首页> 外国专利> Acoustic attenuation panel i.e. acoustic attenuation lining, for propulsion system of aircraft, has cellular structure whose one of characteristics varies acoustic wave to locally oppose acoustic wave to impedance variations

Acoustic attenuation panel i.e. acoustic attenuation lining, for propulsion system of aircraft, has cellular structure whose one of characteristics varies acoustic wave to locally oppose acoustic wave to impedance variations

机译:用于飞机推进系统的声衰减板,即声衰减衬里,具有蜂窝状结构,其特征之一是改变声波以局部地使声波抵抗阻抗变化

摘要

The panel i.e. acoustic attenuation lining (26), has a cellular structure (30) whose one of characteristics e.g. proportion of open surface, influences impedance of the panel. One of the characteristics varies acoustic wave along a propagation axis i.e. longitudinal axis, of a nacelle to locally oppose the wave to impedance variations due to the characteristics related to aerodynamic flow and the wave. The cellular structure is presented in the form of Nida Nomex(RTM: lightweight honeycomb fiber).
机译:面板,即声衰减衬里(26),具有蜂窝状结构(30),其特征之一是例如蜂窝状。开口表面的比例,影响面板的阻抗。特征之一是沿着机舱的传播轴即纵轴改变声波,以使声波由于与空气动力流和声波有关的特性而局部地与阻抗变化相对。细胞结构以Nida Nomex(RTM:轻质蜂窝状纤维)的形式存在。

著录项

  • 公开/公告号FR2915522A1

    专利类型

  • 公开/公告日2008-10-31

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE SOCIETE PAR ACTIONS SIMPLIFIEE;

    申请/专利号FR20070054783

  • 发明设计人 LIDOINE SYLVAIN;

    申请日2007-04-30

  • 分类号F02C7/24;B64D33;

  • 国家 FR

  • 入库时间 2022-08-21 19:46:59

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