FIELD: transport.
SUBSTANCE: invention relates to aviation, in particular, to vertical take-off and landing aircraft. The atmospheric flying saucer has body, jet engine, flight deck with steering wheel, instrument panel, pilot seat and passenger seat. The body consists of radial side members, outer upper rubs, inner upper ribs, outer lower ribs, cabin side members. Engine and fuel tank are installed above flying saucer body in engine nacelle the lower part of which has a nozzle and is mounted on stems of hydraulic cylinders installed on outer upper ribs. Profile of outer upper ribs follows wing upper part form where the front edge is the most distant from vertical symmetry axis of flying saucer, and the rear edge transits into conical surface of inner upper ribs. Profile of outer upper ribs can follow form of upper rear wing part where wing profile rear point is the most distant from symmetry axis of flying saucer, and wing profile bend point coincides with end point of inner upper rib. Chord of wing profile can have angle of slope relative to horizontal line α of 0° to 90°. Vertical component of T-shaped profile of reactive torque equalisers can be made in the form wing profile or in form of arc.
EFFECT: lower fuel consumption and higher lifting force.
6 cl, 28 dwg
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Authors
Dates
2015-04-20—Published
2013-08-06—Filed