Articles having damage-tolerant thermal barrier coating
US-2017145836-A1 · May 25, 2017 · US
US11512383B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11512383-B2 |
| Application number | US-201816104406-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 17, 2018 |
| Priority date | Aug 24, 2017 |
| Publication date | Nov 29, 2022 |
| Grant date | Nov 29, 2022 |
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The present invention relates to a protective layer against CMAS, to a CMAS-resistant article comprising the protective layer according to the invention, and to a process for preparing a corresponding article.
Opening claim text (preview).
The invention claimed is: 1. A protective layer against CMAS, characterized in that said protective layer consists of oxides of iron, yttrium and silicon. 2. The protective layer according to claim 1 , characterized in that the layer thickness of the protective layer is from 10 μm to 200 μm. 3. A CMAS-resistant article, comprising: a basic structure made of a refractory material with a surface, a first coating on this surface, and a protective layer consisting of oxides of iron, yttrium and silicon that has been applied to this first coating. 4. The article according to claim 3 , characterized by being a turbine or an inliner on the combustion chamber. 5. The article according to claim 3 , characterized in that said refractory material comprises an Ni-based superalloy or SiC. 6. The article according to claim 3 , characterized in that said first coating is a thermal insulation layer (TBC) or environmental barrier coating (EBC). 7. A process for preparing an article according to claim 3 , characterized in that the protective layer is applied to the first coating by means of sputter technology or PVD.
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of silicon · CPC title
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