FIELD: technological processes.
SUBSTANCE: invention relates to fibre structure for reinforcing a part made from composite material, a part from composite material, a turbojet engine, an aircraft, a method of making a part from composite material. Fibrous structure for reinforcing a part made of composite material is obtained by multi-layer weaving of a plurality of layers of warp threads and a plurality of layers of weft threads. Fibrous structure also comprises fixing elements at least on one of its faces. Each fixing element comprising a body arranged under threads on a face of fibrous structure, and fixing portions situated above said threads.
EFFECT: invention provides improved physical and mechanical properties.
15 cl, 17 dwg
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