ES2160878T3 - Procedimiento para aplicar un revestimiento en un componente de un motor de una turbina de gas. - Google Patents

Procedimiento para aplicar un revestimiento en un componente de un motor de una turbina de gas.

Info

Publication number
ES2160878T3
ES2160878T3 ES97117725T ES97117725T ES2160878T3 ES 2160878 T3 ES2160878 T3 ES 2160878T3 ES 97117725 T ES97117725 T ES 97117725T ES 97117725 T ES97117725 T ES 97117725T ES 2160878 T3 ES2160878 T3 ES 2160878T3
Authority
ES
Spain
Prior art keywords
component
coating
gas turbine
turbine engine
procedure
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.)
Expired - Lifetime
Application number
ES97117725T
Other languages
English (en)
Inventor
David Kang
Kevin Updegrove
Frank Goodwater
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Chromalloy Gas Turbine Corp
Original Assignee
Chromalloy Gas Turbine Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Chromalloy Gas Turbine Corp filed Critical Chromalloy Gas Turbine Corp
Application granted granted Critical
Publication of ES2160878T3 publication Critical patent/ES2160878T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
    • C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
    • C25D5/00—Electroplating characterised by the process; Pretreatment or after-treatment of workpieces
    • C25D5/02—Electroplating of selected surface areas
    • C25D5/022—Electroplating of selected surface areas using masking means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
    • B23P2700/06—Cooling passages of turbine components, e.g. unblocking or preventing blocking of cooling passages of turbine components

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Engineering & Computer Science (AREA)
  • Electroplating Methods And Accessories (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Chemically Coating (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Details Or Accessories Of Spraying Plant Or Apparatus (AREA)
  • Supercharger (AREA)

Abstract

SE ESTABLECE UN PROCESO PARA APLICAR UN REVESTIMIENTO POR GALVANOPLASTIA A UN COMPONENTE DE UN MOTOR DE TURBINA A GAS SIN PERJUDICAR LA CIRCULACION DE AIRE POR LOS ORIFICIOS DE REFRIGERACION INYECTANDO UN PRODUCTO DE ENMASCARAMIENTO EN EL CONDUCTO DE REFRIGERACION PARA LLENAR LOS ORIFICIOS DE REFRIGERACION CON EL PRODUCTO DE ENMASCARAMIENTO, APLICANDO UN REVESTIMIENTO POR GALVANOPLASTIA A LA SUPERFICIE EXTERNA DEL COMPONENTE Y ELIMINANDO DESPUES EL PRODUCTO DE ENMASCARAMIENTO DEL COMPONENTE.
ES97117725T 1996-10-16 1997-10-14 Procedimiento para aplicar un revestimiento en un componente de un motor de una turbina de gas. Expired - Lifetime ES2160878T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/733,028 US5800695A (en) 1996-10-16 1996-10-16 Plating turbine engine components

Publications (1)

Publication Number Publication Date
ES2160878T3 true ES2160878T3 (es) 2001-11-16

Family

ID=24945921

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97117725T Expired - Lifetime ES2160878T3 (es) 1996-10-16 1997-10-14 Procedimiento para aplicar un revestimiento en un componente de un motor de una turbina de gas.

Country Status (10)

Country Link
US (1) US5800695A (es)
EP (1) EP0843026B1 (es)
JP (1) JP3959161B2 (es)
AT (1) ATE204036T1 (es)
AU (1) AU726305B2 (es)
CA (1) CA2217843C (es)
DE (1) DE69706023T2 (es)
DK (1) DK0843026T3 (es)
ES (1) ES2160878T3 (es)
PT (1) PT843026E (es)

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EP1076107B1 (en) * 1999-08-09 2003-10-08 ALSTOM (Switzerland) Ltd Process of plugging cooling holes of a gas turbine component
DE69911947T2 (de) * 1999-08-09 2004-11-04 Alstom Technology Ltd Verfahren zum Abdecken von Kühlungsöffnungen eines Gasturbinenbauteils
US6296705B1 (en) * 1999-12-15 2001-10-02 United Technologies Corporation Masking fixture and method
DE60042061D1 (de) 2000-05-31 2009-06-04 Alstom Technology Ltd Verfahren zum Einstellen der Grösse von Kühllöchern eines Bauteils einer Gasturbine
US6617003B1 (en) 2000-11-06 2003-09-09 General Electric Company Directly cooled thermal barrier coating system
US6502303B2 (en) * 2001-05-07 2003-01-07 Chromalloy Gas Turbine Corporation Method of repairing a turbine blade tip
US6951623B2 (en) * 2001-11-02 2005-10-04 The Boeing Company Radiation curable maskant and line sealer for protecting metal substrates
JP2003172102A (ja) * 2001-12-07 2003-06-20 Ishikawajima Harima Heavy Ind Co Ltd タービン翼とその製造方法とそのサーマルバリアコート剥離判断方法
EP1327483A1 (de) * 2002-01-15 2003-07-16 Siemens Aktiengesellschaft Verfahren zum Beschichten von einem Substrat mit Löchern
EP1350860A1 (en) * 2002-04-04 2003-10-08 ALSTOM (Switzerland) Ltd Process of masking cooling holes of a gas turbine component
EP1365039A1 (en) * 2002-05-24 2003-11-26 ALSTOM (Switzerland) Ltd Process of masking colling holes of a gas turbine component
JP4031794B2 (ja) * 2002-08-02 2008-01-09 三菱重工業株式会社 遮熱皮膜施工方法，マスキングピン及び燃焼器尾筒
US6884476B2 (en) * 2002-10-28 2005-04-26 General Electric Company Ceramic masking material and application method for protecting turbine airfoil component surfaces during vapor phase aluminiding
US6875476B2 (en) * 2003-01-15 2005-04-05 General Electric Company Methods and apparatus for manufacturing turbine engine components
US6977233B2 (en) * 2003-07-15 2005-12-20 Honeywell International, Inc. Sintered silicon nitride
US20060131789A1 (en) * 2004-12-20 2006-06-22 Hua Sim M Method for recycling coating maskant
DE102005015153B4 (de) * 2005-03-31 2017-03-09 General Electric Technology Gmbh Verfahren zum Reparieren oder Erneuern von Kühllöchern einer beschichteten Komponente und beschichtete Komponente mit Kühllöchern einer Gasturbine
US20060275624A1 (en) * 2005-06-07 2006-12-07 General Electric Company Method and apparatus for airfoil electroplating, and airfoil
US8844090B2 (en) * 2005-06-17 2014-09-30 United Technologies Corporation Tool for filling voids in turbine vanes and other articles
US20070128363A1 (en) * 2005-12-07 2007-06-07 Honeywell International, Inc. Platinum plated powder metallurgy turbine disk for elevated temperature service
DE102006010927A1 (de) * 2006-03-09 2007-09-13 Mtu Aero Engines Gmbh Gasturbinenbauteil sowie Verfahren zur Bearbeitung von Gasturbinenbauteilen im Rahmen der Herstellung oder Instandsetzung dieser Gasturbinenbauteile
DE102006010929B4 (de) * 2006-03-09 2013-10-02 Mtu Aero Engines Gmbh Beschichtungsverfahren
US20080131612A1 (en) * 2006-11-30 2008-06-05 Honeywell International, Inc. Method for making an environment-resistant and thermal barrier coating system on a component
JP5192687B2 (ja) * 2006-12-25 2013-05-08 三菱重工業株式会社 熱処理方法
DE102007008011A1 (de) * 2007-02-15 2008-08-21 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Ausbildung einer Aluminium-Diffusionsschicht zum Oxidationsschutz
US7766617B1 (en) * 2007-03-06 2010-08-03 Florida Turbine Technologies, Inc. Transpiration cooled turbine airfoil
JP5026922B2 (ja) * 2007-10-30 2012-09-19 トヨタ自動車株式会社 多孔質体表面のめっき方法
EP2078578A1 (de) * 2008-01-10 2009-07-15 Siemens Aktiengesellschaft Belotung von Löchern, Verfahren zum Beschichten und Lotgutstäbchen
US20090324841A1 (en) * 2008-05-09 2009-12-31 Siemens Power Generation, Inc. Method of restoring near-wall cooled turbine components
US9206499B2 (en) 2010-08-30 2015-12-08 United Technologies Corporation Minimizing blockage of holes in turbine engine components
DE102011011200A1 (de) 2011-02-14 2012-08-16 Dechema Gesellschaft Für Chemische Technik Und Biotechnologie E.V. Verfahren zur Erzeugung von Diffusionsschichten ohne Aktivator über Metallfolien
US8636890B2 (en) 2011-09-23 2014-01-28 General Electric Company Method for refurbishing PtAl coating to turbine hardware removed from service
US8985049B2 (en) 2011-12-29 2015-03-24 General Electric Company Pressure maskers and pressure masking systems
US9664111B2 (en) * 2012-12-19 2017-05-30 United Technologies Corporation Closure of cooling holes with a filing agent
US9884343B2 (en) 2012-12-20 2018-02-06 United Technologies Corporation Closure of cooling holes with a filling agent
US9126232B2 (en) 2013-02-21 2015-09-08 Pratt & Whitney Canada Corp. Method of protecting a surface
US20140251951A1 (en) * 2013-03-11 2014-09-11 General Electric Company Pressure masking systems and methods for using same in treating techniques
US9840918B2 (en) * 2013-04-26 2017-12-12 Howmet Corporation Internal airfoil component electroplating
DE102013224103A1 (de) * 2013-11-26 2015-06-11 Siemens Aktiengesellschaft Sicherer Stopfenverschluss durch Diffusionsbeschichtung und Verfahren
FR3013996B1 (fr) 2013-12-02 2017-04-28 Office National Detudes Et De Rech Aerospatiales Onera Procede de reparation locale de barrieres thermiques
FR3014115B1 (fr) 2013-12-02 2017-04-28 Office National Detudes Et De Rech Aerospatiales Onera Procede et systeme de depot d'oxyde sur un composant poreux
EP3927492A1 (en) * 2019-02-22 2021-12-29 Dymax Corporation Method of filling cooling holes in an airfoil component

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US3772161A (en) * 1972-01-03 1973-11-13 Borg Warner Method of selectively electroplating thermoplastic substrates using a strippable coating mask
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US4743462A (en) * 1986-07-14 1988-05-10 United Technologies Corporation Method for preventing closure of cooling holes in hollow, air cooled turbine engine components during application of a plasma spray coating
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US5441767A (en) * 1994-01-26 1995-08-15 United Technologies Corporation Pack coating process for articles containing small passageways

Also Published As

Publication number Publication date
EP0843026B1 (en) 2001-08-08
DK0843026T3 (da) 2001-10-08
AU4095197A (en) 1998-04-23
JP3959161B2 (ja) 2007-08-15
AU726305B2 (en) 2000-11-02
PT843026E (pt) 2001-12-28
DE69706023T2 (de) 2002-04-18
CA2217843C (en) 2006-07-11
DE69706023D1 (de) 2001-09-13
EP0843026A1 (en) 1998-05-20
ATE204036T1 (de) 2001-08-15
MX9707942A (es) 1998-08-30
US5800695A (en) 1998-09-01
CA2217843A1 (en) 1998-04-16
JPH10183363A (ja) 1998-07-14

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