Turboshaft engine with reduced noise emission for aircraft

Details Turboshaft engine with reduced noise emission for aircraft Turboshaft engine with reduced noise emission for aircraft

F - Mech Eng,Light,Heat,Weapons

02

K

F02K 1/48 (2006.01)

Patent

CA 2695626

According to the invention, a plurality of embossments (20) having a rectangular section is provided at the inner periphery of the outlet opening (7) of the fan duct (12), said embossments being separated by longitudinal channels (21) having a convergent (22C) and a divergent (22D) for the cold flow (9).

Selon l'invention, à la périphérie interne de l'orifice de sortie (7) du canal de soufflante (12), on agence une pluralité de bossages (20) à section rectangulaire, séparés par des canaux longitudinaux (21) et présentant un convergent (22C) et un divergent (22D) pour le flux froid (9).

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