MX9102816A - Mejoras en revestimientos de titanato de magnesio resistentes a la corrosion para turbinas de gas. - Google Patents

Mejoras en revestimientos de titanato de magnesio resistentes a la corrosion para turbinas de gas.

Info

Publication number
MX9102816A
MX9102816A MX9102816A MX9102816A MX9102816A MX 9102816 A MX9102816 A MX 9102816A MX 9102816 A MX9102816 A MX 9102816A MX 9102816 A MX9102816 A MX 9102816A MX 9102816 A MX9102816 A MX 9102816A
Authority
MX
Mexico
Prior art keywords
corrosion resistant
gas turbines
magnesium titanate
resistant magnesium
titanate coatings
Prior art date
Application number
MX9102816A
Other languages
English (en)
Inventor
Sai Kwing Lau
Original Assignee
Westinghouse Electric Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of MX9102816A publication Critical patent/MX9102816A/es

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • 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
    • C23C4/10—Oxides, borides, carbides, nitrides or silicides; Mixtures thereof
    • 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
    • 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
    • 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
    • Y10T428/12583—Component contains compound of adjacent metal
    • Y10T428/1259—Oxide
    • 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.]
    • Y10T428/12535—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
    • Y10T428/12618—Plural oxides

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • Physics & Mathematics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Physical Vapour Deposition (AREA)
MX9102816A 1991-01-07 1991-12-27 Mejoras en revestimientos de titanato de magnesio resistentes a la corrosion para turbinas de gas. MX9102816A (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/637,913 US5180285A (en) 1991-01-07 1991-01-07 Corrosion resistant magnesium titanate coatings for gas turbines

Publications (1)

Publication Number Publication Date
MX9102816A true MX9102816A (es) 1992-07-01

Family

ID=24557870

Family Applications (1)

Application Number Title Priority Date Filing Date
MX9102816A MX9102816A (es) 1991-01-07 1991-12-27 Mejoras en revestimientos de titanato de magnesio resistentes a la corrosion para turbinas de gas.

Country Status (6)

Country Link
US (1) US5180285A (es)
EP (1) EP0494389A1 (es)
JP (1) JP2601964B2 (es)
KR (1) KR920014951A (es)
CA (1) CA2058781A1 (es)
MX (1) MX9102816A (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114000139A (zh) * 2021-12-31 2022-02-01 常州市业峰汽车部件有限公司 一种铝合金轮毂的防腐工艺

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US5328753A (en) * 1992-10-30 1994-07-12 Ford Motor Company Glass sheets having painted exterior surfaces
DE4303135C2 (de) * 1993-02-04 1997-06-05 Mtu Muenchen Gmbh Wärmedämmschicht aus Keramik auf Metallbauteilen und Verfahren zu ihrer Herstellung
US5427866A (en) * 1994-03-28 1995-06-27 General Electric Company Platinum, rhodium, or palladium protective coatings in thermal barrier coating systems
DE4429756C2 (de) * 1994-08-22 2003-04-30 Alstom Gasturbinenrotor mit mehreren Reihen Laufschaufeln
GB9426257D0 (en) * 1994-12-24 1995-03-01 Rolls Royce Plc Thermal barrier coating for a superalloy article and method of application
EP0718420B1 (en) * 1994-12-24 1999-04-21 Rolls Royce Plc A method of applying a thermal barrier coating to a superalloy article and a thermal barrier coating
WO1996034128A1 (en) * 1995-04-25 1996-10-31 Siemens Aktiengesellschaft Metal substrate with an oxide layer and an anchoring layer
RU2168558C2 (ru) * 1995-07-25 2001-06-10 Сименс Акциенгезелльшафт Изделие с металлическим основным телом и способ его изготовления
US6210791B1 (en) 1995-11-30 2001-04-03 General Electric Company Article with a diffuse reflective barrier coating and a low-emissity coating thereon, and its preparation
DE19545025A1 (de) * 1995-12-02 1997-06-05 Abb Research Ltd Verfahren zur Aufbringung einer metallischen Haftschicht für keramische Wärmedämmschichten auf metallische Bauteile
US5863668A (en) * 1997-10-29 1999-01-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Controlled thermal expansion coat for thermal barrier coatings
JPH11210489A (ja) * 1998-01-29 1999-08-03 Mitsubishi Heavy Ind Ltd ガス化発電方法及びガス化発電設備
US7563504B2 (en) * 1998-03-27 2009-07-21 Siemens Energy, Inc. Utilization of discontinuous fibers for improving properties of high temperature insulation of ceramic matrix composites
US6641907B1 (en) 1999-12-20 2003-11-04 Siemens Westinghouse Power Corporation High temperature erosion resistant coating and material containing compacted hollow geometric shapes
US6977060B1 (en) * 2000-03-28 2005-12-20 Siemens Westinghouse Power Corporation Method for making a high temperature erosion resistant coating and material containing compacted hollow geometric shapes
US6235370B1 (en) 1999-03-03 2001-05-22 Siemens Westinghouse Power Corporation High temperature erosion resistant, abradable thermal barrier composite coating
US6231998B1 (en) 1999-05-04 2001-05-15 Siemens Westinghouse Power Corporation Thermal barrier coating
US6060174A (en) * 1999-05-26 2000-05-09 Siemens Westinghouse Power Corporation Bond coats for turbine components and method of applying the same
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US7690840B2 (en) 1999-12-22 2010-04-06 Siemens Energy, Inc. Method and apparatus for measuring on-line failure of turbine thermal barrier coatings
US6394755B1 (en) * 2000-01-24 2002-05-28 General Electric Company Enhanced coating system for turbine airfoil applications
US6444259B1 (en) 2001-01-30 2002-09-03 Siemens Westinghouse Power Corporation Thermal barrier coating applied with cold spray technique
US6846574B2 (en) * 2001-05-16 2005-01-25 Siemens Westinghouse Power Corporation Honeycomb structure thermal barrier coating
WO2002097162A1 (en) * 2001-05-29 2002-12-05 Mcgill University Thermal barrier coatings and fabrication of same using electrochemical methods
US6780458B2 (en) * 2001-08-01 2004-08-24 Siemens Westinghouse Power Corporation Wear and erosion resistant alloys applied by cold spray technique
US6706319B2 (en) 2001-12-05 2004-03-16 Siemens Westinghouse Power Corporation Mixed powder deposition of components for wear, erosion and abrasion resistant applications
US7504157B2 (en) * 2005-11-02 2009-03-17 H.C. Starck Gmbh Strontium titanium oxides and abradable coatings made therefrom
US7432505B2 (en) * 2006-05-04 2008-10-07 Siemens Power Generation, Inc. Infrared-based method and apparatus for online detection of cracks in steam turbine components
EP1967615A1 (de) * 2007-03-07 2008-09-10 Siemens Aktiengesellschaft Verfahren zum Aufbringen einer Wärmedämmbeschichtung und Turbinenbauteile mit einer Wärmedämmbeschichtung
EP2085498A1 (de) 2008-02-04 2009-08-05 Siemens Aktiengesellschaft Keramische Wärmedämmschichten mit erhöhter Korrosionsbeständigkeit gegen verunreinigte Brennstoffe
JP5049852B2 (ja) * 2008-04-07 2012-10-17 株式会社日立製作所 ガスタービンの部品腐食推定方法、部品寿命推定方法、ガスタービンの設計方法及びガスタービン
CN102137954A (zh) * 2008-08-29 2011-07-27 昭和电工株式会社 表面被覆的金属陶瓷构件及其制造方法
US20130323518A1 (en) * 2012-06-05 2013-12-05 General Electric Company Coating process, coating, and coated component
US11420879B2 (en) 2019-11-06 2022-08-23 Robert Bosch Gmbh Conductive, anticorrosive magnesium titanium oxide material
US11316171B2 (en) * 2019-11-06 2022-04-26 Robert Bosch Gmbh Conductive, anti-corrosive magnesium titanium oxide material
US11342566B2 (en) * 2019-11-06 2022-05-24 Robert Bosch Gmbh Conductive, anti-corrosive magnesium titanium oxide material
US11376565B2 (en) 2019-11-06 2022-07-05 Robert Bosch Gmbh Conductive, anti-corrosive magnesium titanium oxide catalyst support material

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Publication number Priority date Publication date Assignee Title
CN114000139A (zh) * 2021-12-31 2022-02-01 常州市业峰汽车部件有限公司 一种铝合金轮毂的防腐工艺
CN114000139B (zh) * 2021-12-31 2022-03-18 常州市业峰汽车部件有限公司 一种铝合金轮毂的防腐工艺

Also Published As

Publication number Publication date
CA2058781A1 (en) 1992-07-08
JPH04295102A (ja) 1992-10-20
JP2601964B2 (ja) 1997-04-23
US5180285A (en) 1993-01-19
KR920014951A (ko) 1992-08-26
EP0494389A1 (en) 1992-07-15

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Legal Events

Date Code Title Description
FG Grant or registration
MM Annulment or lapse due to non-payment of fees