The invention relates to a wing for generating lift and comprises a trailing edge, a leading edge, an inner end, an outer end, a top surface and a bottom surface. The wing comprises an aerofoil with a chord line and a span direction. The leading edge comprises a kink between the inner end and the outer end. The leading edge comprises a forward sweep part between the inner end and the kink extending towards the kink presenting an angle relative to the span direction. The leading edge comprises a backward sweep part between the kink and the outer end extending from the kink presenting an angle relative to the span direction. The top surface comprises a flow control means for controlling the lift at least partly located between a leading edge part between the kink and the outer end and located between the leading edge and the trailing edge.
WING FOR GENERATING LIFT FROM AN INCIDENT FLOW
FLÜGEL ZUM ERZEUGEN VON AUFTRIEB AUS EINER ANSTRÖMUNG
AILE DESTINÉE À GÉNÉRER UNE PORTANCE À PARTIR D'UN FLUX INCIDENT
2016-10-26
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Asymmetric rotation flapping wing lift force generating device
European Patent Office | 2015
|Engineering Index Backfile | 1944
|Emerald Group Publishing | 1944
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