BRPI0405191A - Método de reparo de componentes recobertos - Google Patents

Método de reparo de componentes recobertos

Info

Publication number
BRPI0405191A
BRPI0405191A BR0405191-2A BRPI0405191A BRPI0405191A BR PI0405191 A BRPI0405191 A BR PI0405191A BR PI0405191 A BRPI0405191 A BR PI0405191A BR PI0405191 A BRPI0405191 A BR PI0405191A
Authority
BR
Brazil
Prior art keywords
thickness
thermal barrier
metal base
barrier cover
engine operation
Prior art date
Application number
BR0405191-2A
Other languages
English (en)
Inventor
Joseph D Rigney
Ching-Pang Lee
Ramgopal Darolia
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BRPI0405191A publication Critical patent/BRPI0405191A/pt

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C26/00—Coating not provided for in groups C23C2/00 - C23C24/00
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/325—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with layers graded in composition or in physical properties
    • C—CHEMISTRY; METALLURGY
    • C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005—Repairing methods or devices
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/80—Repairing, retrofitting or upgrading methods
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/90—Coating; Surface treatment
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • F05D2300/501—Elasticity
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49318—Repairing or disassembling

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Inorganic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Abstract

"MéTODO DE REPARO DE COMPONENTES RECOBERTOS". Em uma forma de realização da invenção, é descrito um método de reparo de um componente recoberto, o qual tenha sido exposto à operação do motor, para restaurar as dimensões recobertas do componente e aumentar a subsequente eficiência operacional do motor. O método compreende fornecer um componente exposto à operação de um motor incluindo um substrato de base metálica. O substrato de base metálica apresenta sobre este um sistema de cobertura de barreira térmica compreendendo uma cobertura adesiva sobre o substrato de base metálica e uma cobertura de barreira térmica cerâmica de topo. A cobertura de barreira térmica cerâmica de topo apresenta uma espessura nominal t. O método ainda compreende remover o sistema de cobertura de barreira térmica, sendo que uma parte do substrato de base metálica é também removido, e determinar a espessura da base metálica removida. A parte do substrato de base metálica removida apresenta uma espessura <30>t. Uma cobertura adesiva é reaplicada ao substrato com uma espessura, a qual é aproximadamente a mesma que a espessura aplicada antes da operação do motor. O método também compreende reaplicar uma cobertura de barreira térmica cerâmica de topo até a espessura nominal de t + <30>t, sendo que <30>t compensa a parte removida do substrato de base metálica. Vantajosamente, as dimensões do componente recoberto são restauradas para aproximadamente as dimensões recobertas que antecederam o funcionamento do motor para aumentar a subsequente eficiência operacional de motor.
BR0405191-2A 2003-11-13 2004-11-12 Método de reparo de componentes recobertos BRPI0405191A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/714,213 US7078073B2 (en) 2003-11-13 2003-11-13 Method for repairing coated components

Publications (1)

Publication Number Publication Date
BRPI0405191A true BRPI0405191A (pt) 2005-07-19

Family

ID=34435695

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0405191-2A BRPI0405191A (pt) 2003-11-13 2004-11-12 Método de reparo de componentes recobertos

Country Status (6)

Country Link
US (1) US7078073B2 (pt)
EP (1) EP1531232B1 (pt)
JP (1) JP4643231B2 (pt)
BR (1) BRPI0405191A (pt)
CA (1) CA2487604C (pt)
SG (1) SG112068A1 (pt)

Families Citing this family (62)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8403037B2 (en) 2009-12-08 2013-03-26 Baker Hughes Incorporated Dissolvable tool and method
US9079246B2 (en) 2009-12-08 2015-07-14 Baker Hughes Incorporated Method of making a nanomatrix powder metal compact
US9109429B2 (en) 2002-12-08 2015-08-18 Baker Hughes Incorporated Engineered powder compact composite material
US9101978B2 (en) 2002-12-08 2015-08-11 Baker Hughes Incorporated Nanomatrix powder metal compact
US9682425B2 (en) 2009-12-08 2017-06-20 Baker Hughes Incorporated Coated metallic powder and method of making the same
FR2860741B1 (fr) * 2003-10-10 2007-04-13 Snecma Moteurs Procede de reparation de pieces metalliques notamment d'aubes de turbine de moteur a turbine a gaz
US7371426B2 (en) * 2003-11-13 2008-05-13 General Electric Company Method for repairing components using environmental bond coatings and resultant repaired components
US20070039175A1 (en) * 2005-07-19 2007-02-22 General Electric Company Methods for repairing turbine engine components
US7264538B2 (en) 2005-08-12 2007-09-04 United Technologies Corporation Method of removing a coating
DE102005049249B4 (de) * 2005-10-14 2018-03-29 MTU Aero Engines AG Verfahren zur Entschichtung eines Gasturbinenbauteils
TW200718805A (en) * 2005-11-07 2007-05-16 United Technologies Corp Coating methods and apparatus
US7575694B2 (en) * 2005-12-29 2009-08-18 General Electric Company Method of selectively stripping a metallic coating
EP1844892A1 (de) * 2006-04-13 2007-10-17 ALSTOM Technology Ltd Verfahren zur Laserentfernung von Beschichtenmaterialen in Kühlenlöchern eines Turbinenbauteiles
US20080160213A1 (en) * 2006-12-29 2008-07-03 Michael Patrick Maly Method for restoring or regenerating an article
US20100254820A1 (en) * 2006-12-29 2010-10-07 Michael Patrick Maly Article with restored or regenerated structure
US20080160208A1 (en) * 2006-12-29 2008-07-03 Michael Patrick Maly System and method for restoring or regenerating an article
DE102007022832A1 (de) * 2007-05-15 2008-11-20 Mtu Aero Engines Gmbh Verfahren zur Entschichtung eines Bauteils
US20080292903A1 (en) * 2007-05-25 2008-11-27 United Technologies Corporation Coated gas turbine engine component repair
US8597724B2 (en) * 2007-07-06 2013-12-03 United Technologies Corporation Corrosion protective coating through cold spray
US20090263574A1 (en) 2008-04-21 2009-10-22 Quinn Daniel E Method of restoring an article
US20100126014A1 (en) * 2008-11-26 2010-05-27 General Electric Company Repair method for tbc coated turbine components
US20100224602A1 (en) * 2009-03-06 2010-09-09 General Electric Company Method and system for removing thermal barrier coating
US10240419B2 (en) 2009-12-08 2019-03-26 Baker Hughes, A Ge Company, Llc Downhole flow inhibition tool and method of unplugging a seat
US9127515B2 (en) 2010-10-27 2015-09-08 Baker Hughes Incorporated Nanomatrix carbon composite
US9090955B2 (en) 2010-10-27 2015-07-28 Baker Hughes Incorporated Nanomatrix powder metal composite
US8631876B2 (en) 2011-04-28 2014-01-21 Baker Hughes Incorporated Method of making and using a functionally gradient composite tool
US9080098B2 (en) 2011-04-28 2015-07-14 Baker Hughes Incorporated Functionally gradient composite article
US9139928B2 (en) 2011-06-17 2015-09-22 Baker Hughes Incorporated Corrodible downhole article and method of removing the article from downhole environment
US8807955B2 (en) * 2011-06-30 2014-08-19 United Technologies Corporation Abrasive airfoil tip
US9707739B2 (en) * 2011-07-22 2017-07-18 Baker Hughes Incorporated Intermetallic metallic composite, method of manufacture thereof and articles comprising the same
US9833838B2 (en) 2011-07-29 2017-12-05 Baker Hughes, A Ge Company, Llc Method of controlling the corrosion rate of alloy particles, alloy particle with controlled corrosion rate, and articles comprising the particle
US9643250B2 (en) 2011-07-29 2017-05-09 Baker Hughes Incorporated Method of controlling the corrosion rate of alloy particles, alloy particle with controlled corrosion rate, and articles comprising the particle
US9057242B2 (en) 2011-08-05 2015-06-16 Baker Hughes Incorporated Method of controlling corrosion rate in downhole article, and downhole article having controlled corrosion rate
US8678644B2 (en) * 2011-08-16 2014-03-25 General Electric Company Hot gas path measurement
US9033055B2 (en) 2011-08-17 2015-05-19 Baker Hughes Incorporated Selectively degradable passage restriction and method
US9856547B2 (en) 2011-08-30 2018-01-02 Bakers Hughes, A Ge Company, Llc Nanostructured powder metal compact
US9090956B2 (en) 2011-08-30 2015-07-28 Baker Hughes Incorporated Aluminum alloy powder metal compact
US9109269B2 (en) 2011-08-30 2015-08-18 Baker Hughes Incorporated Magnesium alloy powder metal compact
US9643144B2 (en) 2011-09-02 2017-05-09 Baker Hughes Incorporated Method to generate and disperse nanostructures in a composite material
US9347119B2 (en) 2011-09-03 2016-05-24 Baker Hughes Incorporated Degradable high shock impedance material
US9133695B2 (en) 2011-09-03 2015-09-15 Baker Hughes Incorporated Degradable shaped charge and perforating gun system
US9010416B2 (en) 2012-01-25 2015-04-21 Baker Hughes Incorporated Tubular anchoring system and a seat for use in the same
US9068428B2 (en) 2012-02-13 2015-06-30 Baker Hughes Incorporated Selectively corrodible downhole article and method of use
EP2644824A1 (de) * 2012-03-28 2013-10-02 Siemens Aktiengesellschaft Verfahren zur Herstellung und Wiederherstellung von keramischen Wärmedämmschichten in Gasturbinen sowie dazugehörige Gasturbine
US9605508B2 (en) 2012-05-08 2017-03-28 Baker Hughes Incorporated Disintegrable and conformable metallic seal, and method of making the same
CN104704200B (zh) 2012-10-05 2016-12-14 西门子公司 用于制造第二燃气轮机的方法以及用于运行燃气轮机设施的方法
JP6004899B2 (ja) * 2012-11-06 2016-10-12 三菱日立パワーシステムズ株式会社 ガスタービン部材の表面検査方法
US9816339B2 (en) 2013-09-03 2017-11-14 Baker Hughes, A Ge Company, Llc Plug reception assembly and method of reducing restriction in a borehole
DE102013226594A1 (de) * 2013-12-19 2015-06-25 Robert Bosch Gmbh Verfahren zum Herstellen eines Laufrads und eines Läufers
US10689740B2 (en) 2014-04-18 2020-06-23 Terves, LLCq Galvanically-active in situ formed particles for controlled rate dissolving tools
US11167343B2 (en) 2014-02-21 2021-11-09 Terves, Llc Galvanically-active in situ formed particles for controlled rate dissolving tools
CA2936851A1 (en) 2014-02-21 2015-08-27 Terves, Inc. Fluid activated disintegrating metal system
US10865465B2 (en) 2017-07-27 2020-12-15 Terves, Llc Degradable metal matrix composite
US9383197B2 (en) 2014-10-13 2016-07-05 General Electric Company System and method for measuring cooling of a component
US9910026B2 (en) 2015-01-21 2018-03-06 Baker Hughes, A Ge Company, Llc High temperature tracers for downhole detection of produced water
US10378303B2 (en) 2015-03-05 2019-08-13 Baker Hughes, A Ge Company, Llc Downhole tool and method of forming the same
US10221637B2 (en) 2015-08-11 2019-03-05 Baker Hughes, A Ge Company, Llc Methods of manufacturing dissolvable tools via liquid-solid state molding
US10016810B2 (en) 2015-12-14 2018-07-10 Baker Hughes, A Ge Company, Llc Methods of manufacturing degradable tools using a galvanic carrier and tools manufactured thereof
FR3055351B1 (fr) * 2016-08-25 2019-11-08 Safran Procede de realisation d'un systeme barriere thermique sur un substrat metallique d'une piece de turbomachine
US11435461B2 (en) 2019-07-19 2022-09-06 GE Precision Healthcare LLC Method and system to prevent depoling of ultrasound transducer
US11464494B2 (en) 2019-07-19 2022-10-11 GE Precision Healthcare LLC Method and system to revert a depoling effect exhibited by an ultrasound transducer
CN115961248A (zh) * 2022-12-07 2023-04-14 中国航发动力股份有限公司 一种单晶叶片热障涂层修复方法

Family Cites Families (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3667985A (en) 1967-12-14 1972-06-06 Gen Electric Metallic surface treatment method
US3570449A (en) * 1969-03-13 1971-03-16 United Aircraft Corp Sensor system for a vacuum deposition apparatus
US4055705A (en) 1976-05-14 1977-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal barrier coating system
US4095003A (en) 1976-09-09 1978-06-13 Union Carbide Corporation Duplex coating for thermal and corrosion protection
US4209348A (en) * 1976-11-17 1980-06-24 United Technologies Corporation Heat treated superalloy single crystal article and process
US4328285A (en) 1980-07-21 1982-05-04 General Electric Company Method of coating a superalloy substrate, coating compositions, and composites obtained therefrom
US5216808A (en) 1990-11-13 1993-06-08 General Electric Company Method for making or repairing a gas turbine engine component
US5236745A (en) 1991-09-13 1993-08-17 General Electric Company Method for increasing the cyclic spallation life of a thermal barrier coating
US5897966A (en) * 1996-02-26 1999-04-27 General Electric Company High temperature alloy article with a discrete protective coating and method for making
US5898994A (en) * 1996-06-17 1999-05-04 General Electric Company Method for repairing a nickel base superalloy article
US6049978A (en) 1996-12-23 2000-04-18 Recast Airfoil Group Methods for repairing and reclassifying gas turbine engine airfoil parts
US5851409A (en) * 1996-12-24 1998-12-22 General Electric Company Method for removing an environmental coating
US5813118A (en) * 1997-06-23 1998-09-29 General Electric Company Method for repairing an air cooled turbine engine airfoil
US6544346B1 (en) * 1997-07-01 2003-04-08 General Electric Company Method for repairing a thermal barrier coating
SG71151A1 (en) * 1997-09-17 2000-03-21 Gen Electric Bond coat for a thermal barrier coating system and method therefor
US5985122A (en) 1997-09-26 1999-11-16 General Electric Company Method for preventing plating of material in surface openings of turbine airfoils
JPH11107780A (ja) * 1997-10-02 1999-04-20 Toshiba Corp ガスタービン部品のコーティングの除去方法
US6174448B1 (en) * 1998-03-02 2001-01-16 General Electric Company Method for stripping aluminum from a diffusion coating
US5972424A (en) * 1998-05-21 1999-10-26 United Technologies Corporation Repair of gas turbine engine component coated with a thermal barrier coating
EP0985745B1 (en) 1998-09-08 2006-07-12 General Electric Company Bond coat for a thermal barrier coating system
US6153313A (en) 1998-10-06 2000-11-28 General Electric Company Nickel aluminide coating and coating systems formed therewith
US6291084B1 (en) * 1998-10-06 2001-09-18 General Electric Company Nickel aluminide coating and coating systems formed therewith
US6074706A (en) * 1998-12-15 2000-06-13 General Electric Company Adhesion of a ceramic layer deposited on an article by casting features in the article surface
US6233822B1 (en) * 1998-12-22 2001-05-22 General Electric Company Repair of high pressure turbine shrouds
US6042880A (en) 1998-12-22 2000-03-28 General Electric Company Renewing a thermal barrier coating system
US6210488B1 (en) * 1998-12-30 2001-04-03 General Electric Company Method of removing a thermal barrier coating
US6344282B1 (en) * 1998-12-30 2002-02-05 General Electric Company Graded reactive element containing aluminide coatings for improved high temperature performance and method for producing
US6334907B1 (en) * 1999-06-30 2002-01-01 General Electric Company Method of controlling thickness and aluminum content of a diffusion aluminide coating
US6305077B1 (en) * 1999-11-18 2001-10-23 General Electric Company Repair of coated turbine components
US6379749B2 (en) 2000-01-20 2002-04-30 General Electric Company Method of removing ceramic coatings
US6238743B1 (en) * 2000-01-20 2001-05-29 General Electric Company Method of removing a thermal barrier coating
EP1123987A1 (en) 2000-02-11 2001-08-16 General Electric Company Repairable diffusion aluminide coatings
US6355116B1 (en) 2000-03-24 2002-03-12 General Electric Company Method for renewing diffusion coatings on superalloy substrates
JP2001303903A (ja) * 2000-04-24 2001-10-31 Toshiba Corp ガスタービン翼の補修方法
US6461746B1 (en) * 2000-04-24 2002-10-08 General Electric Company Nickel-base superalloy article with rhenium-containing protective layer, and its preparation
US6605364B1 (en) * 2000-07-18 2003-08-12 General Electric Company Coating article and method for repairing a coated surface
US6468040B1 (en) * 2000-07-24 2002-10-22 General Electric Company Environmentally resistant squealer tips and method for making
US6434823B1 (en) * 2000-10-10 2002-08-20 General Electric Company Method for repairing a coated article
US6586115B2 (en) * 2001-04-12 2003-07-01 General Electric Company Yttria-stabilized zirconia with reduced thermal conductivity
US6607789B1 (en) 2001-04-26 2003-08-19 General Electric Company Plasma sprayed thermal bond coat system
US6881452B2 (en) * 2001-07-06 2005-04-19 General Electric Company Method for improving the TBC life of a single phase platinum aluminide bond coat by preoxidation heat treatment
US7204019B2 (en) 2001-08-23 2007-04-17 United Technologies Corporation Method for repairing an apertured gas turbine component
US6599416B2 (en) * 2001-09-28 2003-07-29 General Electric Company Method and apparatus for selectively removing coatings from substrates
US6575702B2 (en) * 2001-10-22 2003-06-10 General Electric Company Airfoils with improved strength and manufacture and repair thereof
US20030082297A1 (en) * 2001-10-26 2003-05-01 Siemens Westinghouse Power Corporation Combustion turbine blade tip restoration by metal build-up using thermal spray techniques
US6699101B2 (en) * 2001-11-29 2004-03-02 General Electric Company Method for removing a damaged substrate region beneath a coating
US6914210B2 (en) 2002-10-30 2005-07-05 General Electric Company Method of repairing a stationary shroud of a gas turbine engine using plasma transferred arc welding

Also Published As

Publication number Publication date
EP1531232A2 (en) 2005-05-18
JP4643231B2 (ja) 2011-03-02
CA2487604A1 (en) 2005-05-13
SG112068A1 (en) 2005-06-29
EP1531232A3 (en) 2010-01-20
US7078073B2 (en) 2006-07-18
CA2487604C (en) 2010-09-07
JP2005147149A (ja) 2005-06-09
US20050106316A1 (en) 2005-05-19
EP1531232B1 (en) 2013-07-03

Similar Documents

Publication Publication Date Title
BRPI0405191A (pt) Método de reparo de componentes recobertos
BRPI0405193A (pt) Método de reparo de componentes recobertos empregando coberturas adesivas de niai
BRPI0405194A (pt) Método de reparo de componentes empregando coberturas adesivas ambientais e as coberturas resultantes
BRPI0603304A (pt) método para a restauração de uma parte de um componente de uma turbina
WO2007075497A3 (en) Method and coating for protecting and repairing an airfoil surface
BR9905956A (pt) Renovação de um sistema de revestimento de barreira térmica
SG104974A1 (en) Method for repairing an apertured gas turbine component
BR0007123A (pt) Método para remoção de um revestimento aluminìdeo de um substrato
PL1673490T3 (pl) Część konstrukcyjna z warstwą ochronną do ochrony części konstrukcyjnej przed korozją i utlenianiem w wysokich temperaturach
BR0109520B1 (pt) processo para aplicar um ôprimerö sobre uma superfìcie.
IL215423A0 (en) Methods and compositions for the repair and/or regeneration of damaged myocardium
BR9907927B1 (pt) composição aquosa, método para proporcionar um revestimento protetor sobre um substrato metálico, método para ligação de uma superfìcie de substrato elastomérico a uma superfìcie de substrato metálico, e método para proporcionar um revestimento ou primer protetor sobre uma superfìcie de substrato metálico.
BR0317158A (pt) Sistema de acabamento de superfìcie de pelìcula
BRPI0401920A (pt) Revestimentos de polissiloxana para superfìcies
ATE342428T1 (de) Korrosions- und wärmeschutzschicht für keramische bauteile
AU2002360134A1 (en) Micro- or nano-electronic component comprising a power source and means for protecting the power source
BRPI0506666A (pt) folha de proteção de adesivo fundido bem como processo e dispositivo para a aplicação da mesma
BR0211786A (pt) Processo para reparar superfìcies de substrato revestidas e seu uso
BR0215111A (pt) Processo para preparar superfìcies de substrato revestidas e uso do mesmo
EP1308538A3 (en) Radiation curable maskant and line sealer for protecting metal substrates
ATE486667T1 (de) Verfahren zum temporären schützen blanker oberflächen gegen korrosion und bauteil mit temporärem korrosionsschutz
AR046268A1 (es) Metodo para revestir un sustrato ceramico y dicho sustrato.
MX9301036A (es) Composicion de caucho de silicona, electricamente conductiva.
BRPI0412829A (pt) composição capaz de ser curada, método para revestir um substrato de cerámica e substrato de cerámica revestido
BR0315903B1 (pt) método para a formação de uma boa superfìcie de contato sobre uma barra de suporte de alumìnio e uma barra de suporte.

Legal Events

Date Code Title Description
B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
B09B Patent application refused [chapter 9.2 patent gazette]
B12B Appeal against refusal [chapter 12.2 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]
B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 17A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2644 DE 08-09-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.