Method for carrying out method for implementing energy conversion installation service measures, and energy conversion installation
US-2024392684-A1 · Nov 28, 2024 · US
US2016265367A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016265367-A1 |
| Application number | US-201414578670-A |
| Country | US |
| Kind code | A1 |
| Filing date | Dec 22, 2014 |
| Priority date | Dec 22, 2014 |
| Publication date | Sep 15, 2016 |
| Grant date | — |
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Article includes a substrate, a bond coat disposed on the substrate, an environmental barrier coating disposed on the bond coat, and a patterned abradable coating disposed on the second top coat. The environmental barrier coating includes an intermediate layer disposed on the bond coat, a sealing layer disposed on the intermediate layer, a first top coat disposed on the sealing layer, and a second top coat disposed on the first top coat. The first top coat is different from the second top coat.
Opening claim text (preview).
1 . An article comprising: a substrate; a bond coat disposed on said substrate; an environmental barrier coating disposed on said bond coat, said environmental barrier coating comprising: an intermediate layer disposed on said bond coat; a sealing layer disposed on said intermediate layer; a first top coat disposed on said sealing layer; a second top coat disposed on said first top coat, said first top coat being different from said second top coat; and a patterned abradable coating disposed on said second top coat. 2 . The article of claim 1 wherein said patterned abradable coating comprises solid portions and voids. 3 . The article of claim 2 wherein said solid portions comprises tapered sides extending generally though the thickness of said patterned abradable coating. 4 . The article of claim 1 wherein: said bond coat comprises silicon; said intermediate layer comprises a rare earth disilicate; said sealing layer comprises barium strontium aluminosilicate; said first top coat comprises a rare earth disilicate; and said second top coat comprises a rare earth monosilicate. 5 . The article of claim 4 wherein said patterned abradable coating comprises solid portions and voids. 6 . The article of claim 5 wherein said solid portions comprises tapered sides extending generally though the thickness of said patterned abradable coating. 7 . The article of claim 1 wherein said substrate comprises a ceramic matrix composite, a monolithic ceramic layer, or combination thereof. 8 . The article according to claim 1 wherein said bond coat comprises silicon. 9 . The article according to claim 1 wherein said sealing layer comprises at least one hermetic self-sealing layer formed from a mixture comprising an alkaline earth metal aluminosilicate and a rare-earth silicate. 10 . The article according to claim 1 wherein said sealing layer comprises barium strontium aluminosilicate. 11 . The article of claim 1 wherein said abradable coating comprises a thickness within a range of about 1/10 millimeter and about 2 millimeters. 12 . The article of claim 1 wherein said abradable coating comprises zirconia. 13 . The article of claim 1 wherein said substrate comprises a ceramic matrix composite, a monolithic ceramic layer, or combination thereof. 14 . The article of claim 1 wherein each of said bond coat and said layers of said environmental barrier coating comprises continuous layers. 15 . The article of claim 1 wherein said environmental barrier coating and said patterned abradable coating are capable of withstanding operating temperatures of at least 2,400 degrees Fahrenheit. 16 . The article of claim 1 wherein said substrate comprises a component of a gas turbine assembly. 17 . The article of claim 1 wherein said substrate comprises a shroud of a turbine with an outer surface of said abradable layer disposed adjacent to tips of rotating turbine blades. 18 . A method for forming an article, the method comprising: providing a substrate; forming a bond coat disposed on the substrate; forming an intermediate layer on the bond coat; forming a sealing layer on the intermediate layer; forming first top coat on the sealing layer; forming a second top coat on the first top coat; and forming a patterned abradable coating on the second top coat. 19 . The method of claim 18 wherein forming the patterned abradable coating comprises forming the patterned abradable coating comprising solid portions defining voids. 20 . The method of claim 19 wherein said solid portions comprises tapered sides extending generally though the thickness of said patterned abradable coating. 21 . The method of claim 20 wherein: the bond coat comprises silicon; the intermediate layer comprises a rare earth disilicate; the said sealing layer comprises barium strontium aluminosilicate; the first top coat comprises a rare earth disilicate; and the second top coat comprises a rare earth monosilicate. 22 . The method of claim 20 wherein each of the forming of the bond coat, first intermediate layer, the sealing layer, the first top coat, the second top coat comprises forming continuous coating layers. 23 . The method of claim 20 wherein forming the patterned abradable coating comprises forming the patterned abradable coating comprising solid portions defining voids. 24 . The method of claim 20 wherein said solid portions comprises tapered sides extending generally though the thickness of said patterned abradable coating.
Silicates other than clay, e.g. water glass · CPC title
Alkaline earth metal alumino-silicates other than clay, e.g. cordierite, beryl, micas such as margarite, plagioclase feldspars such as anorthite, zeolites such as chabazite · CPC title
based on rare-earth compounds {(non-oxide rare earth compounds C04B35/5156)} · CPC title
Silicon · CPC title
obtaining ceramic coatings (coating of mortars, concrete, artificial or natural stone or ceramics C04B41/45; laminated ceramic products B32B18/00; coating of glass C03C17/00, applying ceramic coatings on silicon for semi-conductor purposes H10W; coating metallic materials C23) · CPC title
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