JP2015017609A5 - - Google Patents

Download PDF

Info

Publication number
JP2015017609A5
JP2015017609A5 JP2014138207A JP2014138207A JP2015017609A5 JP 2015017609 A5 JP2015017609 A5 JP 2015017609A5 JP 2014138207 A JP2014138207 A JP 2014138207A JP 2014138207 A JP2014138207 A JP 2014138207A JP 2015017609 A5 JP2015017609 A5 JP 2015017609A5
Authority
JP
Japan
Prior art keywords
turbine component
coupled
cover
angled
component according
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
JP2014138207A
Other languages
English (en)
Japanese (ja)
Other versions
JP2015017609A (ja
JP6496499B2 (ja
Filing date
Publication date
Priority claimed from US13/940,806 external-priority patent/US9394796B2/en
Application filed filed Critical
Publication of JP2015017609A publication Critical patent/JP2015017609A/ja
Publication of JP2015017609A5 publication Critical patent/JP2015017609A5/ja
Application granted granted Critical
Publication of JP6496499B2 publication Critical patent/JP6496499B2/ja
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

JP2014138207A 2013-07-12 2014-07-04 タービンコンポーネントおよびそれを組立てる方法 Active JP6496499B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/940,806 US9394796B2 (en) 2013-07-12 2013-07-12 Turbine component and methods of assembling the same
US13/940,806 2013-07-12

Publications (3)

Publication Number Publication Date
JP2015017609A JP2015017609A (ja) 2015-01-29
JP2015017609A5 true JP2015017609A5 (enExample) 2017-08-03
JP6496499B2 JP6496499B2 (ja) 2019-04-03

Family

ID=52107472

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014138207A Active JP6496499B2 (ja) 2013-07-12 2014-07-04 タービンコンポーネントおよびそれを組立てる方法

Country Status (5)

Country Link
US (1) US9394796B2 (enExample)
JP (1) JP6496499B2 (enExample)
CN (1) CN104279006B (enExample)
CH (1) CH708318A2 (enExample)
DE (1) DE102014109182A1 (enExample)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
US9752440B2 (en) * 2015-05-29 2017-09-05 General Electric Company Turbine component having surface cooling channels and method of forming same
US10047613B2 (en) 2015-08-31 2018-08-14 General Electric Company Gas turbine components having non-uniformly applied coating and methods of assembling the same
US10030305B2 (en) * 2015-11-19 2018-07-24 General Electric Company Method to protect features during repair cycle
US10458251B2 (en) * 2016-04-15 2019-10-29 General Electric Company Airfoil cooling using non-line of sight holes
US10767501B2 (en) * 2016-04-21 2020-09-08 General Electric Company Article, component, and method of making a component
US10563294B2 (en) * 2017-03-07 2020-02-18 General Electric Company Component having active cooling and method of fabricating
US10794197B2 (en) * 2017-06-15 2020-10-06 General Electric Company Coated turbine component and method for forming a component
US10933481B2 (en) * 2018-01-05 2021-03-02 General Electric Company Method of forming cooling passage for turbine component with cap element
US10822968B2 (en) * 2018-06-08 2020-11-03 University Of Connecticut Microstructure geometry for thermal barrier coatings to mitigate CMAS attack
US11391161B2 (en) 2018-07-19 2022-07-19 General Electric Company Component for a turbine engine with a cooling hole
US11401818B2 (en) * 2018-08-06 2022-08-02 General Electric Company Turbomachine cooling trench
US11090771B2 (en) 2018-11-05 2021-08-17 Rolls-Royce Corporation Dual-walled components for a gas turbine engine
US11174736B2 (en) 2018-12-18 2021-11-16 General Electric Company Method of forming an additively manufactured component
US11566527B2 (en) 2018-12-18 2023-01-31 General Electric Company Turbine engine airfoil and method of cooling
US11499433B2 (en) 2018-12-18 2022-11-15 General Electric Company Turbine engine component and method of cooling
US11352889B2 (en) 2018-12-18 2022-06-07 General Electric Company Airfoil tip rail and method of cooling
US10767492B2 (en) 2018-12-18 2020-09-08 General Electric Company Turbine engine airfoil
US11305363B2 (en) 2019-02-11 2022-04-19 Rolls-Royce Corporation Repair of through-hole damage using braze sintered preform
US10844728B2 (en) * 2019-04-17 2020-11-24 General Electric Company Turbine engine airfoil with a trailing edge
US11585224B2 (en) 2020-08-07 2023-02-21 General Electric Company Gas turbine engines and methods associated therewith

Family Cites Families (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4664597A (en) 1985-12-23 1987-05-12 United Technologies Corporation Coolant passages with full coverage film cooling slot
US4676719A (en) 1985-12-23 1987-06-30 United Technologies Corporation Film coolant passages for cast hollow airfoils
US4672727A (en) 1985-12-23 1987-06-16 United Technologies Corporation Method of fabricating film cooling slot in a hollow airfoil
US5216808A (en) 1990-11-13 1993-06-08 General Electric Company Method for making or repairing a gas turbine engine component
US5957657A (en) 1996-02-26 1999-09-28 Mitisubishi Heavy Industries, Ltd. Method of forming a cooling air passage in a gas turbine stationary blade shroud
GB9723762D0 (en) 1997-11-12 1998-01-07 Rolls Royce Plc A method of coating a component
US6210488B1 (en) * 1998-12-30 2001-04-03 General Electric Company Method of removing a thermal barrier coating
DE69911948T2 (de) 1999-08-09 2004-11-04 Alstom Technology Ltd Verfahren zum Verschliessen von Kühlungsöffnungen eines Gasturbinebauteils
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
US6243948B1 (en) 1999-11-18 2001-06-12 General Electric Company Modification and repair of film cooling holes in gas turbine engine components
US6329015B1 (en) 2000-05-23 2001-12-11 General Electric Company Method for forming shaped holes
US20040086635A1 (en) 2002-10-30 2004-05-06 Grossklaus Warren Davis Method of repairing a stationary shroud of a gas turbine engine using laser cladding
US7363707B2 (en) 2004-06-14 2008-04-29 General Electric Company Braze repair of shroud block seal teeth in a gas turbine engine
EP1712739A1 (de) * 2005-04-12 2006-10-18 Siemens Aktiengesellschaft Bauteil mit Filmkühlloch
US7653994B2 (en) 2006-03-22 2010-02-02 General Electric Company Repair of HPT shrouds with sintered preforms
US7900458B2 (en) 2007-05-29 2011-03-08 Siemens Energy, Inc. Turbine airfoils with near surface cooling passages and method of making same
US20090142548A1 (en) * 2007-10-18 2009-06-04 David Bruce Patterson Air cooled gas turbine components and methods of manufacturing and repairing the same
CN100552189C (zh) * 2007-11-16 2009-10-21 清华大学 受热壁面冷却结构以及使用该冷却结构的燃气轮机叶片
EP2108477B1 (en) 2008-04-09 2011-03-23 Alstom Technology Ltd Gas turbine hot gas component repair method
US8087565B2 (en) * 2008-09-08 2012-01-03 General Electric Company Process of filling openings in a component
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
US20100239409A1 (en) * 2009-03-18 2010-09-23 General Electric Company Method of Using and Reconstructing a Film-Cooling Augmentation Device for a Turbine Airfoil
US8052378B2 (en) * 2009-03-18 2011-11-08 General Electric Company Film-cooling augmentation device and turbine airfoil incorporating the same
US8905713B2 (en) 2010-05-28 2014-12-09 General Electric Company Articles which include chevron film cooling holes, and related processes
US9028207B2 (en) * 2010-09-23 2015-05-12 Siemens Energy, Inc. Cooled component wall in a turbine engine
US20120087803A1 (en) 2010-10-12 2012-04-12 General Electric Company Curved film cooling holes for turbine airfoil and related method
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
US20120167389A1 (en) * 2011-01-04 2012-07-05 General Electric Company Method for providing a film cooled article
US20130045106A1 (en) * 2011-08-15 2013-02-21 General Electric Company Angled trench diffuser

Similar Documents

Publication Publication Date Title
JP2015017609A5 (enExample)
USD843008S1 (en) Fluid handling tube with cap
USD832694S1 (en) Clamp
USD863988S1 (en) Parking meter
USD742741S1 (en) Composite material for recordable media package assembly
USD724168S1 (en) Submachine gun
USD720348S1 (en) Media controller
USD708598S1 (en) Media controller
USD665481S1 (en) Fluid flow deflector
USD801400S1 (en) Creel roller guide
MX2017001387A (es) Revestimiento de hoja de afeitar.
USD775036S1 (en) Exhaust tip
MX2019002397A (es) Celda de llama compuesta hibrida.
EP3467135A4 (en) THIN STEEL PLATE AND METHOD OF MANUFACTURING THEREOF
PL3494420T3 (pl) Podłoże wyposażone w stos o właściwościach termicznych zawierające co najmniej jedną warstwę zawierającą azotek krzemowo-cyrkonowy bogaty w cyrkon, jego zastosowanie i wytwarzanie
USD743503S1 (en) Ported extension for a gun muzzle
JP2013139816A5 (enExample)
IL286084A (en) Semiconductor package having side wall plating
EP2538027A3 (en) Methods and systems for transferring heat from a transition nozzle
EP3568637A4 (en) FUEL NOZZLE ASSEMBLY WITH MICRO-CHANNEL COOLING
IL285950A (en) Semiconductor package having side wall plating
WO2015069335A3 (en) Fan blades and manufacture methods
JP2014109274A5 (enExample)
EP2741047A3 (en) Heat Exchanger with Variable Thickness Coating
JP2015090229A5 (enExample)