首页> 外国专利> METHOD FOR MANUFACTURING FLAN OF THERMOPLASTIC COMPOSITE MATERIAL, ASSOCIATED TOOLING FOR MANUFACTURING AND APPLICATION OF PROCESS TO REALIZATION OF AIRCRAFT STRUCTURE PARTS

METHOD FOR MANUFACTURING FLAN OF THERMOPLASTIC COMPOSITE MATERIAL, ASSOCIATED TOOLING FOR MANUFACTURING AND APPLICATION OF PROCESS TO REALIZATION OF AIRCRAFT STRUCTURE PARTS

机译:制造热塑性塑料复合材料的翼缘的方法,制造相关工具及其在飞机结构零件实现中的应用

摘要

The invention relates to a novel method for manufacturing a blank made of a thermoplastic composite material in which a pressure and temperature cycle is applied, by pressure on the top of a compacting plate (13) itself above a stack of fabrics (20) of pre-impregnated continuous fibers (20) of a thermoplastic resin, stack (20) previously placed on a marble (12) with contacting of the film (2) enveloping the stack (20) with tabling wedges (14) arranged at the periphery of the marble (12) and, by heating the stack, so as to reach at least the melting temperature of the resin while leaving the film infusible and smooth, and evacuating the gas (s) present in the stack by at least one opening (O) left in the wrapping film and then by at least one opening channel (42) formed in the compacting plate (13) and / or in the marble (12) and / or in the shims (14).
机译:本发明涉及一种用于制造由热塑性复合材料制成的坯料的新颖方法,其中通过在预成型织物(20)的叠层上方的压实板(13)本身的顶部上施加压力来施加压力和温度循环。 -热塑性树脂的浸渍的连续纤维(20),叠层(20)预先放置在大理石(12)上,使薄膜(2)接触,使叠层(20)与布置在其周围的凸楔(14)接触。大理石(12),并通过加热烟囱,使其至少达到树脂的熔融温度,同时使薄膜不熔且光滑,并通过至少一个开口(O)排空烟囱中存在的气体留在包装膜中,然后留在形成在压紧板(13)和/或大理石(12)和/或垫片(14)中的至少一个开口通道(42)中。

著录项

  • 公开/公告号FR2929167A1

    专利类型

  • 公开/公告日2009-10-02

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号FR20080051979

  • 发明设计人 DAVID BOUVET;DIDIER KURTZ;

    申请日2008-03-27

  • 分类号B29C70/34;B29L31/30;

  • 国家 FR

  • 入库时间 2022-08-21 19:07:13

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