JP2011220335A5 - - Google Patents

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Publication number
JP2011220335A5
JP2011220335A5 JP2011077370A JP2011077370A JP2011220335A5 JP 2011220335 A5 JP2011220335 A5 JP 2011220335A5 JP 2011077370 A JP2011077370 A JP 2011077370A JP 2011077370 A JP2011077370 A JP 2011077370A JP 2011220335 A5 JP2011220335 A5 JP 2011220335A5
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JP
Japan
Prior art keywords
fluid
combustor
liner
passage
transition piece
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
JP2011077370A
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English (en)
Japanese (ja)
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JP2011220335A (ja
JP5679883B2 (ja
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Publication date
Priority claimed from US12/756,329 external-priority patent/US8359867B2/en
Application filed filed Critical
Publication of JP2011220335A publication Critical patent/JP2011220335A/ja
Publication of JP2011220335A5 publication Critical patent/JP2011220335A5/ja
Application granted granted Critical
Publication of JP5679883B2 publication Critical patent/JP5679883B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2011077370A 2010-04-08 2011-03-31 流れスリーブを有する燃焼器 Active JP5679883B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/756,329 US8359867B2 (en) 2010-04-08 2010-04-08 Combustor having a flow sleeve
US12/756,329 2010-04-08

Publications (3)

Publication Number Publication Date
JP2011220335A JP2011220335A (ja) 2011-11-04
JP2011220335A5 true JP2011220335A5 (https=) 2013-06-13
JP5679883B2 JP5679883B2 (ja) 2015-03-04

Family

ID=44202906

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011077370A Active JP5679883B2 (ja) 2010-04-08 2011-03-31 流れスリーブを有する燃焼器

Country Status (4)

Country Link
US (1) US8359867B2 (https=)
EP (1) EP2375161B1 (https=)
JP (1) JP5679883B2 (https=)
CN (1) CN102235671B (https=)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120198855A1 (en) * 2011-02-03 2012-08-09 General Electric Company Method and apparatus for cooling combustor liner in combustor
US8650852B2 (en) * 2011-07-05 2014-02-18 General Electric Company Support assembly for transition duct in turbine system
US9182122B2 (en) * 2011-10-05 2015-11-10 General Electric Company Combustor and method for supplying flow to a combustor
US20130269359A1 (en) * 2012-04-16 2013-10-17 General Electric Company Combustor flow sleeve with supplemental air supply
US9366438B2 (en) * 2013-02-14 2016-06-14 Siemens Aktiengesellschaft Flow sleeve inlet assembly in a gas turbine engine
US9163837B2 (en) * 2013-02-27 2015-10-20 Siemens Aktiengesellschaft Flow conditioner in a combustor of a gas turbine engine
KR101557453B1 (ko) 2014-01-15 2015-10-06 두산중공업 주식회사 가스터빈의 이중벽 슬리브 냉각구조를 구비한 라이너 및 그 냉각방법
CN106796034A (zh) 2014-09-05 2017-05-31 西门子公司 联焰导管
US10215418B2 (en) * 2014-10-13 2019-02-26 Ansaldo Energia Ip Uk Limited Sealing device for a gas turbine combustor
DE102015205975A1 (de) * 2015-04-02 2016-10-06 Siemens Aktiengesellschaft Umführungs-Hitzeschildelement
KR101853456B1 (ko) * 2015-06-16 2018-04-30 두산중공업 주식회사 가스터빈용 연소 덕트 조립체
DE112016005084B4 (de) * 2015-11-05 2022-09-22 Mitsubishi Heavy Industries, Ltd. Verbrennungszylinder, Gasturbinenbrennkammer und Gasturbine
EP3287610B1 (en) * 2016-08-22 2019-07-10 Ansaldo Energia Switzerland AG Gas turbine transition duct
KR101986729B1 (ko) * 2017-08-22 2019-06-07 두산중공업 주식회사 실 영역 집중냉각을 위한 냉각유로 구조 및 이를 포함하는 가스 터빈용 연소기
KR102377720B1 (ko) * 2019-04-10 2022-03-23 두산중공업 주식회사 압력 강하가 개선된 라이너 냉각구조 및 이를 포함하는 가스터빈용 연소기

Family Cites Families (19)

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Publication number Priority date Publication date Assignee Title
CA1263243A (en) * 1985-05-14 1989-11-28 Lewis Berkley Davis, Jr. Impingement cooled transition duct
US4719748A (en) 1985-05-14 1988-01-19 General Electric Company Impingement cooled transition duct
JP3590666B2 (ja) 1995-03-30 2004-11-17 株式会社東芝 ガスタービン燃焼器
JPH08284688A (ja) * 1995-04-18 1996-10-29 Hitachi Ltd ガスタービンおよびガスタービン燃焼装置
JP3069522B2 (ja) * 1996-05-31 2000-07-24 株式会社東芝 ガスタービン燃焼器
US6484505B1 (en) 2000-02-25 2002-11-26 General Electric Company Combustor liner cooling thimbles and related method
US7082770B2 (en) * 2003-12-24 2006-08-01 Martling Vincent C Flow sleeve for a low NOx combustor
US7007482B2 (en) * 2004-05-28 2006-03-07 Power Systems Mfg., Llc Combustion liner seal with heat transfer augmentation
US7010921B2 (en) 2004-06-01 2006-03-14 General Electric Company Method and apparatus for cooling combustor liner and transition piece of a gas turbine
US7574865B2 (en) 2004-11-18 2009-08-18 Siemens Energy, Inc. Combustor flow sleeve with optimized cooling and airflow distribution
US7707835B2 (en) * 2005-06-15 2010-05-04 General Electric Company Axial flow sleeve for a turbine combustor and methods of introducing flow sleeve air
US7685823B2 (en) 2005-10-28 2010-03-30 Power Systems Mfg., Llc Airflow distribution to a low emissions combustor
US7571611B2 (en) * 2006-04-24 2009-08-11 General Electric Company Methods and system for reducing pressure losses in gas turbine engines
US7878002B2 (en) * 2007-04-17 2011-02-01 General Electric Company Methods and systems to facilitate reducing combustor pressure drops
US7762075B2 (en) * 2007-08-14 2010-07-27 General Electric Company Combustion liner stop in a gas turbine
US8051663B2 (en) * 2007-11-09 2011-11-08 United Technologies Corp. Gas turbine engine systems involving cooling of combustion section liners
US8096133B2 (en) * 2008-05-13 2012-01-17 General Electric Company Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface
US20100223931A1 (en) * 2009-03-04 2010-09-09 General Electric Company Pattern cooled combustor liner
US8307657B2 (en) 2009-03-10 2012-11-13 General Electric Company Combustor liner cooling system

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