DE69707365T2 - Isolierendes, wärmedämmendes Beschichtungssystem - Google Patents
Isolierendes, wärmedämmendes BeschichtungssystemInfo
- Publication number
- DE69707365T2 DE69707365T2 DE69707365T DE69707365T DE69707365T2 DE 69707365 T2 DE69707365 T2 DE 69707365T2 DE 69707365 T DE69707365 T DE 69707365T DE 69707365 T DE69707365 T DE 69707365T DE 69707365 T2 DE69707365 T2 DE 69707365T2
- Authority
- DE
- Germany
- Prior art keywords
- insulating
- heat
- coating system
- insulating coating
- coating
- 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.)
- Revoked
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
- C23C4/02—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)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Coating By Spraying Or Casting (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US67146696A | 1996-06-27 | 1996-06-27 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69707365D1 DE69707365D1 (de) | 2001-11-22 |
DE69707365T2 true DE69707365T2 (de) | 2002-07-11 |
Family
ID=24694632
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69707365T Revoked DE69707365T2 (de) | 1996-06-27 | 1997-06-27 | Isolierendes, wärmedämmendes Beschichtungssystem |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0816526B1 (de) |
JP (2) | JP3258599B2 (de) |
DE (1) | DE69707365T2 (de) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2379448B (en) * | 1999-06-02 | 2004-03-31 | Abb Research Ltd | Coating composition for high temperature protection |
US6607789B1 (en) * | 2001-04-26 | 2003-08-19 | General Electric Company | Plasma sprayed thermal bond coat system |
EP1411210A1 (de) * | 2002-10-15 | 2004-04-21 | ALSTOM Technology Ltd | Verfahren zur Abscheidung einer ermüdungs- und oxydationsbeständigen MCrAlY-Beschichtung |
KR100509118B1 (ko) * | 2002-10-28 | 2005-08-19 | 한국전력공사 | 열 차폐 코팅의 수명연장을 위한 예산화 방법 |
US6764779B1 (en) | 2003-02-24 | 2004-07-20 | Chromalloy Gas Turbine Corporation | Thermal barrier coating having low thermal conductivity |
US6803135B2 (en) | 2003-02-24 | 2004-10-12 | Chromalloy Gas Turbine Corporation | Thermal barrier coating having low thermal conductivity |
US20050153160A1 (en) | 2004-01-12 | 2005-07-14 | Yourong Liu | Durable thermal barrier coating having low thermal conductivity |
US7927722B2 (en) * | 2004-07-30 | 2011-04-19 | United Technologies Corporation | Dispersion strengthened rare earth stabilized zirconia |
US7246996B2 (en) * | 2005-01-04 | 2007-07-24 | General Electric Company | Methods and apparatus for maintaining rotor assembly tip clearances |
DE102005053531A1 (de) * | 2005-11-08 | 2007-05-10 | Man Turbo Ag | Wärmedämmende Schutzschicht für ein Bauteil innerhalb des Heißgasbereiches einer Gasturbine |
EP1818419A1 (de) * | 2006-01-16 | 2007-08-15 | Siemens Aktiengesellschaft | Legierung, Schutzschicht und Bauteil |
WO2007112783A1 (de) | 2006-04-06 | 2007-10-11 | Siemens Aktiengesellschaft | Layered thermal barrier coating with a high porosity, and a component |
DE112008000455A5 (de) * | 2007-03-14 | 2009-12-03 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Schichtsystem und Verfahren zu dessen Herstellung |
US9725797B2 (en) | 2008-04-30 | 2017-08-08 | United Technologies Corporation | Process for forming an improved durability thick ceramic coating |
FR2947568B1 (fr) * | 2009-07-02 | 2011-07-22 | Snecma | Revetement de protection thermique pour une piece de turbomachine et son procede de realisation |
DE102010033686A1 (de) | 2010-08-06 | 2012-02-09 | Lufthansa Technik Ag | Gasturbine |
DE102012200560B4 (de) | 2012-01-16 | 2014-08-21 | Fraunhofer-Gesellschaft zur Förderung der angewandten Forschung e.V. | Verfahren zur Herstellung einer keramischen Schicht auf einer aus einer Ni-Basislegierung gebildeten Oberfläche und Gegenstand mit keramischer Schicht |
EP2644824A1 (de) | 2012-03-28 | 2013-10-02 | Siemens Aktiengesellschaft | Verfahren zur Herstellung und Wiederherstellung von keramischen Wärmedämmschichten in Gasturbinen sowie dazugehörige Gasturbine |
US20130266678A1 (en) * | 2012-04-09 | 2013-10-10 | Smith International, Inc. | Thermal insulation layer and pressure transfer medium for high pressure high temperature cell |
US9586376B2 (en) | 2012-04-09 | 2017-03-07 | Smith International, Inc. | High pressure high temperature cell |
RU2662003C2 (ru) | 2014-02-25 | 2018-07-23 | Сименс Акциенгезелльшафт | Компонент газовой турбины, газотурбинный двигатель, способ изготовления компонента газотурбинного двигателя |
US9243511B2 (en) | 2014-02-25 | 2016-01-26 | Siemens Aktiengesellschaft | Turbine abradable layer with zig zag groove pattern |
US8939706B1 (en) | 2014-02-25 | 2015-01-27 | Siemens Energy, Inc. | Turbine abradable layer with progressive wear zone having a frangible or pixelated nib surface |
US9151175B2 (en) | 2014-02-25 | 2015-10-06 | Siemens Aktiengesellschaft | Turbine abradable layer with progressive wear zone multi level ridge arrays |
WO2016133582A1 (en) | 2015-02-18 | 2016-08-25 | Siemens Aktiengesellschaft | Turbine shroud with abradable layer having dimpled forward zone |
US10408079B2 (en) | 2015-02-18 | 2019-09-10 | Siemens Aktiengesellschaft | Forming cooling passages in thermal barrier coated, combustion turbine superalloy components |
EP3333284A1 (de) * | 2016-12-08 | 2018-06-13 | Siemens Aktiengesellschaft | Zerstörungsfreies verfahren zur beurteilung der mikrostruktur von segmentierten beschichtungen |
US20190169730A1 (en) * | 2017-12-04 | 2019-06-06 | General Electric Company | Methods of forming a porous thermal barrier coating |
CN114107775B (zh) * | 2021-11-17 | 2022-09-30 | 内蒙古科技大学 | 用于航空发动机涡轮叶片的粘结层合金及其制备方法 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4248940A (en) * | 1977-06-30 | 1981-02-03 | United Technologies Corporation | Thermal barrier coating for nickel and cobalt base super alloys |
US4503130A (en) * | 1981-12-14 | 1985-03-05 | United Technologies Corporation | Prestressed ceramic coatings |
IL84067A (en) * | 1986-10-30 | 1992-03-29 | United Technologies Corp | Thermal barrier coating system |
US4936745A (en) * | 1988-12-16 | 1990-06-26 | United Technologies Corporation | Thin abradable ceramic air seal |
US5536022A (en) * | 1990-08-24 | 1996-07-16 | United Technologies Corporation | Plasma sprayed abradable seals for gas turbine engines |
US5350599A (en) * | 1992-10-27 | 1994-09-27 | General Electric Company | Erosion-resistant thermal barrier coating |
-
1997
- 1997-06-27 EP EP97304676A patent/EP0816526B1/de not_active Revoked
- 1997-06-27 JP JP17138597A patent/JP3258599B2/ja not_active Expired - Fee Related
- 1997-06-27 DE DE69707365T patent/DE69707365T2/de not_active Revoked
-
2001
- 2001-10-02 JP JP2001306089A patent/JP3434504B2/ja not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
JPH1068089A (ja) | 1998-03-10 |
EP0816526B1 (de) | 2001-10-17 |
EP0816526A3 (de) | 1998-01-28 |
DE69707365D1 (de) | 2001-11-22 |
JP2002180270A (ja) | 2002-06-26 |
JP3434504B2 (ja) | 2003-08-11 |
JP3258599B2 (ja) | 2002-02-18 |
EP0816526A2 (de) | 1998-01-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8331 | Complete revocation |