AIR-CONDITIONING SYSTEM FOR FLYING VEHICLES EQUIPPED WITH DOUBLE-FLOW TURBO-JET ENGINES Russian patent published in 2007 - IPC B64D13/06 

FIELD: aeronautical engineering; air-conditioning systems for flying vehicles equipped with double-flow turbo-jet engines.

SUBSTANCE: proposed air-conditioning system includes heat exchanger whose hot line is connected with engine compressor by means of air-bleed line and is communicated with flying vehicle cabin and purging line is connected with engine fan circuit by means of air duct and is communicated with atmosphere. Flap with inlet wing (11) and outlet wing (12) is mounted in air duct by means of hinge (10) and is connected with flow and temperature regulator. Air flow stabilizing unit is made in form of divider (13) mounted in between air-to-air heat exchanger and flap of flow and temperature regulator in segment of air duct section behind outlet wing (12); front surface (15) is equidistant relative to profile of edge of outlet wing (12) in all positions of flap.

EFFECT: increased service life of all components of air-conditioning system.

4 dwg