ATE338150T1 - PROCEDURE FOR APPLYING A MULTI-LAYER SYSTEM - Google Patents

PROCEDURE FOR APPLYING A MULTI-LAYER SYSTEM

Info

Publication number
ATE338150T1
ATE338150T1 AT03405462T AT03405462T ATE338150T1 AT E338150 T1 ATE338150 T1 AT E338150T1 AT 03405462 T AT03405462 T AT 03405462T AT 03405462 T AT03405462 T AT 03405462T AT E338150 T1 ATE338150 T1 AT E338150T1
Authority
AT
Austria
Prior art keywords
coating
procedure
applying
layer system
rivets
Prior art date
Application number
AT03405462T
Other languages
German (de)
Inventor
Andus Suttar Khan
Reinhard Fried
Original Assignee
Alstom Technology Ltd
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 Technology Ltd filed Critical Alstom Technology Ltd
Application granted granted Critical
Publication of ATE338150T1 publication Critical patent/ATE338150T1/en

Links

Classifications

    • 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
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/02Pretreatment of the material to be coated, e.g. for coating on selected surface areas
    • 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
    • C23C28/321Coatings 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
    • C23C28/3215Coatings 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
    • 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
    • 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
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • 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
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Metallurgy (AREA)
  • Inorganic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Plasma & Fusion (AREA)
  • Physics & Mathematics (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Electroplating Methods And Accessories (AREA)
  • Production Of Multi-Layered Print Wiring Board (AREA)
  • Coating By Spraying Or Casting (AREA)

Abstract

Coating an article (1) involves placing a number of rivets (9) on top of the article surface (8) to induce segmentation of the ceramic coating, followed by depositing metallic bond coating (6) on the surface and rivets by electroplating and depositing a ceramic coating (7) on top of the metallic coating.
AT03405462T 2003-06-26 2003-06-26 PROCEDURE FOR APPLYING A MULTI-LAYER SYSTEM ATE338150T1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03405462A EP1491657B1 (en) 2003-06-26 2003-06-26 Method of applying a coating system

Publications (1)

Publication Number Publication Date
ATE338150T1 true ATE338150T1 (en) 2006-09-15

Family

ID=33396105

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03405462T ATE338150T1 (en) 2003-06-26 2003-06-26 PROCEDURE FOR APPLYING A MULTI-LAYER SYSTEM

Country Status (3)

Country Link
EP (1) EP1491657B1 (en)
AT (1) ATE338150T1 (en)
DE (1) DE60308002D1 (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005050873B4 (en) * 2005-10-21 2020-08-06 Rolls-Royce Deutschland Ltd & Co Kg Process for producing a segmented coating and component produced by the process
US8303247B2 (en) * 2007-09-06 2012-11-06 United Technologies Corporation Blade outer air seal
US8818078B2 (en) * 2012-02-03 2014-08-26 Solar Turbines Inc. Apparatus and method for optically measuring creep
WO2013144022A1 (en) 2012-03-28 2013-10-03 Alstom Technology Ltd Method for removing a ceramic
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
US10443444B2 (en) 2014-05-21 2019-10-15 United Technologies Corporation Cost effective manufacturing method for GSAC incorporating a stamped preform
EP3029274B1 (en) 2014-10-30 2020-03-11 United Technologies Corporation Thermal-sprayed bonding of a ceramic structure to a substrate
WO2016133982A1 (en) 2015-02-18 2016-08-25 Siemens Aktiengesellschaft Forming cooling passages in thermal barrier coated, combustion turbine superalloy components
WO2016133581A1 (en) 2015-02-18 2016-08-25 Siemens Aktiengesellschaft Turbine shroud with abradable layer having composite non-inflected triple angle ridges and grooves
US10995620B2 (en) 2018-06-21 2021-05-04 General Electric Company Turbomachine component with coating-capturing feature for thermal insulation

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8706951D0 (en) * 1987-03-24 1988-04-27 Baj Ltd Overlay coating
DE19545025A1 (en) * 1995-12-02 1997-06-05 Abb Research Ltd Method for applying a metallic adhesive layer for ceramic thermal insulation layers on metallic components
DE10057187B4 (en) * 2000-11-17 2011-12-08 Alstom Technology Ltd. Process for the production of composite structures between metallic and non-metallic materials
DE10121019A1 (en) * 2001-04-28 2002-10-31 Alstom Switzerland Ltd Gas turbine seal

Also Published As

Publication number Publication date
DE60308002D1 (en) 2006-10-12
EP1491657B1 (en) 2006-08-30
EP1491657A1 (en) 2004-12-29

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Legal Events

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