Thermal barrier coating, turbine member, gas turbine, and method for producing thermal barrier coating
US-2021054492-A1 · Feb 25, 2021 · US
US12565706B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12565706-B2 |
| Application number | US-202318229338-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 2, 2023 |
| Priority date | Aug 2, 2022 |
| Publication date | Mar 3, 2026 |
| Grant date | Mar 3, 2026 |
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A method of applying a top coat to an article according to an exemplary embodiment of this disclosure, among other possible things includes applying a first feedstock comprising particles of oxide-based material having diameters between about 1 and about 80 microns via a thermal spray process to form a first top coat layer on an article having a bond coat and applying a second feedstock comprising particles of oxide-based material having diameters between about 15 and about 60 microns via the thermal spray process to form a second top coat layer on the first top coat layer. An article and a barrier layer for an article are also disclosed.
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What is claimed is: 1 . A method of applying a top coat to an article comprising: applying a first feedstock comprising particles of oxide-based material having diameters between about 1 and about 80 microns via a thermal spray process to form a first top coat layer on an article having a bond coat; and applying a second feedstock comprising particles of oxide-based material having diameters between about 15 and about 60 microns via the thermal spray process to form a second top coat layer on the first top coat layer, wherein the first top coat layer has a higher porosity than the second top coat layer. 2 . The method of claim 1 , wherein the particles of oxide-based material include particles of at least one of hafnia, hafnium silicates, yttrium silicates, ytterbium silicates, other rare earth silicates or combinations of rare earth silicates, calcium aluminosilicates, mullite, barium strontium aluminosilicate, strontium aluminosilicate. 3 . The method of claim 1 , wherein the thermal spray process is one of air plasma spray, a suspension deposition process, and electrophoretic deposition (EPD). 4 . The method of claim 1 , wherein the second top coat layer is performed without moving the article after the step of applying the first top coat layer. 5 . The method of claim 1 , further comprising curing or sintering the first and second top coat layers. 6 . The method of claim 1 , wherein a surface roughness of the second top coat layer is less than about 6 microns (150 microinches). 7 . The method of claim 1 , wherein the particles in the first feedstock have diameters between about 10 and about 70 microns. 8 . The method of claim 1 , wherein the particles in the second feedstock have diameters between about 20 and about 50 microns. 9 . The method of claim 1 , wherein the particles of oxide-based material include particles of hafnium silicates. 10 . The method of claim 1 , wherein the particles of oxide-based material include particles of yttrium silicates. 11 . The method of claim 1 , wherein the particles of oxide-based material include particles of ytterbium silicates. 12 . The method of claim 1 , wherein the particles of oxide-based material include particles of calcium aluminosilicates. 13 . The method of claim 1 , wherein the particles of oxide-based material include particles of strontium aluminosilicate. 14 . The method of claim 1 , wherein the first top coat layer is between about 1.5 and 2.5 times the thickness of the second top coat layer.
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