AU2003202402A1 - Method for producing a component having a high thermal loading capacity and coated with a heat-protective layer - Google Patents

Method for producing a component having a high thermal loading capacity and coated with a heat-protective layer

Info

Publication number
AU2003202402A1
AU2003202402A1 AU2003202402A AU2003202402A AU2003202402A1 AU 2003202402 A1 AU2003202402 A1 AU 2003202402A1 AU 2003202402 A AU2003202402 A AU 2003202402A AU 2003202402 A AU2003202402 A AU 2003202402A AU 2003202402 A1 AU2003202402 A1 AU 2003202402A1
Authority
AU
Australia
Prior art keywords
coated
producing
heat
component
protective layer
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.)
Abandoned
Application number
AU2003202402A
Other versions
AU2003202402A8 (en
Inventor
Karima Belaroui
Paul Bowen
Heinrich Hofmann
Maxim Konter
Valery Shklover
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Technology GmbH
Original Assignee
Alstom Schweiz AG
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 Alstom Schweiz AG filed Critical Alstom Schweiz AG
Publication of AU2003202402A8 publication Critical patent/AU2003202402A8/en
Publication of AU2003202402A1 publication Critical patent/AU2003202402A1/en
Abandoned legal-status Critical Current

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
    • C23C28/32—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
    • C23C28/3215—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 at least one MCrAlX 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
    • 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
AU2003202402A 2002-02-15 2003-02-11 Method for producing a component having a high thermal loading capacity and coated with a heat-protective layer Abandoned AU2003202402A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH267/02 2002-02-15
CH2672002 2002-02-15
PCT/CH2003/000100 WO2003068673A2 (en) 2002-02-15 2003-02-11 Method for producing a component having a high thermal loading capacity and coated with a heat-protective layer

Publications (2)

Publication Number Publication Date
AU2003202402A8 AU2003202402A8 (en) 2003-09-04
AU2003202402A1 true AU2003202402A1 (en) 2003-09-04

Family

ID=27672004

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003202402A Abandoned AU2003202402A1 (en) 2002-02-15 2003-02-11 Method for producing a component having a high thermal loading capacity and coated with a heat-protective layer

Country Status (2)

Country Link
AU (1) AU2003202402A1 (en)
WO (1) WO2003068673A2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10752999B2 (en) 2016-04-18 2020-08-25 Rolls-Royce Corporation High strength aerospace components
US10763715B2 (en) 2017-12-27 2020-09-01 Rolls Royce North American Technologies, Inc. Nano-crystalline coating for magnet retention in a rotor assembly

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE59201616D1 (en) * 1991-03-27 1995-04-13 Krupp Widia Gmbh COMPOSITE BODY, USE OF THE COMPOSITE BODY AND METHOD FOR THE PRODUCTION THEREOF.
DE4432235A1 (en) * 1994-09-10 1996-03-14 Bayerische Motoren Werke Ag Scratch-resistant coating on a thermally resistant substrate and process for its production
US5683761A (en) * 1995-05-25 1997-11-04 General Electric Company Alpha alumina protective coatings for bond-coated substrates and their preparation
EP0780484B1 (en) * 1995-12-22 2001-09-26 General Electric Company Thermal barrier coated articles and method for coating
DE19807359A1 (en) * 1998-02-21 1999-08-26 Deutsch Zentr Luft & Raumfahrt Thermal insulation layer system with integrated aluminum oxide layer
JP3411823B2 (en) * 1998-06-29 2003-06-03 三菱重工業株式会社 High temperature member and method of manufacturing the same
US6472018B1 (en) * 2000-02-23 2002-10-29 Howmet Research Corporation Thermal barrier coating method

Also Published As

Publication number Publication date
WO2003068673A2 (en) 2003-08-21
AU2003202402A8 (en) 2003-09-04
WO2003068673A3 (en) 2003-10-16

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase