FIELD: ventilation.
SUBSTANCE: air conditioning system for the sealed cabin of the aircraft comprises the air bleeding unit (3), configured to extract the ambient air from outside the aircraft, the air compression module (5), configured to compress the bleed air flow (F1), and the air cooling module (10), which is capable to cool the flow (F2, F3) of the compressed air by means of the cryogenic fluid medium. The cooling module (10) comprises the condenser (12) for condensing the water from the air stream, the water extractor (13) for extracting the mentioned water, the cooler (14) for cooling the dry air stream from the water extractor (13) and the cryogenic fluid tank (15) by which the air stream water is condensed in the condenser (12) and the dry air, coming from the water extractor, is cooled in the cooler (14).
EFFECT: improvement of the air conditioning system.
7 cl, 3 dwg
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