FIELD: transport.
SUBSTANCE: invention relates to rotorcraft, namely, to VTOL aircraft. Aircraft comprises wing, fuselage, two air breathers arranged at fuselage tail one above the other in aircraft mirror plane. Lower air breather incorporates nozzle pivoting in vertical plane to develop vertical thrust component. Lower air breather jet nozzle is arranged closer the fuselage tail than that of upper air breather. Aircraft wing is configured as high-wing. Top air breather air intake is located on fuselage hose top while bottom air intake is arranged at fuselage nose bottom. Generator of compression shocks in said air intakes represents fuselage nose section compose of horizontal multistage wedge.
EFFECT: improved aerodynamics.
11 cl, 6 dwg
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Authors
Dates
2014-10-27—Published
2013-08-07—Filed