EP3863991A1 - Matériau céramique, couche et système de couches - Google Patents
Matériau céramique, couche et système de couchesInfo
- Publication number
- EP3863991A1 EP3863991A1 EP19812714.4A EP19812714A EP3863991A1 EP 3863991 A1 EP3863991 A1 EP 3863991A1 EP 19812714 A EP19812714 A EP 19812714A EP 3863991 A1 EP3863991 A1 EP 3863991A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- oxide
- mol
- layer
- ceramic material
- ceramic
- 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.)
- Pending
Links
Classifications
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- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/48—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on zirconium or hafnium oxides, zirconates, zircon or hafnates
- C04B35/486—Fine ceramics
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- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/62222—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products obtaining ceramic coatings
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/009—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone characterised by the material treated
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- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/45—Coating or impregnating, e.g. injection in masonry, partial coating of green or fired ceramics, organic coating compositions for adhering together two concrete elements
- C04B41/52—Multiple coating or impregnating multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/85—Coating or impregnation with inorganic materials
- C04B41/87—Ceramics
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- C04B41/00—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone
- C04B41/80—After-treatment of mortars, concrete, artificial stone or ceramics; Treatment of natural stone of only ceramics
- C04B41/81—Coating or impregnation
- C04B41/89—Coating or impregnation for obtaining at least two superposed coatings having different compositions
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- 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
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- 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
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- 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
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- 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
- C23C4/11—Oxides
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- 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
- C23C4/12—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the method of spraying
- C23C4/134—Plasma spraying
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- 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
- C23C4/18—After-treatment
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- 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
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- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
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- C04B2235/32—Metal oxides, mixed metal oxides, or oxide-forming salts thereof, e.g. carbonates, nitrates, (oxy)hydroxides, chlorides
- C04B2235/3205—Alkaline earth oxides or oxide forming salts thereof, e.g. beryllium oxide
- C04B2235/3206—Magnesium oxides or oxide-forming salts thereof
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- C04B2235/3208—Calcium oxide or oxide-forming salts thereof, e.g. lime
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- C04B2235/3244—Zirconium oxides, zirconates, hafnium oxides, hafnates, or oxide-forming salts thereof
- C04B2235/3246—Stabilised zirconias, e.g. YSZ or cerium stabilised zirconia
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
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- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/20—Oxide or non-oxide ceramics
- F05D2300/21—Oxide ceramics
- F05D2300/2118—Zirconium oxides
Definitions
- the invention relates to a ceramic material based on zirconium oxide with stabilizers, a layer and a layer system thereof.
- Turbine blades or components for high-temperature use in general are often provided with thermal insulation layers. These are mostly ceramic thermal insulation layers based on zirconium oxide, fully or partially stabilized or based on pyrochlores, such as gadolinium zirconate.
- the requirements for the ceramic thermal insulation layer are high fracture toughness and low sintering behavior, so that the mechanical loads can also be maintained over time.
- the object is achieved by ceramic material according to claim 1, a layer according to claim 12 and a layer system according to claim 15.
- Figures 1, 2 schematically show a layer system based on the invention.
- the ceramic material has a tetragonal and cubic crystal structure, which depends on the proportion of the yttrium oxide stabilizer.
- the tetragonal phase is stabilized by the proportion of yttrium oxide.
- the ceramic material on the basis of zirconium oxide (Zr0 2 ) contains yttrium oxide (Y 2 0 3 ) and at least one further, in particular two, very particularly only two further oxides selected from the group erbium oxide (Er 2 0 3 ) and ytterbium oxide ( Yb 2 0 3 ), which preferably act as stabilizers.
- At least one further oxide is optionally selected from the group:
- the proportion of yttrium oxide (Y 2 0 3 ) is preferably 2.0 mol% - 3.9 mol%, in particular 2.5 mol% - 3.5 mol%.
- erbium oxide Er 2 0 3
- Yb 2 0 3 a mol% - 4.9 mol% erbium oxide
- the proportion of ytterbium oxide (Yb 2 0 3 ) is preferably 3.5 mol% ytterbium oxide (Yb 2 0 3 ).
- the proportion of yttrium oxide (Y 2 0 3 ) is preferably
- Exemplary embodiments are: Zr0 2 / Y2O3 / Yb 2 0 3 +
- a ceramic layer can be produced from this ceramic material. All coating processes from the prior art, such as plasma spraying (APS, VPS, LPPS, ...) or HVOF, can be used to create layers.
- All coating processes from the prior art such as plasma spraying (APS, VPS, LPPS, ...) or HVOF, can be used to create layers.
- a ceramic layer made of this ceramic material has in particular a thickness of 20 ⁇ m, in particular 200 ⁇ m to 2000 ⁇ m, and is produced by atmospheric plasma spraying.
- the layer can also be produced by an EBPVD process and then preferably has a layer thickness of 20 ⁇ m to 100 ⁇ m.
- FIG. 1 shows a layer system 1 made of a substrate 4.
- the substrate 4 is preferably metallic and preferably a nickel- or cobalt-based superalloy.
- the substrate 4 can be ceramic, in particular can have a CMC material.
- connection layer 7 is present on the substrate 4.
- this is preferably a NiCoCrAlY layer 7.
- a single layer 10 made of the ceramic material according to the invention is then present on the connection layer 7.
- FIG. 2 shows a further layer system 1 ', in which the single layer is replaced by a double layer 13 by an inner layer 16, in particular based on yttrium-partially stabilized zirconium oxide, but different from the material of the outer layer and an outer one Layer 19 based on the ceramic material according to the invention.
- the ceramic connection layer 16 below is preferably a partially stabilized yttrium oxide-zirconium oxide layer, in particular with 3 mol% - 4 mol% yttrium oxide (Y2O3).
- At least the outer ceramic layer 10, 19 can be segmented (DVC).
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Ceramic Engineering (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Structural Engineering (AREA)
- Inorganic Chemistry (AREA)
- Manufacturing & Machinery (AREA)
- Composite Materials (AREA)
- General Engineering & Computer Science (AREA)
- Compositions Of Oxide Ceramics (AREA)
- Coating By Spraying Or Casting (AREA)
Abstract
L'invention concerne un matériau céramique comprenant les stabilisateurs oxyde d'yttrium et au moins l'un des matériaux oxyde d'erbium ou oxyde d'ytterbium. Elle vise à obtenir une phase stable au frittage pour un matériau céramique destiné à des couches céramiques et à un système de couches céramiques, qui présente les propriétés mécaniques et thermiques désirées même en cas de mise en oeuvre à hautes températures pendant une longue durée.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102018221940.0A DE102018221940A1 (de) | 2018-12-17 | 2018-12-17 | Keramisches Material, Schicht und Schichtsystem |
PCT/EP2019/081729 WO2020126258A1 (fr) | 2018-12-17 | 2019-11-19 | Matériau céramique, couche et système de couches |
Publications (1)
Publication Number | Publication Date |
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EP3863991A1 true EP3863991A1 (fr) | 2021-08-18 |
Family
ID=68731950
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19812714.4A Pending EP3863991A1 (fr) | 2018-12-17 | 2019-11-19 | Matériau céramique, couche et système de couches |
Country Status (6)
Country | Link |
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US (1) | US20220041510A1 (fr) |
EP (1) | EP3863991A1 (fr) |
KR (1) | KR102685012B1 (fr) |
CN (1) | CN113242845A (fr) |
DE (1) | DE102018221940A1 (fr) |
WO (1) | WO2020126258A1 (fr) |
Families Citing this family (1)
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DE102021201565A1 (de) * | 2021-02-18 | 2022-08-18 | Siemens Energy Global GmbH & Co. KG | Keramisches Material, Pulver sowie Schichtsystem |
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GB9617267D0 (en) * | 1996-08-16 | 1996-09-25 | Rolls Royce Plc | A metallic article having a thermal barrier coating and a method of application thereof |
US6812176B1 (en) * | 2001-01-22 | 2004-11-02 | Ohio Aerospace Institute | Low conductivity and sintering-resistant thermal barrier coatings |
US20080213496A1 (en) * | 2002-02-14 | 2008-09-04 | Applied Materials, Inc. | Method of coating semiconductor processing apparatus with protective yttrium-containing coatings |
US6982126B2 (en) * | 2003-11-26 | 2006-01-03 | General Electric Company | Thermal barrier coating |
US6887595B1 (en) * | 2003-12-30 | 2005-05-03 | General Electric Company | Thermal barrier coatings having lower layer for improved adherence to bond coat |
US7364802B2 (en) * | 2003-12-30 | 2008-04-29 | General Electric Company | Ceramic compositions useful in thermal barrier coatings having reduced thermal conductivity |
US20080107920A1 (en) * | 2006-01-06 | 2008-05-08 | Raymond Grant Rowe | Thermal barrier coated articles and methods of making the same |
EP2581472A1 (fr) * | 2011-10-13 | 2013-04-17 | Siemens Aktiengesellschaft | Couche double céramique à base d'oxyde de zirconium |
DE102017223879A1 (de) * | 2017-12-29 | 2019-07-04 | Siemens Aktiengesellschaft | Keramisches Material, Verfahren zur Herstellung, Schicht und Schichtsystem |
DE102018203895A1 (de) * | 2018-03-14 | 2019-09-19 | Siemens Aktiengesellschaft | Keramisches Material, Schicht und Schichtsystem |
-
2018
- 2018-12-17 DE DE102018221940.0A patent/DE102018221940A1/de not_active Withdrawn
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2019
- 2019-11-19 EP EP19812714.4A patent/EP3863991A1/fr active Pending
- 2019-11-19 CN CN201980082905.9A patent/CN113242845A/zh active Pending
- 2019-11-19 WO PCT/EP2019/081729 patent/WO2020126258A1/fr unknown
- 2019-11-19 KR KR1020217022098A patent/KR102685012B1/ko active IP Right Grant
- 2019-11-19 US US17/312,642 patent/US20220041510A1/en active Pending
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CN113242845A (zh) | 2021-08-10 |
WO2020126258A1 (fr) | 2020-06-25 |
US20220041510A1 (en) | 2022-02-10 |
KR102685012B1 (ko) | 2024-07-17 |
DE102018221940A1 (de) | 2020-06-18 |
KR20210102403A (ko) | 2021-08-19 |
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