US Patent 11873732 Blade made of multiple materials

A vane of a turbine engine blade includes a first portion of structural resistance formed by two end portions including the leading and trailing edges and end strips of the lower surface and the upper surface, and of a core joining them. Two other portions of the blade are constructed of light material, composite for example, between the end portions to reconstitute the complete vane. The core has an oblique or diagonal extension between the end portions.