FIELD: ventilation.
SUBSTANCE: air conditioning system contains primary and secondary heat exchangers, loop heat exchangers and a basic turbo refrigerator. The system further comprises a bypass line connected via a shutter after the primary heat exchanger and comprising an additional turbo chiller connected at the compressor inlet and at the turbine inlet to the engine bleed pipeline, wherein the compressor outlet is included in the main pipeline in front of the secondary heat exchanger, and the turbine outlet is connected to the atmospheric pressure zone.
EFFECT: ensuring a sufficient degree of air compression in the turbocharger compressor at the reduced pressure of air entering the system.
1 dwg
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