UA110643C2 - Стійкий до високотемпературної корозії диск або роздільник газової турбіни і спосіб отримання стійкого до викосотемпературної корозії покриття - Google Patents

Стійкий до високотемпературної корозії диск або роздільник газової турбіни і спосіб отримання стійкого до викосотемпературної корозії покриття

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Publication number
UA110643C2
UA110643C2 UAA201313180A UAA201313180A UA110643C2 UA 110643 C2 UA110643 C2 UA 110643C2 UA A201313180 A UAA201313180 A UA A201313180A UA A201313180 A UAA201313180 A UA A201313180A UA 110643 C2 UA110643 C2 UA 110643C2
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UA
Ukraine
Prior art keywords
resistant
corrosion
gas turbine
vykosotemperaturnoyi
disc
Prior art date
Application number
UAA201313180A
Other languages
English (en)
Inventor
Енн Болкавадж
Рандольф К. Хелмінк
Original Assignee
Роллс-Ройс Корпорейшн
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.)
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Publication date
Application filed by Роллс-Ройс Корпорейшн filed Critical Роллс-Ройс Корпорейшн
Publication of UA110643C2 publication Critical patent/UA110643C2/uk

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    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/02Coating 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 only coatings only including layers of metallic material
    • C23C28/023Coating 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 only coatings only including layers of metallic material only coatings of metal elements only
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/028Blade-carrying members, e.g. rotors the rotor disc being formed of sheet laminae
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/02Pretreatment of the material to be coated
    • C23C14/024Deposition of sublayers, e.g. to promote adhesion of the coating
    • C23C14/025Metallic sublayers
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    • C23COATING 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
    • C23CCOATING 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/06Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material characterised by the coating material
    • C23C14/14Metallic material, boron or silicon
    • C23C14/16Metallic material, boron or silicon on metallic substrates or on substrates of boron or silicon
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    • C23COATING 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
    • C23CCOATING 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
    • C23C14/00Coating by vacuum evaporation, by sputtering or by ion implantation of the coating forming material
    • C23C14/58After-treatment
    • C23C14/5846Reactive treatment
    • C23C14/5853Oxidation
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    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/02Coating 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 only coatings only including layers of metallic material
    • C23C28/021Coating 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 only coatings only including layers of metallic material including at least one metal alloy layer
    • CCHEMISTRY; METALLURGY
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    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321Coatings 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
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/322Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer only coatings of metal elements only
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings 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
    • C23C28/345Coatings 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
    • CCHEMISTRY; METALLURGY
    • C23COATING 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
    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings 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
    • C23C28/345Coatings 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
    • C23C28/3455Coatings 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
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    • C23CCOATING 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
    • C23C28/00Coating 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
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/36Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including layers graded in composition or physical properties
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12583Component contains compound of adjacent metal
    • Y10T428/1259Oxide
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12736Al-base component
    • Y10T428/1275Next to Group VIII or IB metal-base component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12806Refractory [Group IVB, VB, or VIB] metal-base component
    • Y10T428/12826Group VIB metal-base component
    • Y10T428/12847Cr-base component
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12875Platinum group metal-base component

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Physical Vapour Deposition (AREA)
  • Fuel Cell (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)

Abstract

Стійкий до високотемпературної корозії диск або роздільник газової турбіни може включати в себе підкладку з суперсплаву на основі нікелю, бар'єрний для дифузії шар, утворений на підкладці, а також захисний шар, утворений на бар'єрному для дифузії шарі. Бар'єрний для дифузії шар може включати в себе іридій.
UAA201313180A 2011-04-13 2012-04-13 Стійкий до високотемпературної корозії диск або роздільник газової турбіни і спосіб отримання стійкого до викосотемпературної корозії покриття UA110643C2 (uk)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201161474980P 2011-04-13 2011-04-13
PCT/US2012/033538 WO2012142422A1 (en) 2011-04-13 2012-04-13 Interfacial diffusion barrier layer including iridium on a metallic substrate

Publications (1)

Publication Number Publication Date
UA110643C2 true UA110643C2 (uk) 2016-01-25

Family

ID=46001827

Family Applications (1)

Application Number Title Priority Date Filing Date
UAA201313180A UA110643C2 (uk) 2011-04-13 2012-04-13 Стійкий до високотемпературної корозії диск або роздільник газової турбіни і спосіб отримання стійкого до викосотемпературної корозії покриття

Country Status (6)

Country Link
US (1) US9719353B2 (uk)
EP (1) EP2697408B1 (uk)
JP (1) JP5815837B2 (uk)
RU (1) RU2566697C2 (uk)
UA (1) UA110643C2 (uk)
WO (1) WO2012142422A1 (uk)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9719353B2 (en) 2011-04-13 2017-08-01 Rolls-Royce Corporation Interfacial diffusion barrier layer including iridium on a metallic substrate
US9527777B2 (en) 2013-03-11 2016-12-27 Rolls-Royce Corporation Compliant layer for ceramic components and methods of forming the same
JP6226231B2 (ja) * 2013-09-18 2017-11-08 株式会社Ihi 熱遮蔽コーティングしたNi合金部品及びその製造方法
US10266958B2 (en) * 2013-12-24 2019-04-23 United Technologies Corporation Hot corrosion-protected articles and manufacture methods
RU2606815C2 (ru) * 2014-03-06 2017-01-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ нанесения теплозащитного композитного покрытия, содержащего оксид циркония, на металлическую поверхность изделия
EP2918705B1 (en) * 2014-03-12 2017-05-03 Rolls-Royce Corporation Coating including diffusion barrier layer including iridium and oxide layer and method of coating
GB201407151D0 (en) 2014-04-23 2014-06-04 Rolls Royce Plc A method of testing the oxidation resistance of an alloy
RU2607055C2 (ru) * 2014-04-29 2017-01-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" Способ нанесения теплозащитного композитного покрытия, содержащего оксид циркония, на металлическую поверхность изделия
US9822441B2 (en) 2015-03-31 2017-11-21 WD Media, LLC Iridium underlayer for heat assisted magnetic recording media
EP3663706B1 (en) * 2018-12-06 2022-08-24 General Electric Company Quantitative multilayer assessment method
CN110172671A (zh) * 2019-06-18 2019-08-27 南通大学 一种铝或铝合金铸造模具抗开裂保护膜及制备方法
US11746877B2 (en) * 2019-12-11 2023-09-05 Rolls-Royce Corporation High strength vibration damping components
US11378230B2 (en) * 2020-07-10 2022-07-05 Uchicago Argonne, Llc High-temperature and/or high pressure gas enclosure

Family Cites Families (62)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3770487A (en) 1971-01-28 1973-11-06 Mc Donnell Douglas Corp Refractory composites
US4477538A (en) * 1981-02-17 1984-10-16 The United States Of America As Represented By The Secretary Of The Navy Platinum underlayers and overlayers for coatings
US4574015A (en) * 1983-12-27 1986-03-04 United Technologies Corporation Nickle base superalloy articles and method for making
US5499905A (en) 1988-02-05 1996-03-19 Siemens Aktiengesellschaft Metallic component of a gas turbine installation having protective coatings
USRE34173E (en) 1988-10-11 1993-02-02 Midwest Research Technologies, Inc. Multi-layer wear resistant coatings
DE3926479A1 (de) 1989-08-10 1991-02-14 Siemens Ag Rheniumhaltige schutzbeschichtung, mit grosser korrosions- und/oder oxidationsbestaendigkeit
US5059095A (en) 1989-10-30 1991-10-22 The Perkin-Elmer Corporation Turbine rotor blade tip coated with alumina-zirconia ceramic
GB9426257D0 (en) 1994-12-24 1995-03-01 Rolls Royce Plc Thermal barrier coating for a superalloy article and method of application
US5740515A (en) 1995-04-06 1998-04-14 Siemens Aktiengesellschaft Erosion/corrosion protective coating for high-temperature components
WO1996034130A1 (en) 1995-04-27 1996-10-31 Siemens Aktiengesellschaft Metal component with a high-temperature protection coating system and a method of coating the component
US5876860A (en) 1997-12-09 1999-03-02 N.V. Interturbine Thermal barrier coating ceramic structure
US6306524B1 (en) 1999-03-24 2001-10-23 General Electric Company Diffusion barrier layer
CN1223561C (zh) 1999-06-30 2005-10-19 大日本油墨化学工业株式会社 具有四氢化萘骨架的化合物及含有它的液晶组合物
FR2798654B1 (fr) 1999-09-16 2001-10-19 Snecma Composition de barriere thermique de faible conductivite thermique, piece mecanique en superalliage protegee par un revetement de ceramique ayant une telle composition, et methode de realisation du revetement de ceramique
US6207297B1 (en) 1999-09-29 2001-03-27 Siemens Westinghouse Power Corporation Barrier layer for a MCrAlY basecoat superalloy combination
US6830827B2 (en) * 2000-03-07 2004-12-14 Ebara Corporation Alloy coating, method for forming the same, and member for high temperature apparatuses
US6620525B1 (en) 2000-11-09 2003-09-16 General Electric Company Thermal barrier coating with improved erosion and impact resistance and process therefor
US6391479B1 (en) 2000-12-21 2002-05-21 General Electric Company Coating interlayer for improved compatibility between HR-120 and aluminum-containing oxidation resistant metallic coatings
US6635362B2 (en) 2001-02-16 2003-10-21 Xiaoci Maggie Zheng High temperature coatings for gas turbines
US6558813B2 (en) 2001-07-27 2003-05-06 General Electric Co. Article having a protective coating and an iridium-containing oxygen barrier layer
US6630250B1 (en) 2001-07-27 2003-10-07 General Electric Co. Article having an iridium-aluminum protective coating, and its preparation
US6532657B1 (en) 2001-09-21 2003-03-18 General Electric Co., Pre-service oxidation of gas turbine disks and seals
US7205053B2 (en) 2001-10-31 2007-04-17 Japan Science And Technology Agency Re alloy coating for diffusion barrier
US6616410B2 (en) 2001-11-01 2003-09-09 General Electric Company Oxidation resistant and/or abrasion resistant squealer tip and method for casting same
US6720088B2 (en) 2002-02-05 2004-04-13 General Electric Company Materials for protection of substrates at high temperature, articles made therefrom, and method for protecting substrates
US6861157B2 (en) 2002-03-18 2005-03-01 General Electric Company Article for high temperature service and method for manufacture
JP2003277860A (ja) 2002-03-20 2003-10-02 National Institute For Materials Science イリジウム−タンタル被覆ニッケル基超合金
JP3883461B2 (ja) 2002-03-26 2007-02-21 独立行政法人物質・材料研究機構 イリジウム−ハフニウム被覆ニッケル基超合金
US6751863B2 (en) 2002-05-07 2004-06-22 General Electric Company Method for providing a rotating structure having a wire-arc-sprayed aluminum bronze protective coating thereon
US6733908B1 (en) 2002-07-08 2004-05-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Multilayer article having stabilized zirconia outer layer and chemical barrier layer
US6926928B2 (en) 2002-07-19 2005-08-09 General Electric Company Protection of a gas turbine component by a vapor-deposited oxide coating
US7258934B2 (en) 2002-09-25 2007-08-21 Volvo Aero Corporation Thermal barrier coating and a method of applying such a coating
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
US6921251B2 (en) 2003-09-05 2005-07-26 General Electric Company Aluminide or chromide coating of turbine engine rotor component
US6974636B2 (en) 2003-09-22 2005-12-13 General Electric Company Protective coating for turbine engine component
US6933052B2 (en) 2003-10-08 2005-08-23 General Electric Company Diffusion barrier and protective coating for turbine engine component and method for forming
FR2860790B1 (fr) 2003-10-09 2006-07-28 Snecma Moteurs Cible destinee a etre evaporee sous faisceau d'electrons, son procede de fabrication, barriere thermique et revetement obtenus a partir d'une cible, et piece mecanique comportant un tel revetement
US6982126B2 (en) 2003-11-26 2006-01-03 General Electric Company Thermal barrier coating
FR2870858B1 (fr) * 2004-05-28 2007-04-06 Snecma Moteurs Sa Procede de fabrication ou de reparation d'un revetement sur un substrat metallique
US20060040129A1 (en) 2004-08-20 2006-02-23 General Electric Company Article protected by a strong local coating
US7378159B2 (en) 2004-08-20 2008-05-27 General Electric Company Protected article having a layered protective structure overlying a substrate
US7288328B2 (en) 2004-10-29 2007-10-30 General Electric Company Superalloy article having a gamma-prime nickel aluminide coating
US20060121304A1 (en) 2004-12-03 2006-06-08 General Electric Company Article protected by a diffusion-barrier layer and a plantium-group protective layer
DE102005005858A1 (de) 2005-02-08 2006-08-17 Henkel Kgaa Verfahren zur Beschichtung von Metallblech, insbesondere Zinkblech
DE102005011011A1 (de) 2005-03-10 2006-09-14 Mtu Aero Engines Gmbh Bauteil, insbesondere Gasturbinenbauteil
US7666515B2 (en) 2005-03-31 2010-02-23 General Electric Company Turbine component other than airfoil having ceramic corrosion resistant coating and methods for making same
EP1734145A1 (de) 2005-06-13 2006-12-20 Siemens Aktiengesellschaft Schichtsystem für ein Bauteil mit Wärmedämmschicht und metallischer Erosionsschutzschicht, Verfahren zur Herstellung und Verfahren zum Betreiben einer Dampfturbine
US7723249B2 (en) 2005-10-07 2010-05-25 Sulzer Metco (Us), Inc. Ceramic material for high temperature service
US20100068556A1 (en) * 2005-12-09 2010-03-18 General Electric Company Diffusion barrier layer and methods of forming
US7695830B2 (en) 2006-09-06 2010-04-13 Honeywell International Inc. Nanolaminate thermal barrier coatings
US7544424B2 (en) * 2006-11-30 2009-06-09 General Electric Company Ni-base superalloy having a coating system containing a stabilizing layer
US7416790B2 (en) 2006-12-08 2008-08-26 General Electric Company Coating systems containing rhodium aluminide-based layers
US7749570B2 (en) * 2006-12-20 2010-07-06 General Electric Company Method for depositing a platinum-group-containing layer on a substrate
JP4896702B2 (ja) 2006-12-22 2012-03-14 株式会社ディ・ビー・シー・システム研究所 合金皮膜、合金皮膜の製造方法および耐熱性金属部材
US9644273B2 (en) 2007-02-09 2017-05-09 Honeywell International Inc. Protective barrier coatings
US7766617B1 (en) 2007-03-06 2010-08-03 Florida Turbine Technologies, Inc. Transpiration cooled turbine airfoil
GB2452515B (en) 2007-09-06 2009-08-05 Siemens Ag Seal coating between rotor blade and rotor disk slot in gas turbine engine
DE102007050141A1 (de) 2007-10-19 2009-04-23 Mtu Aero Engines Gmbh Verschleißschutzbeschichtung
DE102009010110B4 (de) 2009-02-21 2014-08-28 MTU Aero Engines AG Erosionsschutz-Beschichtungssystem für Gasturbinenbauteile
US8721812B2 (en) 2009-04-07 2014-05-13 Rolls-Royce Corporation Techniques for controlling precipitate phase domain size in an alloy
GB201002679D0 (en) 2010-02-17 2010-04-07 Rolls Royce Plc Turbine disk and blade arrangement
US9719353B2 (en) 2011-04-13 2017-08-01 Rolls-Royce Corporation Interfacial diffusion barrier layer including iridium on a metallic substrate

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EP2697408B1 (en) 2018-09-12
EP2697408A1 (en) 2014-02-19
RU2566697C2 (ru) 2015-10-27
RU2013150514A (ru) 2015-05-20
WO2012142422A1 (en) 2012-10-18
JP2014513210A (ja) 2014-05-29
US9719353B2 (en) 2017-08-01
US20140134455A1 (en) 2014-05-15
JP5815837B2 (ja) 2015-11-17

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