FIELD: transport.
SUBSTANCE: invention relates to equipment for cooling aircraft electronic hardware. Proposed system comprises, at least, one heat-emitting electronic component. Multistage design of proposed system consists in using several circuits for transfer of dissipating heat. Internal heat carrier circulates in closed circuit thermally connected with electronic component to transfer heat therefrom to heat exchanger. Note here that said heat exchanger releases heat to external heat carrier flowing and/or circulating from source outside of aircraft electronic system via heat exchanger to heat absorber outside of said electronic system. Internal heat carrier flows from heat exchanger toward, at least, one electronic component, and/or circulates in closed circuit.
EFFECT: higher efficiency of cooling.
13 cl, 12 dwg
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