SG112068A1 - Method for repairing coated components - Google Patents
Method for repairing coated componentsInfo
- Publication number
- SG112068A1 SG112068A1 SG200406902A SG200406902A SG112068A1 SG 112068 A1 SG112068 A1 SG 112068A1 SG 200406902 A SG200406902 A SG 200406902A SG 200406902 A SG200406902 A SG 200406902A SG 112068 A1 SG112068 A1 SG 112068A1
- Authority
- SG
- Singapore
- Prior art keywords
- coated components
- repairing coated
- repairing
- components
- coated
- 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
-
- 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)
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 |
---|---|
SG112068A1 true SG112068A1 (en) | 2005-06-29 |
Family
ID=34435695
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200406902A SG112068A1 (en) | 2003-11-13 | 2004-11-10 | Method for repairing coated components |
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9079246B2 (en) | 2009-12-08 | 2015-07-14 | Baker Hughes Incorporated | Method of making a nanomatrix powder metal compact |
US9101978B2 (en) | 2002-12-08 | 2015-08-11 | Baker Hughes Incorporated | Nanomatrix powder metal compact |
US8403037B2 (en) | 2009-12-08 | 2013-03-26 | Baker Hughes Incorporated | Dissolvable tool and method |
US9109429B2 (en) | 2002-12-08 | 2015-08-18 | Baker Hughes Incorporated | Engineered powder compact composite material |
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 |
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 |
US9856547B2 (en) | 2011-08-30 | 2018-01-02 | Bakers Hughes, A Ge Company, Llc | Nanostructured powder metal compact |
US9643144B2 (en) | 2011-09-02 | 2017-05-09 | Baker Hughes Incorporated | Method to generate and disperse nanostructures in a composite material |
US9133695B2 (en) | 2011-09-03 | 2015-09-15 | Baker Hughes Incorporated | Degradable shaped charge and perforating gun system |
US9347119B2 (en) | 2011-09-03 | 2016-05-24 | Baker Hughes Incorporated | Degradable high shock impedance material |
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 |
EP2882939B1 (de) | 2012-10-05 | 2020-01-08 | Siemens Aktiengesellschaft | Verfahren zur aufbereitung einer gasturbinenschaufel sowie verwendung einer gasturbine mit derartiger schaufel |
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 |
US10150713B2 (en) | 2014-02-21 | 2018-12-11 | Terves, Inc. | Fluid activated disintegrating metal system |
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 |
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 |
CA3012511A1 (en) | 2017-07-27 | 2019-01-27 | Terves Inc. | Degradable metal matrix composite |
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)
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 |
US6291084B1 (en) * | 1998-10-06 | 2001-09-18 | General Electric Company | Nickel aluminide coating and coating systems formed therewith |
US6153313A (en) | 1998-10-06 | 2000-11-28 | 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 |
US6042880A (en) | 1998-12-22 | 2000-03-28 | General Electric Company | Renewing a thermal barrier coating system |
US6233822B1 (en) * | 1998-12-22 | 2001-05-22 | General Electric Company | Repair of high pressure turbine shrouds |
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 |
-
2003
- 2003-11-13 US US10/714,213 patent/US7078073B2/en not_active Expired - Lifetime
-
2004
- 2004-11-10 SG SG200406902A patent/SG112068A1/en unknown
- 2004-11-10 CA CA2487604A patent/CA2487604C/en not_active Expired - Fee Related
- 2004-11-10 EP EP04256959.0A patent/EP1531232B1/en active Active
- 2004-11-12 BR BR0405191-2A patent/BRPI0405191A/pt not_active IP Right Cessation
- 2004-11-12 JP JP2004328916A patent/JP4643231B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
BRPI0405191A (pt) | 2005-07-19 |
US20050106316A1 (en) | 2005-05-19 |
EP1531232B1 (en) | 2013-07-03 |
EP1531232A2 (en) | 2005-05-18 |
CA2487604C (en) | 2010-09-07 |
US7078073B2 (en) | 2006-07-18 |
JP4643231B2 (ja) | 2011-03-02 |
EP1531232A3 (en) | 2010-01-20 |
CA2487604A1 (en) | 2005-05-13 |
JP2005147149A (ja) | 2005-06-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SG112068A1 (en) | Method for repairing coated components | |
SG112049A1 (en) | Method for repairing coated components using nial bond coats | |
EP1614768A4 (en) | FILMING PROCESS | |
EP1501958A4 (en) | METHOD FOR PRODUCING COATED COMPONENTS | |
AU2003219976A8 (en) | Method for assembling nano objects | |
WO2006040079A8 (de) | Beschichtungsverfahren | |
GB2401563B (en) | Method for forming plural-layered coated film | |
EP1754544A4 (en) | PAINT PROCESS | |
AU2003217985A8 (en) | Methods for aneurysm repair | |
GB2399520B (en) | Method for coated composite film | |
EP1675596A4 (en) | METHOD | |
EP1732394A4 (en) | DEHYDRATION-GRIDING PROCESS | |
EP1675918A4 (en) | PAINTING PROCESS FOR SHIPYARD | |
GB2414693B (en) | Method for electrostatic coating | |
GB2399521B (en) | Method for coated composite film | |
PL1711302T3 (pl) | Sposób łączenia elementów konstrukcyjnych | |
GB0404458D0 (en) | Apparatus & method | |
GB2404886B (en) | Coating method | |
EP1836570A4 (en) | METHOD FOR ASSIGNING TASKS | |
SG108981A1 (en) | Method for inspecting a titanium-based component | |
AU2003253813A8 (en) | Method for colpoplasty | |
EP1701920A4 (en) | METHOD FOR TREATING SUSTAINABLE SOLUTIONS | |
GB2399351B (en) | Method for forming film | |
TWI315261B (en) | Method for transferring-printing | |
PL1685078T3 (pl) | Sposób nanoszenia masy powlekającej |