AIR-CONDITIONING SYSTEM FOR CABIN AND EQUIPMENT COMPARTMENTS OF AEROBATIC AEROPLANE

摘要

FIELD: aviation. SUBSTANCE: air-conditioning system includes main for taking air from engine, cold and hot air lines provided with respective adjusting dampers and connected with main feeding the mixed air to cabin compartment; air-conditioning system contains also cooling turbine. Cold air line after cooling turbine is brought in communication with pipe line feeding the cold air to equipment compartments fitted with shut-off damper operated from altitude sensor and cross-connected with throttle valve by means of bypass line. EFFECT: enhanced efficiency. 1 dwg