SG137669A1 - Method of applying environmental and bond coatings to turbine flowpath parts - Google Patents
Method of applying environmental and bond coatings to turbine flowpath partsInfo
- Publication number
- SG137669A1 SG137669A1 SG200401873-5A SG2004018735A SG137669A1 SG 137669 A1 SG137669 A1 SG 137669A1 SG 2004018735 A SG2004018735 A SG 2004018735A SG 137669 A1 SG137669 A1 SG 137669A1
- Authority
- SG
- Singapore
- Prior art keywords
- bond coatings
- turbine flowpath
- applying environmental
- parts
- flowpath parts
- 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/18—After-treatment
-
- 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
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/405,727 US6887529B2 (en) | 2003-04-02 | 2003-04-02 | Method of applying environmental and bond coatings to turbine flowpath parts |
Publications (1)
Publication Number | Publication Date |
---|---|
SG137669A1 true SG137669A1 (en) | 2007-12-28 |
Family
ID=32850622
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200401873-5A SG137669A1 (en) | 2003-04-02 | 2004-04-02 | Method of applying environmental and bond coatings to turbine flowpath parts |
Country Status (6)
Country | Link |
---|---|
US (1) | US6887529B2 (de) |
EP (1) | EP1464722B1 (de) |
JP (1) | JP4912570B2 (de) |
BR (1) | BRPI0401194B1 (de) |
CA (1) | CA2462318C (de) |
SG (1) | SG137669A1 (de) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7967924B2 (en) * | 2005-05-17 | 2011-06-28 | General Electric Company | Method for making a compositionally graded gas turbine disk |
US20080102291A1 (en) * | 2006-10-31 | 2008-05-01 | Caterpillar Inc. | Method for coating a substrate |
US20080299306A1 (en) * | 2007-05-30 | 2008-12-04 | Caterpillar Inc. | Multi-layer substrate and method of fabrication |
US9062558B2 (en) | 2011-07-15 | 2015-06-23 | United Technologies Corporation | Blade outer air seal having partial coating |
US9995165B2 (en) | 2011-07-15 | 2018-06-12 | United Technologies Corporation | Blade outer air seal having partial coating |
US8678644B2 (en) * | 2011-08-16 | 2014-03-25 | General Electric Company | Hot gas path measurement |
WO2014138416A1 (en) * | 2013-03-06 | 2014-09-12 | United Technologies Corporation | Fixturing for thermal spray coating of gas turbine components |
EP3434864B1 (de) * | 2017-07-27 | 2020-12-16 | General Electric Company | Verfahren und system zur reparatur einer turbomaschine |
US10900371B2 (en) | 2017-07-27 | 2021-01-26 | Rolls-Royce North American Technologies, Inc. | Abradable coatings for high-performance systems |
US10858950B2 (en) | 2017-07-27 | 2020-12-08 | Rolls-Royce North America Technologies, Inc. | Multilayer abradable coatings for high-performance systems |
US11117151B2 (en) * | 2017-08-23 | 2021-09-14 | Raytheon Technologies Corporation | Fixture assembly for coating combustor panels |
US10808565B2 (en) * | 2018-05-22 | 2020-10-20 | Rolls-Royce Plc | Tapered abradable coatings |
CN108950457A (zh) * | 2018-06-11 | 2018-12-07 | 中国航发哈尔滨东安发动机有限公司 | 一种叶轮罩类零件热喷涂方法 |
US11707815B2 (en) * | 2019-07-09 | 2023-07-25 | General Electric Company | Creating 3D mark on protective coating on metal part using mask and metal part so formed |
FR3099186B1 (fr) * | 2019-07-23 | 2023-04-14 | Safran Aircraft Engines | Procédé de fabrication d'un élément d'étanchéité abradable, et élément d'étanchéité abradable |
KR20210120176A (ko) | 2020-03-25 | 2021-10-07 | 삼성디스플레이 주식회사 | 디스플레이 장치 |
Family Cites Families (40)
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US4291448A (en) * | 1977-12-12 | 1981-09-29 | Turbine Components Corporation | Method of restoring the shrouds of turbine blades |
DE2821118C2 (de) | 1978-05-13 | 1986-05-07 | Leybold-Heraeus GmbH, 5000 Köln | Verfahren zum allseitigen Bedampfen von gekrümmten Turbinenschaufeln |
US4222708A (en) * | 1978-06-26 | 1980-09-16 | General Electric Company | Method and apparatus for reducing eccentricity in a turbomachine |
US4764089A (en) * | 1986-08-07 | 1988-08-16 | Allied-Signal Inc. | Abradable strain-tolerant ceramic coated turbine shroud |
JPS6436752A (en) * | 1987-07-31 | 1989-02-07 | Canon Kk | Thermal spraying treatment for metal |
JPH01180955A (ja) * | 1988-01-08 | 1989-07-18 | Kubota Ltd | 溶接肉盛層の形成方法 |
US4978558A (en) * | 1988-06-10 | 1990-12-18 | United Technologies Corporation | Method for applying diffusion coating masks |
US5112683A (en) * | 1990-10-30 | 1992-05-12 | Chomerics, Inc. | High temperature resistance mask |
US5322727A (en) * | 1992-10-21 | 1994-06-21 | Alliedsignal Inc. | Plasma spray masking tape |
DE4310896C1 (de) * | 1993-04-02 | 1994-03-24 | Thyssen Industrie | Verfahren zum Herstellen von verschleißfesten Kanten an Turbinenschaufeln |
US6129991A (en) | 1994-10-28 | 2000-10-10 | Howmet Research Corporation | Aluminide/MCrAlY coating system for superalloys |
US5691018A (en) * | 1995-12-15 | 1997-11-25 | Caterpillar Inc. | Silicone mask for thermal spray coating system |
US5565035A (en) * | 1996-03-14 | 1996-10-15 | United Technologies Corporation | Fixture for masking a portion of an airfoil during application of a coating |
US6095755A (en) * | 1996-11-26 | 2000-08-01 | United Technologies Corporation | Gas turbine engine airfoils having increased fatigue strength |
SE509678C2 (sv) * | 1996-12-11 | 1999-02-22 | Kaj Kidron | Sätt att med återanvändningsbart skydd, skydda ytor vid blästring och målning |
US6049978A (en) | 1996-12-23 | 2000-04-18 | Recast Airfoil Group | Methods for repairing and reclassifying gas turbine engine airfoil parts |
US5975852A (en) * | 1997-03-31 | 1999-11-02 | General Electric Company | Thermal barrier coating system and method therefor |
GB9803561D0 (en) | 1998-02-19 | 1998-04-15 | Monitor Coatings & Eng | Surface treatment of rotors |
EP0939142A1 (de) | 1998-02-27 | 1999-09-01 | Ticona GmbH | Thermisches Sprühpulver enthaltend ein oxidiertes Polyarylensulfid |
GB9811456D0 (en) | 1998-05-29 | 1998-07-29 | Rolls Royce Plc | A metallic article having a thermal barrier coating and a method of application thereof |
SG72959A1 (en) | 1998-06-18 | 2000-05-23 | United Technologies Corp | Article having durable ceramic coating with localized abradable portion |
US6256597B1 (en) | 1998-07-10 | 2001-07-03 | General Electric Company | Three dimensional spray coating method and simulation |
US6083330A (en) | 1998-09-16 | 2000-07-04 | The United States Of America As Represented By The Secretary Of The Navy | Process for forming a coating on a substrate using a stepped heat treatment |
JP2000145406A (ja) * | 1998-11-06 | 2000-05-26 | Ishikawajima Harima Heavy Ind Co Ltd | タービンシュラウド |
US6106231A (en) | 1998-11-06 | 2000-08-22 | General Electric Company | Partially coated airfoil and method for making |
US6233822B1 (en) * | 1998-12-22 | 2001-05-22 | General Electric Company | Repair of high pressure turbine shrouds |
US6190471B1 (en) | 1999-05-26 | 2001-02-20 | General Electric Company | Fabrication of superalloy articles having hafnium- or zirconium-enriched protective layer |
US6451454B1 (en) | 1999-06-29 | 2002-09-17 | General Electric Company | Turbine engine component having wear coating and method for coating a turbine engine component |
US6372299B1 (en) | 1999-09-28 | 2002-04-16 | General Electric Company | Method for improving the oxidation-resistance of metal substrates coated with thermal barrier coatings |
US6383658B1 (en) * | 1999-11-18 | 2002-05-07 | General Electric Company | Thermally sprayed coatings having an interface with controlled cleanliness |
US6250082B1 (en) * | 1999-12-03 | 2001-06-26 | General Electric Company | Combustor rear facing step hot side contour method and apparatus |
US6296705B1 (en) * | 1999-12-15 | 2001-10-02 | United Technologies Corporation | Masking fixture and method |
US6435835B1 (en) | 1999-12-20 | 2002-08-20 | United Technologies Corporation | Article having corrosion resistant coating |
US20020098294A1 (en) * | 2000-02-07 | 2002-07-25 | Yuk-Chiu Lau | Method of providing a protective coating on a metal substrate, and related articles |
US6403165B1 (en) | 2000-02-09 | 2002-06-11 | General Electric Company | Method for modifying stoichiometric NiAl coatings applied to turbine airfoils by thermal processes |
GB2359882B (en) * | 2000-02-29 | 2004-01-07 | Rolls Royce Plc | Wall elements for gas turbine engine combustors |
JP3785028B2 (ja) * | 2000-07-28 | 2006-06-14 | 三菱重工業株式会社 | 熱cvd処理方法 |
US6444259B1 (en) | 2001-01-30 | 2002-09-03 | Siemens Westinghouse Power Corporation | Thermal barrier coating applied with cold spray technique |
US20030232139A1 (en) * | 2002-06-13 | 2003-12-18 | Detura Frank Anthony | Shield and method for spraying coating on a surface |
US20040086635A1 (en) * | 2002-10-30 | 2004-05-06 | Grossklaus Warren Davis | Method of repairing a stationary shroud of a gas turbine engine using laser cladding |
-
2003
- 2003-04-02 US US10/405,727 patent/US6887529B2/en not_active Expired - Lifetime
-
2004
- 2004-03-25 CA CA2462318A patent/CA2462318C/en not_active Expired - Lifetime
- 2004-03-30 EP EP04251899.3A patent/EP1464722B1/de not_active Expired - Lifetime
- 2004-04-01 BR BRPI0401194-5A patent/BRPI0401194B1/pt not_active IP Right Cessation
- 2004-04-02 SG SG200401873-5A patent/SG137669A1/en unknown
- 2004-04-02 JP JP2004109825A patent/JP4912570B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP1464722A2 (de) | 2004-10-06 |
CA2462318A1 (en) | 2004-10-02 |
EP1464722B1 (de) | 2015-07-01 |
JP2004308009A (ja) | 2004-11-04 |
JP4912570B2 (ja) | 2012-04-11 |
CA2462318C (en) | 2010-05-18 |
EP1464722A3 (de) | 2007-04-04 |
BRPI0401194B1 (pt) | 2014-01-07 |
US6887529B2 (en) | 2005-05-03 |
BRPI0401194A (pt) | 2005-01-18 |
US20040197486A1 (en) | 2004-10-07 |
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