Hybrid structure using ceramic tiles and method of manufacture
View Patent ↗A hybrid structure ( 50 ) and method of manufacturing the same including a structural ceramic matrix composite (CMC) material ( 42 ) coated with a layer of ceramic insulating tiles ( 24 ). Individual ceramic tiles are attached to a surface ( 22 ) of a mold ( 20 ). The exterior surface ( 32 ) of the tiles may be subjected to a mechanical process such as machining with the mold in place to provide mechanical support for the tiles. A layer of CMC material is then applied to bond the tiles and the CMC material together into a hybrid structure. The mold may include a fugitive material portion ( 26 ) to facilitate removal of the mold when the hybrid structure has a complex shape. Tiles located in different regions of the structure may have different compositions and/or dimensions. The gaps between adjacent tiles may be filled from the outside before the CMC material is applied or from the inside after the mold is removed.
1. A method of manufacturing a hybrid structure comprising:
applying a plurality of ceramic tiles to a surface of a mold;
applying a layer of ceramic matrix composite material over the ceramic tiles to bond the plurality of ceramic tiles together with the ceramic matrix composite material; and
removing the mold;
further comprising machining an inside surface of the plurality of ceramic tiles to a desired contour after the step of removing the mold.
2. The method of claim 1 , further comprising forming the ceramic tiles to comprise a contour conformably matched to a contour of the surface of the mold.
3. The method of claim 1 , further comprising forming the mold to comprise a fugitive material portion.
4. The method of claim 1 , further comprising machining an outer surface of the plurality of tiles with the tiles supported by the mold prior to the step of applying the layer of ceramic matrix composite material.
5. The method of claim 1 , further comprising at least partially filling gaps between adjacent tiles with a filler material prior to the step of applying a layer of ceramic matrix composite material over the ceramic tiles.
6. The method of claim 1 , further comprising at least partially filling gaps between adjacent files with a filler material after the step of removing the mold.
7. The method of claim 1 , further comprising:
filling gaps between adjacent tiles with a filler material after the step of removing the mold; and
firing the tiles, the ceramic matrix composite material and the filler material together to form a hybrid structure for use in a high temperature environment.
8. The method of claim 1 , further comprising:
applying ceramic tiles having a first composition to a first portion of the surface of the mold; and
applying ceramic tiles having a second composition different than the first composition to a second portion of the surface of the mold.
9. The method of claim 1 , further comprising preparing a surface of at least a portion of the tiles with a surface contour operation.
10. The method of claim 1 , further comprising preparing a surface of at least a portion of the tiles by applying a surface coating material.
11. A method of manufacturing a gas turbine combustor component comprising a ceramic matrix composite structural member having a layer of ceramic insulating material disposed on an inside surface and defining a passageway for hot combustion gasses, the method comprising:
providing a mold comprising a fugitive material;
applying ceramic tiles having a first composition to a first portion of surface of the mold; and
applying ceramic tiles having a second composition different than the first composition to a second portion of the surface of the mold;
applying a layer of ceramic matrix composite material over the ceramic insulating tiles to bond The tiles together with the ceramic matrix composite material; and
transforming the fugitive material and removing the mold.
12. The method of claim 11 , further comprising:
filling gaps between the tiles with a ceramic filler material; and
firing the tiles, the ceramic matrix composite material and the filler material together after the step of removing the mold.
13. The method of claim 12 , further comprising filling the gaps prior to the step of applying the layer of ceramic matrix composite material over the tiles.
14. The method of claim 12 , further comprising filling the gaps after the step of removing the mold.
15. The method of claim 11 , further comprising forming the ceramic tiles to comprise a contour conformably matched to a contour of the surface of the mold.
16. The method of claim 11 , further comprising machining an outer surface of the plurality of tiles with the tiles supported by the mold prior to the step of applying the layer of ceramic matrix composite material.
17. The method of claim 11 , further comprising machining an inside surface of the plurality of ceramic tiles to a desired contour after the step of removing the mold.
18. The method of claim 11 , further comprising preparing a surface of at least a portion of the tiles with a surface contour operation.
19. The method of claim 11 , further comprising preparing a surface of at least a portion of the tiles by applying a surface coating material.
20. A method of manufacturing a hybrid structure for a gas turbine component comprising a generally tubular shape defining an interior passageway through which hot combustion gasses will flow, the method comprising:
providing a mold comprising an outside surface corresponding to a shape of the interior passageway of the gas turbine component;
affixing a plurality of ceramic insulating tiles to the outside surface of the mold;
mechanically preparing an exposed surface of the tiles to achieve a desired surface profile after the tiles are affixed to the mold so that the mold provides mechanical support for the tiles during the preparing step;
forming a layer of ceramic matrix composite material over the ceramic tiles and bonding the tiles together with the layer of ceramic matrix composite material to form a hybrid structure; and
removing the mold after the tiles are bonded to the layer of ceramic matrix composite material; and
processing the hybrid structure to a final configuration after the mold has been removed.
21. The method of claim 20 , wherein the step of mechanically preparing comprises one of the group of machining, grinding and sanding of the exposed surface of the tiles.
22. The method of claim 20 , further comprising at least partially filing gaps between adjacent tiles after the tiles are affixed to the mold so that the mold provides mechanical support for the tiles during the filing step.
23. A method of manufacturing a hybrid structure for a gas turbine component comprising a generally tubular shape defining an interior passageway through which hot combustion gasses will flow, the method comprising:
providing a mold comprising an outside surface corresponding to a shape of the interior passageway of the gas turbine component;
affixing a plurality of ceramic insulating tiles to the outside surface of the mold;
at least partially filling gaps between adjacent tiles with a grout material after the tiles are affixed to the mold so that the mold provides mechanical support for the tiles during the grouting step;
forming a layer of ceramic matrix composite material over The grouted ceramic tiles and at least partially curing the tiles together with the grout and the layer of ceramic matrix composite material to form a hybrid structure; and
removing the mold after the tiles and grout material are bonded to the layer of ceramic matrix composite material; and
processing the hybrid structure to a final configuration after the mold has been removed.
24. A method of manufacturing a hybrid structure comprising:
applying a plurality of ceramic tiles to a surface of a mold with gaps between adjacent tiles being left unfilled;
applying a layer of ceramic matrix composite material over the ceramic tiles and gaps;
drying and at least partially curing the ceramic matrix composite material to bond the tiles and ceramic matrix composite material together, the gaps between adjacent tiles being effective as stress relieving junctions during the drying and curing step;
removing the mold;
at least partially filling the gaps between adjacent tiles with filler material to form the hybrid structure; and
final firing the hybrid structure.