JP2012184763A5 - - Google Patents

Download PDF

Info

Publication number
JP2012184763A5
JP2012184763A5 JP2012044910A JP2012044910A JP2012184763A5 JP 2012184763 A5 JP2012184763 A5 JP 2012184763A5 JP 2012044910 A JP2012044910 A JP 2012044910A JP 2012044910 A JP2012044910 A JP 2012044910A JP 2012184763 A5 JP2012184763 A5 JP 2012184763A5
Authority
JP
Japan
Prior art keywords
layer
cooling channel
braze filler
layers
filler metal
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.)
Pending
Application number
JP2012044910A
Other languages
English (en)
Japanese (ja)
Other versions
JP2012184763A (ja
Filing date
Publication date
Priority claimed from US13/042,167 external-priority patent/US8870523B2/en
Application filed filed Critical
Publication of JP2012184763A publication Critical patent/JP2012184763A/ja
Publication of JP2012184763A5 publication Critical patent/JP2012184763A5/ja
Pending legal-status Critical Current

Links

JP2012044910A 2011-03-07 2012-03-01 高温ガス経路部品及び高温ガス経路タービン部品を製造する方法 Pending JP2012184763A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/042,167 2011-03-07
US13/042,167 US8870523B2 (en) 2011-03-07 2011-03-07 Method for manufacturing a hot gas path component and hot gas path turbine component

Publications (2)

Publication Number Publication Date
JP2012184763A JP2012184763A (ja) 2012-09-27
JP2012184763A5 true JP2012184763A5 (cg-RX-API-DMAC7.html) 2015-04-16

Family

ID=45808283

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2012044910A Pending JP2012184763A (ja) 2011-03-07 2012-03-01 高温ガス経路部品及び高温ガス経路タービン部品を製造する方法

Country Status (4)

Country Link
US (1) US8870523B2 (cg-RX-API-DMAC7.html)
EP (1) EP2497906B1 (cg-RX-API-DMAC7.html)
JP (1) JP2012184763A (cg-RX-API-DMAC7.html)
CN (2) CN105649688A (cg-RX-API-DMAC7.html)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140170433A1 (en) * 2012-12-19 2014-06-19 General Electric Company Components with near-surface cooling microchannels and methods for providing the same
US9828872B2 (en) * 2013-02-07 2017-11-28 General Electric Company Cooling structure for turbomachine
US9713838B2 (en) * 2013-05-14 2017-07-25 General Electric Company Static core tie rods
CN103700775B (zh) 2013-12-31 2017-08-25 北京维信诺科技有限公司 一种有机电致发光器件及其制备方法
US9757936B2 (en) * 2014-12-29 2017-09-12 General Electric Company Hot gas path component
US10309252B2 (en) 2015-12-16 2019-06-04 General Electric Company System and method for cooling turbine shroud trailing edge
US10378380B2 (en) 2015-12-16 2019-08-13 General Electric Company Segmented micro-channel for improved flow
US10767501B2 (en) * 2016-04-21 2020-09-08 General Electric Company Article, component, and method of making a component
US10519861B2 (en) 2016-11-04 2019-12-31 General Electric Company Transition manifolds for cooling channel connections in cooled structures
CN113931702B (zh) * 2020-06-29 2024-09-06 中国航发商用航空发动机有限责任公司 燃气轮机、导向叶片及其导叶缘板

Family Cites Families (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3644060A (en) * 1970-06-05 1972-02-22 John K Bryan Cooled airfoil
CA1110173A (en) * 1978-03-10 1981-10-06 Rodger O. Anderson Liquid cooled gas turbine buckets
JPH0667551B2 (ja) * 1987-05-13 1994-08-31 三菱重工業株式会社 積層耐熱合金板の製作方法
JP2548733B2 (ja) * 1987-07-07 1996-10-30 三菱重工業株式会社 ガスタ−ビン燃焼器の拡散熱処理方法
JPH0639885B2 (ja) 1988-03-14 1994-05-25 株式会社日立製作所 ガスタービン用シュラウド及びガスタービン
US5169287A (en) 1991-05-20 1992-12-08 General Electric Company Shroud cooling assembly for gas turbine engine
JPH0727335A (ja) * 1993-07-09 1995-01-27 Hitachi Ltd ガスタービン用燃焼室ライナーの製作方法
US5516260A (en) * 1994-10-07 1996-05-14 General Electric Company Bonded turbine airfuel with floating wall cooling insert
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
JP3202636B2 (ja) * 1997-02-12 2001-08-27 東北電力株式会社 蒸気冷却燃焼器の冷却壁構造
US6223524B1 (en) 1998-01-23 2001-05-01 Diversitech, Inc. Shrouds for gas turbine engines and methods for making the same
JP3702171B2 (ja) * 2000-11-27 2005-10-05 三菱重工業株式会社 積層耐熱合金板の製作方法
US6528118B2 (en) 2001-02-06 2003-03-04 General Electric Company Process for creating structured porosity in thermal barrier coating
US6551061B2 (en) * 2001-03-27 2003-04-22 General Electric Company Process for forming micro cooling channels inside a thermal barrier coating system without masking material
US6461108B1 (en) 2001-03-27 2002-10-08 General Electric Company Cooled thermal barrier coating on a turbine blade tip
US6565990B2 (en) * 2001-05-30 2003-05-20 General Electric Company Bonded niobium silicide and molybdenum silicide composite articles and method of manufacture
US6726444B2 (en) * 2002-03-18 2004-04-27 General Electric Company Hybrid high temperature articles and method of making
US6679680B2 (en) 2002-03-25 2004-01-20 General Electric Company Built-up gas turbine component and its fabrication
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
US6899518B2 (en) 2002-12-23 2005-05-31 Pratt & Whitney Canada Corp. Turbine shroud segment apparatus for reusing cooling air
FR2850742B1 (fr) * 2003-01-30 2005-09-23 Snecma Propulsion Solide Panneau de refroidissement actif en materiau composite thermostructural et procede pour sa fabrication
US20050044857A1 (en) * 2003-08-26 2005-03-03 Boris Glezer Combustor of a gas turbine engine
US7487641B2 (en) 2003-11-14 2009-02-10 The Trustees Of Columbia University In The City Of New York Microfabricated rankine cycle steam turbine for power generation and methods of making the same
US7063503B2 (en) 2004-04-15 2006-06-20 Pratt & Whitney Canada Corp. Turbine shroud cooling system
US7010921B2 (en) * 2004-06-01 2006-03-14 General Electric Company Method and apparatus for cooling combustor liner and transition piece of a gas turbine
US7284954B2 (en) 2005-02-17 2007-10-23 Parker David G Shroud block with enhanced cooling
US7600967B2 (en) 2005-07-30 2009-10-13 United Technologies Corporation Stator assembly, module and method for forming a rotary machine
DE102005055984A1 (de) 2005-11-24 2007-05-31 Mtu Aero Engines Gmbh Verfahren zur Reparatur eines Mantelringsegments einer Gasturbine
US7653994B2 (en) 2006-03-22 2010-02-02 General Electric Company Repair of HPT shrouds with sintered preforms
US7740442B2 (en) 2006-11-30 2010-06-22 General Electric Company Methods and system for cooling integral turbine nozzle and shroud assemblies
US7900458B2 (en) 2007-05-29 2011-03-08 Siemens Energy, Inc. Turbine airfoils with near surface cooling passages and method of making same
US20090053045A1 (en) 2007-08-22 2009-02-26 General Electric Company Turbine Shroud for Gas Turbine Assemblies and Processes for Forming the Shroud
ATE502720T1 (de) 2008-04-09 2011-04-15 Alstom Technology Ltd VERFAHREN ZUR REPARATUR DER HEIßGASKOMPONENTE EINER GASTURBINE
US20100186415A1 (en) * 2009-01-23 2010-07-29 General Electric Company Turbulated aft-end liner assembly and related cooling method
JP5535495B2 (ja) * 2009-02-25 2014-07-02 三菱重工業株式会社 積層耐熱合金板の製造方法
JP5439041B2 (ja) * 2009-06-02 2014-03-12 三菱重工業株式会社 燃焼器構成部材の製造方法、並びに、燃焼器構成部材、ガスタービン用燃焼器及びガスタービン
US8499566B2 (en) * 2010-08-12 2013-08-06 General Electric Company Combustor liner cooling system
US8684662B2 (en) 2010-09-03 2014-04-01 Siemens Energy, Inc. Ring segment with impingement and convective cooling
JP5356345B2 (ja) 2010-09-28 2013-12-04 株式会社日立製作所 ガスタービンのシュラウド構造
US8673397B2 (en) 2010-11-10 2014-03-18 General Electric Company Methods of fabricating and coating a component

Similar Documents

Publication Publication Date Title
JP2012184763A5 (cg-RX-API-DMAC7.html)
JP2014163379A5 (cg-RX-API-DMAC7.html)
EP2497906A3 (en) Method for manufacturing a hot gas path component and hot gas path turbine component
JP2011040729A5 (ja) 半導体基板の作製方法
FR2972379B1 (fr) Procede de rechargement local de piece thermomecanique endommagee et piece ainsi realisee, en particulier piece de turbine
RU2016138135A (ru) Горючий источник тепла, имеющий закрепленный на нем барьер, и способ изготовления горючего источника тепла
JP2015533685A5 (cg-RX-API-DMAC7.html)
WO2008064257A3 (en) Method for brazing and hot forming a multichannel heat exchanger, the hot forming using the heating energy of the brazing step
JP2013522662A5 (cg-RX-API-DMAC7.html)
UA111712C2 (uk) Системи і способи для обробки зливків із сплавів
JP2015532004A5 (cg-RX-API-DMAC7.html)
JP2013144634A5 (cg-RX-API-DMAC7.html)
JP2011029609A5 (ja) 半導体装置の作製方法
JP2013247036A5 (cg-RX-API-DMAC7.html)
JP2013229457A5 (cg-RX-API-DMAC7.html)
JP2011228680A5 (ja) Ｓｏｉ基板の作製方法、および半導体基板の作製方法
CN109133966A (zh) 一种层状梯度石墨膜/铝复合材料的制备方法
JP2012190865A5 (cg-RX-API-DMAC7.html)
JP2015115363A5 (cg-RX-API-DMAC7.html)
WO2012027855A3 (de) Verfahren zum herstellen von blechstapelkörpern
JP2011089173A5 (ja) 析出硬化型合金薄帯の製造装置、冷却ロール及び析出硬化型合金薄帯の製造方法
JP2015105778A5 (cg-RX-API-DMAC7.html)
BRPI0604247A (pt) protetor térmico em modo de construção tipo sanduìche
JP2012045757A5 (cg-RX-API-DMAC7.html)
EP2754723A3 (en) Method to produce a hot formed part, and part thus formed