JP2013529738A5 - - Google Patents

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Publication number
JP2013529738A5
JP2013529738A5 JP2013514187A JP2013514187A JP2013529738A5 JP 2013529738 A5 JP2013529738 A5 JP 2013529738A5 JP 2013514187 A JP2013514187 A JP 2013514187A JP 2013514187 A JP2013514187 A JP 2013514187A JP 2013529738 A5 JP2013529738 A5 JP 2013529738A5
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JP
Japan
Prior art keywords
wall
side wall
sidewall
diffusion
diffusion zone
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.)
Ceased
Application number
JP2013514187A
Other languages
English (en)
Japanese (ja)
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JP2013529738A (ja
Filing date
Publication date
Priority claimed from US12/813,624 external-priority patent/US9181819B2/en
Application filed filed Critical
Publication of JP2013529738A publication Critical patent/JP2013529738A/ja
Publication of JP2013529738A5 publication Critical patent/JP2013529738A5/ja
Ceased legal-status Critical Current

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JP2013514187A 2010-06-11 2011-05-19 タービンエンジンにおける冷却用の拡散区域を有する部品壁 Ceased JP2013529738A (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/813,624 2010-06-11
US12/813,624 US9181819B2 (en) 2010-06-11 2010-06-11 Component wall having diffusion sections for cooling in a turbine engine
PCT/US2011/037084 WO2012021194A2 (en) 2010-06-11 2011-05-19 Component wall having diffusion sections for cooling in a turbine engine

Publications (2)

Publication Number Publication Date
JP2013529738A JP2013529738A (ja) 2013-07-22
JP2013529738A5 true JP2013529738A5 (enExample) 2014-05-29

Family

ID=45096355

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013514187A Ceased JP2013529738A (ja) 2010-06-11 2011-05-19 タービンエンジンにおける冷却用の拡散区域を有する部品壁

Country Status (7)

Country Link
US (1) US9181819B2 (enExample)
EP (1) EP2580431B1 (enExample)
JP (1) JP2013529738A (enExample)
KR (1) KR20130091722A (enExample)
CN (1) CN103038453A (enExample)
CA (1) CA2802153A1 (enExample)
WO (1) WO2012021194A2 (enExample)

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US9963996B2 (en) 2014-08-22 2018-05-08 Siemens Aktiengesellschaft Shroud cooling system for shrouds adjacent to airfoils within gas turbine engines
US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
WO2016068856A1 (en) * 2014-10-28 2016-05-06 Siemens Aktiengesellschaft Cooling passage arrangement for turbine engine airfoils
US10100659B2 (en) 2014-12-16 2018-10-16 Rolls-Royce North American Technologies Inc. Hanger system for a turbine engine component
US10392947B2 (en) 2015-07-13 2019-08-27 General Electric Company Compositions and methods of attachment of thick environmental barrier coatings on CMC components
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US11149646B2 (en) 2015-09-02 2021-10-19 General Electric Company Piston ring assembly for a turbine engine
US10197278B2 (en) 2015-09-02 2019-02-05 General Electric Company Combustor assembly for a turbine engine
US10168051B2 (en) 2015-09-02 2019-01-01 General Electric Company Combustor assembly for a turbine engine
US9976746B2 (en) 2015-09-02 2018-05-22 General Electric Company Combustor assembly for a turbine engine
US10563867B2 (en) 2015-09-30 2020-02-18 General Electric Company CMC articles having small complex features for advanced film cooling
CN105401983B (zh) * 2015-12-24 2017-04-12 河北工业大学 一种提高组件外部冷却效果的上游结构
US10605091B2 (en) * 2016-06-28 2020-03-31 General Electric Company Airfoil with cast features and method of manufacture
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US20180266687A1 (en) 2017-03-16 2018-09-20 General Electric Company Reducing film scrubbing in a combustor
EP3450682A1 (en) 2017-08-30 2019-03-06 Siemens Aktiengesellschaft Wall of a hot gas component and corresponding hot gas component
US11402097B2 (en) 2018-01-03 2022-08-02 General Electric Company Combustor assembly for a turbine engine
US10933481B2 (en) 2018-01-05 2021-03-02 General Electric Company Method of forming cooling passage for turbine component with cap element
US10612391B2 (en) 2018-01-05 2020-04-07 General Electric Company Two portion cooling passage for airfoil
US10913091B2 (en) * 2018-05-14 2021-02-09 The Boeing Company Templates and methods for controlling application of materials around protuberances
US11034061B2 (en) 2018-05-14 2021-06-15 The Boeing Company Methods for applying materials around protuberances
US11225707B2 (en) 2019-08-13 2022-01-18 General Electric Company Protective shields for improved coating of turbine component cooling features
US11274559B2 (en) * 2020-01-15 2022-03-15 Raytheon Technologies Corporation Turbine blade tip dirt removal feature
CN112282857B (zh) * 2020-10-26 2021-09-28 上海交通大学 一种气膜冷却孔型结构

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