Two-layer ceramic coating system

The two-layer ceramic coating system, featuring a tetragonal zirconium oxide bottom layer and a cubic zirconium oxide top layer, addresses the bonding challenges in existing systems, achieving enhanced thermal insulation and extended service life for high-temperature components.

WO2025108596A1PCT designated stage expired Publication Date: 2025-05-30SIEMENS ENERGY GLOBAL GMBH & CO KG
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Patent Information

Application Number
PCT/EP2024/074873
Authority / Receiving Office
WO · WO
Patent Type
Applications
Current Assignee / Owner
Priority Date
2023-11-20
Filing Date
2024-09-05
Publication Date
2025-05-30

AI Technical Summary

Technical Problem

Existing two-layer ceramic coating systems for high-temperature components, such as gas turbines, face challenges in achieving improved thermal insulation properties and service life due to inadequate bonding between the ceramic sublayer and the fully stabilized zirconium oxide top layer.

Method used

A two-layer ceramic coating system is developed, comprising a ceramic bottom layer made of tetragonal zirconium oxide with ytterbium oxide as a stabilizer, and a ceramic top layer with a cubic structure of zirconium oxide stabilized with yttrium oxide, which together provide enhanced thermal stability and adhesion.

Benefits of technology

The proposed coating system exhibits improved thermal insulation properties and extended service life by ensuring strong adhesion between the layers and maintaining low porosity, thereby effectively addressing the bonding issues in existing systems.

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Abstract

The invention relates to a layer system (1) comprising at least (in % by weight): a metallic substrate (4), optionally a metallic bonding layer (7) on the substrate (4) and a ceramic bottom layer (10) of partially stabilized, tetragonal zirconium oxide, with ytterbium oxide as stabilizer and a ceramic top layer (13) of fully stabilized cubic zirconium oxide on the ceramic bottom layer (10) wherein the proportion of stabilizers is between 17.5% and 25.5%.
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Description

[0001] Two-layer ceramic coating system

[0002] The invention relates to a two-layer ceramic coating system.

[0003] Ceramics generally exhibit high temperature stability and are therefore often used as ceramic coatings on high-temperature components, such as in turbines, in particular in gas turbines .

[0004] Important in this type of application is the use of the ceramic as a coating on a substrate, which is often a metallic substrate.

[0005] Metallic bonding layers on the substrate, such as those based on NiCoCrAlY, but also ceramic bonding layers or TGO are known .

[0006] A two-layer coating system consisting of two ceramic layers is also often used.

[0007] Fully stabilized ceramic zirconium oxide layers with 20YSZ are state of the art, but need to be improved in terms of bonding to a ceramic sublayer.

[0008] The aim is therefore to improve the thermal insulation properties and service life of two layer-ceramic layer system.

[0009] It is therefore the task of the invention to solve the above- mentioned problem.

[0010] The problem is solved by a layer system according to claim 1

[0011] Ceramic layers based on zirconium oxide with stabilizers are known, whereby fully stabilized zirconium oxide is often used here due to its better thermal stability. However, the aim of the idea is to use fully stabilized zirconium oxide with improved, in particular thermal stability, as well as good adhesion to a ceramic sublayer.

[0012] The figure schematically shows an example of the invention.

[0013] The figure and the description are only examples of the invention .

[0014] In a layer system 1, a ceramic layer 10 is applied to a metallic substrate, preferably using nickel- or cobalt-based superalloys as substrate 4, a metallic bonding layer 7 is present, which forms aluminum oxide (TGO, not shown) .

[0015] The metallic bonding layer 7 is preferably also an aluminide, platinum aluminide or a NiCoCrAlY-X alloy as a base, optionally with x = Ta, Re, Fe and / or Si.

[0016] A ceramic top layer 13 can be applied by EB-PVD, plasma spraying (APS, . . . ) , HVOF . . . and preferably has a columnar structure or a segmented structure (DVC) .

[0017] Preferably the porosity of the ceramic top layer 13 is lower than 10%.

[0018] The ceramic top layer 13 preferably has a layer thickness of 100pm to 1000pm.

[0019] A ceramic lower layer 10 is also present, but its layer thickness is at least 20% thinner than that of the ceramic top layer 13, which together with the ceramic top layer 13 form the ceramic layer system.

[0020] A ceramic lower layer 10 can be applied by EB-PVD, plasma spraying (APS, . . . ) , HVOF ... .

[0021] Preferably the porosity of the ceramic lower layer 10 is lower than 10% or not higher than the porosity of the top layer 13. All the following amounts are given in % by weight.

[0022] The ceramic bottom layer 10 comprises tetragonal zirconium oxide with ytterbium oxide as a stabilizer.

[0023] The following amounts are used: 11.5% to 13.5% ytterbium oxide. Particularly preferably, 12.5% ytterbium oxide is used. Equally preferably, only ytterbium oxide is used as a stabilizer. Some minor oxide impurities may be present.

[0024] A ceramic top layer 13 with a cubic structure of zirconium oxide (FSZ) is applied to the ceramic bottom layer 10.

[0025] The cubic zirconium oxide preferably has a yttrium oxide stabilized zirconium oxide (YSZ) : the proportion of yttrium oxide being 18.0% to 22.0%, in particular 20.0%. Preferably, only yttrium oxide is used as a stabilizer. Some minor oxide impurities may be present.

[0026] It is also possible to use cubic zirconium oxide with stabilizers of yttrium oxide, ytterbium oxide and gadolinium oxide :

[0027] Yttrium oxide represents the largest proportion in comparison to the other two stabilizers.

[0028] Preferably, only these stabilizers are used.

[0029] The following proportions are preferably used in each case: 9.0% - 11.0% yttrium oxide, 4.5% - 6.5% ytterbium oxide and 4.0% - 6.0% gadolinium oxide. Particularly preferred are in each case 9.5% - 10.0% yttrium oxide, 5.2% - 6.0% ytterbium oxide and 4.8% - 5.6% gadolinium oxide. Preferably, only these stabilizers yttrium oxide, ytterbium oxide and gadolinium oxide are used. Some minor oxide impurities may be present. The fully stabilized zirconium oxide (FSZ) is preferably also stabilized with 14.0% to 16.0% ytterbium oxide (Yb2O3) in particular with 14.5% to 15.5% ytterbium oxide (Yb2O3) and stabilized with 4.0% to 6.0% yttrium oxide (Y2O3) and optionally hafnium oxide and / or aluminum oxide.

[0030] The ceramic material preferably comprises 4.5% to 5.5% yttrium oxide (Y2O3) .

[0031] The ceramic material preferably optionally comprises: Hafnium oxide (HfO2) with 0.2% to 4.0%, in particular 0.5% to 2.5% hafnium oxide (HfO2) .

[0032] Example for underlayer 10:

[0033] 12.4% Yb2O3- ZrO2examples for top layer 13 in combination with the example above :

[0034] 20.1% Y2O3- ZrO2or

[0035] 15.0% Yb2O3 / 4.9% Y2O3- ZrO2or

[0036] 10.0% Y2O3 / 5.5% Yb2O3 / 5.3% Gd2O3- ZrO2for which good properties were achieved.

Claims

1. Layer system (1) comprising at least (in % by weight) a metallic substrate (4) , optionally a metallic bonding layer (7) on the substrate (4) and a ceramic underlayer (10) of partially stabilized, tetragonal zirconium oxide, with ytterbium oxide as stabilizer, preferably 11.5% - 13.5% ytterbium oxide, particularly preferably 12.5% ytterbium oxide, and a ceramic top layer (13) of fully stabilized cubic zirconium oxide on the ceramic bottom layer (10) , wherein the proportion of stabilizers of the ceramic top layer (13) is between 17.5% and 26.0%.

2. Layer system according to claim 1, in which only ytterbium oxide is used as a stabilizer for the ceramic sublayer (10) .

3. Layer system according to one or both of claims 1 or 2, in which the ceramic top layer (13) comprises (in % by weight) yttrium oxide stabilized zirconium oxide, wherein the proportion of yttrium oxide is 18.0 wt . % to 22.0 wt . % , in particular 20.0% by weight, in particular only yttrium oxide is used.

4. Layer system according to one or both of claims 1 or 2, in which the ceramic top layer (13) comprises (in % by weight) zirconium oxide, wherein stabilizers of yttrium oxide, ytterbium oxide and gadolinium oxide are present, wherein preferably the following proportions are given: 9.0% - 11.0% yttrium oxide, 4.5% - 6.5% ytterbium oxide and 4.0% - 6.0% gadolinium oxide,preferably 9.75% - 10.0% yttrium oxide, preferably 5.2% to 6.0% ytterbium oxide and preferably 4.8% - 5.6% gadolinium oxide are present in each case, in particular only these three stabilizers yttrium oxide, ytterbium oxide and gadolinium oxide are used.

5. Layer system according to one or both of claims 1 or 2, wherein the ceramic top layer (13) comprises zirconium oxide , wherein stabilizers (in % by weight) of yttrium oxide and ytterbium oxide are present, wherein preferably the following proportions are given: ytterbium oxide (Yb2O3) with 14.0% to 16.0%, in particular with 14.5% to 15.5% ytterbium oxide as well as with 4.0% to 6.0% yttrium oxide and optionally hafnium oxide and / or aluminum oxide.

6. Layer system according to claim 5, in which the ceramic top layer (13) comprises zirconium oxide (in % by weight) , wherein stabilizers of yttrium oxide and ytterbium oxide are present, wherein the following proportions are given: 15% ytterbium oxide, 4.5% to 5.5% yttrium oxide, optionally hafnium oxide with 0.2% to 4.0%, in particular 0.5% to 2.5% hafnium oxide.

7. Layer system according to one or more of claims 1, 2, 3, 4 , 5 or 6 , comprising a metallic adhesion promoter layer (7) between the ceramic underlayer (10) and the metallic substrate (4) , in particular directly on the substrate (4) , wherein the adhesion promoter layer (7) comprises analloy of the type NiCoCrAlY-X,X is optionally and selected from the group: Ta, Re and / or Si, in particular NiCoCrAlY or NiCoCrAlY-Ta .

8. Layer system according to one or more of the claims 1, 2, 3, 4, 5, 6 or 7, in which the ceramic sublayer (10) under the ceramic layer (13) is at least 20% thinner.

Citation Information

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