Duct for hot air deicing

Details Duct for hot air deicing Duct for hot air deicing

B - Operations, Transporting

64

D

244/109

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

Patent

CA 1270237

ABSTRACT DUCT FOR HOT AIR Damage to the skin of the annular cowl (11) of the intake duct of a turbo-fan engine of an aircraft by exhaust on to it of hot air used within the cowl for de-icing its leading edge (10) is avoided by channelling spent air through an exhaust duct (15) to an exhaust aperture (21) in the surface of the cowl, and providing a heat shield (23) in the skin downstream of the exhaust aperture (21).

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