FIELD: flying vehicle equipment.
SUBSTANCE: liquid cooling system of aircraft (30) includes air heat exchanger (40) through which liquid flows. Air heat exchanger (40) includes air supply unit (52) and air discharge unit (54); it is mounted in body located in fairing (34) of guide rail of flap (36) connected with aircraft wing (32). Air supply unit (52) of air heat exchanger (40) is connected with air inlet device (42) passing through external surface (46) of fairing (34). Air discharge unit (54) of air heat exchanger (40) is connected with air outlet device (44) which is open on the outside of external surface (46) in such way that air on the outside of aircraft (30) passes through this air heat exchanger (40) for cooling the liquid. Specification gives also versions of aircraft equipped with such system.
EFFECT: improved cooling of liquid.
25 cl, 11 dwg
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