SG120130A1 - Method of repairing a stationary shroud of a gas turbine engine using laser cladding - Google Patents
Method of repairing a stationary shroud of a gas turbine engine using laser claddingInfo
- Publication number
- SG120130A1 SG120130A1 SG200306622A SG200306622A SG120130A1 SG 120130 A1 SG120130 A1 SG 120130A1 SG 200306622 A SG200306622 A SG 200306622A SG 200306622 A SG200306622 A SG 200306622A SG 120130 A1 SG120130 A1 SG 120130A1
- Authority
- SG
- Singapore
- Prior art keywords
- repairing
- gas turbine
- turbine engine
- laser cladding
- stationary shroud
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/20—Bonding
- B23K26/32—Bonding taking account of the properties of the material involved
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/34—Laser welding for purposes other than joining
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
- B23K35/3033—Ni as the principal constituent
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
- B23K35/3046—Co as the principal constituent
-
- 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
- C23C24/00—Coating starting from inorganic powder
- C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
- C23C24/10—Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the 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
- C23C26/02—Coating not provided for in groups C23C2/00 - C23C24/00 applying molten material to the substrate
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2101/00—Articles made by soldering, welding or cutting
- B23K2101/001—Turbines
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/18—Dissimilar materials
- B23K2103/26—Alloys of Nickel and Cobalt and Chromium
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K2103/00—Materials to be soldered, welded or cut
- B23K2103/50—Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Plasma & Fusion (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- General Engineering & Computer Science (AREA)
- Laser Beam Processing (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/286,122 US20040086635A1 (en) | 2002-10-30 | 2002-10-30 | Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
Publications (1)
Publication Number | Publication Date |
---|---|
SG120130A1 true SG120130A1 (en) | 2006-03-28 |
Family
ID=32175356
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200306622A SG120130A1 (en) | 2002-10-30 | 2003-10-28 | Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
Country Status (6)
Country | Link |
---|---|
US (2) | US20040086635A1 (ko) |
EP (1) | EP1442829A3 (ko) |
JP (1) | JP4301402B2 (ko) |
BR (1) | BR0304067A (ko) |
CA (1) | CA2446343A1 (ko) |
SG (1) | SG120130A1 (ko) |
Families Citing this family (58)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7009137B2 (en) * | 2003-03-27 | 2006-03-07 | Honeywell International, Inc. | Laser powder fusion repair of Z-notches with nickel based superalloy powder |
US6887529B2 (en) * | 2003-04-02 | 2005-05-03 | General Electric Company | Method of applying environmental and bond coatings to turbine flowpath parts |
US20050132569A1 (en) * | 2003-12-22 | 2005-06-23 | Clark Donald G. | Method of repairing a part using laser cladding |
US20050178750A1 (en) * | 2004-02-13 | 2005-08-18 | Kenny Cheng | Repair of article by laser cladding |
US7360991B2 (en) * | 2004-06-09 | 2008-04-22 | General Electric Company | Methods and apparatus for fabricating gas turbine engines |
DE102004042878A1 (de) * | 2004-09-04 | 2006-03-09 | Mtu Aero Engines Gmbh | Verfahren zur Reparatur von Turbomaschinenschaufeln |
US7378132B2 (en) * | 2004-12-14 | 2008-05-27 | Honeywell International, Inc. | Method for applying environmental-resistant MCrAlY coatings on gas turbine components |
EP1785583A3 (en) * | 2005-10-12 | 2010-06-23 | Turbine Overhaul Services Private Limited | Blade shroud repair |
US20070079507A1 (en) * | 2005-10-12 | 2007-04-12 | Kenny Cheng | Blade shroud repair |
CN100462189C (zh) * | 2005-12-26 | 2009-02-18 | 沈阳大陆激光技术有限公司 | 一种燃气轮机护环的维修工艺 |
SG134183A1 (en) * | 2006-01-16 | 2007-08-29 | United Technologies Corp | Turbine component trailing edge and platform restoration by laser cladding |
US7653994B2 (en) * | 2006-03-22 | 2010-02-02 | General Electric Company | Repair of HPT shrouds with sintered preforms |
US7851984B2 (en) * | 2006-08-08 | 2010-12-14 | Federal-Mogul World Wide, Inc. | Ignition device having a reflowed firing tip and method of construction |
US20080148708A1 (en) * | 2006-12-20 | 2008-06-26 | General Electric Company | Turbine engine system with shafts for improved weight and vibration characteristic |
US20090053045A1 (en) * | 2007-08-22 | 2009-02-26 | General Electric Company | Turbine Shroud for Gas Turbine Assemblies and Processes for Forming the Shroud |
EP2075416B1 (fr) * | 2007-12-27 | 2011-05-18 | Techspace Aero | Procédé de fabrication d'un élément de turbomachine et dispositif ainsi obtenu |
US8061142B2 (en) * | 2008-04-11 | 2011-11-22 | General Electric Company | Mixer for a combustor |
US20090271983A1 (en) | 2008-04-30 | 2009-11-05 | Rose William M | Method to weld repair blade outer air seals |
EP2226149A1 (de) * | 2009-03-04 | 2010-09-08 | Siemens Aktiengesellschaft | Zweischritt-Schweissverfahren |
US8373089B2 (en) * | 2009-08-31 | 2013-02-12 | General Electric Company | Combustion cap effusion plate laser weld repair |
EP2506980B1 (en) * | 2009-11-30 | 2016-06-01 | United Technologies Corporation | Coating methods and apparatus |
EP2330349B1 (en) * | 2009-12-01 | 2018-10-24 | Siemens Aktiengesellschaft | Pilot burner of a gas turbine engine, combustor, and gas turbine engine |
DE102010010595A1 (de) * | 2010-03-08 | 2011-09-08 | Lufthansa Technik Ag | Verfahren zur Reparatur von Dichtsegmenten in der Rotor-/Statordichtung einer Gasturbine |
US8613590B2 (en) * | 2010-07-27 | 2013-12-24 | United Technologies Corporation | Blade outer air seal and repair method |
US8708659B2 (en) | 2010-09-24 | 2014-04-29 | United Technologies Corporation | Turbine engine component having protective coating |
US8870523B2 (en) | 2011-03-07 | 2014-10-28 | General Electric Company | Method for manufacturing a hot gas path component and hot gas path turbine component |
FR2977177B1 (fr) | 2011-06-30 | 2014-04-04 | Chpolansky Ets | Procede de rechargement d'une piece |
CN102615431B (zh) * | 2012-04-12 | 2014-08-13 | 中国人民解放军装甲兵工程学院 | 一种灰铸铁缸盖自动化激光熔覆再制造方法 |
US9127549B2 (en) | 2012-04-26 | 2015-09-08 | General Electric Company | Turbine shroud cooling assembly for a gas turbine system |
US9828872B2 (en) | 2013-02-07 | 2017-11-28 | General Electric Company | Cooling structure for turbomachine |
US9015944B2 (en) | 2013-02-22 | 2015-04-28 | General Electric Company | Method of forming a microchannel cooled component |
US9394796B2 (en) | 2013-07-12 | 2016-07-19 | General Electric Company | Turbine component and methods of assembling the same |
KR102126866B1 (ko) * | 2013-08-07 | 2020-06-25 | 한화파워시스템 주식회사 | 유체 회전 기계의 임펠러 조립체 및 임펠러 조립체의 제조 방법 |
US9416662B2 (en) | 2013-09-03 | 2016-08-16 | General Electric Company | Method and system for providing cooling for turbine components |
JP6240327B2 (ja) | 2013-11-27 | 2017-11-29 | ゼネラル・エレクトリック・カンパニイ | 流体ロックとパージ装置とを有する燃料ノズル |
CN103659201B (zh) * | 2013-12-15 | 2015-12-30 | 无锡透平叶片有限公司 | 一种采用激光熔覆防水蚀的汽轮机叶片的加工工艺 |
US10190774B2 (en) | 2013-12-23 | 2019-01-29 | General Electric Company | Fuel nozzle with flexible support structures |
JP6606080B2 (ja) | 2013-12-23 | 2019-11-13 | ゼネラル・エレクトリック・カンパニイ | エアアシスト式燃料噴射用の燃料ノズル構造体 |
CN104164665A (zh) * | 2014-07-24 | 2014-11-26 | 新疆汇翔激光科技有限公司 | 一种利用光纤激光对挖盐机缸套的修复方法 |
US10450871B2 (en) | 2015-02-26 | 2019-10-22 | Rolls-Royce Corporation | Repair of dual walled metallic components using directed energy deposition material addition |
EP3061556B1 (en) | 2015-02-26 | 2018-08-15 | Rolls-Royce Corporation | Method for repairing a dual walled metallic component using braze material and such component obtained |
US10669878B2 (en) | 2016-03-23 | 2020-06-02 | Raytheon Technologies Corporation | Outer airseal abradable rub strip |
US10247027B2 (en) | 2016-03-23 | 2019-04-02 | United Technologies Corporation | Outer airseal insulated rub strip |
US10267174B2 (en) | 2016-04-28 | 2019-04-23 | United Technologies Corporation | Outer airseal abradable rub strip |
US10544683B2 (en) | 2016-08-30 | 2020-01-28 | Rolls-Royce Corporation | Air-film cooled component for a gas turbine engine |
US10689984B2 (en) | 2016-09-13 | 2020-06-23 | Rolls-Royce Corporation | Cast gas turbine engine cooling components |
US20180073390A1 (en) | 2016-09-13 | 2018-03-15 | Rolls-Royce Corporation | Additively deposited gas turbine engine cooling component |
CN106521487B (zh) * | 2016-11-10 | 2019-05-17 | 北京睿曼科技有限公司 | 一种服役中期钛合金压气机叶片的再制造方法 |
US10858950B2 (en) | 2017-07-27 | 2020-12-08 | Rolls-Royce North America Technologies, Inc. | Multilayer abradable coatings for high-performance systems |
US10900371B2 (en) | 2017-07-27 | 2021-01-26 | Rolls-Royce North American Technologies, Inc. | Abradable coatings for high-performance systems |
CN107502889A (zh) * | 2017-08-16 | 2017-12-22 | 重庆市科学技术研究院 | 一种精确激光熔覆镍基合金粉末的方法 |
US11338396B2 (en) | 2018-03-08 | 2022-05-24 | Rolls-Royce Corporation | Techniques and assemblies for joining components |
US10808565B2 (en) * | 2018-05-22 | 2020-10-20 | Rolls-Royce Plc | Tapered abradable coatings |
US11090771B2 (en) | 2018-11-05 | 2021-08-17 | Rolls-Royce Corporation | Dual-walled components for a gas turbine engine |
US11305363B2 (en) | 2019-02-11 | 2022-04-19 | Rolls-Royce Corporation | Repair of through-hole damage using braze sintered preform |
CN112695318A (zh) * | 2020-12-22 | 2021-04-23 | 天津修船技术研究所(中国船舶重工集团公司第六三一三研究所) | 一种碟片式分离机中转鼓的喷嘴流道的维修方法 |
CN113058771B (zh) * | 2021-03-31 | 2023-06-20 | 中国航发常州兰翔机械有限责任公司 | 一种航空发动机轴流机匣流道修复用工装及其使用方法 |
US11692446B2 (en) | 2021-09-23 | 2023-07-04 | Rolls-Royce North American Technologies, Inc. | Airfoil with sintered powder components |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0509758A1 (en) * | 1991-04-15 | 1992-10-21 | General Electric Company | Rotary seal member and method for making |
WO2001012381A1 (en) * | 1999-08-16 | 2001-02-22 | Chromalloy Gas Turbine Corporation | Laser cladding a turbine engine vane platform |
CN1322892A (zh) * | 2000-05-10 | 2001-11-21 | 中国科学院金属研究所 | 燃气轮机带冠叶片冠部阻尼面激光敷层工艺方法 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4743733A (en) * | 1984-10-01 | 1988-05-10 | General Electric Company | Method and apparatus for repairing metal in an article |
FR2688803B1 (fr) * | 1992-03-23 | 1994-05-06 | European Gas Turbines Sa | Procede de revetement d'une encoche d'une piece en alliage de nickel par laser. |
US5889254A (en) * | 1995-11-22 | 1999-03-30 | General Electric Company | Method and apparatus for Nd: YAG hardsurfacing |
US5759641A (en) * | 1996-05-15 | 1998-06-02 | Dimitrienko; Ludmila Nikolaevna | Method of applying strengthening coatings to metallic or metal-containing surfaces |
US6269540B1 (en) * | 1998-10-05 | 2001-08-07 | National Research Council Of Canada | Process for manufacturing or repairing turbine engine or compressor components |
US6233822B1 (en) * | 1998-12-22 | 2001-05-22 | General Electric Company | Repair of high pressure turbine shrouds |
US6364971B1 (en) * | 2000-01-20 | 2002-04-02 | Electric Power Research Institute | Apparatus and method of repairing turbine blades |
US6933061B2 (en) * | 2002-12-12 | 2005-08-23 | General Electric Company | Thermal barrier coating protected by thermally glazed layer and method for preparing same |
US7494619B2 (en) * | 2003-12-23 | 2009-02-24 | General Electric Company | High temperature alloys, and articles made and repaired therewith |
US6905728B1 (en) * | 2004-03-22 | 2005-06-14 | Honeywell International, Inc. | Cold gas-dynamic spray repair on gas turbine engine components |
US20080182017A1 (en) * | 2007-01-31 | 2008-07-31 | General Electric Company | Laser net shape manufacturing and repair using a medial axis toolpath deposition method |
GB2449862B (en) * | 2007-06-05 | 2009-09-16 | Rolls Royce Plc | Method for producing abrasive tips for gas turbine blades |
-
2002
- 2002-10-30 US US10/286,122 patent/US20040086635A1/en not_active Abandoned
-
2003
- 2003-10-23 CA CA002446343A patent/CA2446343A1/en not_active Abandoned
- 2003-10-28 SG SG200306622A patent/SG120130A1/en unknown
- 2003-10-29 JP JP2003368209A patent/JP4301402B2/ja not_active Expired - Fee Related
- 2003-10-29 BR BR0304067-4A patent/BR0304067A/pt not_active Application Discontinuation
- 2003-10-30 EP EP03256861A patent/EP1442829A3/en not_active Ceased
-
2007
- 2007-03-12 US US11/685,018 patent/US20070205189A1/en not_active Abandoned
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0509758A1 (en) * | 1991-04-15 | 1992-10-21 | General Electric Company | Rotary seal member and method for making |
WO2001012381A1 (en) * | 1999-08-16 | 2001-02-22 | Chromalloy Gas Turbine Corporation | Laser cladding a turbine engine vane platform |
CN1322892A (zh) * | 2000-05-10 | 2001-11-21 | 中国科学院金属研究所 | 燃气轮机带冠叶片冠部阻尼面激光敷层工艺方法 |
Also Published As
Publication number | Publication date |
---|---|
JP4301402B2 (ja) | 2009-07-22 |
EP1442829A2 (en) | 2004-08-04 |
CA2446343A1 (en) | 2004-04-30 |
US20070205189A1 (en) | 2007-09-06 |
US20040086635A1 (en) | 2004-05-06 |
EP1442829A3 (en) | 2006-01-25 |
JP2004176715A (ja) | 2004-06-24 |
BR0304067A (pt) | 2004-09-08 |
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