US2007175535A1PendingUtilityA1
Orthogonal weaving for complex shape preforms
Est. expiryDec 21, 2024(expired)· nominal 20-yr term from priority
C04B 2235/5256C04B 2235/5228Y10T442/3195B28B 19/00C04B 2235/5244C04B 35/83B29B 11/16D03D 41/004C04B 35/573C04B 2235/5224D03D 25/005
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Claims
Abstract
An orthogonal stitch-weave method and fiber architecture. The architecture allows near-net-shape composite preforms to be fabricated, thereby reducing costs associated with complex preform shapes and increasing desired strengths of the composite.
Claims
exact text as granted — not AI-modified1 . A woven ceramic matrix composite preform for making a finished ceramic matrix composite shape comprising:
a predetermined number weft tows; a predetermined number of stitcher tows; and a predetermined number of warp tows; wherein the weft tows, the stitcher tows and the warp tows are arranged in an orthogonal weave; wherein the orthogonal weave forms a preform of a shape substantially the same as the shape of the finished ceramic matrix composite shape; and wherein the weft tows, stitcher tows and the warp tows include a plurality of individual fibers comprising silicon carbide.
2 . (canceled)
3 . (canceled)
4 . The woven ceramic matrix composite preform of claim 1 , wherein the preform shape is a shape requiring substantially no trimming prior to final fabrication into the final ceramic matrix composite.
5 . (canceled)
6 . The woven ceramic matrix composite preform of claim 1 , wherein the stitcher tows are positioned in the preform shape in a configuration providing transverse fiber reinforcement.
7 . A woven ceramic matrix composite preform for making a finished ceramic matrix composite shape comprising:
a predetermined number weft tows; a predetermined number of stitcher tows; and a predetermined number of warp tows; wherein the weft tows, the stitcher tows and the warp tows are arranged in an orthogonal weave; wherein the orthogonal weave forms a preform of a shape substantially the same as the shape of the finished ceramic matrix composite shape; and wherein the preform shape is an airfoil component for a gas turbine engine.
8 . The woven ceramic matrix composite preform of claim 1 , wherein the weft tows, stitcher tows and the warp tows include a plurality of individual fibers.
9 . The woven ceramic matrix composite preform of claim 1 , wherein the preform shape is a shape requiring substantially no trimming prior to final fabrication into the final ceramic matrix composite.
10 . The woven ceramic matrix composite preform of claim 1 , wherein the stitcher tows are positioned in the preform shape in a configuration providing transverse fiber reinforcement.Join the waitlist — get patent alerts
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