METHOD FOR MANUFACTURING A COMPOSITE MATERIAL VANE WITH AN ATTACHED METAL LEADING EDGE

摘要

A method for manufacturing a composite material vane with an attached metal leading edge for a gas turbine aircraft engine, the method comprising: producing a batch of a plurality of unprocessed vanes (10) from a composite material, generating a digital model of an unprocessed vane from a vane of the batch of the plurality of unprocessed vanes, generating a digital model of a theoretical final vane comprising a leading edge, generating a digital model of a leading edge from the digital model of an unprocessed vane and the final vane model, manufacturing at least one leading edge (21) by means of additive manufacturing from the digital model of the leading edge generated, bonding each manufactured leading edge (21) to an unprocessed vane of the batch of the plurality of unprocessed vanes (10).