Acoustic attenuation panel for aircraft engine nacelle

F - Mech Eng,Light,Heat,Weapons – 02 – K

Patent

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F02K 1/82 (2006.01) B64D 29/00 (2006.01) F02C 7/045 (2006.01) F02C 7/24 (2006.01) G10K 11/162 (2006.01)

Patent

CA 2731974

This acoustic attenuation panel for an aircraft engine nacelle comprises a structuring skin (1) and, by way of acoustic absorption material, a porous material (5) attached to this skin (1).

Ce panneau d'atténuation acoustique pour nacelle de moteur d'aéronef comprend une peau structurante (1 ) et, comme matériau d'absorption acoustique, un matériau poreux (5) rapporté sur cette peau (1).

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