JP2014109274A5 - - Google Patents

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Publication number
JP2014109274A5
JP2014109274A5 JP2013244508A JP2013244508A JP2014109274A5 JP 2014109274 A5 JP2014109274 A5 JP 2014109274A5 JP 2013244508 A JP2013244508 A JP 2013244508A JP 2013244508 A JP2013244508 A JP 2013244508A JP 2014109274 A5 JP2014109274 A5 JP 2014109274A5
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JP
Japan
Prior art keywords
cooling holes
adjacent cooling
mask elements
edge
component
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
JP2013244508A
Other languages
English (en)
Japanese (ja)
Other versions
JP6334145B2 (ja
JP2014109274A (ja
Filing date
Publication date
Priority claimed from US13/693,269 external-priority patent/US9181809B2/en
Application filed filed Critical
Publication of JP2014109274A publication Critical patent/JP2014109274A/ja
Publication of JP2014109274A5 publication Critical patent/JP2014109274A5/ja
Application granted granted Critical
Publication of JP6334145B2 publication Critical patent/JP6334145B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2013244508A 2012-12-04 2013-11-27 被覆されたガスタービン構成要素を用意する方法 Active JP6334145B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/693,269 US9181809B2 (en) 2012-12-04 2012-12-04 Coated article
US13/693,269 2012-12-04

Publications (3)

Publication Number Publication Date
JP2014109274A JP2014109274A (ja) 2014-06-12
JP2014109274A5 true JP2014109274A5 (enExample) 2017-01-12
JP6334145B2 JP6334145B2 (ja) 2018-05-30

Family

ID=49679358

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2013244508A Active JP6334145B2 (ja) 2012-12-04 2013-11-27 被覆されたガスタービン構成要素を用意する方法

Country Status (4)

Country Link
US (1) US9181809B2 (enExample)
EP (1) EP2740899B1 (enExample)
JP (1) JP6334145B2 (enExample)
PL (1) PL2740899T3 (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201419327D0 (en) 2014-10-30 2014-12-17 Rolls Royce Plc A cooled component
US10895157B2 (en) 2017-04-24 2021-01-19 Honeywell International Inc. Gas turbine engine components with air-cooling features, and related methods of manufacturing the same
US10717101B2 (en) 2018-02-16 2020-07-21 General Electric Company Method for making cooling assembly for a turbomachine part
US10760889B2 (en) 2018-09-12 2020-09-01 United Technologies Corporation Fan blade masking/coating check inspection tool
CN109433500B (zh) * 2018-11-08 2020-08-18 宁波雷奥自动化设备有限公司 流水线上的零件涂油装置及涂油方法
US11225707B2 (en) 2019-08-13 2022-01-18 General Electric Company Protective shields for improved coating of turbine component cooling features
US11174738B1 (en) * 2020-05-06 2021-11-16 General Electric Company Sacrificial plug system
US11585224B2 (en) 2020-08-07 2023-02-21 General Electric Company Gas turbine engines and methods associated therewith

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS61152702U (enExample) * 1985-03-13 1986-09-20
JPH04236757A (ja) * 1991-01-17 1992-08-25 Mitsubishi Heavy Ind Ltd タービン翼のマスキング方法
US5565035A (en) 1996-03-14 1996-10-15 United Technologies Corporation Fixture for masking a portion of an airfoil during application of a coating
US5902647A (en) 1996-12-03 1999-05-11 General Electric Company Method for protecting passage holes in a metal-based substrate from becoming obstructed, and related compositions
US5985122A (en) 1997-09-26 1999-11-16 General Electric Company Method for preventing plating of material in surface openings of turbine airfoils
US6234755B1 (en) 1999-10-04 2001-05-22 General Electric Company Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture
EP1275747B1 (de) * 2001-07-11 2011-02-23 Alstom Technology Ltd Verfahren zur Beschichtung eines Hochtemperatur-beständigen Bauteils mit einer thermischen Schutzschicht und Hochtemperatur-beständiges Bauteil
JP2003306760A (ja) * 2002-04-17 2003-10-31 Mitsubishi Heavy Ind Ltd マスキングピン、高温部材のコーティング方法
EP1365039A1 (en) * 2002-05-24 2003-11-26 ALSTOM (Switzerland) Ltd Process of masking colling holes of a gas turbine component
WO2004013368A1 (ja) 2002-08-02 2004-02-12 Mitsubishi Heavy Industries, Ltd. 遮熱皮膜施工方法、マスキングピン及び燃焼器尾筒
US20040265488A1 (en) * 2003-06-30 2004-12-30 General Electric Company Method for forming a flow director on a hot gas path component
US7510375B2 (en) 2005-01-04 2009-03-31 United Technologies Corporation Method of coating and a shield for a component
US7553534B2 (en) * 2006-08-29 2009-06-30 General Electric Company Film cooled slotted wall and method of making the same
JP5271688B2 (ja) * 2008-12-17 2013-08-21 三菱重工業株式会社 ガスタービン用部材
US20110116912A1 (en) 2009-11-13 2011-05-19 Mccall Thomas Zoned discontinuous coating for high pressure turbine component
US8608443B2 (en) * 2010-06-11 2013-12-17 Siemens Energy, Inc. Film cooled component wall in a turbine engine
US9028207B2 (en) 2010-09-23 2015-05-12 Siemens Energy, Inc. Cooled component wall in a turbine engine
JP5517163B2 (ja) * 2010-10-07 2014-06-11 株式会社日立製作所 タービン翼の冷却孔加工方法
US8727727B2 (en) * 2010-12-10 2014-05-20 General Electric Company Components with cooling channels and methods of manufacture
US20120164376A1 (en) * 2010-12-23 2012-06-28 General Electric Company Method of modifying a substrate for passage hole formation therein, and related articles
US20130045106A1 (en) * 2011-08-15 2013-02-21 General Electric Company Angled trench diffuser

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