FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to engine configuration. Engines are arranged at aircraft tail 2. Note here that engines are fixed by pylons to airframe. Note also that airframe comprises structure of torsion boxes 14 arranged across said airframe 2 to allow attachment of pylons 5. Airframe 2 comprises opening 4 to allow passage of engine pylons 5. Note here that described configuration includes extra rotary region 8, power drive 7 and connection part 6 to said power drive 7 to be connected to pylons 5 and torsion box structure 14. Assembly composed by power drive 7 and connection part 7 allows balancing assembly of pylons 5 and engines 3 by rotary region 9 to ensure optimum deflection of thrust vector at every stage of the flight.
EFFECT: better controllability and simplified design.
10 cl, 5 dwg
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