SG104974A1 - Method for repairing an apertured gas turbine component - Google Patents
Method for repairing an apertured gas turbine componentInfo
- Publication number
- SG104974A1 SG104974A1 SG200203981A SG200203981A SG104974A1 SG 104974 A1 SG104974 A1 SG 104974A1 SG 200203981 A SG200203981 A SG 200203981A SG 200203981 A SG200203981 A SG 200203981A SG 104974 A1 SG104974 A1 SG 104974A1
- Authority
- SG
- Singapore
- Prior art keywords
- repairing
- gas turbine
- turbine component
- apertured gas
- apertured
- Prior art date
Links
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
- B23H9/00—Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
- B23H9/10—Working turbine blades or nozzles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23H—WORKING OF METAL BY THE ACTION OF A HIGH CONCENTRATION OF ELECTRIC CURRENT ON A WORKPIECE USING AN ELECTRODE WHICH TAKES THE PLACE OF A TOOL; SUCH WORKING COMBINED WITH OTHER FORMS OF WORKING OF METAL
- B23H9/00—Machining specially adapted for treating particular metal objects or for obtaining special effects or results on metal objects
- B23H9/14—Making holes
-
- 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
-
- 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/18—After-treatment
-
- 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
-
- 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
- B23P2700/00—Indexing scheme relating to the articles being treated, e.g. manufactured, repaired, assembled, connected or other operations covered in the subgroups
- B23P2700/06—Cooling passages of turbine components, e.g. unblocking or preventing blocking of cooling passages of turbine components
-
- 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
- F05D2230/10—Manufacture by removing material
- F05D2230/12—Manufacture by removing material by spark erosion 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
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/23—Three-dimensional prismatic
- F05D2250/232—Three-dimensional prismatic conical
-
- 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
- F05D2260/00—Function
- F05D2260/20—Heat transfer, e.g. cooling
- F05D2260/202—Heat transfer, e.g. cooling by film cooling
-
- 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
-
- 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
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
-
- 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
- Y10T29/49336—Blade making
- Y10T29/49339—Hollow blade
- Y10T29/49341—Hollow blade with cooling passage
-
- 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
- Y10T29/49718—Repairing
- Y10T29/49721—Repairing with disassembling
-
- 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
- Y10T29/49718—Repairing
- Y10T29/49721—Repairing with disassembling
- Y10T29/49723—Repairing with disassembling including reconditioning of part
- Y10T29/49725—Repairing with disassembling including reconditioning of part by shaping
- Y10T29/49726—Removing material
-
- 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
- Y10T29/49718—Repairing
- Y10T29/49721—Repairing with disassembling
- Y10T29/4973—Replacing of defective part
-
- 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
- Y10T29/49718—Repairing
- Y10T29/49746—Repairing by applying fluent material, e.g., coating, casting
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Inorganic Chemistry (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Plasma & Fusion (AREA)
- Ceramic Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/935,896 US7204019B2 (en) | 2001-08-23 | 2001-08-23 | Method for repairing an apertured gas turbine component |
Publications (1)
Publication Number | Publication Date |
---|---|
SG104974A1 true SG104974A1 (en) | 2004-07-30 |
Family
ID=25467858
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200203981A SG104974A1 (en) | 2001-08-23 | 2002-07-02 | Method for repairing an apertured gas turbine component |
Country Status (5)
Country | Link |
---|---|
US (1) | US7204019B2 (fr) |
EP (1) | EP1286020B2 (fr) |
JP (1) | JP2003155935A (fr) |
DE (1) | DE60217590T3 (fr) |
SG (1) | SG104974A1 (fr) |
Families Citing this family (90)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1340567A1 (fr) * | 2002-02-27 | 2003-09-03 | ALSTOM (Switzerland) Ltd | Procédé pour éliminer des défauts de coulée |
US6725540B2 (en) * | 2002-03-09 | 2004-04-27 | United Technologies Corporation | Method for repairing turbine engine components |
US7095495B2 (en) * | 2003-01-31 | 2006-08-22 | General Electric Company | Fluorescent inspection of airfoil cooling holes |
US6723951B1 (en) | 2003-06-04 | 2004-04-20 | Siemens Westinghouse Power Corporation | Method for reestablishing holes in a component |
DE10335657B4 (de) | 2003-08-04 | 2015-04-30 | Alstom Technology Ltd. | Parametrische Herstellung von Kühlbohrungen |
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 |
US7805822B2 (en) * | 2003-12-15 | 2010-10-05 | Turbocombustor Technology, Inc. | Process for removing thermal barrier coatings |
US7216485B2 (en) * | 2004-09-03 | 2007-05-15 | General Electric Company | Adjusting airflow in turbine component by depositing overlay metallic coating |
CA2602628A1 (fr) * | 2005-04-07 | 2006-10-12 | Alstom Technology Ltd. | Procede pour reparer ou remettre en etat des trous de refroidissement d'un composant enduit d'une turbine a gaz |
US8844090B2 (en) | 2005-06-17 | 2014-09-30 | United Technologies Corporation | Tool for filling voids in turbine vanes and other articles |
DE102005060698A1 (de) * | 2005-12-19 | 2007-08-02 | Rolls-Royce Deutschland Ltd & Co Kg | Sekundärfluidkanalherstellungsverfahren |
EP1839801A1 (fr) * | 2006-03-30 | 2007-10-03 | Siemens Aktiengesellschaft | Méthode de réparation pour la remise en état de pièces |
EP1867838A1 (fr) * | 2006-06-12 | 2007-12-19 | Siemens Aktiengesellschaft | Une méthode pour substituer un élément de composition d'un revêtement d'une turbine |
US20080131612A1 (en) * | 2006-11-30 | 2008-06-05 | Honeywell International, Inc. | Method for making an environment-resistant and thermal barrier coating system on a component |
US20080189946A1 (en) * | 2007-02-14 | 2008-08-14 | United Technologies Corporation One Financial Plaz | Dimensional restoration of stator inner shrouds |
US20080264444A1 (en) * | 2007-04-30 | 2008-10-30 | United Technologies Corporation | Method for removing carbide-based coatings |
CA2695630A1 (fr) * | 2007-08-28 | 2009-03-12 | Rem Technologies, Inc. | Procede pour inspecter et remettre en etat des composants mecaniques |
SG151113A1 (en) * | 2007-09-10 | 2009-04-30 | Turbine Overhaul Services Pte | Microwave assisted post-fpi cleaning method |
US7640793B2 (en) * | 2007-09-12 | 2010-01-05 | United Technologies Corporation | Systems and methods for determining airflow parameters of gas turbine engine components |
US20090071002A1 (en) * | 2007-09-18 | 2009-03-19 | United Technologies Corp. | Methods for Repairing Gas Turbine Engine Components |
US7685870B2 (en) * | 2007-09-27 | 2010-03-30 | United Technologies Corporation | Systems and methods for performing cooling airflow analysis of gas turbine engine components |
US20090106130A1 (en) * | 2007-10-17 | 2009-04-23 | United Technologies Corp. | Systems and Methods Involving Rotable Components |
US20090142548A1 (en) * | 2007-10-18 | 2009-06-04 | David Bruce Patterson | Air cooled gas turbine components and methods of manufacturing and repairing the same |
WO2009079470A2 (fr) * | 2007-12-14 | 2009-06-25 | University Of Florida Research Foundation, Inc. | Refroidissement par film actif pour aubes de turbine |
US8296945B2 (en) * | 2007-12-29 | 2012-10-30 | General Electric Company | Method for repairing a turbine nozzle segment |
US20090169361A1 (en) * | 2007-12-29 | 2009-07-02 | Michael Scott Cole | Cooled turbine nozzle segment |
US20090165275A1 (en) * | 2007-12-29 | 2009-07-02 | Michael Scott Cole | Method for repairing a cooled turbine nozzle segment |
US7639777B2 (en) * | 2008-02-26 | 2009-12-29 | United Technologies Corp. | Computed tomography systems and related methods involving forward collimation |
US20090213984A1 (en) * | 2008-02-26 | 2009-08-27 | United Technologies Corp. | Computed Tomography Systems and Related Methods Involving Post-Target Collimation |
US20090225954A1 (en) * | 2008-03-06 | 2009-09-10 | United Technologies Corp. | X-Ray Collimators, and Related Systems and Methods Involving Such Collimators |
US8238521B2 (en) * | 2008-03-06 | 2012-08-07 | United Technologies Corp. | X-ray collimators, and related systems and methods involving such collimators |
US20090252987A1 (en) * | 2008-04-02 | 2009-10-08 | United Technologies Corporation | Inspection and repair process using thermal acoustic imaging |
US7876875B2 (en) * | 2008-04-09 | 2011-01-25 | United Technologies Corp. | Computed tomography systems and related methods involving multi-target inspection |
US20090263574A1 (en) * | 2008-04-21 | 2009-10-22 | Quinn Daniel E | Method of restoring an article |
US20090274264A1 (en) * | 2008-04-30 | 2009-11-05 | United Technologies Corp. | Computed Tomography Systems and Related Methods Involving Localized Bias |
US7888647B2 (en) * | 2008-04-30 | 2011-02-15 | United Technologies Corp. | X-ray detector assemblies and related computed tomography systems |
US20090286102A1 (en) * | 2008-05-15 | 2009-11-19 | Tubine Overhaul Services Pte Ltd. | Induced capillary action brazing using metallic foam matrix |
US20090314748A1 (en) * | 2008-06-21 | 2009-12-24 | United Technologies Corporation | Ultrasonic assisted electrodischarge machining |
US8563889B2 (en) | 2009-06-09 | 2013-10-22 | Pratt & Whitney Services Pte Ltd | Electrical discharge assembly and method for repairing diffusion cooling passages |
US9890647B2 (en) * | 2009-12-29 | 2018-02-13 | Rolls-Royce North American Technologies Inc. | Composite gas turbine engine component |
US8857055B2 (en) * | 2010-01-29 | 2014-10-14 | General Electric Company | Process and system for forming shaped air holes |
US8742279B2 (en) * | 2010-02-01 | 2014-06-03 | United Technologies Corporation | Method of creating an airfoil trench and a plurality of cooling holes within the trench |
FR2960242B1 (fr) * | 2010-05-18 | 2015-05-01 | C R M A | Procede de fabrication de pieces multicouches comportant des trous inclines et devant resister a des contraintes thermiques elevees et utilisation du procede pour la reparation de pieces |
US9175568B2 (en) | 2010-06-22 | 2015-11-03 | Honeywell International Inc. | Methods for manufacturing turbine components |
US8632297B2 (en) * | 2010-09-29 | 2014-01-21 | General Electric Company | Turbine airfoil and method for cooling a turbine airfoil |
JP5517163B2 (ja) * | 2010-10-07 | 2014-06-11 | 株式会社日立製作所 | タービン翼の冷却孔加工方法 |
US8739404B2 (en) * | 2010-11-23 | 2014-06-03 | General Electric Company | Turbine components with cooling features and methods of manufacturing the same |
US20120167389A1 (en) * | 2011-01-04 | 2012-07-05 | General Electric Company | Method for providing a film cooled article |
US9085980B2 (en) * | 2011-03-04 | 2015-07-21 | Honeywell International Inc. | Methods for repairing turbine components |
US8506836B2 (en) | 2011-09-16 | 2013-08-13 | Honeywell International Inc. | Methods for manufacturing components from articles formed by additive-manufacturing processes |
US8915713B2 (en) * | 2011-09-27 | 2014-12-23 | General Electric Company | Offset counterbore for airfoil cooling hole |
US20130086784A1 (en) * | 2011-10-06 | 2013-04-11 | General Electric Company | Repair methods for cooled components |
US9266170B2 (en) | 2012-01-27 | 2016-02-23 | Honeywell International Inc. | Multi-material turbine components |
US10100650B2 (en) * | 2012-06-30 | 2018-10-16 | General Electric Company | Process for selectively producing thermal barrier coatings on turbine hardware |
US9120151B2 (en) | 2012-08-01 | 2015-09-01 | Honeywell International Inc. | Methods for manufacturing titanium aluminide components from articles formed by consolidation processes |
US10441962B2 (en) | 2012-10-29 | 2019-10-15 | South Dakota Board Of Regents | Cold spray device and system |
US10099322B2 (en) * | 2012-10-29 | 2018-10-16 | South Dakota Board Of Regents | Methods for cold spray repair |
US8720526B1 (en) | 2012-11-13 | 2014-05-13 | Siemens Energy, Inc. | Process for forming a long gas turbine engine blade having a main wall with a thin portion near a tip |
EP2733310A1 (fr) * | 2012-11-16 | 2014-05-21 | Siemens Aktiengesellschaft | Surface modifiée autour d'un trou |
US20140161585A1 (en) * | 2012-12-10 | 2014-06-12 | General Electric Company | Turbo-machine component and method |
US9664111B2 (en) * | 2012-12-19 | 2017-05-30 | United Technologies Corporation | Closure of cooling holes with a filing agent |
US9884343B2 (en) | 2012-12-20 | 2018-02-06 | United Technologies Corporation | Closure of cooling holes with a filling agent |
WO2014120152A1 (fr) * | 2013-01-30 | 2014-08-07 | United Technologies Corporation | Procédé de revêtement pour un composant de moteur à turbine à gaz comportant des trous de refroidissement |
JP5456192B1 (ja) * | 2013-02-26 | 2014-03-26 | 三菱重工業株式会社 | タービン翼の加工方法、加工工具及びタービン翼 |
EP2971674B1 (fr) * | 2013-03-14 | 2022-10-19 | Raytheon Technologies Corporation | Refroidissement de plateforme d'ailette statorique de moteur à turbine à gaz |
WO2015057304A1 (fr) * | 2013-10-18 | 2015-04-23 | Burd Steven W | Panneaux à trous de refroidissement et ses procédés de fabrication |
US9988932B2 (en) | 2013-12-06 | 2018-06-05 | Honeywell International Inc. | Bi-cast turbine nozzles and methods for cooling slip joints therein |
HUE057069T2 (hu) | 2014-04-25 | 2022-04-28 | South Dakota Board Of Regents | Nagykapacitású elektródok |
US9885245B2 (en) | 2014-05-20 | 2018-02-06 | Honeywell International Inc. | Turbine nozzles and cooling systems for cooling slip joints therein |
US10376998B2 (en) * | 2014-07-03 | 2019-08-13 | United Technologies Corporation | Methods and tools for use in repairing gas engine turbine blades |
GB201413456D0 (en) * | 2014-07-30 | 2014-09-10 | Rolls Royce Plc | Gas turbine engine end-wall component |
US20160090843A1 (en) * | 2014-09-30 | 2016-03-31 | General Electric Company | Turbine components with stepped apertures |
EP3034803A1 (fr) | 2014-12-16 | 2016-06-22 | Rolls-Royce Corporation | Système de suspension d'un composant de moteur à turbine |
US20160228995A1 (en) * | 2015-02-05 | 2016-08-11 | Siemens Energy, Inc. | Material repair process using laser and ultrasound |
US9962792B2 (en) * | 2015-02-20 | 2018-05-08 | General Electric Company | Component repair using confined laser drilling |
JP6685721B2 (ja) * | 2015-12-28 | 2020-04-22 | 三菱日立パワーシステムズ株式会社 | タービン翼の補修方法 |
JP6685722B2 (ja) * | 2015-12-28 | 2020-04-22 | 三菱日立パワーシステムズ株式会社 | タービン翼の補修方法 |
US20180010457A1 (en) * | 2016-07-08 | 2018-01-11 | General Electric Company | Coupon for hot gas path component having manufacturing assist features |
JP2018173023A (ja) * | 2017-03-31 | 2018-11-08 | 株式会社東芝 | タービン部品の補修方法 |
US10641102B2 (en) * | 2017-09-01 | 2020-05-05 | United Technologies Corporation | Turbine vane cluster including enhanced vane cooling |
US10468674B2 (en) | 2018-01-09 | 2019-11-05 | South Dakota Board Of Regents | Layered high capacity electrodes |
JP6609017B2 (ja) * | 2018-10-09 | 2019-11-20 | 株式会社東芝 | タービン動翼の補修方法 |
US11021966B2 (en) * | 2019-04-24 | 2021-06-01 | Raytheon Technologies Corporation | Vane core assemblies and methods |
US11504813B2 (en) * | 2020-05-18 | 2022-11-22 | Rolls-Royce Plc | Methods for health monitoring of ceramic matrix composite components in gas turbine engines |
CN114393340B (zh) * | 2022-01-28 | 2023-08-22 | 安徽马钢设备检修有限公司 | 一种大型泵体外壳开裂处焊接工艺 |
CN115074726B (zh) * | 2022-06-29 | 2023-10-17 | 中国航发动力股份有限公司 | 一种涡轮工作叶片异型气膜孔激光修复方法 |
US11821337B1 (en) * | 2022-08-05 | 2023-11-21 | Rtx Corporation | Internal aluminide coating for vanes and blades and method of manufacture |
CN115595581B (zh) * | 2022-11-10 | 2024-04-26 | 上海电气燃气轮机有限公司 | 一种服役后热部件粘接层的去除方法 |
Family Cites Families (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4073639A (en) | 1975-01-06 | 1978-02-14 | United Technologies Corporation | Metallic filler material |
US4008844A (en) | 1975-01-06 | 1977-02-22 | United Technologies Corporation | Method of repairing surface defects using metallic filler material |
US4209348A (en) | 1976-11-17 | 1980-06-24 | United Technologies Corporation | Heat treated superalloy single crystal article and process |
US4197443A (en) * | 1977-09-19 | 1980-04-08 | General Electric Company | Method and apparatus for forming diffused cooling holes in an airfoil |
US4321311A (en) | 1980-01-07 | 1982-03-23 | United Technologies Corporation | Columnar grain ceramic thermal barrier coatings |
US4401697A (en) | 1980-01-07 | 1983-08-30 | United Technologies Corporation | Method for producing columnar grain ceramic thermal barrier coatings |
US4405659A (en) | 1980-01-07 | 1983-09-20 | United Technologies Corporation | Method for producing columnar grain ceramic thermal barrier coatings |
US4321310A (en) | 1980-01-07 | 1982-03-23 | United Technologies Corporation | Columnar grain ceramic thermal barrier coatings on polished substrates |
US4414249A (en) | 1980-01-07 | 1983-11-08 | United Technologies Corporation | Method for producing metallic articles having durable ceramic thermal barrier coatings |
US4405660A (en) | 1980-01-07 | 1983-09-20 | United Technologies Corporation | Method for producing metallic articles having durable ceramic thermal barrier coatings |
US4585481A (en) | 1981-08-05 | 1986-04-29 | United Technologies Corporation | Overlays coating for superalloys |
USRE32121E (en) | 1981-08-05 | 1986-04-22 | United Technologies Corporation | Overlay coatings for superalloys |
US4643782A (en) | 1984-03-19 | 1987-02-17 | Cannon Muskegon Corporation | Single crystal alloy technology |
US4719080A (en) | 1985-06-10 | 1988-01-12 | United Technologies Corporation | Advanced high strength single crystal superalloy compositions |
US4738588A (en) * | 1985-12-23 | 1988-04-19 | Field Robert E | Film cooling passages with step diffuser |
US5068084A (en) | 1986-01-02 | 1991-11-26 | United Technologies Corporation | Columnar grain superalloy articles |
US4726104A (en) * | 1986-11-20 | 1988-02-23 | United Technologies Corporation | Methods for weld repairing hollow, air cooled turbine blades and vanes |
US5262245A (en) | 1988-08-12 | 1993-11-16 | United Technologies Corporation | Advanced thermal barrier coated superalloy components |
GB2227190B (en) * | 1989-01-24 | 1992-12-16 | Refurbished Turbine Components | Turbine blade repair |
DE69032417T2 (de) * | 1989-03-28 | 1999-02-11 | Refurbished Turbine Components Ltd., Droitwich, Hereford And Worchester | Reparaturverfahren für Turbinenschaufeln |
GB9000580D0 (en) * | 1990-01-10 | 1990-03-14 | Refurbished Turbine Components | Apparatus for and methods of the repair of turbine blades |
US5156321A (en) * | 1990-08-28 | 1992-10-20 | Liburdi Engineering Limited | Powder metallurgy repair technique |
JP3032295B2 (ja) | 1992-05-06 | 2000-04-10 | ユナイテッド・テクノロジーズ・コーポレイション | コバルトベース超合金物品の熱処理及び修理 |
US5605639A (en) * | 1993-12-21 | 1997-02-25 | United Technologies Corporation | Method of producing diffusion holes in turbine components by a multiple piece electrode |
US5437737A (en) | 1994-02-07 | 1995-08-01 | United Technologies Corporation | Repair coating for superalloy articles, such as gas turbine engine components |
US5658614A (en) * | 1994-10-28 | 1997-08-19 | Howmet Research Corporation | Platinum aluminide CVD coating method |
US5702288A (en) * | 1995-08-30 | 1997-12-30 | United Technologies Corporation | Method of removing excess overlay coating from within cooling holes of aluminide coated gas turbine engine components |
WO1999023273A1 (fr) * | 1997-11-03 | 1999-05-14 | Siemens Aktiengesellschaft | Procede d'application de revetement et dispositif |
JP3040747B2 (ja) * | 1998-03-19 | 2000-05-15 | 川崎重工業株式会社 | セラミックス遮熱コーティング |
US5972424A (en) * | 1998-05-21 | 1999-10-26 | United Technologies Corporation | Repair of gas turbine engine component coated with a thermal barrier coating |
EP0985802B1 (fr) * | 1998-09-10 | 2003-10-29 | ALSTOM (Switzerland) Ltd | Méthode de formation d'un orifice pour le refroidissement par pellicule |
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 |
JP2001055928A (ja) * | 1999-08-12 | 2001-02-27 | Toshiba Corp | ガスタービン高温部品の補修再生処理方法 |
US6243948B1 (en) * | 1999-11-18 | 2001-06-12 | General Electric Company | Modification and repair of film cooling holes in gas turbine engine components |
US6370752B1 (en) * | 2000-04-21 | 2002-04-16 | General Electric Company | Method for repositioning or repairing holes |
US6375425B1 (en) * | 2000-11-06 | 2002-04-23 | General Electric Company | Transpiration cooling in thermal barrier coating |
-
2001
- 2001-08-23 US US09/935,896 patent/US7204019B2/en not_active Expired - Lifetime
-
2002
- 2002-06-21 EP EP02254349.0A patent/EP1286020B2/fr not_active Expired - Lifetime
- 2002-06-21 DE DE60217590T patent/DE60217590T3/de not_active Expired - Lifetime
- 2002-07-02 SG SG200203981A patent/SG104974A1/en unknown
- 2002-08-23 JP JP2002242854A patent/JP2003155935A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
EP1286020B2 (fr) | 2013-08-14 |
EP1286020A3 (fr) | 2003-12-17 |
US7204019B2 (en) | 2007-04-17 |
DE60217590D1 (de) | 2007-03-08 |
EP1286020A2 (fr) | 2003-02-26 |
DE60217590T3 (de) | 2013-10-10 |
DE60217590T2 (de) | 2007-10-11 |
US20030037436A1 (en) | 2003-02-27 |
JP2003155935A (ja) | 2003-05-30 |
EP1286020B1 (fr) | 2007-01-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SG104974A1 (en) | Method for repairing an apertured gas turbine component | |
SG121725A1 (en) | Dianostic method and system for turbine engines | |
GB2393504B (en) | Method for liquefying methane-rich gas | |
SG112068A1 (en) | Method for repairing coated components | |
EP1555407A4 (fr) | Procede et systeme de regulation d'un moteur de turbine a gaz | |
IL153771A0 (en) | Method for inspecting patterns | |
SG91909A1 (en) | Apparatus and method for masking multiple turbine components | |
AU2003286427A1 (en) | Gas turbine apparatus | |
GB2381224B (en) | Method for repairing a turbine vane | |
EP1831505A4 (fr) | Composant de turbine de gaz statique et procede de reparation d'un tel procede | |
EP1408134A4 (fr) | Procede pour reparer un composant en alliage a base de nickel | |
EP1485592A4 (fr) | Dispositif a turbine a gaz | |
EP1468180A4 (fr) | Dispositif de turbine a gaz | |
AU2002363146A1 (en) | Turbine component inspection system | |
ZA200304719B (en) | Methods and apparatus for operating gas turbine engines. | |
GB2398798B (en) | Methods and apparatus for manufacturing turbine engine components | |
AU2003290069A1 (en) | Turbo-machine and method for operating the same | |
AU2002367402A1 (en) | Method and apparatus for assessing the impact of individual parts of a gas turbine component on the overall thermal performance of a gas turbine | |
PL366078A1 (en) | Turbine nozzle and method for welding turbine nozzle | |
EP1394361A4 (fr) | Turbine a gaz | |
AU2003239900A1 (en) | Turbine engine apparatus and method | |
EP1474596A4 (fr) | Appareil pour turbine a gaz | |
HK1088657A1 (en) | Method and circuit for igniting a gas flow | |
GB0220760D0 (en) | Coating gas generator and method | |
AU2002354057A1 (en) | Method for supplying atmosphere gas |