VANE MADE OF COMPOSITE MATERIAL FOR A TURBINE ENGINE STATOR INCLUDING A HOLLOW CORE MADE OF NON-POROUS PLASTIC

A vane for a turbine engine includes a body in the form of an aerodynamic profile formed by a shell produced from a composite material formed from a three-dimensional textile of reinforcement fibres consolidated by a hardened resin. The shell forms a pressure surface and a suction surface of the van...

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Bibliographic Details
Main Authors GRELIN, Hervé, BAROUMES, Laurent, Jean-Baptiste
Format Patent
LanguageEnglish
French
German
Published 21.12.2022
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Summary:A vane for a turbine engine includes a body in the form of an aerodynamic profile formed by a shell produced from a composite material formed from a three-dimensional textile of reinforcement fibres consolidated by a hardened resin. The shell forms a pressure surface and a suction surface of the vane connected to each other while forming on one side a leading edge and on the opposite side a trailing edge of the vane, and a core including a core body surrounded by the shell. The core is produced from non-porous plastics material, and the core body is in the form of an aerodynamic profile and delimits at least one closed cavity of the core.
Bibliography:Application Number: EP20210709069