Slots and pre-weakened region in 3D woven components
A method of forming a ceramic matrix composite includes forming a preform by weaving a plurality of warp tows with a plurality of weft tows, weaving a plurality of fugitive yarns into a region of the preform in at least one of a warp position or weft position, and subsequently, decomposing the fugitive yarns to transform the region into a pre-weakened region, the pre-weakened region having a higher porosity than a remainder of the preform.
1 . A method of forming a ceramic matrix composite, the method comprising:
forming a preform by:
weaving a plurality of warp tows with a plurality of weft tows, wherein weaving the plurality of warp tows comprises redirecting a subset of the plurality of warp tows around a region of the preform such that the region is free of the plurality of warp tows;
weaving a plurality of fugitive yarns into the region of the preform in at least one of a warp position or weft position, wherein weaving the plurality of warp tows, the plurality of weft tows, and the plurality of fugitive yarns comprises a three-dimensional weaving technique and wherein redirecting the subset of the plurality of warp tows comprises routing the subset of the plurality of warp tows along a border of the region to provide a reinforced area along a periphery of the region;
subsequently, decomposing the fugitive yarns to transform the region into a pre-weakened region, the pre-weakened region having a higher porosity than a remainder of the preform;
densifying the preform with a ceramic matrix; and
machining the pre-weakened region to form a slot in the ceramic matrix composite.
2 . The method of claim 1 , wherein densifying the preform with a ceramic matrix is conducted using one of: chemical vapor infiltration, polymer infiltration and pyrolysis, and slurry infiltration.
3 . The method of claim 2 , wherein the plurality of fugitive yarns is decomposed during or prior to densifying the preform.
4 . The method of claim 1 , wherein the plurality of fugitive yarns is formed from polyvinyl alcohol.
5 . The method of claim 1 , wherein the matrix comprises silicon carbide.
6 . The method of claim 1 , wherein the step of machining the pre-weakened region comprises at least one of drilling and grinding.
7 . The method of claim 1 , and further comprising: inserting a sealing element into the slot.
8 . The method of claim 1 , wherein the step of decomposing the fugitive yarns comprises at least one of a thermal and a chemical decomposition process.
9 . The method of claim 1 , wherein the ceramic matrix composite is a component for a gas turbine engine.
10 . The method of claim 1 , wherein the region comprises a subset of the plurality of the weft tows.