TOOLING FOR MANUFACTURING A TURBOMACHINE PART

Abstract

The invention relates to tooling (50) for manufacturing a turbomachine part, particularly for aircraft, the part comprising a fibrous preform embedded in a matrix. The tooling comprises: - a flexible mold (100) having a first internal cavity (110) for receiving a resin and the fibrous preform, - a rigid mold (200) having a second internal cavity (210) configured to receive the flexible mold (100), wherein the flexible mold (100) includes at least one resin channel (120) opening into the first internal cavity (110). Figure 6 (for the abstract)