FIELD: transport.
SUBSTANCE: proposed aircraft comprises fuselage 1 top 2 and bottom 1 decks, front wing arranged in nose section above fuselage bottom section top surface, rear wing 4 arranged in pylon at tail section on fuselage deck surface, spaced apart vertical tail 9 arranged on tips of rear wing 4, engines 11 and landing gear 12. Rear rotary wing 4 is mounted on pylon. Top deck 2 is displaced relative to bottom deck 1 over fuselage length through the distance that allows arranging front rotary wing 3 below rear rotary wing 4. Aircraft incorporates automatic pitch hold system comprising interceptors or control surfaces.
EFFECT: reduced weight, between aerodynamic characteristics.
6 dwg
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