JP2013544345A5 - - Google Patents

Download PDF

Info

Publication number
JP2013544345A5
JP2013544345A5 JP2013541324A JP2013541324A JP2013544345A5 JP 2013544345 A5 JP2013544345 A5 JP 2013544345A5 JP 2013541324 A JP2013541324 A JP 2013541324A JP 2013541324 A JP2013541324 A JP 2013541324A JP 2013544345 A5 JP2013544345 A5 JP 2013544345A5
Authority
JP
Japan
Prior art keywords
sleeve
flange
supply pipe
bore
gas supply
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
JP2013541324A
Other languages
English (en)
Japanese (ja)
Other versions
JP5791731B2 (ja
JP2013544345A (ja
Filing date
Publication date
Priority claimed from US12/957,476 external-priority patent/US20120137691A1/en
Application filed filed Critical
Publication of JP2013544345A publication Critical patent/JP2013544345A/ja
Publication of JP2013544345A5 publication Critical patent/JP2013544345A5/ja
Application granted granted Critical
Publication of JP5791731B2 publication Critical patent/JP5791731B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2013541324A 2010-12-01 2011-11-30 ガスタービンアセンブリとその組立方法 Active JP5791731B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/957,476 US20120137691A1 (en) 2010-12-01 2010-12-01 Gas turbine assembly and method therefor
US12/957,476 2010-12-01
PCT/EP2011/071340 WO2012072659A1 (en) 2010-12-01 2011-11-30 Gas turbine assembly and method therefor

Publications (3)

Publication Number Publication Date
JP2013544345A JP2013544345A (ja) 2013-12-12
JP2013544345A5 true JP2013544345A5 (enExample) 2014-04-17
JP5791731B2 JP5791731B2 (ja) 2015-10-07

Family

ID=45092354

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013541324A Active JP5791731B2 (ja) 2010-12-01 2011-11-30 ガスタービンアセンブリとその組立方法

Country Status (5)

Country Link
US (1) US20120137691A1 (enExample)
EP (1) EP2622278B1 (enExample)
JP (1) JP5791731B2 (enExample)
CN (1) CN103228993B (enExample)
WO (1) WO2012072659A1 (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9032735B2 (en) * 2012-04-26 2015-05-19 General Electric Company Combustor and a method for assembling the combustor
US10533750B2 (en) 2014-09-05 2020-01-14 Siemens Aktiengesellschaft Cross ignition flame duct
WO2016064391A1 (en) 2014-10-23 2016-04-28 Siemens Energy, Inc. Flexible fuel combustion system for turbine engines
US11230976B2 (en) * 2017-07-14 2022-01-25 General Electric Company Integrated fuel nozzle connection

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1602836A (en) * 1977-05-11 1981-11-18 Lucas Industries Ltd Sealing arrangement for use in a combustion assembly
GB2097112B (en) * 1981-04-16 1984-12-12 Rolls Royce Fuel burners and combustion equipment for use in gas turbine engines
JPH04124522A (ja) * 1990-09-17 1992-04-24 Hitachi Ltd 燃焼装置の燃料供給方法、燃料供給系統および拡散燃料ノズル
JP2002350092A (ja) * 2001-05-28 2002-12-04 Kawasaki Heavy Ind Ltd 熱交換器とこれを用いたガスタービン装置
US7900456B2 (en) * 2006-05-19 2011-03-08 Delavan Inc Apparatus and method to compensate for differential thermal growth of injector components
FR2903172B1 (fr) * 2006-06-29 2008-10-17 Snecma Sa Agencement pour chambre de combustion de turbomachine ayant un defecteur a collerette
WO2009039142A2 (en) * 2007-09-17 2009-03-26 Delavan Inc Flexure seal for fuel injection nozzle
US8266912B2 (en) * 2008-09-16 2012-09-18 General Electric Company Reusable weld joint for syngas fuel nozzles
EP2189720A1 (de) * 2008-11-21 2010-05-26 Siemens Aktiengesellschaft Brenneranordnung
US8899010B2 (en) * 2010-11-17 2014-12-02 General Electric Company Pulse detonation combustor

Similar Documents

Publication Publication Date Title
CN105135101B (zh) 一种用于管路接头的锁紧装置
EP2378200A3 (en) Combustor liner cooling at transition duct interface and related method
JP6300675B2 (ja) タービンハウジング
JP2012067745A5 (enExample)
JP2014173841A5 (enExample)
JP2014181701A5 (enExample)
EP2518408A3 (en) A head part of an annular combustion chamber
JP2016035336A5 (enExample)
JP2014181894A5 (enExample)
JP2013195057A5 (enExample)
EP2144003A3 (en) A combustion liner for a gas turbine engine
RU2007135200A (ru) Статор турбины газотурбинного двигателя и газотурбинный двигатель
JP2013544345A5 (enExample)
WO2010014125A3 (en) Combustor apparatus in a gas turbine engine
EP2208933A3 (en) Combustor assembly and cap for a turbine engine
RU2014137104A (ru) Устройство впрыска воздуха и топлива для камеры сгорания турбомашины
JP2012207565A5 (enExample)
EP4310401A3 (en) Combustor assembly for a turbine engine
JP2016044630A5 (enExample)
WO2015069338A3 (en) Gas turbine engine blade outer air seal thermal control system
JP2014102067A (ja) 自在入れ子式伸縮クロスファイア管および燃焼器構造の組み立て方法
EP2112362A3 (en) Rear fan case for a gas turbine engine
US20150260043A1 (en) Removal device
CN103061919A (zh) 固液火箭发动机燃烧室气密检查装置
JP2016164400A5 (ja) 燃料供給装置及びベローズ式ダンパ