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Ceramic matrix composite vane with hybrid construction
A component for use in a gas turbine engine is made from ceramic materials. The component is made from a core preform containing ceramic reinforcement fibers. A plurality of preform tows are applied on at least a portion of the core preform and extend along at least a portion of the core preform to provide an outermost surface. The core preform and the plurality of preform tows are infiltrated with ceramic matrix material to form a ceramic matrix composite component.
Ceramic matrix composite vane with hybrid construction
A component for use in a gas turbine engine is made from ceramic materials. The component is made from a core preform containing ceramic reinforcement fibers. A plurality of preform tows are applied on at least a portion of the core preform and extend along at least a portion of the core preform to provide an outermost surface. The core preform and the plurality of preform tows are infiltrated with ceramic matrix material to form a ceramic matrix composite component.
Ceramic matrix composite vane with hybrid construction
RAZZELL ANTHONY G (author) / WHITTLE MICHAEL J (author) / EDMONDS IAN M (author)
2022-09-06
Patent
Electronic Resource
English
IPC:
C04B
Kalk
,
LIME
CERAMIC MATRIX COMPOSITE TURBINE VANE AND METHOD FOR MAKING
| European Patent Office | 2020