초록 ▼

A ceramic seal element (200) for use in a turbo-machine comprises a first, rigid portion (210) comprising ceramic fibers (212) bound within a ceramic matrix binder (214), a second, flexible portion (220) comprising ceramic fibers (222), and a third, rigid portion (230) comprising ceramic fibers (232

A ceramic seal element (200) for use in a turbo-machine comprises a first, rigid portion (210) comprising ceramic fibers (212) bound within a ceramic matrix binder (214), a second, flexible portion (220) comprising ceramic fibers (222), and a third, rigid portion (230) comprising ceramic fibers (232) bound within a ceramic matrix binder (234). Ceramic fibers (222) retain a desired flexibility because they are not bound in ceramic matrix binder. In some embodiments the ceramic fibers (212, 222, 232) are stacked as horizontally disposed layers (225). Also, the fibers (212, 222, 232) of any layer (225) comprise bundles of fibers wherein some of the bundles extend continuously across portions (210, 220, 230). An alternative sealing element (300) comprises a first, rigid portion (310) comprising ceramic fibers (312) that are bound within a ceramic matrix binder (314), and a second, flexible portion (320) that comprises ceramic fibers (313) that retain a desired flexibility. Methods of manufacture are disclosed.

대표청구항 ▼

The invention claimed is: 1. A turbo-machine ceramic seal element comprising: a first, rigid portion comprising ceramic fibers rigidly bound within a ceramic matrix binder; and a second, flexible portion, having a first end meeting the first rigid portion, a second end, and comprising ceramic fiber

The invention claimed is: 1. A turbo-machine ceramic seal element comprising: a first, rigid portion comprising ceramic fibers rigidly bound within a ceramic matrix binder; and a second, flexible portion, having a first end meeting the first rigid portion, a second end, and comprising ceramic fibers; a third, rigid portion comprising ceramic fibers rigidly within a ceramic matrix binder, and disposed at the second end of the second, flexible portion wherein the first, rigid portion is sized for positioning in a groove of a turbo-machine component in need of sealing with said ceramic seal element. 2. The turbo-machine ceramic seal element of claim 1, wherein the ceramic fibers of the first, rigid portion, the second, flexible portion, and the third, rigid portion are provided, at least in part, as one or more continuous bundle(s) of ceramic fibers. 3. The turbo-machine ceramic seal element of claim 2, wherein the ceramic fibers in the second, flexible portion are prepared so as to provide a designed fluid leakage rate through the ceramic seal element. 4. The turbo-machine ceramic seal element of claim 1, wherein the first, rigid portion and the third, rigid portion are sized to fit into side grooves of adjacent turbine vanes or blades. 5. The turbo-machine ceramic seal element of claim 4, wherein the ceramic fibers of the first, rigid portion, the second, flexible portion, and the third, rigid portion are provided, at least in part, as one or more continuous bundle(s) of ceramic fibers. 6. The turbo-machine ceramic seal element of claim 4, wherein the second, flexible portion is sized to extend beyond a gap between the adjacent turbine vanes or blades. 7. The turbo-machine ceramic seal element of claim 4, wherein the second, flexible portion is sized to be more narrow than the gap between the adjacent turbine vanes or blades. 8. A turbo-machine comprising a seal element positioned between two turbo-machine components in need of a flexible sealing, the seal element comprising two rigid end portions, each rigid end portion comprising ceramic fibers and a rigid ceramic matrix surrounding the ceramic fibers, and a flexible portion between the two rigid end portions, the flexible portion comprising ceramic fibers not made rigid within the ceramic matrix. 9. The turbo-machine of claim 8, wherein each of the two rigid end portions fit into side grooves of adjacent turbine vanes or blades. 10. A method for manufacture of selectively flexible ceramic seal elements for turbo-machines, comprising: applying a pre-ceramic slurry to one or more portions of one or more pieces of ceramic fiber-containing tape or fabric, however leaving at least one portion of each said pieces without the slurry, to yield a partially slurried tape or fabric; forming one or more pieces of the partially slurried tape or fabric into a desired shape of a ceramic seal element; heating the one or more pieces of partially slurried tape or fabric to a curing temperature for a desired time period; and heating the one or more pieces of cured partially slurried tape or fabric to a sintering temperature for a desired time period. 11. The method of claim 10, additionally comprising applying a fugitive material to the at least one portion without the slurry prior to the applying step. 12. The method of claim 10, wherein the forming step comprises placing the one or more pieces of partially slurried tape or fabric into a mold. 13. The method of claim 10, wherein at least two pieces are used, and additionally comprising compressing the two or more pieces prior to the heating steps. 14. The method of claim 13, wherein the forming step comprises placing the compressed two or more pieces of partially slurried tape or fabric into a mold.