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Noise reduced and rib assembly for a high-lift device of an aircraft

机译:用于飞机的高升降装置的噪声减少和肋骨组件

摘要

An end rib assembly for a high-lift device of an aircraft to reduce the noise caused by the transition between the wing and a high-lift device as well as the noise caused by the lateral side edge of the end rib assembly. An end rib assembly includes a noise-reducing portion configured to reduce noise caused by an airflow around the end rib assembly, and a guiding portion configured for guiding the end rib assembly along a pre-determined path when the high-lift device is moved between a retracted position and an extended position, wherein the guiding portion is formed such that an airflow impinging on the guiding portion is partly guided towards the noise-reducing portion.
机译:用于飞机的高升程装置的端部肋组件,以减少由机翼和高升降装置之间的过渡引起的噪声以及由端肋组件的横向侧边缘引起的噪声。 端部肋组件包括噪声减小部分,该噪声减小部分被配置为减少由端部肋组件周围的气流引起的噪声,以及当高升程装置移动时,构造用于沿着预先确定的路径引导端肋组件的引导部分 缩回位置和伸展位置,其中形成引导部分,使得撞击在引导部分上的气流部分地朝向降噪部分被引导。

著录项

  • 公开/公告号GB2580454B

    专利类型

  • 公开/公告日2021-08-04

    原文格式PDF

  • 申请/专利权人 AIRBUS DEFENCE AND SPACE GMBH;

    申请/专利号GB20190012556

  • 发明设计人 WOLFGANG MACHUNZE;HEIKO FIETZEK;

    申请日2019-09-02

  • 分类号B64C9/08;B64C9/02;B64C9/16;B64C9/18;

  • 国家 GB

  • 入库时间 2022-08-24 20:27:16

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