SG161232A1 - Method for forming a thermal barrier coating - Google Patents
Method for forming a thermal barrier coatingInfo
- Publication number
- SG161232A1 SG161232A1 SG201002339-8A SG2010023398A SG161232A1 SG 161232 A1 SG161232 A1 SG 161232A1 SG 2010023398 A SG2010023398 A SG 2010023398A SG 161232 A1 SG161232 A1 SG 161232A1
- Authority
- SG
- Singapore
- Prior art keywords
- coating
- overlay coating
- barrier coating
- oxidized
- forming
- 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
- C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
-
- 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
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/073—Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
-
- 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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Plasma & Fusion (AREA)
- Physics & Mathematics (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
- Physical Vapour Deposition (AREA)
Abstract
Method including providing a nickel aluminide intermetallic overlay coating (24) on a superalloy substrate (22) and growing a controlled aluminum oxide on the overlay coating. The overlay coating is pre-oxidized to promote the growth of predominantly alpha phase alumina scale (28). The pre-oxidizing conditions may include heating the coated substrate to 1121 degree C for two to eight hours under vacuum. The pre-oxidized overlay coating may be used as an environmental coating or as a bond coat for a thermally insulating ceramic barrier coating (26). FIG.1
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US54360906A | 2006-10-05 | 2006-10-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
SG161232A1 true SG161232A1 (en) | 2010-05-27 |
Family
ID=38885294
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG201002339-8A SG161232A1 (en) | 2006-10-05 | 2007-10-05 | Method for forming a thermal barrier coating |
SG200716652-3A SG141412A1 (en) | 2006-10-05 | 2007-10-05 | Method for forming a thermal barrier coating |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200716652-3A SG141412A1 (en) | 2006-10-05 | 2007-10-05 | Method for forming a thermal barrier coating |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP1908857A3 (en) |
JP (1) | JP2008095191A (en) |
BR (1) | BRPI0705144A (en) |
CA (1) | CA2604570A1 (en) |
SG (2) | SG161232A1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2715958A1 (en) * | 2009-10-12 | 2011-04-12 | General Electric Company | Process of forming a coating system, coating system formed thereby, and components coated therewith |
US9315905B2 (en) | 2010-03-04 | 2016-04-19 | United Technologies Corporation | Coated article and coating process therefor |
US8481117B2 (en) * | 2010-03-08 | 2013-07-09 | United Technologies Corporation | Method for applying a thermal barrier coating |
US9181814B2 (en) | 2010-11-24 | 2015-11-10 | United Technology Corporation | Turbine engine compressor stator |
JP6040308B2 (en) | 2012-05-16 | 2016-12-07 | バブコック アンド ウイルコックス ボルンド エイ/エス | Heat exchanger with excellent corrosion resistance |
US9581042B2 (en) | 2012-10-30 | 2017-02-28 | United Technologies Corporation | Composite article having metal-containing layer with phase-specific seed particles and method therefor |
FR3064648B1 (en) * | 2017-03-30 | 2019-06-07 | Safran | SUPERALLIATION TURBINE PIECE AND METHOD OF MANUFACTURING THE SAME |
FR3071272B1 (en) * | 2017-09-21 | 2019-09-20 | Safran | SUPERALLY TURBINE PIECE COMPRISING RHENIUM AND / OR RUTHENIUM AND PROCESS FOR PRODUCING THE SAME |
EP3935199A4 (en) * | 2019-03-07 | 2022-10-12 | Oerlikon Metco (US) Inc. | Advanced bond coat materials for tbc with improved thermal cyclic fatigue and sulfidation resistance |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5716720A (en) * | 1995-03-21 | 1998-02-10 | Howmet Corporation | Thermal barrier coating system with intermediate phase bondcoat |
US6291084B1 (en) * | 1998-10-06 | 2001-09-18 | General Electric Company | Nickel aluminide coating and coating systems formed therewith |
US6881452B2 (en) * | 2001-07-06 | 2005-04-19 | General Electric Company | Method for improving the TBC life of a single phase platinum aluminide bond coat by preoxidation heat treatment |
DE102005036162A1 (en) * | 2005-08-02 | 2007-02-08 | Mtu Aero Engines Gmbh | Corrosion- and/or oxidation-resistant coating for nickel-based substrates, e.g. gas turbine component, comprises platinum-aluminum region with outer 2-phase and inner single-phase zones |
-
2007
- 2007-09-27 CA CA002604570A patent/CA2604570A1/en not_active Abandoned
- 2007-10-01 EP EP07117636A patent/EP1908857A3/en not_active Withdrawn
- 2007-10-03 BR BRPI0705144-1A patent/BRPI0705144A/en not_active IP Right Cessation
- 2007-10-03 JP JP2007259328A patent/JP2008095191A/en not_active Withdrawn
- 2007-10-05 SG SG201002339-8A patent/SG161232A1/en unknown
- 2007-10-05 SG SG200716652-3A patent/SG141412A1/en unknown
Also Published As
Publication number | Publication date |
---|---|
EP1908857A2 (en) | 2008-04-09 |
EP1908857A3 (en) | 2009-10-14 |
CA2604570A1 (en) | 2008-04-05 |
BRPI0705144A (en) | 2008-10-21 |
SG141412A1 (en) | 2008-04-28 |
JP2008095191A (en) | 2008-04-24 |
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