JPH10196952A5 - - Google Patents

Info

Publication number
JPH10196952A5
JPH10196952A5 JP1997365231A JP36523197A JPH10196952A5 JP H10196952 A5 JPH10196952 A5 JP H10196952A5 JP 1997365231 A JP1997365231 A JP 1997365231A JP 36523197 A JP36523197 A JP 36523197A JP H10196952 A5 JPH10196952 A5 JP H10196952A5
Authority
JP
Japan
Prior art keywords
fuel
longitudinal axis
passage
cylindrical
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.)
Pending
Application number
JP1997365231A
Other languages
English (en)
Japanese (ja)
Other versions
JPH10196952A (ja
Filing date
Publication date
Priority claimed from US08/771,408 external-priority patent/US5899076A/en
Application filed filed Critical
Publication of JPH10196952A publication Critical patent/JPH10196952A/ja
Publication of JPH10196952A5 publication Critical patent/JPH10196952A5/ja
Pending legal-status Critical Current

Links

JP9365231A 1996-12-20 1997-12-19 燃料ノズルアセンブリ Pending JPH10196952A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/771,408 1996-12-20
US08/771,408 US5899076A (en) 1996-12-20 1996-12-20 Flame disgorging two stream tangential entry nozzle

Publications (2)

Publication Number Publication Date
JPH10196952A JPH10196952A (ja) 1998-07-31
JPH10196952A5 true JPH10196952A5 (OSRAM) 2005-07-28

Family

ID=25091715

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9365231A Pending JPH10196952A (ja) 1996-12-20 1997-12-19 燃料ノズルアセンブリ

Country Status (5)

Country Link
US (1) US5899076A (OSRAM)
JP (1) JPH10196952A (OSRAM)
CN (1) CN1115514C (OSRAM)
CA (1) CA2225319A1 (OSRAM)
RU (1) RU2193686C2 (OSRAM)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6067790A (en) * 1996-01-05 2000-05-30 Choi; Kyung J. Lean direct wall fuel injection method and devices
US6176087B1 (en) * 1997-12-15 2001-01-23 United Technologies Corporation Bluff body premixing fuel injector and method for premixing fuel and air
US6178752B1 (en) * 1998-03-24 2001-01-30 United Technologies Corporation Durability flame stabilizing fuel injector with impingement and transpiration cooled tip
US6141954A (en) * 1998-05-18 2000-11-07 United Technologies Corporation Premixing fuel injector with improved flame disgorgement capacity
US6098407A (en) * 1998-06-08 2000-08-08 United Technologies Corporation Premixing fuel injector with improved secondary fuel-air injection
DE10049203A1 (de) * 2000-10-05 2002-05-23 Alstom Switzerland Ltd Verfahren zur Brennstoffeinleitung in einen Vormischbrenner
DE10104695B4 (de) * 2001-02-02 2014-11-20 Alstom Technology Ltd. Vormischbrenner für eine Gasturbine
RU2289367C1 (ru) * 2005-03-22 2006-12-20 Государственное учреждение "Межотраслевой научно-технический комплекс "Микрохирургия глаза" имени академика С.Н. Федорова Министерства здравоохранения и социального развития Российской Федерации Способ рецессии мышц горизонтального действия при содружественном косоглазии
US8528337B2 (en) * 2008-01-22 2013-09-10 General Electric Company Lobe nozzles for fuel and air injection
US20100024425A1 (en) * 2008-07-31 2010-02-04 General Electric Company Turbine engine fuel nozzle
JP5083302B2 (ja) * 2009-12-14 2012-11-28 株式会社日立製作所 燃焼器とガスタービン燃焼器、及び空気を燃焼器に供給する方法
EP2519770B1 (en) * 2009-12-30 2017-05-31 Hysytech S.r.l. Burner and combustion device comprising said burner
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
US9127844B2 (en) * 2011-08-02 2015-09-08 General Electric Company Fuel nozzle
US9182124B2 (en) 2011-12-15 2015-11-10 Solar Turbines Incorporated Gas turbine and fuel injector for the same
US9939151B2 (en) 2013-03-15 2018-04-10 Honeywell International Inc. Oxygen-fuel burner with staged oxygen supply
CN103267290B (zh) * 2013-05-29 2015-02-25 河南乾丰暖通科技股份有限公司 具有步进式混风功能的燃烧器箱体装置
CN104214800B (zh) * 2014-09-03 2016-08-24 北京华清燃气轮机与煤气化联合循环工程技术有限公司 燃气轮机燃烧室轴向进气喷嘴
FR3099547B1 (fr) * 2019-07-29 2021-10-08 Safran Aircraft Engines Nez d'injecteur de carburant pour turbomachine comprenant une chambre de mise en rotation intérieurement délimitée par un pion
DE102021001580A1 (de) * 2021-03-25 2022-09-29 Mercedes-Benz Group AG Brenner für ein Kraftfahrzeug sowie Kraftfahrzeug mit wenigstens einem solchen Brenner

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3982392A (en) * 1974-09-03 1976-09-28 General Motors Corporation Combustion apparatus
FR2596102B1 (fr) * 1986-03-20 1988-05-27 Snecma Dispositif d'injection a vrille axialo-centripete
RU2008509C1 (ru) * 1990-12-26 1994-02-28 Институт проблем машиностроения АН Украины Форсунка для двигателя внутреннего сгорания
US5307634A (en) * 1992-02-26 1994-05-03 United Technologies Corporation Premix gas nozzle
US5309718A (en) * 1992-09-14 1994-05-10 Hughes Aircraft Company Liquid fuel turbocharged power plant and method
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
US5461865A (en) * 1994-02-24 1995-10-31 United Technologies Corporation Tangential entry fuel nozzle
US5479773A (en) * 1994-10-13 1996-01-02 United Technologies Corporation Tangential air entry fuel nozzle
US5671597A (en) * 1994-12-22 1997-09-30 United Technologies Corporation Low nox fuel nozzle assembly
US5761897A (en) * 1996-12-20 1998-06-09 United Technologies Corporation Method of combustion with a two stream tangential entry nozzle
US5791562A (en) * 1996-12-20 1998-08-11 United Technologies Corporation Conical centerbody for a two stream tangential entry nozzle

Similar Documents

Publication Publication Date Title
JPH10196952A5 (OSRAM)
US5423173A (en) Fuel injector and method of operating the fuel injector
US5899076A (en) Flame disgorging two stream tangential entry nozzle
US5865609A (en) Method of combustion with low acoustics
JPH10196954A5 (OSRAM)
EP0939275A2 (en) Fuel nozzle and nozzle guide for gas turbine engine
JPH10196955A5 (OSRAM)
US5896739A (en) Method of disgorging flames from a two stream tangential entry nozzle
JPH10196958A5 (OSRAM)
EP0849527B1 (en) Method of combustion with a two stream tangential entry nozzle
CN115451431A (zh) 一种用于燃气轮机燃烧室的燃料喷嘴预混系统
EP1297283A1 (en) Fuel injector for low emissions premixing gas turbine combustor
US5146741A (en) Gaseous fuel injector
JPH11515089A (ja) 燃焼装置用の燃料噴射装置
US5791562A (en) Conical centerbody for a two stream tangential entry nozzle
US5735466A (en) Two stream tangential entry nozzle
EP0849530A2 (en) Fuel nozzles and centerbodies therefor
US5426933A (en) Dual feed injection nozzle with water injection
US5887795A (en) Premix fuel injector with low acoustics
US5908160A (en) Centerbody for a two stream tangential entry nozzle
EP0849529B1 (en) Tangential entry fuel nozzle
EP0849528A2 (en) Two stream tangential entry nozzle