Patent ID: 11879361
Assignee: SAFRAN AIRCRAFT ENGINES
Field: Other special machines (Mechanical engineering)
Classification: CPC F  B  Y | IPC B  F

Claim 0:
1. A vane for a turbine engine, comprising:
a body in the form of an aerodynamic profile formed by a shell produced from a composite material formed by a three-dimensional textile of reinforcement fibres consolidated by a hardened resin, the shell forming a pressure surface of the vane and a suction surface of the vane connected to each other while forming, on one side, a leading edge of the vane, and on the opposite side a trailing edge of the vane, and
a core comprising a core body surrounded by the shell,
wherein the core is produced from a 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.