WO2019179722A1 - Keramisches material auf der basis von zirkonoxid mit weiteren oxiden - Google Patents

Keramisches material auf der basis von zirkonoxid mit weiteren oxiden Download PDF

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Publication number
WO2019179722A1
WO2019179722A1 PCT/EP2019/054650 EP2019054650W WO2019179722A1 WO 2019179722 A1 WO2019179722 A1 WO 2019179722A1 EP 2019054650 W EP2019054650 W EP 2019054650W WO 2019179722 A1 WO2019179722 A1 WO 2019179722A1
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Prior art keywords
oxide
ceramic material
material according
oxides
base
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PCT/EP2019/054650
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English (en)
French (fr)
Inventor
Arturo Flores Renteria
Werner Stamm
Original Assignee
Siemens Aktiengesellschaft
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Publication date
Application filed by Siemens Aktiengesellschaft filed Critical Siemens Aktiengesellschaft
Priority to CN201980021284.3A priority Critical patent/CN111971261A/zh
Priority to EP19710306.2A priority patent/EP3743402A1/de
Priority to RU2020127787A priority patent/RU2020127787A/ru
Priority to US16/979,099 priority patent/US20200407282A1/en
Publication of WO2019179722A1 publication Critical patent/WO2019179722A1/de

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    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/30Composition of layers of ceramic laminates or of ceramic or metallic articles to be joined by heating, e.g. Si substrates
    • C04B2237/40Metallic
    • C04B2237/405Iron metal group, e.g. Co or Ni
    • CCHEMISTRY; METALLURGY
    • C04CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
    • C04BLIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
    • C04B2237/00Aspects relating to ceramic laminates or to joining of ceramic articles with other articles by heating
    • C04B2237/50Processing aspects relating to ceramic laminates or to the joining of ceramic articles with other articles by heating
    • C04B2237/70Forming laminates or joined articles comprising layers of a specific, unusual thickness
    • C04B2237/704Forming laminates or joined articles comprising layers of a specific, unusual thickness of one or more of the ceramic layers or articles
    • 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
    • F01D5/284Selection of ceramic materials
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/30Manufacture with deposition of material
    • F05D2230/31Layer deposition
    • F05D2230/313Layer deposition by physical vapour deposition
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/90Coating; Surface treatment
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/10Metals, alloys or intermetallic compounds
    • F05D2300/17Alloys
    • F05D2300/175Superalloys
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/21Oxide ceramics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/20Oxide or non-oxide ceramics
    • F05D2300/21Oxide ceramics
    • F05D2300/2118Zirconium oxides

Definitions

  • the invention relates to a ceramic material, which in particular special for the use of ceramic layers can be used.
  • the use of zirconia-based ceramic materials is known from the use of solid ceramic ceramic blades or ceramic protective coatings on turbine blades or high temperature components. It is important that a high sintering resistance, a phase stability, a high fracture toughness and high expansion tolerance is given.
  • the object is achieved by a ceramic material according to claim 1.
  • the figures 1, 2 schematically layer systems of a ceramic material.
  • CeCg cerium oxide
  • CaO calcium oxide
  • MgO magnesium oxide
  • Er203 erbium oxide
  • Yb203 ytterbium oxide
  • Such a ceramic layer has, in particular, a layer thickness of 20 ⁇ m to 100 ⁇ m, in particular up to 2000 ⁇ m, and can preferably be produced by means of thermal spraying, in particular APS or EB-PVD.
  • the ceramic material has a high sintering resistance, a high elongation tolerance and high fracture toughness and has a lower thermal conductivity.
  • FIG. 1 shows a layer system 1 according to the invention.
  • the layer system 1 has a substrate 4.
  • the substrate 4 is in particular a nickel-base superalloy or represents a CMC substrate.
  • a bonding layer is present, in particular in a nickel-based superalloy a
  • NiCoCrAlY-based alloy or an aluminide or a platinum aluminide layer.
  • TGO An oxide layer (TGO) is formed on this metallic adhesion promoter layer during coating or during operation.
  • a ceramic to binding layer 13 is present for the purpose of adaptation of thermal expansion coefficients or adaptation of the porosities.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Organic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Inorganic Chemistry (AREA)
  • Structural Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Composite Materials (AREA)
  • Manufacturing & Machinery (AREA)
  • Health & Medical Sciences (AREA)
  • Toxicology (AREA)
  • General Engineering & Computer Science (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

Durch gezielte Auswahl der Zugaben von Oxiden zu Zirkonoxid wird ein keramisches Material bereitgestellt, insbesondere für die Verwendung eines Schichtsystems, das einen hohen Sinterwiderstand, hohe Dehnungstoleranz und geringe Wärmeleitfähigkeit aufweist.

Description

Keramisches Material auf der Basis von Zirkonoxid mit weiteren Oxiden
Die Erfindung betrifft ein keramisches Material, was insbe sondere zur Verwendung von keramischen Schichten verwendet werden kann. Die Verwendung von Zirkonoxid-basierten kerami schen Materialien sind aus der Verwendung für keramische Hit zeschilde aus Vollmaterial oder keramische Schutzschichten auf Turbinenschaufeln oder Hochtemperaturbauteilen bekannt. Dabei ist es wichtig, dass ein hoher Sinterwiderstand, eine Phasenstabilität, eine hohe Bruchzähigkeit und hohe Dehnungs toleranz gegeben ist.
Es ist daher Aufgabe der Erfindung bestehende Materialsysteme zu verbessern.
Die Aufgabe wird gelöst durch ein keramisches Material gemäß Anspruch 1.
In den weiteren Unteransprüchen sind weitere Vorteile aufge listet, die beliebig miteinander kombiniert werden können, um weitere Vorteile zu erzielen.
Es zeigen die Figuren 1, 2 schematisch Schichtsysteme aus einem keramischen Material.
Es wird vorgeschlagen, 4mol% bis 30mol% Ceroxid (CeCg) , Cal ciumoxid (CaO) und/oder Magnesiumoxid (MgO) als weitere op tionale Oxide und als Basisoxid 2mol% bis 30mol% Erbiumoxid (Er203) und/oder Ytterbiumoxid (Yb203) zu verwenden.
Eine solche keramische Schicht hat insbesondere eine Schicht dicke von 20ym bis lOOOym, insbesondere bis 2000ym und kann vorzugsweise mittels thermischem Spritzen, insbesondere APS oder EB-PVD hergestellt werden. Das keramische Material hat einen hohen Sinterwiderstand, eine hohe Dehnungstoleranz und hohe Bruchzähigkeit sowie weist es eine geringere Wärmeleitfähigkeit auf.
Ausführungsbeispiele :
ZrO2 +
- Er2<D3 + Yb203
- Yb203
- Er2<D3 (3 Varianten mit Basisoxiden)
Zu diesen 3 Varianten können jeweils
- Ce02
- CaO
- MgO
- Ce02 + CaO
- Ce02 + MgO
- CaO + MgO
- Ce02 + CaO + MgO
als weitere Oxide hinzugegeben werden, also insgesamt 21 Varianten .
Figur 1 zeigt ein erfindungsgemäßes Schichtsystem 1.
Das Schichtsystem 1 weist ein Substrat 4 auf. Das Substrat 4 ist insbesondere eine Nickelbasis-Superlegierung oder stellt ein CMC-Substrat dar.
Auf dem Substrat 4 ist eine Anbindungsschicht vorhanden, die insbesondere bei einer Nickelbasis-Superlegierung eine
NiCoCrAlY-basierte Legierung oder eine Aluminid- bzw. eine Platin-Aluminidschicht darstellt .
Auf dieser metallischen Haftvermittlerschicht bildet sich während des Beschichtens oder während des Betriebs eine Oxid schicht (TGO) aus.
Auf dieser Oxidschicht (TGO) oder auf der metallischen Haft vermittlerschicht 7 ist eine keramische Schicht gemäß dem keramischen Material aufgebracht. Im Falle eines keramischen Substrats 4 (CMC) ist gegebenen falls keine Anbindungsschicht für die keramische Schicht 10 notwendig . In Figur 2 ist eine Variante gezeigt, bei der das Schichtsys tem 1 ' bezüglich der keramischen Schutzschicht zweilagig aus gebildet ist. Bezüglich des Substrats und/oder der Substrat materialien der Anbindungsschicht 7 gilt vergleichbares bei Figur 1. Jedoch bildet die äußerste keramische Schicht 16 hier das keramische Material der Erfindung.
Unter dieser keramischen Schicht 16 ist eine keramische An bindungsschicht 13 vorhanden zwecks Anpassung von thermischen Ausdehnungskoeffizienten oder Anpassung der Porositäten.

Claims

Patentansprüche
1. Keramisches Material
auf der Basis von Zirkonoxid (Zr02)
mit Ytterbiumoxid (Yb203) und/oder Erbiumoxid (E^Ct) als Basisoxid oder Basisoxide sowie
optional zumindest einem weiteren Oxid ausgewählt aus der Gruppe: Ceroxid (Ce02) , Calciumoxid (CaO) und Magnesiumoxid (MgO) ,
insbesondere daraus besteht.
2 Keramisches Material nach Anspruch 1,
bei dem Erbiumoxid (Er203) und Ytterbiumoxid (Yb203) als Basisoxide verwendet werden,
insbesondere nur diese beiden als Oxide.
3. Keramisches Material nach Anspruch 1,
bei dem nur Erbiumoxid (Er203) als Basisoxid verwendet wird,
insbesondere nur dieses als Oxid.
4. Keramisches Material nach Anspruch 1,
bei dem nur Ytterbiumoxid (Yb203) als Basisoxid verwendet wird,
insbesondere nur dieses als Oxid.
5. Keramisches Material nach einem oder mehreren der An sprüche 1, 2, 3 oder 4,
aufweisend ein Basisoxid oder Basisoxide sowie zumindest ein weiteres Oxid.
6. Keramisches Material nach Anspruch 1, 2, 3, 4 oder 5, bei dem Calciumoxid (CaO) und Ceroxid (CeÜ2) als weitere Oxide verwendet werden,
insbesondere nur diese als weitere Oxide.
7. Keramisches Material nach Anspruch 1, 2, 3, 4 oder 5, bei dem Calciumoxid (CaO) und Magnesiumoxid (MgO) als wei tere Oxide verwendet werden,
insbesondere nur diese als weitere Oxide.
8. Keramisches Material nach Anspruch 1, 2, 3, 4 oder 5, bei dem Magnesiumoxid (MgÜ2) und Ceroxid (CeÜ2) als weitere Oxide verwendet werden,
insbesondere nur diese als weitere Oxide.
9. Keramisches Material nach Anspruch 1, 2, 3, 4 oder 5, bei dem Ceroxid (CeÜ2) als weiteres Oxid verwendet wird, insbesondere nur dieses als weiteres Oxid.
10. Keramisches Material nach einem oder mehreren der An sprüche 1, 2, 3, 4 oder 5,
bei dem Magnesiumoxid (MgO) als weiteres Oxid verwendet wird,
insbesondere nur dieses als weiteres Oxid.
11. Keramisches Material nach einem oder mehreren der An sprüche 1, 2, 3, 4 oder 5,
bei dem Magnesiumoxid (MgO) , Calciumoxid (CaO) und Ceroxid (CeÜ2) als weitere Oxide verwendet werden,
insbesondere nur diese als weitere Oxide.
12. Keramisches Material nach einem oder mehreren der An sprüche 1 bis 11,
das 2mol% - 30mol% Ytterbiumoxid (Yb203) und/oder Erbium oxid (Er203) aufweist.
13. Keramisches Material nach einem oder mehreren der An sprüche 1 bis 12,
das 4mol% - 30mol% Ceroxid (Ce02 ) , Calciumoxid (CaO) und/oder Magnesiumoxid (MgO) aufweist.
14. Schichtsystem,
aufweisend ein Substrat,
insbesondere ein metallisches Substrat,
auf der Basis einer Nickel- oder Kobalt-basierten Super legierung,
eine Anbindungsschicht,
insbesondere eine Anbindungsschicht auf der Basis
NiCoCrAlY,
sowie eine keramische Schicht auf der Basis eines kerami schen Materials nach einem oder mehreren der vorherigen An sprüche 1 bis 13.
15. Schichtsystem nach Anspruch 14,
aufweisend eine Schichtdicke für die keramische Schicht von 20ym bis lOOOym,
insbesondere bis 2000ym,
ganz insbesondere hergestellt mittels thermischem Spritzen, insbesondere APS oder EB-PVD.
PCT/EP2019/054650 2018-03-23 2019-02-26 Keramisches material auf der basis von zirkonoxid mit weiteren oxiden WO2019179722A1 (de)

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CN201980021284.3A CN111971261A (zh) 2018-03-23 2019-02-26 基于氧化锆并且具有其他氧化物的陶瓷材料
EP19710306.2A EP3743402A1 (de) 2018-03-23 2019-02-26 Keramisches material auf der basis von zirkonoxid mit weiteren oxiden
RU2020127787A RU2020127787A (ru) 2018-03-23 2019-02-26 Керамический материал на основе оксида циркония с дополнительными оксидами
US16/979,099 US20200407282A1 (en) 2018-03-23 2019-02-26 Ceramic material based on zirconium oxide with further oxides

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US20200407282A1 (en) 2020-12-31
RU2020127787A (ru) 2022-02-21

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