A system for supplying an aircraft with cool air

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 13/08 (2006.01) B64D 13/02 (2006.01)

Patent

CA 2380893

The cool air inlet is fed with air cooled in a heat exchanger swept by a flow of external air from a static air inlet of the aircraft. The system further includes ejector means for circulating external air in the exchanger. The ejector means include a nozzle fed with air from a cabin of the aircraft via a cabin air outlet.

L'orifice d'entrée d'air froid est alimenté de l'air refroidi dans un échangeur de chaleur balayé par un flux d'air extérieur à partir d'un orifice d'entrée d'air statique de l'aéronef. Le dispositif comprend en outre des moyens d'éjection pour faire circuler de l'air extérieur dans l'échangeur. Les moyens d'éjection comprennent une buse alimentée de l'air provenant d'une cabine de l'aéronef par l'intermédiaire d'un orifice de sortie d'air de la cabine.

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