JP2019105437A5 - - Google Patents

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Publication number
JP2019105437A5
JP2019105437A5 JP2018188724A JP2018188724A JP2019105437A5 JP 2019105437 A5 JP2019105437 A5 JP 2019105437A5 JP 2018188724 A JP2018188724 A JP 2018188724A JP 2018188724 A JP2018188724 A JP 2018188724A JP 2019105437 A5 JP2019105437 A5 JP 2019105437A5
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JP
Japan
Prior art keywords
facing surface
rear frame
downstream
microchannels
cooling
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JP2018188724A
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English (en)
Japanese (ja)
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JP7242237B2 (ja
JP2019105437A (ja
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Priority claimed from US15/783,291 external-priority patent/US10684016B2/en
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Publication of JP2019105437A publication Critical patent/JP2019105437A/ja
Publication of JP2019105437A5 publication Critical patent/JP2019105437A5/ja
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Publication of JP7242237B2 publication Critical patent/JP7242237B2/ja
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JP2018188724A 2017-10-13 2018-10-04 ガスタービンのトランジションピースのための後部フレームアセンブリ Active JP7242237B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/783,291 2017-10-13
US15/783,291 US10684016B2 (en) 2017-10-13 2017-10-13 Aft frame assembly for gas turbine transition piece

Publications (3)

Publication Number Publication Date
JP2019105437A JP2019105437A (ja) 2019-06-27
JP2019105437A5 true JP2019105437A5 (cg-RX-API-DMAC7.html) 2022-12-22
JP7242237B2 JP7242237B2 (ja) 2023-03-20

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JP2018188724A Active JP7242237B2 (ja) 2017-10-13 2018-10-04 ガスタービンのトランジションピースのための後部フレームアセンブリ

Country Status (4)

Country Link
US (1) US10684016B2 (cg-RX-API-DMAC7.html)
EP (1) EP3470628B1 (cg-RX-API-DMAC7.html)
JP (1) JP7242237B2 (cg-RX-API-DMAC7.html)
KR (1) KR20190041933A (cg-RX-API-DMAC7.html)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10577957B2 (en) * 2017-10-13 2020-03-03 General Electric Company Aft frame assembly for gas turbine transition piece
US10718224B2 (en) 2017-10-13 2020-07-21 General Electric Company AFT frame assembly for gas turbine transition piece
US11859818B2 (en) 2019-02-25 2024-01-02 General Electric Company Systems and methods for variable microchannel combustor liner cooling
EP3954870B1 (en) * 2020-08-14 2024-02-07 Ansaldo Energia Switzerland AG Transition duct for a gas turbine plant and gas turbine plant comprising said transition duct
US11187152B1 (en) * 2020-09-30 2021-11-30 General Electric Company Turbomachine sealing arrangement having a cooling flow director

Family Cites Families (23)

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Publication number Priority date Publication date Assignee Title
US6412268B1 (en) * 2000-04-06 2002-07-02 General Electric Company Cooling air recycling for gas turbine transition duct end frame and related method
DE60137099D1 (de) * 2000-04-13 2009-02-05 Mitsubishi Heavy Ind Ltd Kühlstruktur für das Endstück einer Gasturbinenbrennkammer
JP3846169B2 (ja) * 2000-09-14 2006-11-15 株式会社日立製作所 ガスタービンの補修方法
JP2002243154A (ja) * 2001-02-16 2002-08-28 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器尾筒出口構造及びガスタービン燃焼器
US20090324387A1 (en) * 2008-06-30 2009-12-31 General Electric Company Aft frame with oval-shaped cooling slots and related method
US8186167B2 (en) * 2008-07-07 2012-05-29 General Electric Company Combustor transition piece aft end cooling and related method
US8245515B2 (en) 2008-08-06 2012-08-21 General Electric Company Transition duct aft end frame cooling and related method
US20110162378A1 (en) * 2010-01-06 2011-07-07 General Electric Company Tunable transition piece aft frame
EP2353763A1 (en) * 2010-02-10 2011-08-10 Siemens Aktiengesellschaft A method of manufacturing a hot-gas component with a cooling channel by brazing a sintered sheet on a carrier ;corresponding hot-gas component
US8651805B2 (en) * 2010-04-22 2014-02-18 General Electric Company Hot gas path component cooling system
US8499566B2 (en) 2010-08-12 2013-08-06 General Electric Company Combustor liner cooling system
US8353165B2 (en) * 2011-02-18 2013-01-15 General Electric Company Combustor assembly for use in a turbine engine and methods of fabricating same
US9255484B2 (en) * 2011-03-16 2016-02-09 General Electric Company Aft frame and method for cooling aft frame
US8956104B2 (en) 2011-10-12 2015-02-17 General Electric Company Bucket assembly for turbine system
US9297262B2 (en) 2012-05-24 2016-03-29 General Electric Company Cooling structures in the tips of turbine rotor blades
US20140000267A1 (en) 2012-06-29 2014-01-02 General Electric Company Transition duct for a gas turbine
US20140360155A1 (en) * 2013-06-07 2014-12-11 General Electric Company Microchannel systems and methods for cooling turbine components of a gas turbine engine
US9574498B2 (en) * 2013-09-25 2017-02-21 General Electric Company Internally cooled transition duct aft frame with serpentine cooling passage and conduit
US9909432B2 (en) 2013-11-26 2018-03-06 General Electric Company Gas turbine transition piece aft frame assemblies with cooling channels and methods for manufacturing the same
EP3026219B1 (en) * 2014-11-27 2017-07-26 Ansaldo Energia Switzerland AG Support segment for a transition piece between combustor and turbine
EP3390781B1 (en) 2015-12-15 2020-08-12 Siemens Aktiengesellschaft Cooling features for a gas turbine engine transition duct and corresponding method for forming
EP3287610B1 (en) * 2016-08-22 2019-07-10 Ansaldo Energia Switzerland AG Gas turbine transition duct
US10830142B2 (en) * 2016-10-10 2020-11-10 General Electric Company Combustor aft frame cooling

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