JPH10183363A5 - - Google Patents

Info

Publication number
JPH10183363A5
JPH10183363A5 JP1997283908A JP28390897A JPH10183363A5 JP H10183363 A5 JPH10183363 A5 JP H10183363A5 JP 1997283908 A JP1997283908 A JP 1997283908A JP 28390897 A JP28390897 A JP 28390897A JP H10183363 A5 JPH10183363 A5 JP H10183363A5
Authority
JP
Japan
Prior art keywords
component
maskant
plating
deposit
cooling holes
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
JP1997283908A
Other languages
English (en)
Japanese (ja)
Other versions
JP3959161B2 (ja
JPH10183363A (ja
Filing date
Publication date
Priority claimed from US08/733,028 external-priority patent/US5800695A/en
Application filed filed Critical
Publication of JPH10183363A publication Critical patent/JPH10183363A/ja
Publication of JPH10183363A5 publication Critical patent/JPH10183363A5/ja
Application granted granted Critical
Publication of JP3959161B2 publication Critical patent/JP3959161B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

JP28390897A 1996-10-16 1997-10-16 タービンエンジン構成部品のメッキ方法 Expired - Lifetime JP3959161B2 (ja)

Applications Claiming Priority (2)

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

Publications (3)

Publication Number Publication Date
JPH10183363A JPH10183363A (ja) 1998-07-14
JPH10183363A5 true JPH10183363A5 (enExample) 2005-06-30
JP3959161B2 JP3959161B2 (ja) 2007-08-15

Family

ID=24945921

Family Applications (1)

Application Number Title Priority Date Filing Date
JP28390897A Expired - Lifetime JP3959161B2 (ja) 1996-10-16 1997-10-16 タービンエンジン構成部品のメッキ方法

Country Status (10)

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

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5985122A (en) 1997-09-26 1999-11-16 General Electric Company Method for preventing plating of material in surface openings of turbine airfoils
US5902471A (en) * 1997-10-01 1999-05-11 United Technologies Corporation Process for selectively electroplating an airfoil
DE19859763A1 (de) 1998-12-23 2000-06-29 Abb Alstom Power Ch Ag Verfahren zum Unschädlichmachen von beim Beschichten mit einer Schutzschicht entstehenden Verengungen in den Kühllöchern von gasgekühlten Teilen
DE69911948T2 (de) 1999-08-09 2004-11-04 Alstom Technology Ltd Verfahren zum Verschliessen von Kühlungsöffnungen eines Gasturbinebauteils
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
EP1160352B1 (en) 2000-05-31 2009-04-22 ALSTOM Technology Ltd Method of adjusting the size of cooling holes of a gas turbine component
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
CN100368588C (zh) * 2002-08-02 2008-02-13 三菱重工业株式会社 热障涂层形成方法、掩蔽销以及燃烧室过渡连接件
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
ES2859572T3 (es) * 2013-04-26 2021-10-04 Howmet Corp Electrodeposición del componente del perfil alar interno
DE102013224103A1 (de) * 2013-11-26 2015-06-11 Siemens Aktiengesellschaft Sicherer Stopfenverschluss durch Diffusionsbeschichtung und Verfahren
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
FR3013996B1 (fr) 2013-12-02 2017-04-28 Office National Detudes Et De Rech Aerospatiales Onera Procede de reparation locale de barrieres thermiques
EP3927492A1 (en) * 2019-02-22 2021-12-29 Dymax Corporation Method of filling cooling holes in an airfoil component

Family Cites Families (11)

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Publication number Priority date Publication date Assignee Title
US2999771A (en) * 1958-04-17 1961-09-12 Norman I Gaynes Chrome plating and anodizing stopoff composition
NL133909C (enExample) * 1966-04-18
US3772161A (en) * 1972-01-03 1973-11-13 Borg Warner Method of selectively electroplating thermoplastic substrates using a strippable coating mask
US3749654A (en) * 1972-01-14 1973-07-31 United Aircraft Corp Method for electrolytically machining holes in hollow articles
US4089686A (en) * 1976-04-19 1978-05-16 Western Electric Company, Inc. Method of depositing a metal on a surface
US4224118A (en) * 1979-09-04 1980-09-23 General Motors Corporation Method of masking plated article with a poly(isobutyl methacrylate) and poly(vinyl toluene) containing coating
US4501776A (en) * 1982-11-01 1985-02-26 Turbine Components Corporation Methods of forming a protective diffusion layer on nickel, cobalt and iron base alloys
DE3526178C1 (de) * 1985-07-23 1986-08-14 Langguth GmbH & Co, 4400 Münster Beleimungsverfahren fuer Behaelter in Etikettiermaschinen unter Verwendung z.B. von Schmelzklebern
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
US4978558A (en) * 1988-06-10 1990-12-18 United Technologies Corporation Method for applying diffusion coating masks
US5441767A (en) * 1994-01-26 1995-08-15 United Technologies Corporation Pack coating process for articles containing small passageways

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