BRPI0405193A - Método de reparo de componentes recobertos empregando coberturas adesivas de niai - Google Patents
Método de reparo de componentes recobertos empregando coberturas adesivas de niaiInfo
- Publication number
- BRPI0405193A BRPI0405193A BR0405193-9A BRPI0405193A BRPI0405193A BR PI0405193 A BRPI0405193 A BR PI0405193A BR PI0405193 A BRPI0405193 A BR PI0405193A BR PI0405193 A BRPI0405193 A BR PI0405193A
- Authority
- BR
- Brazil
- Prior art keywords
- thermal barrier
- metal base
- cover
- component
- thickness
- Prior art date
Links
- 239000000853 adhesive Substances 0.000 title abstract 6
- 230000001070 adhesive effect Effects 0.000 title abstract 6
- 239000002184 metal Substances 0.000 abstract 7
- 239000000758 substrate Substances 0.000 abstract 6
- 230000004888 barrier function Effects 0.000 abstract 5
- 239000000919 ceramic Substances 0.000 abstract 3
- 229910000943 NiAl Inorganic materials 0.000 abstract 2
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 abstract 2
Classifications
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- 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
- B23P6/00—Restoring or reconditioning objects
- B23P6/002—Repairing turbine components, e.g. moving or stationary blades, rotors
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/02—Pretreatment of the material to be coated
-
- 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
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/60—After-treatment
-
- 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
- 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
- C23C28/3215—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 at least one MCrAlX 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
- 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
-
- 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
-
- 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
- C23C28/36—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D7/00—Electroplating characterised by the article coated
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D7/00—Electroplating characterised by the article coated
- C25D7/008—Thermal barrier coatings
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D3/00—Electroplating: Baths therefor
- C25D3/02—Electroplating: Baths therefor from solutions
- C25D3/50—Electroplating: Baths therefor from solutions of platinum group metals
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/30—Manufacture with deposition of material
- F05B2230/31—Layer deposition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/90—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
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2253/00—Other material characteristics; Treatment of material
- F05C2253/12—Coating
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Electrochemistry (AREA)
- Ceramic Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
Abstract
"MéTODO DE REPARO DE COMPONENTES RECOBERTO EMPREGANDO COBERTURAS ADESIVAS DE NIAL". 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 usado 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 removida, e determinar a espessura da base metálica removida. A parte do substrato de base metálica removida apresenta uma espessura <30>t. O método também compreende aplicar uma cobertura adesiva de sobrecamada de NiAl de fase <225>, e determinar a diferença de espessura, <30>x, entre a cobertura adesiva de sobrecamada de NiAl de fase <225> e a cobertura adesiva previamente removida. O método também compreende reaplicar uma cobertura de barreira térmica cerâmica de topo até a espessura nominal de t + <30>t - <30>x, 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.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/714,430 US7094444B2 (en) | 2003-11-13 | 2003-11-13 | Method for repairing coated components using NiAl bond coats |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| BRPI0405193A true BRPI0405193A (pt) | 2005-07-19 |
| BRPI0405193B1 BRPI0405193B1 (pt) | 2013-08-06 |
Family
ID=34435699
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0405193-9B1A BRPI0405193B1 (pt) | 2003-11-13 | 2004-11-12 | método para restaurar as distâncias do passo de palheta a palheta de um componente recoberto e método para restaurar as distâncias do passo de palheta a palheta de uma palheta recoberta de uma turbina de alta pressão |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US7094444B2 (pt) |
| EP (1) | EP1533396B1 (pt) |
| JP (1) | JP5036965B2 (pt) |
| BR (1) | BRPI0405193B1 (pt) |
| CA (1) | CA2486841C (pt) |
| SG (1) | SG112049A1 (pt) |
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| US20100224602A1 (en) * | 2009-03-06 | 2010-09-09 | General Electric Company | Method and system for removing thermal barrier coating |
| CN102449428B (zh) * | 2009-05-26 | 2014-07-30 | 乌多·W·布赫 | 涂料样品特征的测量方法和仪器 |
| DE102010031795B4 (de) * | 2010-07-20 | 2015-05-28 | Lufthansa Technik Ag | Verfahren zur Reparatur von Gasturbinenbauteilen aus keramischen Verbundwerkstoffen und Vorrichtung zur Durchführung des Verfahrens |
| US8834126B2 (en) | 2011-06-30 | 2014-09-16 | United Technologies Corporation | Fan blade protection system |
| US8956700B2 (en) | 2011-10-19 | 2015-02-17 | General Electric Company | Method for adhering a coating to a substrate structure |
| FR2985057B1 (fr) * | 2011-12-23 | 2014-12-12 | Snecma | Procede et dispositif d'estimation d'une epaisseur d'un revetement de barriere thermique en ceramique |
| EP2644824A1 (de) * | 2012-03-28 | 2013-10-02 | Siemens Aktiengesellschaft | Verfahren zur Herstellung und Wiederherstellung von keramischen Wärmedämmschichten in Gasturbinen sowie dazugehörige Gasturbine |
| 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 |
| WO2014108199A1 (de) * | 2013-01-11 | 2014-07-17 | Siemens Aktiengesellschaft | Verfahren zur herstellung von gasturbinen und verfahren zum betreiben von gasturbinenanlagen |
| US10363584B2 (en) * | 2013-08-30 | 2019-07-30 | General Electric Company | Methods for removing barrier coatings, bondcoat and oxide layers from ceramic matrix composites |
| WO2015088876A1 (en) * | 2013-12-10 | 2015-06-18 | Lei Chen | Nickel-chromium-aluminum composite by electrodeposition |
| EP3080321B1 (en) * | 2013-12-10 | 2019-07-31 | United Technologies Corporation | Method for electrodepositing a nickel-chromium alloy |
| US10378118B2 (en) | 2013-12-11 | 2019-08-13 | United Technologies Corporation | Electroformed nickel-chromium alloy |
| RU2591098C2 (ru) * | 2014-05-05 | 2016-07-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Способ нанесения композитного оксидного покрытия на металлическую поверхность |
| RU2591024C2 (ru) * | 2014-05-05 | 2016-07-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Способ обработки рабочих поверхностей деталей газотурбинных установок |
| RU2588973C2 (ru) * | 2014-05-06 | 2016-07-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Способ обработки рабочих поверхностей деталей лопастных машин |
| RU2588956C2 (ru) * | 2014-05-06 | 2016-07-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Способ обработки рабочих поверхностей газотурбинных установок |
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| GB201514724D0 (en) * | 2015-08-19 | 2015-09-30 | Rolls Royce Plc | Methods, apparatus, computer programs, and non-transitory computer readble storage mediums for repairing aerofoils of gas turbine engines |
| DE102019207479A1 (de) * | 2019-05-22 | 2020-11-26 | Siemens Aktiengesellschaft | Verfahren zur Durchführung von Servicemaßnahmen an einer Energieumwandlungsanlage und Energieumwandlungsanlage |
| US11143620B2 (en) * | 2019-06-12 | 2021-10-12 | Mitsubishi Power Americas, Inc. | Electromagnetic probe testing of bond coat |
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| 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 |
| US6238743B1 (en) * | 2000-01-20 | 2001-05-29 | General Electric Company | Method of removing a thermal barrier coating |
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| 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 |
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| 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 |
| JP3686319B2 (ja) * | 2000-08-30 | 2005-08-24 | 株式会社日立製作所 | ガスタービン動翼の溶接方法 |
| 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 |
| 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 |
-
2003
- 2003-11-13 US US10/714,430 patent/US7094444B2/en not_active Expired - Fee Related
-
2004
- 2004-11-04 CA CA2486841A patent/CA2486841C/en not_active Expired - Fee Related
- 2004-11-10 EP EP04256967A patent/EP1533396B1/en not_active Expired - Lifetime
- 2004-11-12 BR BRPI0405193-9B1A patent/BRPI0405193B1/pt not_active IP Right Cessation
- 2004-11-12 SG SG200406658A patent/SG112049A1/en unknown
- 2004-11-15 JP JP2004331235A patent/JP5036965B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP1533396B1 (en) | 2011-08-03 |
| JP2005194623A (ja) | 2005-07-21 |
| EP1533396A2 (en) | 2005-05-25 |
| US7094444B2 (en) | 2006-08-22 |
| BRPI0405193B1 (pt) | 2013-08-06 |
| SG112049A1 (en) | 2005-06-29 |
| EP1533396A3 (en) | 2005-06-01 |
| JP5036965B2 (ja) | 2012-09-26 |
| US20060029723A1 (en) | 2006-02-09 |
| CA2486841A1 (en) | 2005-05-13 |
| CA2486841C (en) | 2010-12-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B07A | Application suspended after technical examination (opinion) [chapter 7.1 patent gazette] | ||
| B07A | Application suspended after technical examination (opinion) [chapter 7.1 patent gazette] | ||
| B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
| B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 12/11/2004, OBSERVADAS AS CONDICOES LEGAIS. |
|
| B21F | Lapse acc. art. 78, item iv - on non-payment of the annual fees in time | ||
| B24J | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12) |