JP2008174838A5 - - Google Patents

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Publication number
JP2008174838A5
JP2008174838A5 JP2008006352A JP2008006352A JP2008174838A5 JP 2008174838 A5 JP2008174838 A5 JP 2008174838A5 JP 2008006352 A JP2008006352 A JP 2008006352A JP 2008006352 A JP2008006352 A JP 2008006352A JP 2008174838 A5 JP2008174838 A5 JP 2008174838A5
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JP
Japan
Prior art keywords
coating
thermal barrier
barrier coating
dvc
thermal
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.)
Ceased
Application number
JP2008006352A
Other languages
English (en)
Japanese (ja)
Other versions
JP2008174838A (ja
Filing date
Publication date
Priority claimed from US11/654,182 external-priority patent/US8007246B2/en
Application filed filed Critical
Publication of JP2008174838A publication Critical patent/JP2008174838A/ja
Publication of JP2008174838A5 publication Critical patent/JP2008174838A5/ja
Ceased legal-status Critical Current

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JP2008006352A 2007-01-17 2008-01-16 ガスタービンエンジンの被覆方法及び装置 Ceased JP2008174838A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/654,182 US8007246B2 (en) 2007-01-17 2007-01-17 Methods and apparatus for coating gas turbine engines

Publications (2)

Publication Number Publication Date
JP2008174838A JP2008174838A (ja) 2008-07-31
JP2008174838A5 true JP2008174838A5 (cg-RX-API-DMAC7.html) 2012-12-27

Family

ID=39683712

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008006352A Ceased JP2008174838A (ja) 2007-01-17 2008-01-16 ガスタービンエンジンの被覆方法及び装置

Country Status (5)

Country Link
US (1) US8007246B2 (cg-RX-API-DMAC7.html)
EP (1) EP1978210A1 (cg-RX-API-DMAC7.html)
JP (1) JP2008174838A (cg-RX-API-DMAC7.html)
KR (1) KR20080067980A (cg-RX-API-DMAC7.html)
CN (1) CN101225753A (cg-RX-API-DMAC7.html)

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US8273231B2 (en) 2007-12-21 2012-09-25 Rolls-Royce Corporation Methods of depositing coatings with γ-Ni + γ′-Ni3A1 phase constitution
US8501273B2 (en) 2008-10-02 2013-08-06 Rolls-Royce Corporation Mixture and technique for coating an internal surface of an article
US9624583B2 (en) 2009-04-01 2017-04-18 Rolls-Royce Corporation Slurry-based coating techniques for smoothing surface imperfections
US8511993B2 (en) * 2009-08-14 2013-08-20 Alstom Technology Ltd. Application of dense vertically cracked and porous thermal barrier coating to a gas turbine component
US20110086177A1 (en) * 2009-10-14 2011-04-14 WALBAR INC. Peabody Industrial Center Thermal spray method for producing vertically segmented thermal barrier coatings
US8967957B2 (en) * 2011-11-03 2015-03-03 General Electric Company Rotating airfoil component of a turbomachine
CA2882736C (en) * 2012-08-24 2021-10-26 Barson Composites Corporation Coatings for fluid energy device components
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
CA2906667C (en) 2013-03-15 2020-07-07 Rolls-Royce Corporation Slurry-based coating restoration
US9737970B2 (en) 2013-07-10 2017-08-22 United Technologies Corporation Vibratory mass media fixture with tip protector
US9840926B2 (en) 2013-07-10 2017-12-12 United Technologies Corporation Abrasive flow media fixture with end contour
US9289917B2 (en) 2013-10-01 2016-03-22 General Electric Company Method for 3-D printing a pattern for the surface of a turbine shroud
US9243511B2 (en) 2014-02-25 2016-01-26 Siemens Aktiengesellschaft Turbine abradable layer with zig zag groove pattern
WO2015130527A2 (en) 2014-02-25 2015-09-03 Siemens Aktiengesellschaft Turbine component thermal barrier coating with depth-varying material properties
US9151175B2 (en) 2014-02-25 2015-10-06 Siemens Aktiengesellschaft Turbine abradable layer with progressive wear zone multi level ridge arrays
US8939706B1 (en) 2014-02-25 2015-01-27 Siemens Energy, Inc. Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface
US10190435B2 (en) 2015-02-18 2019-01-29 Siemens Aktiengesellschaft Turbine shroud with abradable layer having ridges with holes
WO2016133982A1 (en) 2015-02-18 2016-08-25 Siemens Aktiengesellschaft Forming cooling passages in thermal barrier coated, combustion turbine superalloy components
EP3168323B1 (en) 2015-11-13 2020-01-22 General Electric Technology GmbH Power plant component
US10174412B2 (en) 2016-12-02 2019-01-08 General Electric Company Methods for forming vertically cracked thermal barrier coatings and articles including vertically cracked thermal barrier coatings
CN110080826B (zh) * 2019-05-31 2023-09-15 南京赛达机械制造有限公司 一种汽轮机叶片及其制备方法
KR20240156110A (ko) 2023-04-21 2024-10-29 터보파워텍(주) 진공주조와 3d프린팅에 의한 가스터빈 블레이드 제조방법

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US5419971A (en) * 1993-03-03 1995-05-30 General Electric Company Enhanced thermal barrier coating system
EP0688047A1 (en) * 1994-06-13 1995-12-20 Mitsubishi Materials Corporation Aluminium nitride substrate and method of producing the same
EP0705911B1 (en) * 1994-10-04 2001-12-05 General Electric Company Thermal barrier coating
US6465090B1 (en) * 1995-11-30 2002-10-15 General Electric Company Protective coating for thermal barrier coatings and coating method therefor
US6210791B1 (en) * 1995-11-30 2001-04-03 General Electric Company Article with a diffuse reflective barrier coating and a low-emissity coating thereon, and its preparation
US5683825A (en) * 1996-01-02 1997-11-04 General Electric Company Thermal barrier coating resistant to erosion and impact by particulate matter
US6306517B1 (en) * 1996-07-29 2001-10-23 General Electric Company Thermal barrier coatings having an improved columnar microstructure
US6057030A (en) * 1997-07-21 2000-05-02 Kanebo Ltd. Porous ceramic body and kiln furniture made from a porous ceramic body
US6047539A (en) * 1998-04-30 2000-04-11 General Electric Company Method of protecting gas turbine combustor components against water erosion and hot corrosion
US6165600A (en) * 1998-10-06 2000-12-26 General Electric Company Gas turbine engine component having a thermal-insulating multilayer ceramic coating
US6007919A (en) * 1998-12-22 1999-12-28 General Electric Company High temperature high band heat reflecting coating material and coated article
US6177186B1 (en) * 1999-04-30 2001-01-23 General Electric Company Heat reflective, erosion and wear resistant coating mixture, method and coated article
US6294261B1 (en) * 1999-10-01 2001-09-25 General Electric Company Method for smoothing the surface of a protective coating
US6432487B1 (en) * 2000-12-28 2002-08-13 General Electric Company Dense vertically cracked thermal barrier coating process to facilitate post-coat surface finishing
EP1484427A3 (en) * 2003-06-06 2005-10-26 General Electric Company Top coating system for industrial turbine nozzle airfoils and other hot gas path components and related method
US7368164B2 (en) * 2004-06-18 2008-05-06 General Electric Company Smooth outer coating for combustor components and coating method therefor
US8511993B2 (en) * 2009-08-14 2013-08-20 Alstom Technology Ltd. Application of dense vertically cracked and porous thermal barrier coating to a gas turbine component

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