FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Cooler 10 for aircraft cooling system 100 comprises matrix case 12 with multiple channels 16 for coolant extending from first surface 18 of matrix case to its second surface 20 to allow coolant to flow through said matrix case. Said matrix case 12 makes the aircraft outer skin section.
EFFECT: efficient operation of cooling system for heat removal from heat-emitting device.
26 cl, 16 dwg
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