TURBINE ENGINE PART FORMING A COMPRESSOR STATOR OR TURBINE NOZZLE, AND METHOD FOR MANUFACTURING SAME

摘要

The invention relates to a turbine engine part forming a compressor stator or turbine nozzle and including an inner shroud, an outer shroud and blades extending substantially radially between the inner and outer shrouds and being rigidly connected to the latter. The part is made of a composite material and is produced by densifying a fibrous preform with a matrix. The fibrous preform includes a set of threads continuously extending along a path longitudinally extending over the preform portions (242) of at least two consecutive blades while passing into the preform portion (220) of the inner shroud and into the preform portion (260) of the outer shroud, and woven fibrous reinforcement threads continuously extending in the circumferential direction along an inner shroud segment and along an outer shroud segment between which the consecutive blades extend.