Ceramic seal component for gas turbine engine and process of making the same
US-2018266261-A1 · Sep 20, 2018 · US
US11519282B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11519282-B2 |
| Application number | US-201916679923-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 11, 2019 |
| Priority date | Nov 11, 2019 |
| Publication date | Dec 6, 2022 |
| Grant date | Dec 6, 2022 |
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A seal includes a ceramic matrix composite ply having woven ceramic-based fibers in a ceramic-based matrix. The ceramic matrix composite ply has at least one bend formed about a bend axis and defines at least one rounded portion. A sealed assembly and a method of making a seal are also disclosed.
Opening claim text (preview).
What is claimed is: 1. A seal, comprising: a ceramic matrix composite ply having woven ceramic-based fibers in a ceramic-based matrix, the ceramic matrix composite ply having a W-shape defined by first bend formed about a first bend axis and defining a first rounded portion and a second bend formed about a second bend axis and defining a second rounded portion, wherein the first bend axis and second bend axis are parallel to one another, and wherein the woven ceramic based fibers include a first set of fibers oriented in a first direction and a second set of fibers oriented in a second direction and woven with the first set of fibers, and the first set of fibers is angled with respect to the first and second bend axes at an angle between about 0 and 60 degrees. 2. The seal of claim 1 , wherein the woven ceramic based fibers include a first set of fibers oriented in a first direction and a second set of fibers oriented in a second direction and woven with the first set of fibers, wherein the relative volume fractions of the first set of fibers and the second set of fibers is between about 5% and 60%. 3. The seal of claim 1 , wherein the woven ceramic based fibers include a first set of fibers oriented in a first direction, a second set of fibers oriented in a second direction and woven with the first set of fibers, and a third set of fibers oriented in a third direction and woven with the first and second sets of fibers. 4. The seal of claim 1 , wherein the ceramic matrix composite ply includes a central portion extending between the first and second bends. 5. A sealed assembly, comprising a first component; a second component; and a seal sealing the first component with respect to the second component, the seal including a ceramic matrix composite ply having woven ceramic-based fibers in a ceramic-based matrix, the ceramic matrix composite ply having a W-shape defined by a first bend formed about a first bend axis and defining a first rounded portion and a second bend and a second bend formed about a second bend axis and defining a second rounded portion, wherein the first bend axis and second bend axis are parallel to one another, and wherein the woven ceramic based fibers include a first set of fibers oriented in a first direction and a second set of fibers oriented in a second direction and woven with the first set of fibers, and the first set of fibers is angled with respect to the bend axes at an angle between about 0 and 60 degrees. 6. The sealed assembly of claim 5 , wherein the woven ceramic based fibers include a first set of fibers oriented in a first direction and a second set of fibers oriented in a second direction and woven with the first set of fibers, and the first set of fibers is angled with respect to the first and second bend axes at an angle between about 30 and 60 degrees. 7. The sealed assembly of claim 5 , wherein the woven ceramic based fibers include a first set of fibers oriented in a first direction and a second set of fibers oriented in a second direction and woven with the first set of fibers, wherein the relative volume fractions of the first set of fibers and the second set of fibers is between about 5% and 60%. 8. The sealed assembly of claim 5 , wherein the woven ceramic based fibers include a first set of fibers oriented in a first direction and a second set of fibers oriented in a second direction and woven with the first set of fibers, wherein the relative volume fractions of the first set of fibers and the second set of fibers is between about 5% and 60%, and wherein the first set of fibers is angled with respect to the first and second bend axes at an angle between about 30 and 60 degrees. 9. The sealed assembly of claim 5 , wherein each of the first and second components have at least one mating face mating with the seal, and the at least one mating face is non-abrasive with respect to the seal. 10. The sealed assembly of claim 9 , wherein the at least one mating face is deformable with respect to the seal. 11. The sealed assembly of claim 9 , wherein the at least one mating face includes a coating, and the coating is deformable with respect to the seal. 12. The sealed assembly of claim 5 , wherein the sealed component is in a gas turbine engine. 13. The sealed assembly of claim 5 , wherein the ceramic matrix composite ply includes a central portion extending between the first and second bends. 14. A method of making a seal, comprising: forming a single ceramic matrix composite ply comprising woven ceramic-based fibers in a ceramic-based matrix into a W-shape including a first bend about a first bend axis and a second bend about a second bend axis, the first bend axis and the second bend axis being parallel to one another, wherein the woven ceramic-based fibers define a weave direction, the woven ceramic based fibers include a first set of fibers oriented in a first direction and a second set of fibers oriented in a second direction and woven with the first set of fibers, and the first set of fibers is angled with respect to the first and second bend axes at an angle between about 0 and 60 degrees. 15. The method of claim 14 , wherein the forming includes forming the first bend, and forming the second bend after forming the first bend. 16. The method of claim 14 , wherein the forming includes introducing at least one of the first and second bends into the ceramic matrix composite ply, and rigidizing the ceramic matrix composite ply after introducing at least one of the first and second bends. 17. The method of claim 14 , further comprising forming the ceramic matrix composite ply to include a central portion extending between the first and second bends. 18. The method of claim 14 , wherein the forming is by molding the ceramic matrix composite ply into the W-shape.
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