首页> 外国专利> A method of making an acoustic absorption structure comprising a skin forming a plurality of enclosures, an acoustic absorption structure obtained by said method and an aircraft comprising said acoustic absorption structure

A method of making an acoustic absorption structure comprising a skin forming a plurality of enclosures, an acoustic absorption structure obtained by said method and an aircraft comprising said acoustic absorption structure

机译:一种制造包括形成多个外壳的蒙皮的吸声结构的方法,通过所述方法获得的吸声结构以及包括所述吸声结构的飞机

摘要

Method for producing an acoustic absorption structure comprising a skin forming a plurality of enclosures, an acoustic absorption structure obtained according to said method and an aircraft comprising said acoustic absorption structure The subject of the invention is a method for producing a sound absorption structure comprising an acoustically resistive structure, a honeycomb structure (54), a reflective layer as well as a plurality of acoustic elements positioned in the honeycomb structure (54), against the acoustically resistive structure, the method comprising : a step of forming a skin (68) forming enclosures of the acoustic elements by attaching a resin to a mold (74) having a base (76) on which are positioned protruding shapes (78) shaped as the delimited cavities by the enclosures of the acoustic elements, a step of docking the mold (74) supporting the resin and the honeycomb structure (54), the resin being both interposed between the mold (74) and the honeycomb structure (54), a resin polymerization step in order to simultaneously obtain hardening of the skin (68) as well as the junction between the skin (68) and the honeycomb structure (54), and a step of placing the acoustically resistive structure and the reflective layer. Figure 9
机译:用于制造包括形成多个外壳的蒙皮的吸声结构的方法,根据所述方法获得的吸声结构以及包括所述吸声结构的飞机。本发明的主题是一种用于制造包括吸声结构的吸声结构的方法。抵抗结构,蜂窝结构(54),反射层以及位于蜂窝结构(54)中的多个声学元件,抵靠所述声学结构,所述方法包括:形成表皮(68)的步骤通过将树脂附着到具有底座(76)的模具(74)上来固定声学元件的外罩,通过声学元件的外罩将凸出形状(78)定位为定型腔,该步骤是将模具对接的步骤( 74)支撑树脂和蜂窝结构(54),树脂都插入在模具(74)和蜂窝结构(54)之间,为了同时获得表皮(68)以及表皮(68)和蜂窝结构(54)之间的接合处的硬化的树脂聚合步骤,以及放置声阻结构和反射层的步骤。图9

著录项

  • 公开/公告号FR3092844A1

    专利类型

  • 公开/公告日2020-08-21

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS (S.A.S.);

    申请/专利号FR20190001469

  • 发明设计人 FRANCK DOBIGEON;THÉO RICCOBENE;

    申请日2019-02-14

  • 分类号E04B1/84;B64C1/40;

  • 国家 FR

  • 入库时间 2022-08-21 11:00:21

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