| 摘要 |
The invention relates to an air conditioning system for the pressurized cabin of an aircraft. The system (1) comprises an air intake module (3) that is designed to draw in ambient air external to the aircraft, an air compression module (5) that is designed to compress the drawn-in air flow (F1), and an air cooling module (10) that is designed to cool the compressed air flow (F2, F3) from a cryogenic fluid, said cooling module (10) comprising a condenser (12) for condensing the water in the air flow, a water extractor (13) for extracting said water, a cooler (14) for cooling the dry air flow originating from the water extractor (13) and a tank (15) of a cryogenic fluid by means of which the water from the air flow is condensed in the condenser (12) and the dry air resulting from the extractor is cooled in the cooler (14). |
