JP2014141961A5 - - Google Patents

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Publication number
JP2014141961A5
JP2014141961A5 JP2013238395A JP2013238395A JP2014141961A5 JP 2014141961 A5 JP2014141961 A5 JP 2014141961A5 JP 2013238395 A JP2013238395 A JP 2013238395A JP 2013238395 A JP2013238395 A JP 2013238395A JP 2014141961 A5 JP2014141961 A5 JP 2014141961A5
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JP
Japan
Prior art keywords
channels
effusion
effusion plate
turbine
distal surface
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
JP2013238395A
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English (en)
Japanese (ja)
Other versions
JP6310680B2 (ja
JP2014141961A (ja
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Publication date
Priority claimed from US13/748,568 external-priority patent/US9309809B2/en
Application filed filed Critical
Publication of JP2014141961A publication Critical patent/JP2014141961A/ja
Publication of JP2014141961A5 publication Critical patent/JP2014141961A5/ja
Application granted granted Critical
Publication of JP6310680B2 publication Critical patent/JP6310680B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013238395A 2013-01-23 2013-11-19 付加製造法を用いたエフュージョンプレート Active JP6310680B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/748,568 2013-01-23
US13/748,568 US9309809B2 (en) 2013-01-23 2013-01-23 Effusion plate using additive manufacturing methods

Publications (3)

Publication Number Publication Date
JP2014141961A JP2014141961A (ja) 2014-08-07
JP2014141961A5 true JP2014141961A5 (enExample) 2016-12-22
JP6310680B2 JP6310680B2 (ja) 2018-04-11

Family

ID=51064359

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013238395A Active JP6310680B2 (ja) 2013-01-23 2013-11-19 付加製造法を用いたエフュージョンプレート

Country Status (3)

Country Link
US (1) US9309809B2 (enExample)
JP (1) JP6310680B2 (enExample)
DE (1) DE102013112939B4 (enExample)

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US10941937B2 (en) 2017-03-20 2021-03-09 Raytheon Technologies Corporation Combustor liner with gasket for gas turbine engine
US10718222B2 (en) 2017-03-27 2020-07-21 General Electric Company Diffuser-deswirler for a gas turbine engine
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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
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US12065936B2 (en) 2020-09-18 2024-08-20 Ge Avio S.R.L. Probe placement within a duct of a gas turbine engine
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
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