-12-07 川崎重工業株式会社 ガスタービン燃焼器
US8955329B2 (en) 2011-10-21 2015-02-17 General Electric Company Diffusion nozzles for low-oxygen fuel nozzle assembly and method
US9182124B2 (en) 2011-12-15 2015-11-10 Solar Turbines Incorporated Gas turbine and fuel injector for the same
US9297535B2 (en) 2013-02-25 2016-03-29 General Electric Company Fuel/air mixing system for fuel nozzle
EP2971684B1 (en) 2013-03-14 2018-07-18 United Technologies Corporation Hollow-wall heat shield for fuel injector component
US9556795B2 (en) * 2013-09-06 2017-01-31 Delavan Inc Integrated heat shield
CN103672968A (zh) * 2013-12-01 2014-03-26 北京航空航天大学 一种燃油预膜空气雾化喷嘴加氢辅助燃烧结构
GB201401581D0 (en) * 2014-01-30 2014-03-19 Rolls Royce Plc A fuel manifold and fuel injector arrangement
US10288291B2 (en) * 2014-08-15 2019-05-14 General Electric Company Air-shielded fuel injection assembly to facilitate reduced NOx emissions in a combustor system
JP6417620B2 (ja) * 2014-10-24 2018-11-07 三菱日立パワーシステムズ株式会社 燃焼器、ガスタービン
GB2543803B (en) * 2015-10-29 2019-10-30 Rolls Royce Plc A combustion chamber assembly
CN108474558B (zh) * 2015-12-30 2020-08-04 通用电气公司 用于双燃料燃烧器的液体燃料喷嘴
US10774748B2 (en) * 2017-01-17 2020-09-15 Delavan Inc. Internal fuel manifolds
US10954859B2 (en) * 2017-07-25 2021-03-23 Raytheon Technologies Corporation Low emissions combustor assembly for gas turbine engine
RU2667820C1 (ru) * 2017-09-22 2018-09-24 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Фронтовое устройство камеры сгорания газотурбинного двигателя
CN108072053B (zh) * 2017-11-28 2020-12-01 中国航发沈阳发动机研究所 一种旋流雾化装置
US10947923B2 (en) * 2019-01-17 2021-03-16 Ford Global Technologies, Llc Method and system for determining fuel injector variability
US11378275B2 (en) * 2019-12-06 2022-07-05 Raytheon Technologies Corporation High shear swirler with recessed fuel filmer for a gas turbine engine
JP7320466B2 (ja) * 2020-02-28 2023-08-03 本田技研工業株式会社 ガスタービン用燃料噴射装置
RU2767856C1 (ru) * 2021-03-30 2022-03-22 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Двухканальная топливная форсунка камеры сгорания турбомашины
US11988386B2 (en) * 2021-12-03 2024-05-21 Honeywell International Inc. Gas turbine engine injector module with thermally coupled fuel lines having respective outlets
US11873993B1 (en) 2023-02-02 2024-01-16 Pratt & Whitney Canada Corp. Combustor for gas turbine engine with central fuel injection ports

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Also Published As

Publication number Publication date
GB2214630A (en) 1989-09-06
JPH01182530A (ja) 1989-07-20
GB2214630B (en) 1991-11-13
SE466710B (sv) 1992-03-23
FR2626043B1 (fr) 1993-06-11
DE3830185A1 (de) 1989-07-27
IT8821907A0 (it) 1988-09-13
US4854127A (en) 1989-08-08
SG15892G (en) 1992-04-16
CN1034259A (zh) 1989-07-26
FR2626043A1 (fr) 1989-07-21
SE8803242D0 (sv) 1988-09-14
GB8821461D0 (en) 1988-10-12
CN1018384B (zh) 1992-09-23
SE8803242L (sv) 1989-07-15
CA1289756C (en) 1991-10-01
IT1227060B (it) 1991-03-14

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