FIELD: manufacture of aircraft. SUBSTANCE: transport aircraft with blunted tail section 5 of fuselage mainly contains two jet engines 4 integrated directly into tail section of fuselage. Air sucked into engines is fed through diffuser 6 located around two engines in close proximity to their inlet section; air is sucked from boundary layer through suction slots 8 by means of combination device consisting of ejector 12 and diffusers 6. This device is located in area of tail section of fuselage. This air is directed to common flow of air sucked into engine. EFFECT: enhanced reliability. 9 cl, 8 dwg
