Aircraft engine exhaust nozzle

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

Patent

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Details

F02K 1/40 (2006.01) B64D 33/04 (2006.01)

Patent

CA 2542717

Tuyère d'éjection (14) d'un moteur d'engin volant, comprenant un corps tubulaire à deux canaux de sortie (16, 18) et des boîtiers (26, 28) d'injection de gaz dans les canaux de sortie pour l'orientation de poussée, ces boîtiers comportant des fenêtres (38) alignées avec des fentes (39) formées dans les canaux de sortie, et des moyens commandés de réglage du débit de gaz injecté dans les canaux de sortie.

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