BR9905956A - Renovação de um sistema de revestimento de barreira térmica - Google Patents
Renovação de um sistema de revestimento de barreira térmicaInfo
- Publication number
- BR9905956A BR9905956A BR9905956-8A BR9905956A BR9905956A BR 9905956 A BR9905956 A BR 9905956A BR 9905956 A BR9905956 A BR 9905956A BR 9905956 A BR9905956 A BR 9905956A
- Authority
- BR
- Brazil
- Prior art keywords
- renovation
- article
- thermal barrier
- coating
- bonding coating
- Prior art date
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
- 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
- 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
- C23C28/325—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
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Inorganic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Ceramic Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Laminated Bodies (AREA)
Abstract
Patente de Invenção: <B>"RENOVAçãO DE UM SISTEMA DE REVESTIMENTO DE BARREIRA TéRMICA"<D>. Trata-se de um sistema de revestimento de barreira térmica (TBC) que compreende um revestimento de ligação metálico sobre uma superfície do artigo 14 e em que um TBC cerâmico externo é reparado por renovação sem remover o revestimento de ligação. O TBC cerâmico externo é removido de modo a expor um substrato do revestimento de ligação. Pelo menos uma área superficial discreta local 16, 18 da superfície do artigo 14 sujeita a degradação do revestimento de ligação é selecionada de um padrão térmico único à superfície do artigo de operação em serviço. Pelo menos um metal de renovação selecionado dentre Pt, Rh e Pd é aplicado pelo menos à área da superfície local discreta selecionada 16, 18 e aquecido para difundir o metal de renovação no substrato do revestimento de ligação. Um revestimento resistente ao ambiente selecionado de aluminetos e ligas incluindo alumínio é aplicado pelo menos à área superficial discreta 16, 18 sobre o metal de renovação. Depois disso, um TBC cerâmico externo é aplicado à superfície do artigo 14.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/219,163 US6042880A (en) | 1998-12-22 | 1998-12-22 | Renewing a thermal barrier coating system |
Publications (2)
Publication Number | Publication Date |
---|---|
BR9905956A true BR9905956A (pt) | 2000-09-12 |
BR9905956B1 BR9905956B1 (pt) | 2010-11-16 |
Family
ID=22818144
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI9905956-8A BR9905956B1 (pt) | 1998-12-22 | 1999-12-22 | método para a renovação de um sistema de revestimento de barreira térmica (tbc) sobre uma superficie de artigo. |
Country Status (8)
Country | Link |
---|---|
US (1) | US6042880A (pt) |
EP (1) | EP1013796B1 (pt) |
JP (1) | JP4405020B2 (pt) |
BR (1) | BR9905956B1 (pt) |
CA (1) | CA2292384C (pt) |
DE (1) | DE69934766T2 (pt) |
SG (1) | SG82047A1 (pt) |
TR (1) | TR199903182A2 (pt) |
Families Citing this family (56)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6148517A (en) * | 1999-01-29 | 2000-11-21 | Chromalloy Gas Turbine Corporation | Repair of turbine exhaust case |
US6283714B1 (en) * | 1999-08-11 | 2001-09-04 | General Electric Company | Protection of internal and external surfaces of gas turbine airfoils |
US6352636B1 (en) * | 1999-10-18 | 2002-03-05 | General Electric Company | Electrochemical system and process for stripping metallic coatings |
US6243948B1 (en) * | 1999-11-18 | 2001-06-12 | General Electric Company | Modification and repair of film cooling holes in gas turbine engine components |
US6305077B1 (en) * | 1999-11-18 | 2001-10-23 | General Electric Company | Repair of coated turbine components |
US6235352B1 (en) * | 1999-11-29 | 2001-05-22 | Electric Power Research Institute, Inc. | Method of repairing a thermal barrier coating |
EP1162284A1 (en) * | 2000-06-05 | 2001-12-12 | Alstom (Switzerland) Ltd | Process of repairing a coated component |
US6605160B2 (en) | 2000-08-21 | 2003-08-12 | Robert Frank Hoskin | Repair of coatings and surfaces using reactive metals coating processes |
US6602356B1 (en) | 2000-09-20 | 2003-08-05 | General Electric Company | CVD aluminiding process for producing a modified platinum aluminide bond coat for improved high temperature performance |
US6465040B2 (en) | 2001-02-06 | 2002-10-15 | General Electric Company | Method for refurbishing a coating including a thermally grown oxide |
US6560870B2 (en) * | 2001-05-08 | 2003-05-13 | General Electric Company | Method for applying diffusion aluminide coating on a selective area of a turbine engine component |
US6502304B2 (en) * | 2001-05-15 | 2003-01-07 | General Electric Company | Turbine airfoil process sequencing for optimized tip performance |
FR2827311B1 (fr) * | 2001-07-12 | 2003-09-19 | Snecma Moteurs | Procede de reparation locale de pieces revetues d'une barriere thermique |
US6599416B2 (en) | 2001-09-28 | 2003-07-29 | General Electric Company | Method and apparatus for selectively removing coatings from substrates |
US20030101587A1 (en) * | 2001-10-22 | 2003-06-05 | Rigney Joseph David | Method for replacing a damaged TBC ceramic layer |
US6758914B2 (en) | 2001-10-25 | 2004-07-06 | General Electric Company | Process for partial stripping of diffusion aluminide coatings from metal substrates, and related compositions |
US6908288B2 (en) * | 2001-10-31 | 2005-06-21 | General Electric Company | Repair of advanced gas turbine blades |
US6725540B2 (en) * | 2002-03-09 | 2004-04-27 | United Technologies Corporation | Method for repairing turbine engine components |
US6652914B1 (en) | 2002-09-27 | 2003-11-25 | General Electric Aviation Service Operation Pte. Ltd. | Method for selective surface protection of a gas turbine blade which has previously been in service |
US6969457B2 (en) * | 2002-10-21 | 2005-11-29 | General Electric Company | Method for partially stripping a coating from the surface of a substrate, and related articles and compositions |
US20070023142A1 (en) * | 2002-12-19 | 2007-02-01 | Lagraff John R | Airfoil refurbishment method |
US7094450B2 (en) * | 2003-04-30 | 2006-08-22 | General Electric Company | Method for applying or repairing thermal barrier coatings |
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 |
US6994920B2 (en) * | 2003-10-31 | 2006-02-07 | General Electric Company | Fusion welding method and welded article |
US7094444B2 (en) * | 2003-11-13 | 2006-08-22 | General Electric Company | Method for repairing coated components using NiAl bond coats |
US7078073B2 (en) | 2003-11-13 | 2006-07-18 | General Electric Company | Method for repairing coated components |
US7371426B2 (en) * | 2003-11-13 | 2008-05-13 | General Electric Company | Method for repairing components using environmental bond coatings and resultant repaired components |
US7509735B2 (en) * | 2004-04-22 | 2009-03-31 | Siemens Energy, Inc. | In-frame repairing system of gas turbine components |
EP1591561A1 (de) * | 2004-04-28 | 2005-11-02 | ALSTOM (Switzerland) Ltd | Verfahren zum Aufbringen einer schützenden Beschichtung auf ein thermisch beanspruchtes Bauteil |
US20060040129A1 (en) * | 2004-08-20 | 2006-02-23 | General Electric Company | Article protected by a strong local coating |
US8367963B2 (en) | 2004-10-29 | 2013-02-05 | United Technologies Corporation | Method and apparatus for microplasma spray coating a portion of a turbine vane in a gas turbine engine |
DE602005014066D1 (de) * | 2004-10-29 | 2009-06-04 | United Technologies Corp | Verfahren und Vorrichtung zum Mikroplasmaspritzbeschichten eines Teils einer Verdichterschaufel eines Düsentriebwerkes |
US8367967B2 (en) * | 2004-10-29 | 2013-02-05 | United Technologies Corporation | Method and apparatus for repairing thermal barrier coatings |
US20070023402A1 (en) * | 2005-07-26 | 2007-02-01 | United Technologies Corporation | Methods for repairing workpieces using microplasma spray coating |
DE602005014604D1 (de) * | 2004-10-29 | 2009-07-09 | United Technologies Corp | Verfahren zur Wärmdammschichtreparierungen |
US7763823B2 (en) * | 2004-10-29 | 2010-07-27 | United Technologies Corporation | Method and apparatus for microplasma spray coating a portion of a compressor blade in a gas turbine engine |
US7115832B1 (en) | 2005-07-26 | 2006-10-03 | United Technologies Corporation | Microplasma spray coating apparatus |
JP2006131999A (ja) * | 2004-10-29 | 2006-05-25 | United Technol Corp <Utc> | マイクロプラズマ溶射を用いたワークピースを修復する方法 |
JP2006131997A (ja) * | 2004-10-29 | 2006-05-25 | United Technol Corp <Utc> | ワークピースの修復方法 |
US20070087129A1 (en) * | 2005-10-19 | 2007-04-19 | Blankenship Donn R | Methods for repairing a workpiece |
ATE447049T1 (de) * | 2004-10-29 | 2009-11-15 | United Technologies Corp | Verfahren zum mikroplasmaspritzbeschichten eines teil einer gasturbinenleitschaufel eines düsentriebwerkes |
US20060222776A1 (en) * | 2005-03-29 | 2006-10-05 | Honeywell International, Inc. | Environment-resistant platinum aluminide coatings, and methods of applying the same onto turbine components |
US7597762B2 (en) * | 2005-09-21 | 2009-10-06 | General Electric Company | Methods and apparatus for manufacturing components |
US20090110953A1 (en) * | 2007-10-29 | 2009-04-30 | General Electric Company | Method of treating a thermal barrier coating and related articles |
EP2166125A1 (en) | 2008-09-19 | 2010-03-24 | ALSTOM Technology Ltd | Method for the restoration of a metallic coating |
US20100126014A1 (en) * | 2008-11-26 | 2010-05-27 | General Electric Company | Repair method for tbc coated turbine components |
JP5574683B2 (ja) * | 2009-11-30 | 2014-08-20 | 三菱重工業株式会社 | 補修方法およびそれにより補修されたガスタービンの耐熱部材 |
US10309018B2 (en) * | 2011-05-31 | 2019-06-04 | United Technologies Corporation | Composite article having layer with co-continuous material regions |
EP2971563A2 (en) * | 2013-03-15 | 2016-01-20 | Siemens Energy, Inc. | Component repair using brazed surface textured superalloy foil |
US9745849B2 (en) | 2015-06-26 | 2017-08-29 | General Electric Company | Methods for treating field operated components |
PL416283A1 (pl) | 2016-02-26 | 2017-08-28 | General Electric Company | Wyrób z ulepszonym układem powłok oraz sposoby jego wytwarzania |
US10052724B2 (en) * | 2016-03-02 | 2018-08-21 | General Electric Company | Braze composition, brazing process, and brazed article |
US10920590B2 (en) | 2016-06-30 | 2021-02-16 | General Electric Company | Turbine assembly maintenance methods |
US10646894B2 (en) | 2016-06-30 | 2020-05-12 | General Electric Company | Squeegee apparatus and methods of use thereof |
US10384978B2 (en) | 2016-08-22 | 2019-08-20 | General Electric Company | Thermal barrier coating repair compositions and methods of use thereof |
GB201903484D0 (en) | 2019-03-14 | 2019-05-01 | Rolls Royce Plc | A method of removing a ceramic coating from a ceramic coated metallic article |
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US3544348A (en) * | 1968-10-25 | 1970-12-01 | United Aircraft Corp | Overhaul process for aluminide coated gas turbine engine components |
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 |
US4328285A (en) * | 1980-07-21 | 1982-05-04 | General Electric Company | Method of coating a superalloy substrate, coating compositions, and composites obtained therefrom |
ES2074151T3 (es) * | 1989-11-27 | 1995-09-01 | United Technologies Corp | Eliminacion mediante chorro liquido de las capas sinterizadas y metalizadas con pistola de plasma. |
US5216808A (en) * | 1990-11-13 | 1993-06-08 | General Electric Company | Method for making or repairing a gas turbine engine component |
US5254413A (en) * | 1991-01-31 | 1993-10-19 | General Electric Company | Method for repair and restoration of a ceramic thermal barrier-coated substrate by providing an intermetallic coating |
US5236745A (en) * | 1991-09-13 | 1993-08-17 | General Electric Company | Method for increasing the cyclic spallation life of a thermal barrier coating |
GB9204791D0 (en) * | 1992-03-05 | 1992-04-22 | Rolls Royce Plc | A coated article |
US5658614A (en) * | 1994-10-28 | 1997-08-19 | Howmet Research Corporation | Platinum aluminide CVD coating method |
EP0713957A1 (en) * | 1994-11-25 | 1996-05-29 | FINMECCANICA S.p.A. AZIENDA ANSALDO | Method of repairing the coating of turbine blades |
WO1997002947A1 (en) * | 1995-07-13 | 1997-01-30 | Advanced Materials Technologies, Inc. | Method for bonding thermal barrier coatings to superalloy substrates |
US5723078A (en) * | 1996-05-24 | 1998-03-03 | General Electric Company | Method for repairing a thermal barrier coating |
US5813118A (en) * | 1997-06-23 | 1998-09-29 | General Electric Company | Method for repairing an air cooled turbine engine airfoil |
US5972424A (en) * | 1998-05-21 | 1999-10-26 | United Technologies Corporation | Repair of gas turbine engine component coated with a thermal barrier coating |
-
1998
- 1998-12-22 US US09/219,163 patent/US6042880A/en not_active Expired - Lifetime
-
1999
- 1999-12-14 SG SG9906363A patent/SG82047A1/en unknown
- 1999-12-16 CA CA002292384A patent/CA2292384C/en not_active Expired - Fee Related
- 1999-12-21 TR TR1999/03182A patent/TR199903182A2/xx unknown
- 1999-12-21 JP JP36209999A patent/JP4405020B2/ja not_active Expired - Lifetime
- 1999-12-22 BR BRPI9905956-8A patent/BR9905956B1/pt not_active IP Right Cessation
- 1999-12-22 EP EP99310398A patent/EP1013796B1/en not_active Expired - Lifetime
- 1999-12-22 DE DE69934766T patent/DE69934766T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP2000234182A (ja) | 2000-08-29 |
US6042880A (en) | 2000-03-28 |
BR9905956B1 (pt) | 2010-11-16 |
EP1013796A1 (en) | 2000-06-28 |
DE69934766D1 (de) | 2007-02-22 |
SG82047A1 (en) | 2001-07-24 |
EP1013796B1 (en) | 2007-01-10 |
DE69934766T2 (de) | 2007-10-11 |
JP4405020B2 (ja) | 2010-01-27 |
CA2292384A1 (en) | 2000-06-22 |
TR199903182A2 (xx) | 2000-07-21 |
CA2292384C (en) | 2005-12-06 |
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