JP2002201962A5 - - Google Patents

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Publication number
JP2002201962A5
JP2002201962A5 JP2001363608A JP2001363608A JP2002201962A5 JP 2002201962 A5 JP2002201962 A5 JP 2002201962A5 JP 2001363608 A JP2001363608 A JP 2001363608A JP 2001363608 A JP2001363608 A JP 2001363608A JP 2002201962 A5 JP2002201962 A5 JP 2002201962A5
Authority
JP
Japan
Prior art keywords
groove
component
removable material
filling
removable
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
JP2001363608A
Other languages
English (en)
Japanese (ja)
Other versions
JP4398616B2 (ja
JP2002201962A (ja
Filing date
Publication date
Priority claimed from US09/726,004 external-priority patent/US6427327B1/en
Application filed filed Critical
Publication of JP2002201962A publication Critical patent/JP2002201962A/ja
Publication of JP2002201962A5 publication Critical patent/JP2002201962A5/ja
Application granted granted Critical
Publication of JP4398616B2 publication Critical patent/JP4398616B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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JP2001363608A 2000-11-29 2001-11-29 冷却されるタービン部品を改造する方法及び改造された部品 Expired - Fee Related JP4398616B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/726,004 US6427327B1 (en) 2000-11-29 2000-11-29 Method of modifying cooled turbine components
US09/726004 2000-11-29

Publications (3)

Publication Number Publication Date
JP2002201962A JP2002201962A (ja) 2002-07-19
JP2002201962A5 true JP2002201962A5 (enExample) 2005-07-14
JP4398616B2 JP4398616B2 (ja) 2010-01-13

Family

ID=24916818

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001363608A Expired - Fee Related JP4398616B2 (ja) 2000-11-29 2001-11-29 冷却されるタービン部品を改造する方法及び改造された部品

Country Status (4)

Country Link
US (1) US6427327B1 (enExample)
EP (1) EP1211385B1 (enExample)
JP (1) JP4398616B2 (enExample)
DE (1) DE60129779T2 (enExample)

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US7220934B2 (en) * 2005-06-07 2007-05-22 United Technologies Corporation Method of producing cooling holes in highly contoured airfoils
US7540083B2 (en) 2005-09-28 2009-06-02 Honeywell International Inc. Method to modify an airfoil internal cooling circuit
US7717677B1 (en) 2007-01-31 2010-05-18 Florida Turbine Technologies, Inc. Multi-metering and diffusion transpiration cooled airfoil
US7766617B1 (en) 2007-03-06 2010-08-03 Florida Turbine Technologies, Inc. Transpiration cooled turbine airfoil
US8376706B2 (en) * 2007-09-28 2013-02-19 General Electric Company Turbine airfoil concave cooling passage using dual-swirl flow mechanism and method
US20100284800A1 (en) * 2009-05-11 2010-11-11 General Electric Company Turbine nozzle with sidewall cooling plenum
JP5578864B2 (ja) 2010-01-20 2014-08-27 三菱重工業株式会社 流路付き壁部材の補修方法
US20140271974A1 (en) * 2013-03-14 2014-09-18 Honda Motor Co., Ltd. Conforming cooling method and mold
US8673397B2 (en) 2010-11-10 2014-03-18 General Electric Company Methods of fabricating and coating a component
US9249491B2 (en) 2010-11-10 2016-02-02 General Electric Company Components with re-entrant shaped cooling channels and methods of manufacture
US8739404B2 (en) * 2010-11-23 2014-06-03 General Electric Company Turbine components with cooling features and methods of manufacturing the same
US8753071B2 (en) 2010-12-22 2014-06-17 General Electric Company Cooling channel systems for high-temperature components covered by coatings, and related processes
US8528208B2 (en) * 2011-04-11 2013-09-10 General Electric Company Methods of fabricating a coated component using multiple types of fillers
US8601691B2 (en) * 2011-04-27 2013-12-10 General Electric Company Component and methods of fabricating a coated component using multiple types of fillers
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US9249672B2 (en) 2011-09-23 2016-02-02 General Electric Company Components with cooling channels and methods of manufacture
US20130086784A1 (en) 2011-10-06 2013-04-11 General Electric Company Repair methods for cooled components
US9249670B2 (en) 2011-12-15 2016-02-02 General Electric Company Components with microchannel cooling
CH706107A1 (de) * 2012-02-17 2013-08-30 Alstom Technology Ltd Bauteil für eine thermische Maschine, insbesondere eine Gasturbine.
CH706090A1 (de) 2012-02-17 2013-08-30 Alstom Technology Ltd Verfahren zum Herstellen eines oberflächennahen Kühlkanals in einem thermisch hoch beanspruchten Bauteil sowie Bauteil mit einem solchen Kanal.
US9435208B2 (en) 2012-04-17 2016-09-06 General Electric Company Components with microchannel cooling
US9243503B2 (en) 2012-05-23 2016-01-26 General Electric Company Components with microchannel cooled platforms and fillets and methods of manufacture
DE102013109116A1 (de) 2012-08-27 2014-03-27 General Electric Company (N.D.Ges.D. Staates New York) Bauteil mit Kühlkanälen und Verfahren zur Herstellung
US8974859B2 (en) 2012-09-26 2015-03-10 General Electric Company Micro-channel coating deposition system and method for using the same
US9242294B2 (en) 2012-09-27 2016-01-26 General Electric Company Methods of forming cooling channels using backstrike protection
US9238265B2 (en) 2012-09-27 2016-01-19 General Electric Company Backstrike protection during machining of cooling features
US9200521B2 (en) 2012-10-30 2015-12-01 General Electric Company Components with micro cooled coating layer and methods of manufacture
US9562436B2 (en) 2012-10-30 2017-02-07 General Electric Company Components with micro cooled patterned coating layer and methods of manufacture
US20140126995A1 (en) * 2012-11-06 2014-05-08 General Electric Company Microchannel cooled turbine component and method of forming a microchannel cooled turbine component
US9003657B2 (en) * 2012-12-18 2015-04-14 General Electric Company Components with porous metal cooling and methods of manufacture
WO2014123841A1 (en) * 2013-02-10 2014-08-14 United Technologies Corporation Removable film for airfoil surfaces
US9278462B2 (en) 2013-11-20 2016-03-08 General Electric Company Backstrike protection during machining of cooling features
US9803939B2 (en) * 2013-11-22 2017-10-31 General Electric Company Methods for the formation and shaping of cooling channels, and related articles of manufacture
US9476306B2 (en) 2013-11-26 2016-10-25 General Electric Company Components with multi-layered cooling features and methods of manufacture
US20160312654A1 (en) * 2013-12-19 2016-10-27 United Technologies Corporation Turbine airfoil cooling
CN104625655A (zh) * 2015-02-14 2015-05-20 杨光华 一种曲线形液压通道的制造方法
US10815782B2 (en) 2016-06-24 2020-10-27 General Electric Company Methods for repairing airfoil trailing edges to include ejection slots therein
US10465526B2 (en) 2016-11-15 2019-11-05 Rolls-Royce Corporation Dual-wall airfoil with leading edge cooling slot
US10648341B2 (en) 2016-11-15 2020-05-12 Rolls-Royce Corporation Airfoil leading edge impingement cooling
US10450873B2 (en) 2017-07-31 2019-10-22 Rolls-Royce Corporation Airfoil edge cooling channels

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US5075966A (en) * 1990-09-04 1991-12-31 General Electric Company Method for fabricating a hollow component for a rocket engine
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US5328331A (en) * 1993-06-28 1994-07-12 General Electric Company Turbine airfoil with double shell outer wall
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