Jet engine nose inlet cowl with de-icing protection

Details Jet engine nose inlet cowl with de-icing protection Jet engine nose inlet cowl with de-icing protection

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/047 (2006.01) B64D 15/04 (2006.01) B64D 33/02 (2006.01)

Patent

CA 2380677

- According to the invention, an air extraction opening (34) is made in the partition (20) to place the isolation volume (28) enclosing the pressurized hot air feedpipe (10) in communication with the internal peripheral chamber (21) of said leading edge (16), and the passage cross section of said extraction opening (34) is chosen to give the injector (12), in the event of damage to said feedpipe (10), a pressurized hot air flow rate at least equal to 50% of the hot air flow rate through said feedpipe (10).

- Selon l'invention, une ouverture d'extraction d'air (34) est pratiquée dans la cloison (20), pour mettre en communication le volume d'isolation (28) enfermant la conduite (10) d'alimentation en air chaud sous pression avec la chambre périphérique interne (21) dudit bord d'attaque (16) et l'aire de la section de passage de ladite ouverture d'extraction (34) est choisie pour assurer à l'injecteur (12), en cas d'avarie de ladite conduite d'alimentation (10), un débit d'air chaud sous pression au moins égal à 50% du débit d'air chaud dans ladite conduite d'alimentation (10).

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