| 摘要 |
The invention relates to a vane (10) for a turbine engine, made of a composite material including a fiber reinforcement obtained by means of three-dimensional weaving of threads and densified by a matrix. The vane includes a blade (12) and a vane base (14) that form a single part, the vane base having two substantially planar, opposite side flanks closed between two separate composite material plates (24) that are attached onto the side flanks of the vane base such as to form a bulb-shaped vane base. |
