Jet engine nose inlet cowl having de-icing means

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

Patent

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F02C 7/047 (2006.01) B64D 15/04 (2006.01) F01D 25/08 (2006.01)

Patent

CA 2356328

Selon l'invention, le bord d'attaque creux (16) dudit capot (9) comporte un mélangeur (19) pour former, à chaque instant, le mélange du flux d'air chaud (20) en cours d'injection avec une partie du flux d'air en recirculation, injectée antérieurement. On obtient ainsi l'homogénéisation de la température à l'intérieur dudit bord d'attaque (16) avec suppression des points chauds et optimisation du dégivrage.

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