Manufacture of CMC articles having small complex features
The present invention is ceramic matrix composite gas turbine engine component comprising a plurality of cured ceramic matrix composite plies 44, each ply 44 comprising ceramic fiber tows 46, each ceramic fiber tow 46 comprising a plurality of ceramic fibers 72, the tows 46 in each ply 44 lying adja...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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