COMPOSITE BLADE FOR AN AIRCRAFT ENGINE AND METHOD FOR MANUFACTURING SAME
Disclosed is a method for manufacturing a composite material blade (10) for a turbomachine, in particular an aircraft turbomachine, the blade (10) comprising a metal shield (1) extending along a leading edge (12a) of the aerofoil (12), the method comprising the steps consisting in cutting a film along the edges of the shield (1) so that the cut film forms at least one template (5) delimiting a region (15) for applying adhesive located under the shield (1), positioning a film of adhesive (7) on said region (15), cutting the film of adhesive (7) according to the shape of the or each template • (5), removing the or each template (5), positioning the shield (1) on the film of adhesive • (7), and curing the resulting assembly in a thermocompression mould. The invention also relates to a blade (10) manufactured by such a method.