JP2010071641A5 - - Google Patents

Download PDF

Info

Publication number
JP2010071641A5
JP2010071641A5 JP2009209871A JP2009209871A JP2010071641A5 JP 2010071641 A5 JP2010071641 A5 JP 2010071641A5 JP 2009209871 A JP2009209871 A JP 2009209871A JP 2009209871 A JP2009209871 A JP 2009209871A JP 2010071641 A5 JP2010071641 A5 JP 2010071641A5
Authority
JP
Japan
Prior art keywords
turbine system
axial
tubular member
fuel nozzle
tubular
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.)
Granted
Application number
JP2009209871A
Other languages
English (en)
Japanese (ja)
Other versions
JP2010071641A (ja
JP5399178B2 (ja
Filing date
Publication date
Priority claimed from US12/212,576 external-priority patent/US8261554B2/en
Application filed filed Critical
Publication of JP2010071641A publication Critical patent/JP2010071641A/ja
Publication of JP2010071641A5 publication Critical patent/JP2010071641A5/ja
Application granted granted Critical
Publication of JP5399178B2 publication Critical patent/JP5399178B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2009209871A 2008-09-17 2009-09-11 燃料ノズルチップ組立体 Expired - Fee Related JP5399178B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/212,576 2008-09-17
US12/212,576 US8261554B2 (en) 2008-09-17 2008-09-17 Fuel nozzle tip assembly

Publications (3)

Publication Number Publication Date
JP2010071641A JP2010071641A (ja) 2010-04-02
JP2010071641A5 true JP2010071641A5 (enExample) 2012-10-18
JP5399178B2 JP5399178B2 (ja) 2014-01-29

Family

ID=41694061

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2009209871A Expired - Fee Related JP5399178B2 (ja) 2008-09-17 2009-09-11 燃料ノズルチップ組立体

Country Status (4)

Country Link
US (1) US8261554B2 (enExample)
JP (1) JP5399178B2 (enExample)
CN (1) CN101676535B (enExample)
DE (1) DE102009044026A1 (enExample)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120137695A1 (en) * 2010-12-01 2012-06-07 General Electric Company Fuel nozzle with gas only insert
US8794544B2 (en) * 2011-06-06 2014-08-05 General Electric Company Combustor nozzle and method for modifying the combustor nozzle
US9052113B1 (en) * 2011-06-06 2015-06-09 General Electric Company Combustor nozzle and method for modifying the combustor nozzle
US20130104553A1 (en) * 2011-11-01 2013-05-02 General Electric Company Injection apparatus
US9228498B2 (en) * 2012-03-01 2016-01-05 Solar Turbines Incorporated Laser clad fuel injector premix barrel
US9174309B2 (en) * 2012-07-24 2015-11-03 General Electric Company Turbine component and a process of fabricating a turbine component
US20150167983A1 (en) * 2013-12-13 2015-06-18 General Electric Company Bundled tube fuel injector tube tip
US10364982B2 (en) * 2015-11-19 2019-07-30 Ansaldo Energia Switzerland AG Method for reconditioning fuel nozzle assemblies
US10228140B2 (en) * 2016-02-18 2019-03-12 General Electric Company Gas-only cartridge for a premix fuel nozzle
JP6654487B2 (ja) * 2016-03-30 2020-02-26 三菱重工業株式会社 燃焼器、及びガスタービン
US11098900B2 (en) * 2017-07-21 2021-08-24 Delavan Inc. Fuel injectors and methods of making fuel injectors
JP7774176B1 (ja) * 2025-05-19 2025-11-20 三菱重工業株式会社 タービン静翼、タービン、及びガスタービン

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2038473B (en) * 1978-12-27 1982-12-01 Lucas Industries Ltd Fuel injector assembly
US4850196A (en) * 1987-10-13 1989-07-25 Westinghouse Electric Corp. Fuel nozzle assembly for a gas turbine engine
CN2073938U (zh) * 1990-03-19 1991-03-27 李玉涛 星形燃气轮机
US6082113A (en) * 1998-05-22 2000-07-04 Pratt & Whitney Canada Corp. Gas turbine fuel injector
US6256995B1 (en) * 1999-11-29 2001-07-10 Pratt & Whitney Canada Corp. Simple low cost fuel nozzle support
US6363724B1 (en) * 2000-08-31 2002-04-02 General Electric Company Gas only nozzle fuel tip
JP2003003933A (ja) * 2001-06-20 2003-01-08 Toyota Central Res & Dev Lab Inc 燃料噴射ノズル
JP2003314300A (ja) * 2002-04-17 2003-11-06 Mitsubishi Heavy Ind Ltd 油焚ガスタービンの燃焼器、油焚ガスタービン及びガスタービンプラント
US7290394B2 (en) * 2002-11-21 2007-11-06 Parker-Hannifin Corporation Fuel injector flexible feed with moveable nozzle tip
US7036302B2 (en) * 2004-03-15 2006-05-02 General Electric Company Controlled pressure fuel nozzle system
US7237730B2 (en) * 2005-03-17 2007-07-03 Pratt & Whitney Canada Corp. Modular fuel nozzle and method of making
US7216594B2 (en) * 2005-05-03 2007-05-15 Alstom Technology, Ltc. Multiple segment ceramic fuel nozzle tip
US20070119183A1 (en) * 2005-11-28 2007-05-31 General Electric Company Gas turbine engine combustor
US20070277530A1 (en) * 2006-05-31 2007-12-06 Constantin Alexandru Dinu Inlet flow conditioner for gas turbine engine fuel nozzle
US8166763B2 (en) * 2006-09-14 2012-05-01 Solar Turbines Inc. Gas turbine fuel injector with a removable pilot assembly

Similar Documents

Publication Publication Date Title
JP2010071641A5 (enExample)
JP2010526274A5 (enExample)
JP5789084B2 (ja) テールパイプの排気温度を低下させる装置
CN101509427A (zh) 用于提高燃气轮机功率输出的排气道及发电系统
US9046269B2 (en) Impingement cooling device
JP2010175244A5 (enExample)
JP2011045877A5 (enExample)
JP2010085089A5 (enExample)
EP2065645A3 (en) Burner and gas turbine combustor
WO2010075393A3 (en) Gas turbine engine and system for servicing a gas turbine engine
CN101676535B (zh) 燃料喷嘴顶端组件
EP2241815A3 (en) Gas turbine premixer with internal cooling
JP2014132211A5 (enExample)
JP2013231582A5 (enExample)
EP2216599A3 (en) Premixed direct injection nozzle
JP2011137629A5 (enExample)
JP2015063994A5 (enExample)
CN103089315A (zh) 涡轮机的涡轮
WO2009136998A3 (en) Tail pipe exhaust cooling device
WO2009017914A3 (en) Wetted wall cyclone system and methods
JP4057014B2 (ja) 排気ノズルフラップに冷却空気を供給する装置
JP2014153052A5 (enExample)
CA2617719A1 (en) Radially expanding turbine engine exhaust cylinder interface
CA2617340A1 (en) Piping having fluid-mixing region
JP2014132211A (ja) ターボ機械における関節式トランジションダクト本発明は、エネルギー省から授与された契約番号第ｄｅ−ｆｃ２６−０５ｎｔ４２６４３号に基づいて政府の支持を得てなされたものである。政府は本発明に関して一定の権利を有する。