JP2010216479A5 - - Google Patents

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Publication number
JP2010216479A5
JP2010216479A5 JP2010055244A JP2010055244A JP2010216479A5 JP 2010216479 A5 JP2010216479 A5 JP 2010216479A5 JP 2010055244 A JP2010055244 A JP 2010055244A JP 2010055244 A JP2010055244 A JP 2010055244A JP 2010216479 A5 JP2010216479 A5 JP 2010216479A5
Authority
JP
Japan
Prior art keywords
prefilmer
fuel
heat source
fuel nozzle
air passage
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.)
Ceased
Application number
JP2010055244A
Other languages
English (en)
Japanese (ja)
Other versions
JP2010216479A (ja
Filing date
Publication date
Priority claimed from US12/405,195 external-priority patent/US8186165B2/en
Application filed filed Critical
Publication of JP2010216479A publication Critical patent/JP2010216479A/ja
Publication of JP2010216479A5 publication Critical patent/JP2010216479A5/ja
Ceased legal-status Critical Current

Links

JP2010055244A 2009-03-16 2010-03-12 熱制御を有するタービン燃料ノズル Ceased JP2010216479A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/405,195 US8186165B2 (en) 2009-03-16 2009-03-16 Turbine fuel nozzle having heat control

Publications (2)

Publication Number Publication Date
JP2010216479A JP2010216479A (ja) 2010-09-30
JP2010216479A5 true JP2010216479A5 (https=) 2012-09-27

Family

ID=42237322

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010055244A Ceased JP2010216479A (ja) 2009-03-16 2010-03-12 熱制御を有するタービン燃料ノズル

Country Status (4)

Country Link
US (1) US8186165B2 (https=)
EP (1) EP2236937A3 (https=)
JP (1) JP2010216479A (https=)
CN (1) CN101839178A (https=)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8950188B2 (en) * 2011-09-09 2015-02-10 General Electric Company Turning guide for combustion fuel nozzle in gas turbine and method to turn fuel flow entering combustion chamber
US20130189632A1 (en) * 2012-01-23 2013-07-25 General Electric Company Fuel nozzel
US9353949B2 (en) 2012-04-17 2016-05-31 Siemens Energy, Inc. Device for improved air and fuel distribution to a combustor
US20130277447A1 (en) * 2012-04-23 2013-10-24 General Electric Company Method and system to control a fuel injector
US9810427B2 (en) * 2015-03-26 2017-11-07 Ansaldo Energia Switzerland AG Fuel nozzle with hemispherical dome air inlet
KR101857280B1 (ko) * 2015-06-30 2018-05-11 두산중공업 주식회사 향상된 연료 유동 분포를 위한 장치가 구비된 가스 터빈 발전장치.
KR101853442B1 (ko) * 2015-06-30 2018-04-30 두산중공업 주식회사 향상된 연료 유동 분포를 위한 장치를 포함한 가스 터빈 발전장치.
US10989118B2 (en) * 2017-12-20 2021-04-27 Wrightspeed, Inc. Controlled evaporation and heating of fuels for turbine engines
DE102024132232A1 (de) 2024-11-05 2026-05-07 Rolls-Royce Deutschland Ltd & Co Kg Düse zur Zufuhr von Luft und flüssigem Kraftstoff in eine Brennkammer und Triebwerk

Family Cites Families (24)

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Publication number Priority date Publication date Assignee Title
US3018626A (en) * 1960-02-02 1962-01-30 Gen Electric Vapor combustion system
US4262482A (en) * 1977-11-17 1981-04-21 Roffe Gerald A Apparatus for the premixed gas phase combustion of liquid fuels
JPS6026251Y2 (ja) * 1980-02-16 1985-08-07 ダイニチ工業株式会社 石油燃焼器の気化装置
US4365753A (en) * 1980-08-22 1982-12-28 Parker-Hannifin Corporation Boundary layer prefilmer airblast nozzle
WO1991019083A1 (fr) * 1990-06-04 1991-12-12 Nippon Clean Engine Research Institute Co., Ltd. Moteur a combustion interne du type a allumage par impact contre une surface chaude et allumage d'un tel moteur par impact du carburant contre une surface chaude
US5328355A (en) * 1991-09-26 1994-07-12 Hitachi, Ltd. Combustor and combustion apparatus
US5461865A (en) * 1994-02-24 1995-10-31 United Technologies Corporation Tangential entry fuel nozzle
JP3034859B1 (ja) * 1999-01-26 2000-04-17 川崎重工業株式会社 ガスタ―ビンの燃焼器
EP1036988A3 (en) * 1999-02-26 2001-05-16 R. Jan Mowill Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
US6925809B2 (en) * 1999-02-26 2005-08-09 R. Jan Mowill Gas turbine engine fuel/air premixers with variable geometry exit and method for controlling exit velocities
US6601776B1 (en) * 1999-09-22 2003-08-05 Microcoating Technologies, Inc. Liquid atomization methods and devices
US6547163B1 (en) * 1999-10-01 2003-04-15 Parker-Hannifin Corporation Hybrid atomizing fuel nozzle
US20020083714A1 (en) * 2000-11-01 2002-07-04 Daniel Bakholdin Liquid fuel combustion system and method
US6622488B2 (en) * 2001-03-21 2003-09-23 Parker-Hannifin Corporation Pure airblast nozzle
JP2003042453A (ja) * 2001-07-26 2003-02-13 Mitsubishi Heavy Ind Ltd ガスタービンの予混合ノズルまたは予混合燃焼器
US6920749B2 (en) * 2002-03-15 2005-07-26 Parker-Hannifin Corporation Multi-function simplex/prefilmer nozzle
US6779513B2 (en) * 2002-03-22 2004-08-24 Chrysalis Technologies Incorporated Fuel injector for an internal combustion engine
GB0219458D0 (en) * 2002-08-21 2002-09-25 Rolls Royce Plc Fuel injection apparatus
CN1748108A (zh) * 2003-02-28 2006-03-15 韦巴斯托股份公司 将液体燃料雾化的喷嘴
GB2404729B (en) * 2003-08-08 2008-01-23 Rolls Royce Plc Fuel injection
US7334410B2 (en) * 2004-04-07 2008-02-26 United Technologies Corporation Swirler
US7251940B2 (en) * 2004-04-30 2007-08-07 United Technologies Corporation Air assist fuel injector for a combustor
US20060156733A1 (en) * 2005-01-14 2006-07-20 Pratt & Whitney Canada Corp. Integral heater for fuel conveying member
US8240151B2 (en) * 2006-01-20 2012-08-14 Parker-Hannifin Corporation Fuel injector nozzles for gas turbine engines

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