SE0202833D0 - A thermal barrier coating and a method of applying such a coating - Google Patents

A thermal barrier coating and a method of applying such a coating

Info

Publication number
SE0202833D0
SE0202833D0 SE0202833A SE0202833A SE0202833D0 SE 0202833 D0 SE0202833 D0 SE 0202833D0 SE 0202833 A SE0202833 A SE 0202833A SE 0202833 A SE0202833 A SE 0202833A SE 0202833 D0 SE0202833 D0 SE 0202833D0
Authority
SE
Sweden
Prior art keywords
coating
thermal barrier
applying
barrier coating
layer
Prior art date
Application number
SE0202833A
Other languages
Swedish (sv)
Other versions
SE525925C2 (en
SE0202833L (en
Inventor
Jan Wigren
Mats-Olov Hansson
Original Assignee
Volvo Aero 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 Volvo Aero Corp filed Critical Volvo Aero Corp
Priority to SE0202833A priority Critical patent/SE525925C2/en
Publication of SE0202833D0 publication Critical patent/SE0202833D0/en
Priority to PCT/SE2003/001472 priority patent/WO2004029330A1/en
Priority to EP03798629A priority patent/EP1549782A1/en
Priority to JP2004539704A priority patent/JP4616648B2/en
Priority to AU2003265038A priority patent/AU2003265038A1/en
Priority to RU2005112706/02A priority patent/RU2325467C2/en
Publication of SE0202833L publication Critical patent/SE0202833L/en
Publication of SE525925C2 publication Critical patent/SE525925C2/en

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
    • 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
    • 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
    • C23C28/04—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 only coatings of inorganic non-metallic material
    • C23C28/042—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 only coatings of inorganic non-metallic material including a refractory ceramic layer, e.g. refractory metal oxides, ZrO2, rare earth oxides
    • 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
    • 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
    • C23C30/00—Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • 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
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Combustion & Propulsion (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Coating By Spraying Or Casting (AREA)

Abstract

A thermal barrier coating (TBC) layer (1) is deposited directly or through an intermediate bond coating (3), with respect to a metallic substrate (2). The TBC layer has an inner TBC layer (4) with a different microstructure than the outer TBC layer (5), attached directly to the substrate or to the intermediate bond coating. - Independent claims are also included for the following: - (1) coated metallic substrate; and - (2) ceramic thermal barrier coating applying method.
SE0202833A 2002-09-25 2002-09-25 Ceramic thermal barrier coating for blades of gas turbine engine, has inner thermal barrier coating layer with different microstructure than outer thermal barrier coating layer SE525925C2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
SE0202833A SE525925C2 (en) 2002-09-25 2002-09-25 Ceramic thermal barrier coating for blades of gas turbine engine, has inner thermal barrier coating layer with different microstructure than outer thermal barrier coating layer
PCT/SE2003/001472 WO2004029330A1 (en) 2002-09-25 2003-09-17 A thermal barrier coating and a method of applying such a coating
EP03798629A EP1549782A1 (en) 2002-09-25 2003-09-17 A thermal barrier coating and a method of applying such a coating
JP2004539704A JP4616648B2 (en) 2002-09-25 2003-09-17 Thermal barrier coating and method of applying such a coating
AU2003265038A AU2003265038A1 (en) 2002-09-25 2003-09-17 A thermal barrier coating and a method of applying such a coating
RU2005112706/02A RU2325467C2 (en) 2002-09-25 2003-09-17 Method of forming thermal barrier coating

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE0202833A SE525925C2 (en) 2002-09-25 2002-09-25 Ceramic thermal barrier coating for blades of gas turbine engine, has inner thermal barrier coating layer with different microstructure than outer thermal barrier coating layer

Publications (3)

Publication Number Publication Date
SE0202833D0 true SE0202833D0 (en) 2002-09-25
SE0202833L SE0202833L (en) 2004-03-26
SE525925C2 SE525925C2 (en) 2005-05-31

Family

ID=20289089

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0202833A SE525925C2 (en) 2002-09-25 2002-09-25 Ceramic thermal barrier coating for blades of gas turbine engine, has inner thermal barrier coating layer with different microstructure than outer thermal barrier coating layer

Country Status (1)

Country Link
SE (1) SE525925C2 (en)

Also Published As

Publication number Publication date
SE525925C2 (en) 2005-05-31
SE0202833L (en) 2004-03-26

Similar Documents

Publication Publication Date Title
MXPA04004205A (en) Method for applying or repairing thermal barrier coatings.
ATE434684T1 (en) CERAMIC WALL CLADDING COMPOSITE
TW200738907A (en) Thermal barrier coatings and processes for applying same
GB2469762B (en) Method for improving resistance to CMAS infiltration
ATE350512T1 (en) SUBSTRATE WITH INTERMEDIATE COATING AND HARD CARBON COATING
WO2007005832A3 (en) Reliant thermal barrier coating system and related methods and apparatus of making the same
SE0203224D0 (en) Method of making structured ceramic coatings and coated devices prepared with the method
DE60237691D1 (en) COATING COMPOSITIONS WITH IMPROVED ADHESION, COATED OBJECTS AND COATING PROCESSES
MXPA03006871A (en) Corrosion resistant coating giving polished effect.
ATE246268T1 (en) CONDENSATION COATING PROCESS
ATE485246T1 (en) THIN FILM COATING WITH A TRANSPARENT PRIMER LAYER
ITRM20030602A1 (en) MULTILAYER COATING PRODUCTION PROCEDURE
EP1959099A3 (en) Thermal barrier coating material, thermal barrier member, and member coated with thermal barrier and method for manufacturing the same
NO20013080L (en) Dirt-resistant layer for glass surfaces
SG144016A1 (en) Thermal barrier coating
DE602004021957D1 (en) HEAT-TREATABLE COATED PART WITH DIAMOND CARBON COAT (DLC) COATING
NO20082261L (en) Method of coating a component
DE60334343D1 (en) Hybrid thermal barrier coating and method of making the same
WO2002053298A3 (en) Coating method and coating agent
WO2005113175A3 (en) Functionally graded alumina-based thin film systems
FR2837218B1 (en) METAL SUBSTRATE COATING COMPOSITION
NO20041977L (en) Coating process and method of coating a substrate with a resistant layer
SG132654A1 (en) Method for applying a bond coat and a thermal barrier coating over an aluminided surface
WO2006063855A3 (en) Fine-laminar barrier protection layer
SE0202833D0 (en) A thermal barrier coating and a method of applying such a coating

Legal Events

Date Code Title Description
NUG Patent has lapsed