Aircraft acoustic attenuation member and method for forming...

Details Aircraft acoustic attenuation member and method for forming... Aircraft acoustic attenuation member and method for forming...

G - Physics

10

K

G10K 11/172 (2006.01) F02C 7/045 (2006.01) F02K 1/82 (2006.01)

Patent

CA 2754782

An aircraft acoustic attenuation member comprises a cone fairing (10) having an inner thermal layer (24), an injection moulded cellular structure having an inwardly facing wall (28) and square cells (30), and an outer perforated skin (32).

Un organe d'atténuation acoustique d'aéronef comprend un carénage conique (10) comportant une couche thermique interne (24), une structure alvéolaire moulée par injection comportant une paroi tournée vers l'intérieur (28) et des alvéoles carrées (30), et un revêtement externe perforé (32).

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