Cowling for turbine engine nozzle with jet noise reduction...

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

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F02C 7/24 (2006.01) F02K 1/04 (2006.01) F02K 1/44 (2006.01)

Patent

CA 2511892

Capot (14, 16) pour tuyère (10) de turbomachine comportant une pluralité de motifs (26) répétitifs disposés de façon circonférentielle sur un bord de fuite (14a), chaque motif (26) étant dissymétrique par rapport à un plan médian du motif passant par un axe longitudinal (X-X) dudit capot (14, 16) et chaque motif (26) comportant une première portion inclinée radialement vers l'intérieur du capot (14, 16) et une seconde portion inclinée radialement vers l'extérieur du capot (14, 16).

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