FIELD: aircraft engineering.
SUBSTANCE: invention relates to the air conditioning systems in the field of aviation. Aircraft air conditioning system contains the air from the main engines takeoff subsystems, air cooling units for cargo compartments, crew and front compartments, pressure and temperature measuring instruments. System further comprises the cross-feed valve and the takeoff flap from the auxiliary plant.
EFFECT: enabling compliance with the microclimate in the pressurized cabin required parameters and the onboard equipment cooling in the entire range of the object operating modes, performing optimization of the air temperature, flow rate and pressure during the ventilation process in accordance with the flight mode and conditions; enabling the system high reliability and testability.
3 cl, 3 dwg
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