CPC D03D 1/00 (2013.01) [D03D 13/004 (2013.01); D03D 25/005 (2013.01); B29B 11/16 (2013.01); D10B 2505/02 (2013.01)] | 13 Claims |
1. A method for weaving a fibrous structure intended to form the fibrous reinforcement of a turbomachine blade made of composite material comprising a fibrous reinforcement densified by a matrix, the fibrous structure being woven as a single piece on a loom by three-dimensional or multilayer weaving between a plurality of warp yarn layers and a plurality of weft yarn layers, the fibrous structure comprising a blade root preform, the method comprising at least one first weaving step in which the warp yarns and the weft yarns are woven according to a first type of weave so as to form a first portion of the blade root preform of the fibrous structure, and a second weaving step in which the warp yarns and the weft yarns are woven according to a second type of weave so as to form a second portion of the blade root preform of the fibrous structure continuing on from the first portion and located downstream of the first portion in the direction of advance of the fibrous structure at an outlet of the loom, the warp yarns and the weft yarns having a degree of interweaving in the first type of weave greater than the degree of interweaving of the warp yarns and the weft yarns present in the second type of weave, the degree of interweaving corresponding to a ratio of a number of layers of yarns crossed by the warp yarns or the weft yarns divided by a product of the weave ratio, a spacing between two weft columns and a spacing between two warp columns.
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