FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed unit 22 for aircraft with multiple climatic zones (12 to 20) comprises the main branching system 26 incorporating system of air feed channels with mixing chamber 28 and multiple branching subsystems 30, primary temperature control means 32 and individual temperature control means (36, 38, 40, 42). Individual temperature control means (36, 38, 40, 42) are used for individual temperature regulation of air fed in each branching subsystem 30 depending upon desirable temperature of climatic zone and comprise one combined thermal power engine 44 running in compliance with thermodynamic operating cycle.
EFFECT: efficient air conditioning of multi-zone space.
11 cl, 3 dwg
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