FIELD: heat exchange.
SUBSTANCE: system for ensuring thermal regime of instrument compartment of aircraft contains heat-insulated casing and two-circuit cooling system with open external evaporative circuit, internal circuit in form of contour heat pipes installed on heat-stressed devices and equipped with regulator of heat flow and evaporator and associated with seats of corresponding heat-stressed devices, while capacitors are located in heat exchanger of external evaporative circuit.
EFFECT: increase in efficiency of cooling and thermostabilization of onboard equipment of aircraft.
1 cl, 1 dwg
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RU2705402C1 |
