FIBROUS TEXTURE FOR MANUFACTURING A FAN BLADE MADE OF COMPOSITE MATERIAL

摘要

The invention relates to a fibrous texture (10) for forming the fibrous reinforcement of a vane of a turbine engine from composite material, comprising a zone (24) of reduced rigidity with warp threads made from second fibres having an elongation at break greater than a first elongation, the zone of reduced rigidity extending in the longitudinal direction (DL) from the stilt zone and up to a height less than or equal to 30% of the height, extending in the transverse direction (DT) between a first zone (23) and a second zone (25), the first zone extending over a length (21) from an edge (16) of the texture intended to form a leading edge, and the second zone extending over a second length (22) from an edge (17) of the texture intended to form a trailing edge.