| 摘要 |
<p>The invention relates to a method for hybrid manufacturing of a straightener vane for an aircraft gas-turbine engine, the straightener vane including blading made of composite material, the method including placing, (E20) in an injection tool, a braid of thermoplastic material that adapts to the aerofoil of the vane; closing (E30) the injection tool; injecting a thermoplastic resin under pressure (E40) into the injection tool such as to fill the inner space of the braid and to shape the braid; compacting (E40-3) the assembly; solidifying (E40-4) the resin such as to consolidate the braid; and removing (E60) the resulting straightener vane from the mould.</p> |
