Ceramic matrix composite vane with integrated platform joint

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United States of America Patent

PATENT NO 11415013
SERIAL NO

17491472

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Abstract

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An integral, one-piece ceramic matrix composite turbine vane adapted for use in a gas turbine engine includes an airfoil and two platforms. The airfoil extends radially relative to an axis of the gas turbine engine between the first platform and the second platform. The platforms extend circumferentially partway about the axis of the gas turbine engine.

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Patent Owner(s)

Patent OwnerAddress
ROLLS-ROYCE PLCKINGS PLACE 90 YORK WAY LONDON N1 9FX

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bootle, Laurie London, GB 1 1
Whittle, Michael J London, GB 88 314

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