SG107586A1 - Improved plasma sprayed thermal bond coat system - Google Patents
Improved plasma sprayed thermal bond coat systemInfo
- Publication number
- SG107586A1 SG107586A1 SG200202358A SG200202358A SG107586A1 SG 107586 A1 SG107586 A1 SG 107586A1 SG 200202358 A SG200202358 A SG 200202358A SG 200202358 A SG200202358 A SG 200202358A SG 107586 A1 SG107586 A1 SG 107586A1
- Authority
- SG
- Singapore
- Prior art keywords
- bond coat
- thermal bond
- plasma sprayed
- coat system
- improved plasma
- 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
- C23C28/3455—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/32—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
- C23C28/321—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy 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
- 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
- C23C28/30—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
- C23C28/34—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
- C23C28/345—Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide 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
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
- Y10T428/12611—Oxide-containing component
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12771—Transition metal-base component
- Y10T428/12861—Group VIII or IB metal-base component
- Y10T428/12944—Ni-base component
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Inorganic Chemistry (AREA)
- Metallurgy (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Ceramic Engineering (AREA)
- Coating By Spraying Or Casting (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/842,503 US6607789B1 (en) | 2001-04-26 | 2001-04-26 | Plasma sprayed thermal bond coat system |
Publications (1)
Publication Number | Publication Date |
---|---|
SG107586A1 true SG107586A1 (en) | 2004-12-29 |
Family
ID=25287477
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG200202358A SG107586A1 (en) | 2001-04-26 | 2002-04-22 | Improved plasma sprayed thermal bond coat system |
Country Status (6)
Country | Link |
---|---|
US (1) | US6607789B1 (de) |
EP (1) | EP1254967B1 (de) |
JP (1) | JP4191427B2 (de) |
BR (1) | BR0201425A (de) |
DE (1) | DE60234484D1 (de) |
SG (1) | SG107586A1 (de) |
Families Citing this family (53)
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US7150922B2 (en) * | 2000-03-13 | 2006-12-19 | General Electric Company | Beta-phase nickel aluminide overlay coatings and process therefor |
EP1327702A1 (de) | 2002-01-10 | 2003-07-16 | ALSTOM (Switzerland) Ltd | MCrAlY-Haftschicht und Verfahren zur Herstellung einer MCrAlY-Haftschichtbeschichtung |
US6887589B2 (en) * | 2003-04-18 | 2005-05-03 | General Electric Company | Nickel aluminide coating and coating systems formed therewith |
US7094450B2 (en) * | 2003-04-30 | 2006-08-22 | General Electric Company | Method for applying or repairing thermal barrier coatings |
US20050123783A1 (en) * | 2003-07-31 | 2005-06-09 | Gregory Otto J. | Composite used for thermal spray instrumentation and method for making the same |
FR2858613B1 (fr) * | 2003-08-07 | 2006-12-08 | Snecma Moteurs | Composition de barriere thermique, piece mecanique en superalliage munie d'un revetement ayant une telle composition, revetement de ceramique, et procede de fabrication du revetement |
US6933052B2 (en) * | 2003-10-08 | 2005-08-23 | General Electric Company | Diffusion barrier and protective coating for turbine engine component and method for forming |
US7371426B2 (en) | 2003-11-13 | 2008-05-13 | General Electric Company | Method for repairing components using environmental bond coatings and resultant repaired components |
US7094444B2 (en) * | 2003-11-13 | 2006-08-22 | General Electric Company | Method for repairing coated components using NiAl bond coats |
US7078073B2 (en) | 2003-11-13 | 2006-07-18 | General Electric Company | Method for repairing coated components |
US20070104886A1 (en) * | 2005-11-10 | 2007-05-10 | General Electric Company | Electrostatic spray for coating aircraft engine components |
US7509735B2 (en) * | 2004-04-22 | 2009-03-31 | Siemens Energy, Inc. | In-frame repairing system of gas turbine components |
US20060045785A1 (en) * | 2004-08-30 | 2006-03-02 | Yiping Hu | Method for repairing titanium alloy components |
US20070023402A1 (en) * | 2005-07-26 | 2007-02-01 | United Technologies Corporation | Methods for repairing workpieces using microplasma spray coating |
US7416788B2 (en) * | 2005-06-30 | 2008-08-26 | Honeywell International Inc. | Thermal barrier coating resistant to penetration by environmental contaminants |
US7462378B2 (en) * | 2005-11-17 | 2008-12-09 | General Electric Company | Method for coating metals |
CA2568971A1 (en) * | 2005-11-29 | 2007-05-29 | General Electric Company | Method for applying a bond coat and a thermal barrier coating over an aluminided surface |
US7413778B2 (en) * | 2005-12-05 | 2008-08-19 | General Electric Company | Bond coat with low deposited aluminum level and method therefore |
CN100387775C (zh) * | 2006-04-13 | 2008-05-14 | 山东科技大学 | 耐磨型造纸涂布刮刀 |
CN100432333C (zh) * | 2006-05-12 | 2008-11-12 | 戴亚洲 | 一种陶瓷涂层刮刀及其制造方法 |
JP4716328B2 (ja) * | 2006-07-05 | 2011-07-06 | 財団法人電力中央研究所 | 遮熱コーティングの寿命管理方法 |
JP4716329B2 (ja) * | 2006-07-05 | 2011-07-06 | 財団法人電力中央研究所 | 遮熱コーティングの寿命管理方法 |
US20080066288A1 (en) * | 2006-09-08 | 2008-03-20 | General Electric Company | Method for applying a high temperature anti-fretting wear coating |
US20080145643A1 (en) * | 2006-12-15 | 2008-06-19 | United Technologies Corporation | Thermal barrier coating |
US7763326B2 (en) * | 2006-12-20 | 2010-07-27 | United Technologies Corporation | Photocurable maskant composition and method of use |
EP1939315A1 (de) * | 2006-12-21 | 2008-07-02 | Siemens AG | Bauteil mit einem Substrat und einer Schutzschicht |
US20090035485A1 (en) * | 2007-08-02 | 2009-02-05 | United Technologies Corporation | Method for forming active-element aluminide diffusion coatings |
US20090134035A1 (en) * | 2007-08-02 | 2009-05-28 | United Technologies Corporation | Method for forming platinum aluminide diffusion coatings |
US20090136664A1 (en) * | 2007-08-02 | 2009-05-28 | United Technologies Corporation | Method for forming aluminide diffusion coatings |
US8608049B2 (en) | 2007-10-10 | 2013-12-17 | Zimmer, Inc. | Method for bonding a tantalum structure to a cobalt-alloy substrate |
EP2217736B1 (de) * | 2007-10-26 | 2019-03-27 | The Secretary, Department Of Atomic Energy, Govt. of India | Verfahren zur herstellung einer beschichtung aus kubisch-raumzentriertem (b2) nickelaluminid (nial) mit kontrollierter dicke auf nickelbasislegierungsoberflächen |
EP2072205A1 (de) * | 2007-12-17 | 2009-06-24 | Rovalma SA | Verfahren zum Herstellen von Teilen mit hoher mechanischer Belastung und insbesondere Werkzeuge aus kostengünstigen Keramiken oder Polymeren |
JP4591722B2 (ja) * | 2008-01-24 | 2010-12-01 | 信越化学工業株式会社 | セラミックス溶射部材の製造方法 |
US8128887B2 (en) * | 2008-09-05 | 2012-03-06 | Uop Llc | Metal-based coatings for inhibiting metal catalyzed coke formation in hydrocarbon conversion processes |
US20100081009A1 (en) * | 2008-09-26 | 2010-04-01 | General Electric Company | Spray Application of Liquid Precursors for CMAS Resistant Coatings |
WO2010070982A1 (ja) * | 2008-12-16 | 2010-06-24 | 旭硝子株式会社 | フロートガラス製造設備用皮膜付き金属部材およびフロートガラス製造方法 |
US8722202B2 (en) * | 2008-12-31 | 2014-05-13 | General Electric Company | Method and system for enhancing heat transfer of turbine engine components |
FR2941963B1 (fr) * | 2009-02-10 | 2011-03-04 | Snecma | Methode de fabrication d'une barriere thermique recouvrant un substrat metallique en superalliage et piece thermomecanique resultant de cette methode de fabrication |
US20100243464A1 (en) * | 2009-03-26 | 2010-09-30 | Honeywell International Inc. | Methods of forming coatings on substrates |
US8481117B2 (en) * | 2010-03-08 | 2013-07-09 | United Technologies Corporation | Method for applying a thermal barrier coating |
FR2961528B1 (fr) * | 2010-06-18 | 2012-07-20 | Snecma | Procede d'aluminisation d'une surface avec depot prealable d'une couche de platine et de nickel |
CN103047852A (zh) * | 2012-12-17 | 2013-04-17 | 吴江市金平华纺织有限公司 | 一种印染机用烘干筒 |
CN103911620B (zh) * | 2013-01-09 | 2017-11-10 | 中国科学院宁波材料技术与工程研究所 | 一种抗热冲击金属基涂层的制备方法 |
EP2884048A1 (de) * | 2013-12-13 | 2015-06-17 | Siemens Aktiengesellschaft | Wärmedämmbeschichtung einer Turbinenschaufel |
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 |
WO2015130521A2 (en) | 2014-02-25 | 2015-09-03 | Siemens Aktiengesellschaft | Turbine component cooling hole within a microsurface feature that protects adjoining thermal barrier coating |
US9151175B2 (en) | 2014-02-25 | 2015-10-06 | Siemens Aktiengesellschaft | Turbine abradable layer with progressive wear zone multi level ridge arrays |
WO2016133581A1 (en) | 2015-02-18 | 2016-08-25 | Siemens Aktiengesellschaft | Turbine shroud with abradable layer having composite non-inflected triple angle ridges and grooves |
WO2016133982A1 (en) | 2015-02-18 | 2016-08-25 | Siemens Aktiengesellschaft | Forming cooling passages in thermal barrier coated, combustion turbine superalloy components |
RU2665647C2 (ru) * | 2017-01-30 | 2018-09-03 | Федеральное государственное бюджетное учреждение науки Институт теоретической и прикладной механики им. С.А. Христиановича Сибирского отделения Российской академии наук (ИТПМ СО РАН) | Способ плазменного напыления износостойких покрытий толщиной более 2мм |
EP3904555A4 (de) * | 2018-12-29 | 2022-10-19 | Kunming University Of Science And Technology | Ultralimit-legierung und herstellungsverfahren dafür |
CN112553625B (zh) * | 2020-12-04 | 2022-05-06 | 中国科学院金属研究所 | 一种活性元素Hf改性的β-NiAl涂层及其制备工艺 |
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DE4417384C1 (de) * | 1994-05-18 | 1995-01-12 | Hans Leistner Gmbh Suedd Metal | Beschichtung für Flugkörper, insbesondere für die Vorderkante des Höhenleitwerkes von Flugzeugen und Verfahren zum Aufbringen der Beschichtung |
DE69707365T2 (de) * | 1996-06-27 | 2002-07-11 | United Technologies Corp., Hartford | Isolierendes, wärmedämmendes Beschichtungssystem |
US5817371A (en) * | 1996-12-23 | 1998-10-06 | General Electric Company | Thermal barrier coating system having an air plasma sprayed bond coat incorporating a metal diffusion, and method therefor |
US5975852A (en) | 1997-03-31 | 1999-11-02 | General Electric Company | Thermal barrier coating system and method therefor |
JP3386689B2 (ja) * | 1997-05-16 | 2003-03-17 | スズキ株式会社 | 摺動部材 |
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US5817372A (en) | 1997-09-23 | 1998-10-06 | General Electric Co. | Process for depositing a bond coat for a thermal barrier coating system |
US6096381A (en) | 1997-10-27 | 2000-08-01 | General Electric Company | Process for densifying and promoting inter-particle bonding of a bond coat for a thermal barrier coating |
US6190124B1 (en) * | 1997-11-26 | 2001-02-20 | United Technologies Corporation | Columnar zirconium oxide abrasive coating for a gas turbine engine seal system |
US5972424A (en) | 1998-05-21 | 1999-10-26 | United Technologies Corporation | Repair of gas turbine engine component coated with a thermal barrier coating |
EP0985745B1 (de) * | 1998-09-08 | 2006-07-12 | General Electric Company | Haftbeschichtung für wärmedämmendes Beschichtungssystem |
US6153313A (en) * | 1998-10-06 | 2000-11-28 | General Electric Company | Nickel aluminide coating and coating systems formed therewith |
US6074706A (en) | 1998-12-15 | 2000-06-13 | General Electric Company | Adhesion of a ceramic layer deposited on an article by casting features in the article surface |
US6165628A (en) * | 1999-08-30 | 2000-12-26 | General Electric Company | Protective coatings for metal-based substrates and related processes |
-
2001
- 2001-04-26 US US09/842,503 patent/US6607789B1/en not_active Expired - Lifetime
-
2002
- 2002-04-16 EP EP02252672A patent/EP1254967B1/de not_active Revoked
- 2002-04-16 DE DE60234484T patent/DE60234484D1/de not_active Expired - Lifetime
- 2002-04-22 SG SG200202358A patent/SG107586A1/en unknown
- 2002-04-25 BR BR0201425-4A patent/BR0201425A/pt not_active IP Right Cessation
- 2002-04-26 JP JP2002125432A patent/JP4191427B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US6607789B1 (en) | 2003-08-19 |
BR0201425A (pt) | 2003-06-10 |
EP1254967B1 (de) | 2009-11-25 |
EP1254967A1 (de) | 2002-11-06 |
DE60234484D1 (de) | 2010-01-07 |
JP4191427B2 (ja) | 2008-12-03 |
US20030157363A1 (en) | 2003-08-21 |
JP2002348681A (ja) | 2002-12-04 |
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