The invention relates to a ceramic material which can, in particular, be employed in the use of ceramic layers.
The use of zirconium oxide-based ceramic materials is known from the use for ceramic heat shields made from solid material or ceramic protective layers on turbine blades or high-temperature components. It is important here that a high sintering resistance, phase stability, a high fracture toughness and high expansion tolerance is present.
It is therefore an object of the invention to improve existing material systems.
The object is achieved by a ceramic material as claimed.
Further advantages are listed in the further dependent claims, and these can be combined with one another in any way in order to achieve further advantages.
It is proposed that from 4 mol % to 30 mol % of cerium oxide (CeO2), calcium oxide (CaO) and/or magnesium oxide (MgO) be used as further optional oxides and from 2 mol % to 30 mol % of erbium oxide (Er2O3) and/or ytterbium oxide (Yb2O3) be used as base oxide.
Such a ceramic layer has, in particular, a layer thickness of from 20 μm to 1000 μm, in particular up to 2000 μm, and can advantageously be produced by means of thermal spraying, in particular APS or EB-PVD.
The ceramic material has a high sintering resistance, a high expansion tolerance and high fracture toughness and also has a relatively low thermal conductivity.
Working examples:
ZrO2+
The following can in each case be added as further oxides
The layer system 1 has a substrate 4. The substrate 4 is, in particular, a nickel-based superalloy or is a CMC substrate.
A bonding layer which, particularly in the case of a nickel-based superalloy, is an NiCoCrAlY-based alloy or an aluminide layer or a platinum-aluminide layer is present on the substrate 4.
During coating or during operation, an oxide layer (TGO) is formed on this metallic bonding agent layer.
A ceramic layer as per the ceramic material has been applied on top of this oxide layer (TGO) or on the metallic bonding agent layer 7.
In the case of a ceramic substrate 4 (CMC), a bonding layer for the ceramic layer 10 may not be necessary.
A ceramic bonding layer 13 is present under this ceramic layer 16 for the purpose of matching coefficients of thermal expansion or matching the porosities.
Number | Date | Country | Kind |
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10 2018 204 498.8 | Mar 2018 | DE | national |
This application is the U.S. National Stage of International Application No. PCT/EP2019/054650 filed 26 Feb. 2019, and claims the benefit thereof. The International Application claims the benefit of German Application No. DE 10 2018 204 498.8 filed 23 Mar. 2018. All of the applications are incorporated by reference herein in their entirety.
Filing Document | Filing Date | Country | Kind |
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PCT/EP2019/054650 | 2/26/2019 | WO | 00 |