An air conditioning system

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 13/08 (2006.01) B64D 13/06 (2006.01)

Patent

CA 2397048

An air conditioning system for an aeroplane cabin, comprising a heat exchanger for cooling compressed air from an aeroplane engine or an auxiliary unit and at least one expansion device per air cycle machine for the expansion and cooling of compressed air, disposed after the heat exchanger and connected with a mixing chamber or the cabin. High cooling performance is achieved on the failure of one of the expansion devices or of an air cycle machine by splitting the heat exchanger into two heat exchanger units which are connected such that a flow of the compressed air from one heat exchanger unit to the other heat exchanger unit is prevented and with the heat exchanger units connected to the space to be air conditioned or to the mixing chamber or to the outlet of the air conditioning system, through a bypass line.

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