Turbine with a shroud ring around rotor blades and method of limiting leakage of working fluid in a turbine
US-2024280031-A1 · Aug 22, 2024 · US
US9556743B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9556743-B2 |
| Application number | US-201514789676-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jul 1, 2015 |
| Priority date | Jul 3, 2014 |
| Publication date | Jan 31, 2017 |
| Grant date | Jan 31, 2017 |
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In some examples, a coating may include at least one feature that facilitates visual determination of a thickness of the coating. For example, the coating may include a plurality of microspheres disposed at a predetermined depth of the coating. The plurality of microspheres may define a distinct visual characteristic. By inspecting the coating and viewing at least one of the microspheres, the thickness of the coating may be estimated. In some examples, the plurality of microspheres may be embedded in a matrix material, and the distinct visual characteristic of the microspheres may be different than the visual characteristic of the matrix material. In other examples, the at least one feature may include at least one distinct layer in the coating system that includes a distinct visual characteristic, such as a color of the distinct layer.
Opening claim text (preview).
What is claimed is: 1. An article comprising: a substrate; a coating on the substrate, wherein the coating comprises: at least one abradable layer; a neodymium silicate layer; an erbium silicate layer; and a gadolinium silicate layer, wherein the neodymium silicate layer, the erbium silicate layer, and the gadolinium silicate layer are adjacent to each other within the coating. 2. The article of claim 1 , wherein the at least one abradable layer comprises a first abradable layer and a second abradable layer, and wherein the neodymium silicate layer, the erbium silicate layer, and the gadolinium silicate layer are between the first abradable layer and the second abradable layer. 3. The article of claim 1 , wherein the coating further comprises an environmental barrier coating layer, wherein the environmental barrier coating layer comprises at least one rare earth silicate, and wherein the environmental barrier coating layer is between the substrate and the at least one abradable layer. 4. The article of claim 1 , wherein the coating further comprises a bond layer between the substrate and the at least one abradable layer, wherein the bond layer comprises silicon. 5. The article of claim 1 , wherein the neodymium silicate layer comprises at least one of neodymium monosilicate or neodymium disilicate, wherein the erbium silicate layer comprises at least one of erbium monosilicate or erbium disilicate, and wherein the gadolinium silicate layer comprises at least one of gadolinium monosilicate or gadolinium disilicate. 6. The article of claim 1 , wherein at least one of the neodymium silicate layer, the erbium silicate layer, or the gadolinium silicate layer is doped with between about 0.1 at. % and about 10 at. % of an element selected from the lanthanide series of the periodic table, excluding ytterbium. 7. The article of claim 1 , wherein the at least one abradable layer includes porosity between about between about 25 volume percent and about 50 volume percent. 8. The article of claim 1 , wherein the at least one abradable layer includes porosity between about between about 35 volume percent and about 45 volume percent. 9. The article of claim 1 , wherein the neodymium silicate layer, the erbium silicate layer, and the gadolinium silicate layer are located at respective predetermined depths from an outer surface of the coating. 10. The article of claim 9 , wherein respective predetermined depths approximately correspond to a depth to which the coating is abraded during use of the article. 11. A method comprising: forming a coating on a substrate, wherein the coating comprises: at least one abradable layer; a neodymium silicate layer; a erbium silicate layer; and a gadolinium silicate layer, wherein the neodymium silicate layer, the erbium silicate layer, and the gadolinium silicate layer are adjacent to each other within the coating. 12. The method of claim 11 , the at least one abradable layer comprises a first abradable layer and a second abradable layer, and wherein forming the coating on the substrate comprises forming the neodymium silicate layer, the erbium silicate layer, and the gadolinium silicate layer on the first abradable layer and forming the second abradable layer on the neodymium silicate layer, the erbium silicate layer, and the gadolinium silicate layer.
by plasma spraying · CPC title
Silicates (C04B41/5022 takes precedence; silico-fluorides C04B41/5018) · CPC title
Luminescent or fluorescent materials · CPC title
characterised by the material treated · CPC title
of coating · CPC title
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