FIELD: machine building.
SUBSTANCE: airborne vehicle has at least one power plant equipped at least with one temperature cooling and control system of units of that power plant. System has the first heat exchange means between lubrication circuits at least of two above described units and heat carrier medium contained in a closed circuit, and the second heat exchange means between heat carrier medium and at least one cooling medium. The first heat exchange means are located locally at the level of each of the above units. The second heat exchange means are located at some distance from the above first means. Closed circuit passes at least between two of the units and the second heat exchange means. The system is connected to heat carrier medium network, which serves the units of the airborne vehicle, which are external in relation to the power plant.
EFFECT: minimisation of lubrication oil circulation of the units outside cooled units and separation of lubrication and cooling functions.
11 cl, 6 dwg
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