Method for hybrid manufacturing of a straightener vane for an aircraft gas-turbine engine
作者： Sébastien Pautard , Mathieu Renaud
DOI:
关键词: Thermoplastic 、 Airfoil 、 Materials science 、 Gas turbines 、 Braid 、 Mechanical engineering
摘要: The invention relates to a method for hybrid manufacturing of straightener vane an aircraft gas-turbine engine, the including blading made composite material, placing, (E20) in injection tool, braid thermoplastic material that adapts aerofoil vane; closing (E30) tool; injecting resin under pressure (E40) into tool such as fill inner space and shape braid; compacting (E40-3) assembly; solidifying (E40-4) consolidate removing (E60) resulting from mould.
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