FIELD: transport.
SUBSTANCE: aircraft comprises wing 5 with positive dihedral angle, edge and wing edge device 7 secured in the area of edge. Wing edge device extends, generally, downward and has area 7d beveled at more than 180°C. Area 7d serves to create lift in flight. Said area 7d beveled at more than 180°C may be arranged at distal end 11 of wing edge device 7. Part of wing edge device located in proximal end has no area beveled at more than 180°C. Wing edge may be swept and elastically strained in flight.
EFFECT: higher operating performances.
15 cl, 12 dwg
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Authors
Dates
2013-01-20—Published
2006-09-12—Filed