FIELD: transport.
SUBSTANCE: invention relates to cooling systems designed to cool heat generating devices aboard the aircraft. Proposed system comprises central cold generation device, cold consuming devices and cold transfer system. The latter comprises cooling circuit which feeds cooled coolant from central cold generation device to cold consumers and back to central generation device. Cold consumers receive cold from aforesaid cold generation device via coolant circulating in cooling circuit. Central cold generation device comprises refrigerators which work independently and are connected in parallel to cold transfer system. There are several independent cooling circuits. At least two cooling circuits have thermal communication with cold consumers via central cold generation device.
EFFECT: increased efficiency and reliability of aircraft cooling system.
21 cl, 2 dwg
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