Safran

Magali Mélanie Coulaud

Nicolas Pierre Lanfant

Adrien Touze

Nicolas Cuvillier

Mathieu Loïc Ducousso

Matthieu Stackler

A process for manufacturing a blade made of composite material for a turbomachine is provided. The blade includes an airfoil having a pressure side and a suction side which extend from a leading edge to a trailing edge of the airfoil. The blade further includes a metal sheath that extends along the leading edge of the airfoil. The process includes the steps of: a) placing a preform, made by three-dimensionally weaving fibers, in a mold, a polymerizable adhesive being inserted between the sheath and the edge of the preform; and b) injecting polymerizable resin into the mold to impregnate the preform so as to form the airfoil after solidifying, wherein the resin is injected within a time interval during which the adhesive reaches a freezing point.

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Moissy-Cramayel, France

Magali Mélanie Coulaud