DE69615517D1 - Körper mit Hochtemperatur-Schutzschicht und Verfahren zum Beschichten - Google Patents
Körper mit Hochtemperatur-Schutzschicht und Verfahren zum BeschichtenInfo
- Publication number
- DE69615517D1 DE69615517D1 DE69615517T DE69615517T DE69615517D1 DE 69615517 D1 DE69615517 D1 DE 69615517D1 DE 69615517 T DE69615517 T DE 69615517T DE 69615517 T DE69615517 T DE 69615517T DE 69615517 D1 DE69615517 D1 DE 69615517D1
- Authority
- DE
- Germany
- Prior art keywords
- coating
- high temperature
- protective layer
- temperature protective
- layer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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
- 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
-
- 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
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US57716995A | 1995-12-22 | 1995-12-22 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69615517D1 true DE69615517D1 (de) | 2001-10-31 |
DE69615517T2 DE69615517T2 (de) | 2002-05-16 |
Family
ID=24307550
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69615517T Expired - Fee Related DE69615517T2 (de) | 1995-12-22 | 1996-12-13 | Körper mit Hochtemperatur-Schutzschicht und Verfahren zum Beschichten |
Country Status (4)
Country | Link |
---|---|
US (1) | US5780110A (de) |
EP (1) | EP0780484B1 (de) |
JP (1) | JP4072213B2 (de) |
DE (1) | DE69615517T2 (de) |
Families Citing this family (47)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE69509202T2 (de) * | 1994-12-24 | 1999-09-09 | Rolls Royce Plc | Wärmedämmschicht sowie Methode zu deren Auftragung auf einen Superlegierungskörper |
US6930066B2 (en) * | 2001-12-06 | 2005-08-16 | Siemens Westinghouse Power Corporation | Highly defective oxides as sinter resistant thermal barrier coating |
US5891267A (en) * | 1997-01-16 | 1999-04-06 | General Electric Company | Thermal barrier coating system and method therefor |
WO1999023277A1 (de) * | 1997-11-03 | 1999-05-14 | Siemens Aktiengesellschaft | Für eine heissgasbeaufschlagung ausgelegtes erzeugnis und verfahren zur herstellung einer beschichtung für ein für dieses erzeugnis |
US6146692A (en) * | 1998-12-14 | 2000-11-14 | General Electric Company | Caustic process for replacing a thermal barrier coating |
US6174380B1 (en) * | 1998-12-22 | 2001-01-16 | General Electric Company | Method of removing hot corrosion products from a diffusion aluminide coating |
US6210812B1 (en) | 1999-05-03 | 2001-04-03 | General Electric Company | Thermal barrier coating system |
US6335105B1 (en) * | 1999-06-21 | 2002-01-01 | General Electric Company | Ceramic superalloy articles |
US6589600B1 (en) * | 1999-06-30 | 2003-07-08 | General Electric Company | Turbine engine component having enhanced heat transfer characteristics and method for forming same |
US6294260B1 (en) | 1999-09-10 | 2001-09-25 | Siemens Westinghouse Power Corporation | In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components |
US6270318B1 (en) * | 1999-12-20 | 2001-08-07 | United Technologies Corporation | Article having corrosion resistant coating |
US6485845B1 (en) | 2000-01-24 | 2002-11-26 | General Electric Company | Thermal barrier coating system with improved bond coat |
US6472018B1 (en) * | 2000-02-23 | 2002-10-29 | Howmet Research Corporation | Thermal barrier coating method |
FR2813318B1 (fr) * | 2000-08-28 | 2003-04-25 | Snecma Moteurs | Formation d'un revetement aluminiure incorporant un element reactif, sur un substrat metallique |
US20030211245A1 (en) * | 2001-08-31 | 2003-11-13 | Irene Spitsberg | Fabrication of an article having a thermal barrier coating system, and the article |
US6761956B2 (en) | 2001-12-20 | 2004-07-13 | General Electric Company | Ventilated thermal barrier coating |
WO2003068673A2 (de) * | 2002-02-15 | 2003-08-21 | Alstom Technology Ltd | Verfahren zum herstellen eines thermisch hoch belastbaren, mit einer wärmeschutzschicht beschichteten bauteils |
US6677064B1 (en) | 2002-05-29 | 2004-01-13 | Siemens Westinghouse Power Corporation | In-situ formation of multiphase deposited thermal barrier coatings |
US6749396B2 (en) | 2002-06-17 | 2004-06-15 | General Electric Company | Failsafe film cooled wall |
US6926928B2 (en) * | 2002-07-19 | 2005-08-09 | General Electric Company | Protection of a gas turbine component by a vapor-deposited oxide coating |
US7157151B2 (en) * | 2002-09-11 | 2007-01-02 | Rolls-Royce Corporation | Corrosion-resistant layered coatings |
US6933061B2 (en) | 2002-12-12 | 2005-08-23 | General Electric Company | Thermal barrier coating protected by thermally glazed layer and method for preparing same |
JP4173762B2 (ja) | 2003-04-04 | 2008-10-29 | 株式会社神戸製鋼所 | α型結晶構造主体のアルミナ皮膜の製造方法および積層皮膜被覆部材の製造方法 |
US20040247869A1 (en) * | 2003-06-03 | 2004-12-09 | Farshad Ghasripoor | Aluminum oxide coated fiber metal for S2S and S3S sealing system with extended oxidation life |
US7455890B2 (en) * | 2003-08-05 | 2008-11-25 | General Electric Company | Ion implantation of turbine engine rotor component |
US6921251B2 (en) * | 2003-09-05 | 2005-07-26 | General Electric Company | Aluminide or chromide coating of turbine engine rotor component |
US6979498B2 (en) * | 2003-11-25 | 2005-12-27 | General Electric Company | Strengthened bond coats for thermal barrier coatings |
US6983599B2 (en) * | 2004-02-12 | 2006-01-10 | General Electric Company | Combustor member and method for making a combustor assembly |
US20060057418A1 (en) * | 2004-09-16 | 2006-03-16 | Aeromet Technologies, Inc. | Alluminide coatings containing silicon and yttrium for superalloys and method of forming such coatings |
WO2006052277A2 (en) * | 2004-09-16 | 2006-05-18 | Aeromet Technologies, Inc. | Gas turbine engine components with aluminide coatings and method of forming such aluminide coatings on gas turbine engine components |
JP2006117975A (ja) * | 2004-10-19 | 2006-05-11 | Kawasaki Heavy Ind Ltd | 遮熱コーティング構造および遮熱コーティング製造方法 |
US7186091B2 (en) * | 2004-11-09 | 2007-03-06 | General Electric Company | Methods and apparatus for cooling gas turbine engine components |
US7429424B2 (en) * | 2004-12-06 | 2008-09-30 | General Electric Company | Sintering resistant, low conductivity, high stability thermal barrier coating/environmental barrier coating system for a ceramic-matrix composite (CMC) article to improve high temperature capability |
US7364807B2 (en) * | 2004-12-06 | 2008-04-29 | General Electric Company | Thermal barrier coating/environmental barrier coating system for a ceramic-matrix composite (CMC) article to improve high temperature capability |
US7476453B2 (en) * | 2004-12-06 | 2009-01-13 | General Electric Company | Low thermal conductivity thermal barrier coating system and method therefor |
US9133718B2 (en) * | 2004-12-13 | 2015-09-15 | Mt Coatings, Llc | Turbine engine components with non-aluminide silicon-containing and chromium-containing protective coatings and methods of forming such non-aluminide protective coatings |
US7838083B1 (en) * | 2005-01-28 | 2010-11-23 | Sandia Corporation | Ion beam assisted deposition of thermal barrier coatings |
US20070292624A1 (en) * | 2005-06-28 | 2007-12-20 | General Electric Company | Low conductivity, thermal barrier coating system for ceramic matrix composite (CMC) articles |
US8603930B2 (en) | 2005-10-07 | 2013-12-10 | Sulzer Metco (Us), Inc. | High-purity fused and crushed zirconia alloy powder and method of producing same |
US20070082131A1 (en) * | 2005-10-07 | 2007-04-12 | Sulzer Metco (Us), Inc. | Optimized high purity coating for high temperature thermal cycling applications |
US7556840B2 (en) * | 2006-06-30 | 2009-07-07 | Caterpillar Inc. | Coating using metal organic chemical vapor deposition |
US7989020B2 (en) * | 2007-02-08 | 2011-08-02 | Honeywell International Inc. | Method of forming bond coating for a thermal barrier coating |
US7927714B2 (en) | 2008-08-20 | 2011-04-19 | The Trustees Of Princeton University | Barium-doped bond coat for thermal barrier coatings |
US20110139486A1 (en) * | 2009-12-16 | 2011-06-16 | General Electric Company | Electrical insulating coating and method for harsh environment |
US9249514B2 (en) | 2012-08-31 | 2016-02-02 | General Electric Company | Article formed by plasma spray |
US9970305B2 (en) * | 2015-09-18 | 2018-05-15 | General Electric Company | Treatment process, oxide-forming treatment composition, and treated component |
DE102016002630A1 (de) * | 2016-03-07 | 2017-09-07 | Forschungszentrum Jülich GmbH | Haftvermittlerschicht zur Anbindung einer Hochtemperaturschutzschicht auf einem Substrat, sowie Verfahren zur Herstellung derselben |
Family Cites Families (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3542530A (en) | 1968-05-23 | 1970-11-24 | United Aircraft Corp | Nickel or cobalt base with a coating containing iron chromium and aluminum |
DE1796175C2 (de) | 1968-09-14 | 1974-05-30 | Deutsche Edelstahlwerke Gmbh, 4150 Krefeld | Hochtemperaturkorrosions- und zunderbeständige Diffusionsschutzschicht auf Gegenständen aus hochwarmfesten Legierungen auf Nickel- und/oder Kobaltbasis |
US3754903A (en) | 1970-09-15 | 1973-08-28 | United Aircraft Corp | High temperature oxidation resistant coating alloy |
US3676085A (en) | 1971-02-18 | 1972-07-11 | United Aircraft Corp | Cobalt base coating for the superalloys |
US3928026A (en) | 1974-05-13 | 1975-12-23 | United Technologies Corp | High temperature nicocraly coatings |
US3955935A (en) | 1974-11-27 | 1976-05-11 | General Motors Corporation | Ductile corrosion resistant chromium-aluminum coating on superalloy substrate and method of forming |
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 |
US4321310A (en) * | 1980-01-07 | 1982-03-23 | United Technologies Corporation | Columnar grain ceramic thermal barrier coatings on polished substrates |
US4401697A (en) * | 1980-01-07 | 1983-08-30 | United Technologies Corporation | Method for producing columnar grain ceramic thermal barrier coatings |
US4321311A (en) * | 1980-01-07 | 1982-03-23 | United Technologies Corporation | Columnar grain ceramic thermal barrier coatings |
US4335190A (en) * | 1981-01-28 | 1982-06-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal barrier coating system having improved adhesion |
US4490191A (en) * | 1981-12-16 | 1984-12-25 | General Electric Company | Coated product and process |
US4485151A (en) * | 1982-05-06 | 1984-11-27 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Thermal barrier coating system |
US5514482A (en) * | 1984-04-25 | 1996-05-07 | Alliedsignal Inc. | Thermal barrier coating system for superalloy components |
IL75304A (en) * | 1984-06-08 | 1989-03-31 | United Technologies Corp | Coated superalloy articles and method of strengthening same |
JPS61174385A (ja) * | 1984-09-10 | 1986-08-06 | Hitachi Ltd | セラミツク被覆耐熱部材及びその製造方法 |
US4900640A (en) * | 1988-04-19 | 1990-02-13 | Inco Limited | Low coefficient of expansion alloys having a thermal barrier |
JP2695835B2 (ja) | 1988-05-06 | 1998-01-14 | 株式会社日立製作所 | セラミック被覆耐熱部材 |
US4851300A (en) * | 1988-05-09 | 1989-07-25 | United Technologies Corporation | Precoat for improving platinum thin film adhesion |
US4880614A (en) | 1988-11-03 | 1989-11-14 | Allied-Signal Inc. | Ceramic thermal barrier coating with alumina interlayer |
US4916022A (en) * | 1988-11-03 | 1990-04-10 | Allied-Signal Inc. | Titania doped ceramic thermal barrier coatings |
US5238752A (en) * | 1990-05-07 | 1993-08-24 | General Electric Company | Thermal barrier coating system with intermetallic overlay bond coat |
US5236745A (en) * | 1991-09-13 | 1993-08-17 | General Electric Company | Method for increasing the cyclic spallation life of a thermal barrier coating |
GB9204791D0 (en) * | 1992-03-05 | 1992-04-22 | Rolls Royce Plc | A coated article |
CA2091472A1 (en) * | 1992-04-17 | 1993-10-18 | William R. Young | Whisker-anchored thermal barrier coating |
US5302465A (en) * | 1992-10-26 | 1994-04-12 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Plasma sprayed ceramic thermal barrier coating for NiAl-based intermetallic alloys |
GB9426257D0 (en) * | 1994-12-24 | 1995-03-01 | Rolls Royce Plc | Thermal barrier coating for a superalloy article and method of application |
US5716720A (en) * | 1995-03-21 | 1998-02-10 | Howmet Corporation | Thermal barrier coating system with intermediate phase bondcoat |
US5512382A (en) * | 1995-05-08 | 1996-04-30 | Alliedsignal Inc. | Porous thermal barrier coating |
-
1996
- 1996-12-13 EP EP96309109A patent/EP0780484B1/de not_active Expired - Lifetime
- 1996-12-13 DE DE69615517T patent/DE69615517T2/de not_active Expired - Fee Related
- 1996-12-20 JP JP34029896A patent/JP4072213B2/ja not_active Expired - Lifetime
-
1997
- 1997-03-18 US US08/819,344 patent/US5780110A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JP4072213B2 (ja) | 2008-04-09 |
EP0780484A1 (de) | 1997-06-25 |
EP0780484B1 (de) | 2001-09-26 |
DE69615517T2 (de) | 2002-05-16 |
US5780110A (en) | 1998-07-14 |
JPH09296702A (ja) | 1997-11-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8328 | Change in the person/name/address of the agent |
Representative=s name: RUEGER UND KOLLEGEN, 73728 ESSLINGEN |
|
8339 | Ceased/non-payment of the annual fee |