FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed airframe, wings, two turbojet sustainer engines, VTOL jet engines equally spaced apart from aircraft center of gravity and driven by sustainer turbojet engines, ACS hardware. Every sustainer turbojet engine comprises low-pressure and low-pressure compressors, front device to ignite fuel with air from high-pressure compressor and air- and fuel main lines connected with each jet engine by confuser-diffuser sleeve arranged gas bearing. One jet engine is arranged at aircraft tail end. One of jet engine is pivoted to every wing pylon at front section and via shackles at front section with hydraulic cylinder hinged to appropriate wing. Ballistic flaps-shutters are arranged in the zone of said hinge.
EFFECT: improved operating performances of aircraft units.
5 dwg
