JP2004093125A5 - - Google Patents

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Publication number
JP2004093125A5
JP2004093125A5 JP2003305610A JP2003305610A JP2004093125A5 JP 2004093125 A5 JP2004093125 A5 JP 2004093125A5 JP 2003305610 A JP2003305610 A JP 2003305610A JP 2003305610 A JP2003305610 A JP 2003305610A JP 2004093125 A5 JP2004093125 A5 JP 2004093125A5
Authority
JP
Japan
Prior art keywords
dome
heat shield
distance
combustor
annular end
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
JP2003305610A
Other languages
English (en)
Japanese (ja)
Other versions
JP2004093125A (ja
JP4441217B2 (ja
Filing date
Publication date
Priority claimed from US10/233,356 external-priority patent/US6758045B2/en
Application filed filed Critical
Publication of JP2004093125A publication Critical patent/JP2004093125A/ja
Publication of JP2004093125A5 publication Critical patent/JP2004093125A5/ja
Application granted granted Critical
Publication of JP4441217B2 publication Critical patent/JP4441217B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

JP2003305610A 2002-08-30 2003-08-29 ガスタービンエンジンを作動させるための方法及び装置 Expired - Fee Related JP4441217B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/233,356 US6758045B2 (en) 2002-08-30 2002-08-30 Methods and apparatus for operating gas turbine engines

Publications (3)

Publication Number Publication Date
JP2004093125A JP2004093125A (ja) 2004-03-25
JP2004093125A5 true JP2004093125A5 (https=) 2006-10-12
JP4441217B2 JP4441217B2 (ja) 2010-03-31

Family

ID=31495416

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003305610A Expired - Fee Related JP4441217B2 (ja) 2002-08-30 2003-08-29 ガスタービンエンジンを作動させるための方法及び装置

Country Status (3)

Country Link
US (1) US6758045B2 (https=)
EP (1) EP1394470A3 (https=)
JP (1) JP4441217B2 (https=)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7065972B2 (en) * 2004-05-21 2006-06-27 Honeywell International, Inc. Fuel-air mixing apparatus for reducing gas turbine combustor exhaust emissions
US7316117B2 (en) * 2005-02-04 2008-01-08 Siemens Power Generation, Inc. Can-annular turbine combustors comprising swirler assembly and base plate arrangements, and combinations
US7631504B2 (en) * 2006-02-21 2009-12-15 General Electric Company Methods and apparatus for assembling gas turbine engines
US7617689B2 (en) * 2006-03-02 2009-11-17 Honeywell International Inc. Combustor dome assembly including retaining ring
US8596071B2 (en) * 2006-05-05 2013-12-03 General Electric Company Method and apparatus for assembling a gas turbine engine
US7600370B2 (en) 2006-05-25 2009-10-13 Siemens Energy, Inc. Fluid flow distributor apparatus for gas turbine engine mid-frame section
US7775050B2 (en) * 2006-10-31 2010-08-17 General Electric Company Method and apparatus for reducing stresses induced to combustor assemblies
US8365533B2 (en) * 2009-09-22 2013-02-05 General Electric Company Universal multi-nozzle combustion system and method
US8943835B2 (en) 2010-05-10 2015-02-03 General Electric Company Gas turbine engine combustor with CMC heat shield and methods therefor
US9052113B1 (en) 2011-06-06 2015-06-09 General Electric Company Combustor nozzle and method for modifying the combustor nozzle
US8916011B2 (en) 2011-06-24 2014-12-23 United Technologies Corporation Fireshield fastener hood
US8893382B2 (en) * 2011-09-30 2014-11-25 General Electric Company Combustion system and method of assembling the same
US9322415B2 (en) 2012-10-29 2016-04-26 United Technologies Corporation Blast shield for high pressure compressor
FR3022613B1 (fr) * 2014-06-24 2019-04-19 Safran Helicopter Engines Bossage pour chambre de combustion.
US10337736B2 (en) * 2015-07-24 2019-07-02 Pratt & Whitney Canada Corp. Gas turbine engine combustor and method of forming same
US10724740B2 (en) 2016-11-04 2020-07-28 General Electric Company Fuel nozzle assembly with impingement purge
US10634353B2 (en) * 2017-01-12 2020-04-28 General Electric Company Fuel nozzle assembly with micro channel cooling
WO2020181134A2 (en) * 2019-03-06 2020-09-10 Industrom Power, Llc Compact axial turbine for high density working fluid
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles
US11859819B2 (en) 2021-10-15 2024-01-02 General Electric Company Ceramic composite combustor dome and liners
CN114719293B (zh) * 2022-03-24 2023-05-26 西北工业大学 一种环腔加力燃烧室结构

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1377184A (en) 1971-02-02 1974-12-11 Secr Defence Gas turbine engine combustion apparatus
GB1547374A (en) 1975-12-06 1979-06-13 Rolls Royce Fuel injection for gas turbine engines
GB1597968A (en) 1977-06-10 1981-09-16 Rolls Royce Fuel burners for gas turbine engines
US5323604A (en) * 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
US5630319A (en) * 1995-05-12 1997-05-20 General Electric Company Dome assembly for a multiple annular combustor
US5680767A (en) * 1995-09-11 1997-10-28 General Electric Company Regenerative combustor cooling in a gas turbine engine
US5657633A (en) * 1995-12-29 1997-08-19 General Electric Company Centerbody for a multiple annular combustor
US5680766A (en) 1996-01-02 1997-10-28 General Electric Company Dual fuel mixer for gas turbine combustor
US5675971A (en) 1996-01-02 1997-10-14 General Electric Company Dual fuel mixer for gas turbine combustor
US5778676A (en) 1996-01-02 1998-07-14 General Electric Company Dual fuel mixer for gas turbine combustor
US5899075A (en) 1997-03-17 1999-05-04 General Electric Company Turbine engine combustor with fuel-air mixer
US6141967A (en) 1998-01-09 2000-11-07 General Electric Company Air fuel mixer for gas turbine combustor
US6415594B1 (en) * 2000-05-31 2002-07-09 General Electric Company Methods and apparatus for reducing gas turbine engine emissions

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