FIELD: transport.
SUBSTANCE: set of inventions relates to aircraft air conditioning systems. Cooling system comprises air intake 4 to force air from ambient atmosphere into pressure air duct 2. The latter has air exhaust opening 6. Heat exchanger 10 is arranged in said pressure air duct 2 to feed cooling power by incident flow from pressure air duct 2 into cabin air conditioning system. Ventilation device 8 communicates with pressure air duct via aforesaid flow. Besides, distribution line 12 is communicated with said pressure air duct to cool, at least, one heat-loaded component of aircraft, in particular, cabin air conditioning system, and/or to vent mounting compartment of said heat-loaded component.
EFFECT: decreased space required to accommodate vent system.
12 cl, 6 dwg
