首页> 外国专利> ACOUSTIC PANEL OF AIR INTAKE OF AN AIRCRAFT NACELLE WITH CRENELLATED RESISTIVE SKIN, AND PROPULSION ASSEMBLY AND AIRCRAFT PROVIDED WITH SUCH ACOUSTIC PANELS

ACOUSTIC PANEL OF AIR INTAKE OF AN AIRCRAFT NACELLE WITH CRENELLATED RESISTIVE SKIN, AND PROPULSION ASSEMBLY AND AIRCRAFT PROVIDED WITH SUCH ACOUSTIC PANELS

机译:带有Crenellated Telsive皮肤的飞机机舱的空气摄入的声学板,以及带有这种声学板的推进组件和飞机

摘要

The invention relates to an aircraft nacelle air intake acoustic panel comprising a resistive skin (1) pierced with sound absorption holes (10), and a core (2) against which the resistive skin extends. (1). characterized in that the resistive skin (1) has a smooth visible face (11) and a crenellated rear face (12) having an alternation of crenellations (14) and trenches (13), the sound absorption holes (10) being formed only in the trenches (13) that is to say in an area where the thickness of the skin is less, which makes it possible to produce holes having a diameter that is both greater than the thickness of the skin. skin and small enough to have no impact on the drag. The smaller thickness of the resistive skin at the level of the trenches does not make it more flexible than the previous skins, the mechanical strength of the resistive skin according to the invention being guaranteed by the crenellations.
机译:本发明涉及一种飞机机舱进气进气声学板,其包括具有吸声孔(10)的电阻性皮肤(1),以及电阻皮肤延伸的芯(2)。 (1)。其特征在于,电阻性皮肤(1)具有平滑的可见面(11)和具有克里尔(14)和沟槽(13)的交替的Crenellated后表面(12),所述吸声孔(10)仅在其中形成即在皮肤厚度较少的区域中可以说的沟槽(13),这使得可以产生直径大于皮肤厚度的直径的孔。皮肤和小足以对阻力没有影响。沟槽水平的电阻皮肤的较小厚度不会使其比先前的皮肤更柔韧,根据本发明的裂扰物的电阻皮的机械强度。

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