| 摘要 |
A composite vane for a turbine engine, the vane having a pressure side face (12) and a suction side face (14) that define the aerodynamic profile of the vane, the vane (10) comprising: a metallic core (20) forming the pressure side face (12) or the suction side face (14) of the vane; and an organic matrix (30) associated with the metallic core (20). |
