Coating for acoustic treatment including a rime hot-air...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 33/02 (2006.01)

Patent

CA 2689495

The invention relates to a coating for acoustic treatment at the surface of an aircraft, in particular at the leading edge such as the air intake of an aircraft nacelle, said coating including an acoustically resistive layer (28), at least one cellular structure (30) and a reflective layer (32), characterised in that it comprises ducts (34) provided between said cellular structure (30) and the acoustically resistive structure (28), the ducts being each defined by a wall (36) separate from the walls of the cellular structure (30) and one end of the ducts being connected to a hot air supply.

L'objet de l' invention est un revêtement pour le traitement acoustique rapporté au niveau d'une surface d'un aéronef, notamment au niveau d'un bord d'attaque tel qu'une entrée d'air d'une nacelle d'aéronef, ledit revêtement comprenant une couche acoustiquement résistive (28), au moins une structure alvéolaire (30) et une couche réflectrice (32), caractérisé en ce qu'il comprend des conduits (34) placés entre ladite structure alvéolaire (30) et la structure acoustiquement résistive (28), les conduits étant délimités chacun par une paroi (36) distincte des parois de la structure alvéolaire (30) et une des extrémités des conduits étant reliée à une arrivée d'air chaud.

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