SG104998A1 - Method for repairing turbine engine components - Google Patents
Method for repairing turbine engine componentsInfo
- Publication number
- SG104998A1 SG104998A1 SG200301110A SG200301110A SG104998A1 SG 104998 A1 SG104998 A1 SG 104998A1 SG 200301110 A SG200301110 A SG 200301110A SG 200301110 A SG200301110 A SG 200301110A SG 104998 A1 SG104998 A1 SG 104998A1
- Authority
- SG
- Singapore
- Prior art keywords
- component
- turbine engine
- engine components
- repairing turbine
- depleted
- 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
-
- 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
- C23G—CLEANING OR DE-GREASING OF METALLIC MATERIAL BY CHEMICAL METHODS OTHER THAN ELECTROLYSIS
- C23G1/00—Cleaning or pickling metallic material with solutions or molten salts
- C23G1/14—Cleaning or pickling metallic material with solutions or molten salts with alkaline solutions
- C23G1/20—Other heavy metals
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C10/00—Solid state diffusion of only metal elements or silicon into metallic material surfaces
- C23C10/02—Pretreatment of the material to be coated
-
- 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
- Y10T29/49721—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
- Y10T29/49732—Repairing by attaching repair preform, e.g., remaking, restoring, or patching
- Y10T29/49734—Repairing by attaching repair preform, e.g., remaking, restoring, or patching and removing damaged material
- Y10T29/49737—Metallurgically attaching preform
-
- 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)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- General Chemical & Material Sciences (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 |
---|---|---|---|
US10/094,702 US6725540B2 (en) | 2002-03-09 | 2002-03-09 | Method for repairing turbine engine components |
Publications (1)
Publication Number | Publication Date |
---|---|
SG104998A1 true SG104998A1 (en) | 2004-07-30 |
Family
ID=27788158
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200301110A SG104998A1 (en) | 2002-03-09 | 2003-03-04 | Method for repairing turbine engine components |
Country Status (7)
Country | Link |
---|---|
US (1) | US6725540B2 (ko) |
EP (1) | EP1354977B1 (ko) |
JP (1) | JP2003269190A (ko) |
KR (1) | KR100612532B1 (ko) |
AT (1) | ATE457368T1 (ko) |
DE (1) | DE60331203D1 (ko) |
SG (1) | SG104998A1 (ko) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7509735B2 (en) * | 2004-04-22 | 2009-03-31 | Siemens Energy, Inc. | In-frame repairing system of gas turbine components |
US20060040129A1 (en) * | 2004-08-20 | 2006-02-23 | General Electric Company | Article protected by a strong local coating |
US20070023402A1 (en) * | 2005-07-26 | 2007-02-01 | United Technologies Corporation | Methods for repairing workpieces using microplasma spray coating |
FR2881146B1 (fr) * | 2005-01-27 | 2007-10-19 | Snecma Moteurs Sa | Procede de reparation d'une surface de frottement d'une aube a calage variable de turbomachine |
US7360678B2 (en) * | 2005-01-27 | 2008-04-22 | United Technologies Corporation | Repair and reclassification of superalloy components |
US20060200963A1 (en) * | 2005-03-11 | 2006-09-14 | United Technologies Corporation | Method for repairing parts composed of superalloys |
US20060219330A1 (en) * | 2005-03-29 | 2006-10-05 | Honeywell International, Inc. | Nickel-based superalloy and methods for repairing gas turbine components |
US8205334B2 (en) * | 2005-07-15 | 2012-06-26 | United Technologies Corporation | Method for repairing a gas turbine engine component |
JP4680067B2 (ja) * | 2006-01-05 | 2011-05-11 | 株式会社日立製作所 | タービン翼の補修方法及びタービン翼 |
US20070207328A1 (en) * | 2006-03-01 | 2007-09-06 | United Technologies Corporation | High density thermal barrier coating |
US20080028605A1 (en) * | 2006-07-28 | 2008-02-07 | Lutz Andrew J | Weld repair of metallic components |
DE102007046386B3 (de) * | 2007-09-21 | 2008-10-02 | Siemens Ag | Verfahren zur Reparatur eines Bauteils durch Beschichten |
US7836594B2 (en) * | 2007-10-16 | 2010-11-23 | United Technologies Corporation | Method for restoring airfoil tip contour |
US20090094831A1 (en) * | 2007-10-16 | 2009-04-16 | Schwartz Brian J | Method for restoring airfoil contour on integrally bladed rotors |
US20090271983A1 (en) * | 2008-04-30 | 2009-11-05 | Rose William M | Method to weld repair blade outer air seals |
US8186946B2 (en) * | 2009-04-17 | 2012-05-29 | United Technologies Corporation | Abrasive thermal coating |
US20120110848A1 (en) * | 2010-11-08 | 2012-05-10 | United Technologies Corporation | Low and extra low sulfur alloys for repair |
US20120255635A1 (en) * | 2011-04-11 | 2012-10-11 | Applied Materials, Inc. | Method and apparatus for refurbishing gas distribution plate surfaces |
US8807955B2 (en) | 2011-06-30 | 2014-08-19 | United Technologies Corporation | Abrasive airfoil tip |
EP2570520B1 (en) * | 2011-09-15 | 2017-11-22 | General Electric Company | Method of rejuvenating a multilayer structure |
US9657570B2 (en) | 2013-03-11 | 2017-05-23 | United Technologies Corporation | Pulse jet liquid gas cleaning system |
US20150165569A1 (en) * | 2013-12-18 | 2015-06-18 | Petya M. Georgieva | Repair of turbine engine components using waterjet ablation process |
US20170101347A1 (en) * | 2015-10-08 | 2017-04-13 | General Electric Company | Method for coating removal |
US10544698B2 (en) | 2016-06-20 | 2020-01-28 | United Technologies Corporation | Air seal abrasive coating and method |
CN114368174B (zh) * | 2021-11-24 | 2023-12-26 | 中国南方航空股份有限公司 | 一种v2500发动机平移门尖端修理双曲面外形恢复方法 |
KR102480317B1 (ko) | 2022-09-02 | 2022-12-23 | 터보파워텍(주) | 터빈로터 수리용 레이저 클래딩 자동화장치 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5783318A (en) * | 1994-06-22 | 1998-07-21 | United Technologies Corporation | Repaired nickel based superalloy |
US5723078A (en) * | 1996-05-24 | 1998-03-03 | General Electric Company | Method for repairing a thermal barrier coating |
US5794338A (en) * | 1997-04-04 | 1998-08-18 | General Electric Company | Method for repairing a turbine engine member damaged tip |
US5972424A (en) * | 1998-05-21 | 1999-10-26 | United Technologies Corporation | Repair of gas turbine engine component coated with a thermal barrier coating |
US6042880A (en) * | 1998-12-22 | 2000-03-28 | General Electric Company | Renewing a thermal barrier coating system |
US6158957A (en) * | 1998-12-23 | 2000-12-12 | United Technologies Corporation | Thermal barrier removal process |
US6328810B1 (en) * | 1999-04-07 | 2001-12-11 | General Electric Company | Method for locally removing oxidation and corrosion product from the surface of turbine engine components |
US6339878B1 (en) * | 2000-03-27 | 2002-01-22 | United Technologies Corporation | Method of repairing an airfoil |
US20020076573A1 (en) * | 2000-12-19 | 2002-06-20 | Neal James Wesley | Vapor deposition repair of superalloy articles |
US6490791B1 (en) * | 2001-06-22 | 2002-12-10 | United Technologies Corporation | Method for repairing cracks in a turbine blade root trailing edge |
US7204019B2 (en) * | 2001-08-23 | 2007-04-17 | United Technologies Corporation | Method for repairing an apertured gas turbine component |
-
2002
- 2002-03-09 US US10/094,702 patent/US6725540B2/en not_active Expired - Lifetime
-
2003
- 2003-03-04 SG SG200301110A patent/SG104998A1/en unknown
- 2003-03-07 DE DE60331203T patent/DE60331203D1/de not_active Expired - Lifetime
- 2003-03-07 EP EP03251391A patent/EP1354977B1/en not_active Expired - Lifetime
- 2003-03-07 AT AT03251391T patent/ATE457368T1/de not_active IP Right Cessation
- 2003-03-08 KR KR1020030014567A patent/KR100612532B1/ko not_active IP Right Cessation
- 2003-03-10 JP JP2003063986A patent/JP2003269190A/ja not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US20030167636A1 (en) | 2003-09-11 |
DE60331203D1 (de) | 2010-03-25 |
KR20030074321A (ko) | 2003-09-19 |
ATE457368T1 (de) | 2010-02-15 |
EP1354977A3 (en) | 2004-06-30 |
EP1354977B1 (en) | 2010-02-10 |
EP1354977A2 (en) | 2003-10-22 |
JP2003269190A (ja) | 2003-09-25 |
US6725540B2 (en) | 2004-04-27 |
KR100612532B1 (ko) | 2006-08-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
SG104998A1 (en) | Method for repairing turbine engine components | |
EP1505168B1 (en) | Turbine element repair | |
US20170283930A1 (en) | Laser assisted oxide removal | |
EP1270141B1 (en) | Method for repairing cracks in a turbine blade root trailing edge | |
US6758985B2 (en) | Method of removing a ceramic coating | |
US9527777B2 (en) | Compliant layer for ceramic components and methods of forming the same | |
EP2524069B1 (en) | Features for mitigating thermal or mechanical stress on an environmental barrier coating | |
US7966707B2 (en) | Method for repairing superalloy components using inserts | |
US8647073B2 (en) | Abrasive single-crystal turbine blade | |
US6379749B2 (en) | Method of removing ceramic coatings | |
EP2171124B1 (en) | Method for manufacturing an abrasive coating on a gas turbine component | |
EP1531232A3 (en) | Method for repairing a high pressure turbine blade | |
US20070044306A1 (en) | Superalloy repair methods | |
EP1752559A2 (en) | Method for restoring portion of turbine component | |
JP2006036632A (ja) | 7FA+e第1段アブレイダブル被膜及びその作製方法 | |
EP1258598A3 (en) | Turbine airfoil tip | |
JP2002348682A (ja) | セラミック皮膜を修理する方法 | |
JP4913297B2 (ja) | レーザー溶接又はレーザードリルの間に使用するためのマスキング剤 | |
US20090302004A1 (en) | Method for removing the coating from a gas turbine component | |
MY135527A (en) | Method of reconditioning a turbine blade | |
US6645926B2 (en) | Fluoride cleaning masking system | |
US7101448B2 (en) | Process for producing a cladding for a metallic component | |
US20090232975A1 (en) | Method for repairing turbine vanes |