Turbomachine component comprising a fibrous preform

A turbomachine component made of composite material comprising a fibrous reinforcement formed by a fibrous preform, and a matrix densifying the fibrous reinforcement, said fibrous preform having a three-dimensional weave formed by a plurality of woven strands;

• wherein, in a shear plane of the component, all or part of the strands present in said shear plane have fibers forming an angle comprised between 10° and 50° with their centerline and wherein said shear plane corresponds to the plane defined by warp and weft directions of the three-dimensional weave, or to the plane defined by the warp direction and a thickness direction of the three-dimensional weave, or to the plane defined by the weft direction and the thickness direction of the three-dimensional weave.