JP2013194667A5 - - Google Patents

Download PDF

Info

Publication number
JP2013194667A5
JP2013194667A5 JP2012064713A JP2012064713A JP2013194667A5 JP 2013194667 A5 JP2013194667 A5 JP 2013194667A5 JP 2012064713 A JP2012064713 A JP 2012064713A JP 2012064713 A JP2012064713 A JP 2012064713A JP 2013194667 A5 JP2013194667 A5 JP 2013194667A5
Authority
JP
Japan
Prior art keywords
blade
trailing edge
gas turbine
turbine cooling
coating material
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
JP2012064713A
Other languages
English (en)
Japanese (ja)
Other versions
JP2013194667A (ja
JP5661060B2 (ja
Filing date
Publication date
Application filed filed Critical
Priority to JP2012064713A priority Critical patent/JP5661060B2/ja
Priority claimed from JP2012064713A external-priority patent/JP5661060B2/ja
Publication of JP2013194667A publication Critical patent/JP2013194667A/ja
Publication of JP2013194667A5 publication Critical patent/JP2013194667A5/ja
Application granted granted Critical
Publication of JP5661060B2 publication Critical patent/JP5661060B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2012064713A 2012-03-22 2012-03-22 ガスタービン冷却翼 Active JP5661060B2 (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2012064713A JP5661060B2 (ja) 2012-03-22 2012-03-22 ガスタービン冷却翼

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2012064713A JP5661060B2 (ja) 2012-03-22 2012-03-22 ガスタービン冷却翼

Publications (3)

Publication Number Publication Date
JP2013194667A JP2013194667A (ja) 2013-09-30
JP2013194667A5 true JP2013194667A5 (enExample) 2014-04-10
JP5661060B2 JP5661060B2 (ja) 2015-01-28

Family

ID=49393929

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012064713A Active JP5661060B2 (ja) 2012-03-22 2012-03-22 ガスタービン冷却翼

Country Status (1)

Country Link
JP (1) JP5661060B2 (enExample)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10100650B2 (en) 2012-06-30 2018-10-16 General Electric Company Process for selectively producing thermal barrier coatings on turbine hardware
WO2017025995A1 (ja) * 2015-08-11 2017-02-16 株式会社 東芝 タービン翼、タービン翼の製造方法及び軸流タービン
JP6550000B2 (ja) * 2016-02-26 2019-07-24 三菱日立パワーシステムズ株式会社 タービン翼
CN114776388B (zh) * 2022-05-26 2022-09-23 中国航发四川燃气涡轮研究院 航空发动机涡轮叶片尾缘主动强化冷却结构

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7014A (en) * 1850-01-15 Folding bedstead
JPS5820902A (ja) * 1981-07-29 1983-02-07 Hitachi Ltd 熱遮へいコ−テイング冷却翼
US6733907B2 (en) * 1998-03-27 2004-05-11 Siemens Westinghouse Power Corporation Hybrid ceramic material composed of insulating and structural ceramic layers
DE502006003548D1 (de) * 2006-08-23 2009-06-04 Siemens Ag Beschichtete Turbinenschaufel
US8070454B1 (en) * 2007-12-12 2011-12-06 Florida Turbine Technologies, Inc. Turbine airfoil with trailing edge

Similar Documents

Publication Publication Date Title
WO2017080645A8 (en) Turbine clearance control coatings and method
WO2015130521A3 (en) Turbine component cooling hole within a microsurface feature that protects adjoining thermal barrier coating
RU2015124079A (ru) Сопловой сегмент для газовой турбины, покрытый покрытием mcraly и накладками тбп
JP2013194667A5 (enExample)
WO2014042720A3 (en) Gas turbine engine turbine blade airfoil profile
JP2015017609A5 (enExample)
WO2012134833A3 (en) High camber compressor rotor blade
WO2013066562A3 (en) Polarizable nanoparticles and electrorheological fluid comprising same
MX2021011642A (es) Metodo para la fabricacion de una hoja metalica con un revestimiento de znal con una centrifugacion optimizada, hoja metalica, parte y vehiculo correspondientes.
WO2014090922A3 (en) Metal powder suitable for thermal spraying
WO2014107204A3 (en) Additive manufacture of turbine component with multiple materials
HK1207888A1 (en) Coatings, coated surfaces, and methods for production thereof
WO2014065928A3 (en) Thermal barrier coating for gas turbine engine components
WO2014092833A3 (en) Gas turbine engine fan blade airfoil profile
WO2014149996A3 (en) Methods to improve hot workability of metal alloys
EP2612948A3 (en) Process for coating a turbine rotor and articles thereof
JP2011099437A5 (enExample)
JP2009286127A5 (enExample)
JP2017125837A5 (enExample)
WO2013064643A8 (de) Beschichtete, nasschemisch oxidierte aluminiumeffektpigmente, verfahren zu deren herstellung, beschichtungsmittel und beschichteter gegenstand
JP2011116638A5 (enExample)
WO2014042724A3 (en) Turbine compressor blade tip resistant to metal transfer
WO2015112240A3 (en) Rotor blade platform cooling passage
FR2971540B1 (fr) Ensemble pale-plateforme pour ecoulement supersonique
WO2015189612A3 (en) A method of coating a sheet of steel