SG66445A1 - Method for repairing a turbine engine member damaged tip - Google Patents
Method for repairing a turbine engine member damaged tipInfo
- Publication number
- SG66445A1 SG66445A1 SG1998000590A SG1998000590A SG66445A1 SG 66445 A1 SG66445 A1 SG 66445A1 SG 1998000590 A SG1998000590 A SG 1998000590A SG 1998000590 A SG1998000590 A SG 1998000590A SG 66445 A1 SG66445 A1 SG 66445A1
- Authority
- SG
- Singapore
- Prior art keywords
- repairing
- turbine engine
- engine member
- damaged tip
- member damaged
- 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
- B23P6/007—Repairing turbine components, e.g. moving or stationary blades, rotors using only additive methods, e.g. build-up welding
-
- 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
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- 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
- F05D2230/10—Manufacture by removing material
-
- 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
-
- 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
-
- 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
- Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
-
- 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
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US08/825,982 US5794338A (en) | 1997-04-04 | 1997-04-04 | Method for repairing a turbine engine member damaged tip |
Publications (1)
Publication Number | Publication Date |
---|---|
SG66445A1 true SG66445A1 (en) | 1999-07-20 |
Family
ID=25245386
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG1998000590A SG66445A1 (en) | 1997-04-04 | 1998-03-20 | Method for repairing a turbine engine member damaged tip |
Country Status (5)
Country | Link |
---|---|
US (1) | US5794338A (fr) |
EP (1) | EP0869259A3 (fr) |
JP (1) | JPH10339103A (fr) |
BR (1) | BR9801147A (fr) |
SG (1) | SG66445A1 (fr) |
Families Citing this family (69)
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---|---|---|---|---|
DE19922012C1 (de) * | 1999-05-12 | 2000-10-19 | Mtu Muenchen Gmbh | Verfahren zur Fertigung angepaßter, strömungstechnischer Oberflächen |
US6224337B1 (en) | 1999-09-17 | 2001-05-01 | General Electric Company | Thermal barrier coated squealer tip cavity |
US6332272B1 (en) * | 2000-01-07 | 2001-12-25 | Siemens Westinghouse Power Corporation | Method of repairing a turbine blade |
EP1143030A1 (fr) | 2000-04-03 | 2001-10-10 | ABB Alstom Power N.V. | Matériau pour extrémité d'une aube de turbine et procédé de sa fabrication ou réparation |
US6418618B1 (en) * | 2000-04-11 | 2002-07-16 | General Electric Company | Method of controlling the side wall thickness of a turbine nozzle segment for improved cooling |
EP1162284A1 (fr) * | 2000-06-05 | 2001-12-12 | Alstom (Switzerland) Ltd | Procédé de réparation d'un composant revêtu |
DE10030776C2 (de) * | 2000-06-23 | 2002-06-20 | Mtu Aero Engines Gmbh | Verfahren zur Instandsetzung von metallischen Bauteilen insbesondere für Gasturbinen |
US6468040B1 (en) | 2000-07-24 | 2002-10-22 | General Electric Company | Environmentally resistant squealer tips and method for making |
US6413051B1 (en) * | 2000-10-30 | 2002-07-02 | General Electric Company | Article including a composite laminated end portion with a discrete end barrier and method for making and repairing |
US6502304B2 (en) * | 2001-05-15 | 2003-01-07 | General Electric Company | Turbine airfoil process sequencing for optimized tip performance |
US6558119B2 (en) * | 2001-05-29 | 2003-05-06 | General Electric Company | Turbine airfoil with separately formed tip and method for manufacture and repair thereof |
US6901648B2 (en) | 2001-08-31 | 2005-06-07 | General Electric Company | Method of manufacturing a nickel-base alloy welding filler metal |
US6532656B1 (en) | 2001-10-10 | 2003-03-18 | General Electric Company | Gas turbine engine compressor blade restoration method |
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 |
US6892931B2 (en) * | 2002-12-27 | 2005-05-17 | General Electric Company | Methods for replacing portions of turbine shroud supports |
US20040261265A1 (en) * | 2003-06-25 | 2004-12-30 | General Electric Company | Method for improving the wear resistance of a support region between a turbine outer case and a supported turbine vane |
US6901758B2 (en) * | 2003-08-08 | 2005-06-07 | General Electric Company | Method for repairing an air cooled combustor liner segment edge portion and repaired segment |
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 |
US20050102835A1 (en) * | 2003-11-14 | 2005-05-19 | Trewiler Gary E. | Method for repairing gas turbine rotor blades |
US7001151B2 (en) * | 2004-03-02 | 2006-02-21 | General Electric Company | Gas turbine bucket tip cap |
US20050205415A1 (en) * | 2004-03-19 | 2005-09-22 | Belousov Igor V | Multi-component deposition |
US20050217110A1 (en) * | 2004-04-06 | 2005-10-06 | Topal Valeriy I | Deposition repair of hollow items |
US7404986B2 (en) * | 2004-05-07 | 2008-07-29 | United Technologies Corporation | Multi-component deposition |
US7587818B2 (en) * | 2004-12-23 | 2009-09-15 | General Electric Company | Repair of gas turbine blade tip without recoating the repaired blade tip |
US7278829B2 (en) * | 2005-02-09 | 2007-10-09 | General Electric Company | Gas turbine blade having a monocrystalline airfoil with a repair squealer tip, and repair method |
US7687151B2 (en) * | 2005-04-12 | 2010-03-30 | General Electric Company | Overlay for repairing spline and seal teeth of a mated component |
US7591057B2 (en) * | 2005-04-12 | 2009-09-22 | General Electric Company | Method of repairing spline and seal teeth of a mated component |
US7282681B2 (en) * | 2005-05-05 | 2007-10-16 | General Electric Company | Microwave fabrication of airfoil tips |
FR2885310B1 (fr) * | 2005-05-09 | 2008-12-26 | Snecma Services Sa | Procede de fabrication d'une aube creuse comportant un sommet en forme de baignoire, procede de reparation d'une telle aube et aube obtenue par l'un de ces procedes |
US7140952B1 (en) * | 2005-09-22 | 2006-11-28 | Pratt & Whitney Canada Corp. | Oxidation protected blade and method of manufacturing |
US7600977B2 (en) * | 2006-05-08 | 2009-10-13 | General Electric Company | Turbine blade tip cap |
US20070267109A1 (en) * | 2006-05-17 | 2007-11-22 | General Electric Company | High pressure turbine airfoil recovery device and method of heat treatment |
DE102006031388A1 (de) * | 2006-07-07 | 2008-01-17 | Mtu Aero Engines Gmbh | Verfahren für die Reparatur und/oder den Austausch von Einzelelementen eines Bauteils einer Gasturbine |
US20100236067A1 (en) * | 2006-08-01 | 2010-09-23 | Honeywell International, Inc. | Hybrid welding repair of gas turbine superalloy components |
US20080263863A1 (en) * | 2007-04-27 | 2008-10-30 | United Technologies Corporation | Dimensional restoration of turbine blade knife edge seals |
US20080267775A1 (en) * | 2007-04-30 | 2008-10-30 | General Electric Company | Nozzle segments and method of repairing the same |
US20090014421A1 (en) * | 2007-07-10 | 2009-01-15 | Sujith Sathian | Weld Repair Method for a Turbine Bucket Tip |
US20090028707A1 (en) * | 2007-07-26 | 2009-01-29 | United Technologies Corporation | Apparatus and method for repairing airfoil tips |
US20090094831A1 (en) * | 2007-10-16 | 2009-04-16 | Schwartz Brian J | Method for restoring airfoil contour on integrally bladed rotors |
US7836594B2 (en) * | 2007-10-16 | 2010-11-23 | United Technologies Corporation | Method for restoring airfoil tip contour |
US8360734B2 (en) * | 2007-12-13 | 2013-01-29 | United Technologies Corporation | Method for repairing an airfoil |
US8925200B2 (en) * | 2008-03-27 | 2015-01-06 | United Technologies Corporation | Method for repairing an airfoil |
US8510926B2 (en) * | 2008-05-05 | 2013-08-20 | United Technologies Corporation | Method for repairing a gas turbine engine component |
US20100008816A1 (en) * | 2008-07-11 | 2010-01-14 | Honeywell International Inc. | Nickel-based superalloys, repaired turbine engine components, and methods for repairing turbine components |
CH699312A1 (de) | 2008-08-15 | 2010-02-15 | Alstom Technology Ltd | Schaufelanordnung einer gasturbine. |
DE102008047043A1 (de) * | 2008-09-13 | 2010-03-18 | Mtu Aero Engines Gmbh | Ersatzteil für eine Gasturbinen-Schaufel einer Gasturbine, Gasturbinen-Schaufel sowie ein Verfahren zur Reparatur einer Gasturbinen-Schaufel |
US8678267B2 (en) * | 2008-10-10 | 2014-03-25 | The Boeing Company | System and method for integrally forming a stiffener with a fiber metal laminate |
US20100095525A1 (en) * | 2008-10-22 | 2010-04-22 | Shaw Alan Terence | Gas turbine combustor repair using a make-up ring |
US8726501B2 (en) * | 2009-08-31 | 2014-05-20 | General Electric Company | Method of welding single crystal turbine blade tips with an oxidation-resistant filler material |
EP2316988B1 (fr) * | 2009-11-02 | 2015-07-08 | Alstom Technology Ltd | Aube de turbine résistant à l'usure et à l'oxydation |
US9056372B2 (en) * | 2010-10-12 | 2015-06-16 | Alstom Technology Ltd | Extending useful life of a cobalt-based gas turbine component |
US9181814B2 (en) * | 2010-11-24 | 2015-11-10 | United Technology Corporation | Turbine engine compressor stator |
DE102011080187A1 (de) * | 2011-08-01 | 2013-02-07 | Siemens Aktiengesellschaft | Verfahren zum Erzeugen einer Schaufel für eine Strömungskraftmaschine und Schaufel für eine Strömungskraftmaschine |
EP2604797B1 (fr) * | 2011-12-13 | 2020-01-22 | MTU Aero Engines GmbH | Aube de rotor dotée d'un agencement de nervures avec revêtement abrasif |
US9145781B2 (en) * | 2012-06-11 | 2015-09-29 | United Technologies Corporation | Vane support assembly |
EP2756907A1 (fr) * | 2013-01-21 | 2014-07-23 | Siemens Aktiengesellschaft | Soudage par beurrage avec contour de cadre extérieur épais |
CN106103899B (zh) * | 2014-03-03 | 2017-11-17 | 西门子股份公司 | 具有用于检查同心度的表面的转子部件 |
US9777574B2 (en) * | 2014-08-18 | 2017-10-03 | Siemens Energy, Inc. | Method for repairing a gas turbine engine blade tip |
CA2977757A1 (fr) | 2016-09-22 | 2018-03-22 | Sulzer Management Ag | Methode de fabrication ou de reparation d'une composante d'une machine rotative ainsi qu'une composante fabriquee ou reparee au moyen d'une telle methode |
CA2977751A1 (fr) * | 2016-09-22 | 2018-03-22 | Sulzer Management Ag | Methode de fabrication ou de reparation d'une composante d'une machine rotative ainsi qu'une composante fabriquee ou reparee au moyen d'une telle methode |
US10415579B2 (en) | 2016-09-28 | 2019-09-17 | General Electric Company | Ceramic coating compositions for compressor blade and methods for forming the same |
DE102017201645A1 (de) | 2017-02-02 | 2018-08-02 | MTU Aero Engines AG | Verfahren und Vorrichtung zum Reparieren einer beschädigten Schaufelspitze einer gepanzerten und mit einer Schaufelbeschichtung versehenen Turbinenschaufel |
EP3434864B1 (fr) | 2017-07-27 | 2020-12-16 | General Electric Company | Procédé et système de réparation d'une turbomachine |
EP3517237A1 (fr) | 2018-01-30 | 2019-07-31 | General Electric Company | Réparation de diaphragme de turbine à gaz |
KR102626244B1 (ko) * | 2019-07-30 | 2024-01-17 | 지멘스 에너지, 인코포레이티드 | 고온 가스 터빈 컴포넌트들을 보수하기 위한 시스템 및 방법 |
US11795832B2 (en) | 2019-11-13 | 2023-10-24 | Siemens Energy, Inc. | System and method for repairing high-temperature gas turbine components |
WO2022125075A1 (fr) * | 2020-12-08 | 2022-06-16 | General Electric Company | Procédés de formation ou de réparation d'une pièce à section en porte-à-faux, et pièce de turbomachine associée |
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US3667985A (en) | 1967-12-14 | 1972-06-06 | Gen Electric | Metallic surface treatment method |
US4004047A (en) | 1974-03-01 | 1977-01-18 | General Electric Company | Diffusion coating method |
US4028788A (en) * | 1976-01-12 | 1977-06-14 | Demusis Ralph T | Method of refurbishing turbine blade air seal flanges |
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 |
US4169742A (en) | 1976-12-16 | 1979-10-02 | General Electric Company | Cast nickel-base alloy article |
US4128929A (en) * | 1977-03-15 | 1978-12-12 | Demusis Ralph T | Method of restoring worn turbine components |
US4214355A (en) * | 1977-12-21 | 1980-07-29 | General Electric Company | Method for repairing a turbomachinery blade tip |
US4176433A (en) * | 1978-06-29 | 1979-12-04 | United Technologies Corporation | Method of remanufacturing turbine vane clusters for gas turbine engines |
US4390320A (en) * | 1980-05-01 | 1983-06-28 | General Electric Company | Tip cap for a rotor blade and method of replacement |
US4837389A (en) * | 1984-06-04 | 1989-06-06 | Turbine Components Corporation | Composite alloy structures |
US4657171A (en) * | 1985-06-13 | 1987-04-14 | General Electric Company | Repair of a member having a projection |
US4808055A (en) * | 1987-04-15 | 1989-02-28 | Metallurgical Industries, Inc. | Turbine blade with restored tip |
US4897519A (en) * | 1988-03-14 | 1990-01-30 | Westinghouse Electric Co. | More creep resistant turbine rotor, and procedures for repear welding of low alloy ferrous turbine components |
US4940390A (en) * | 1988-05-05 | 1990-07-10 | Westinghouse Electric Corp. | Turbine system having more failure resistant rotors and repair welding of low alloy ferrous turbine components by controlled weld build-up |
US4903888A (en) * | 1988-05-05 | 1990-02-27 | Westinghouse Electric Corp. | Turbine system having more failure resistant rotors and repair welding of low alloy ferrous turbine components by controlled weld build-up |
US5048183A (en) * | 1988-08-26 | 1991-09-17 | Solar Turbines Incorporated | Method of making and repairing turbine blades |
US5173255A (en) | 1988-10-03 | 1992-12-22 | General Electric Company | Cast columnar grain hollow nickel base alloy articles and alloy and heat treatment for making |
US4893388A (en) * | 1988-12-08 | 1990-01-16 | Westinghouse Electric Corp. | Method of modifying turbine rotor discs |
US5031313A (en) * | 1989-02-17 | 1991-07-16 | General Electric Company | Method of forming F.O.D.-resistant blade |
US5071054A (en) * | 1990-12-18 | 1991-12-10 | General Electric Company | Fabrication of cast articles from high melting temperature superalloy compositions |
US5193736A (en) * | 1991-03-01 | 1993-03-16 | Interturbine Corporation | Method for repairing turbine vanes |
US5183390A (en) * | 1991-07-10 | 1993-02-02 | Westinghouse Electric Corp. | Method of forming a trailing edge on a steam turbine blade and the blade made thereby |
GB2264446A (en) * | 1992-02-27 | 1993-09-01 | Turbine Blading Ltd | Turbine blade repair |
US5655701A (en) * | 1995-07-10 | 1997-08-12 | United Technologies Corporation | Method for repairing an abradable seal |
US5697151A (en) * | 1995-08-07 | 1997-12-16 | General Electric Company | Method for repairing partitions of a turbine diaphragm |
-
1997
- 1997-04-04 US US08/825,982 patent/US5794338A/en not_active Expired - Lifetime
-
1998
- 1998-03-20 SG SG1998000590A patent/SG66445A1/en unknown
- 1998-04-01 EP EP98302570A patent/EP0869259A3/fr not_active Withdrawn
- 1998-04-03 BR BR9801147-2A patent/BR9801147A/pt not_active IP Right Cessation
- 1998-04-03 JP JP10091140A patent/JPH10339103A/ja not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
EP0869259A3 (fr) | 2000-08-02 |
US5794338A (en) | 1998-08-18 |
JPH10339103A (ja) | 1998-12-22 |
EP0869259A2 (fr) | 1998-10-07 |
BR9801147A (pt) | 1999-09-28 |
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