JP2014163379A5 - - Google Patents

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Publication number
JP2014163379A5
JP2014163379A5 JP2014029031A JP2014029031A JP2014163379A5 JP 2014163379 A5 JP2014163379 A5 JP 2014163379A5 JP 2014029031 A JP2014029031 A JP 2014029031A JP 2014029031 A JP2014029031 A JP 2014029031A JP 2014163379 A5 JP2014163379 A5 JP 2014163379A5
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Japan
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relatively planar
cover member
plate
relatively
placing
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JP2014029031A
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English (en)
Japanese (ja)
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JP6283232B2 (ja
JP2014163379A (ja
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Priority claimed from US13/774,275 external-priority patent/US9015944B2/en
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Publication of JP2014163379A5 publication Critical patent/JP2014163379A5/ja
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JP2014029031A 2013-02-22 2014-02-19 マイクロチャンネル冷却構成要素を形成する方法 Active JP6283232B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/774,275 US9015944B2 (en) 2013-02-22 2013-02-22 Method of forming a microchannel cooled component
US13/774,275 2013-02-22

Publications (3)

Publication Number Publication Date
JP2014163379A JP2014163379A (ja) 2014-09-08
JP2014163379A5 true JP2014163379A5 (enExample) 2017-03-16
JP6283232B2 JP6283232B2 (ja) 2018-02-21

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JP2014029031A Active JP6283232B2 (ja) 2013-02-22 2014-02-19 マイクロチャンネル冷却構成要素を形成する方法

Country Status (4)

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US (1) US9015944B2 (enExample)
JP (1) JP6283232B2 (enExample)
CH (1) CH707663A2 (enExample)
DE (1) DE102014101976A1 (enExample)

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US20180100437A1 (en) * 2016-10-10 2018-04-12 General Electric Company Combustor igniter cooling
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US10544941B2 (en) 2016-12-07 2020-01-28 General Electric Company Fuel nozzle assembly with micro-channel cooling
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US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US12037912B2 (en) 2021-06-18 2024-07-16 Rtx Corporation Advanced passive clearance control (APCC) control ring produced by field assisted sintering technology (FAST)
EP4105440A1 (en) 2021-06-18 2022-12-21 Raytheon Technologies Corporation Hybrid superalloy article and method of manufacture thereof
EP4105449A1 (en) * 2021-06-18 2022-12-21 Raytheon Technologies Corporation Hybrid bonded configuration for blade outer airseal (boas)
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