JP2013227979A5 - - Google Patents

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Publication number
JP2013227979A5
JP2013227979A5 JP2013090841A JP2013090841A JP2013227979A5 JP 2013227979 A5 JP2013227979 A5 JP 2013227979A5 JP 2013090841 A JP2013090841 A JP 2013090841A JP 2013090841 A JP2013090841 A JP 2013090841A JP 2013227979 A5 JP2013227979 A5 JP 2013227979A5
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JP
Japan
Prior art keywords
microchannels
shroud
turbine
shroud component
cooling assembly
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
JP2013090841A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013227979A (ja
JP6216146B2 (ja
Filing date
Publication date
Priority claimed from US13/456,407 external-priority patent/US9127549B2/en
Application filed filed Critical
Publication of JP2013227979A publication Critical patent/JP2013227979A/ja
Publication of JP2013227979A5 publication Critical patent/JP2013227979A5/ja
Application granted granted Critical
Publication of JP6216146B2 publication Critical patent/JP6216146B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013090841A 2012-04-26 2013-04-24 ガスタービンシステムのタービンシュラウド組立体 Active JP6216146B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/456,407 2012-04-26
US13/456,407 US9127549B2 (en) 2012-04-26 2012-04-26 Turbine shroud cooling assembly for a gas turbine system

Publications (3)

Publication Number Publication Date
JP2013227979A JP2013227979A (ja) 2013-11-07
JP2013227979A5 true JP2013227979A5 (enExample) 2016-06-09
JP6216146B2 JP6216146B2 (ja) 2017-10-18

Family

ID=48182814

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013090841A Active JP6216146B2 (ja) 2012-04-26 2013-04-24 ガスタービンシステムのタービンシュラウド組立体

Country Status (5)

Country Link
US (1) US9127549B2 (enExample)
EP (1) EP2657451B1 (enExample)
JP (1) JP6216146B2 (enExample)
CN (1) CN103375202B (enExample)
RU (1) RU2638099C2 (enExample)

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US20150198063A1 (en) * 2014-01-14 2015-07-16 Alstom Technology Ltd Cooled stator heat shield
US9757936B2 (en) 2014-12-29 2017-09-12 General Electric Company Hot gas path component
US10309252B2 (en) 2015-12-16 2019-06-04 General Electric Company System and method for cooling turbine shroud trailing edge
US10378380B2 (en) 2015-12-16 2019-08-13 General Electric Company Segmented micro-channel for improved flow
US10221719B2 (en) 2015-12-16 2019-03-05 General Electric Company System and method for cooling turbine shroud
US10519861B2 (en) * 2016-11-04 2019-12-31 General Electric Company Transition manifolds for cooling channel connections in cooled structures
US10634353B2 (en) 2017-01-12 2020-04-28 General Electric Company Fuel nozzle assembly with micro channel cooling
US10876407B2 (en) * 2017-02-16 2020-12-29 General Electric Company Thermal structure for outer diameter mounted turbine blades
US10436041B2 (en) 2017-04-07 2019-10-08 General Electric Company Shroud assembly for turbine systems
CN111502774B (zh) * 2020-04-23 2024-08-09 中国核动力研究设计院 一种水冷式超临界二氧化碳透平干气密封装置
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
EP4105450A1 (en) 2021-06-18 2022-12-21 Raytheon Technologies Corporation Passive clearance control (apcc) system produced by field assisted sintering technology (fast)
EP4105449A1 (en) * 2021-06-18 2022-12-21 Raytheon Technologies Corporation Hybrid bonded configuration for blade outer airseal (boas)
EP4105440A1 (en) 2021-06-18 2022-12-21 Raytheon Technologies Corporation Hybrid superalloy article and method of manufacture thereof
GB202212532D0 (en) 2022-08-30 2022-10-12 Rolls Royce Plc Turbine shroud segment and its manufacture

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