Composite material blade for an aircraft turbomachine

Abstract

Composite material blade for an aircraft turbomachine. The present invention relates to a composite material blade, comprising: - a 3D woven fibrous reinforcement (100f) including a blade portion (102f) extending in a radial direction and at least one platform portion (105f) extending from a radial end of the blade portion, said at least one platform portion including a debond defining a housing (106) extending in an axial direction (A) and opening onto at least one of the axial ends (100fa) of the reinforcement, - at least one metallic mounting insert (200), each mounting insert including at least one connecting portion (202) located in a corresponding housing and integral with the reinforcement, and a mounting portion (204) located outside the reinforcement and configured to secure the blade to a ferrule, and - an organic matrix densifying the fibrous reinforcement. Fig. 5.