Patent ID: 9708917
Date: 2017-07-18
CPC Classifications: B29B,B29C,C04B,D03D,F01D,F04D,F05D,Y02T,Y10T

Claim:
1. A turbine engine part forming a compressor stator or a turbine nozzle comprising: an inner shroud; an outer shroud; and vanes extending substantially radially between the inner and outer shrouds and secured thereto, wherein the inner shroud, the outer shroud, and the vanes are made of composite material having woven fiber reinforcement densified by a matrix, and the fiber reinforcement includes a set of yams extending continuously along a path traveling longitudinally through at least two consecutive vanes and passing through the inner shroud and the outer shroud, the at least two consecutive vanes extending between an inner shroud segment and an outer shroud segment with yarns of the woven fiber reinforcement passing continuously along a complete circumference of the inner shroud segment and with yarns of the woven fiber reinforcement passing continuously along a complete circumference of the outer shroud segment.