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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Main Authors | , |
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Format | Patent |
Language | English French German |
Published |
21.12.2022
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Subjects | |
Online Access | Get full text |
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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. |
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Bibliography: | Application Number: EP20210709069 |