FIELD: aircraft engineering.
SUBSTANCE: in compliance with first version, electric aircraft top and bottom wall fragmentation wings 6, bearing systems composed of prop fans fitted on fuselage front pylons 1 with set of wing fragments 10 on fuselage sides, air intakes 17 of jet ejection system behind every last fragments of the set, and power plant 3 with thrust reversal integrated in fuselage tail. Other versions of said aircraft are characterised by configuration and arrangement of abode said units characterised in appropriate claims. Every method is characterised by employment of said electric aircraft.
EFFECT: higher flight efficiency.
28 cl, 18 dwg
Authors
Dates
2012-11-20—Published
2010-05-18—Filed