FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to control over aircraft airfoils. Wing structure with flow influencing device comprises aircraft wing T including main wing 10, at least, one flap 20 attached to main wing 10 to increase lift and, at least, one spoiler 30 attached to main wing to turn thereabout. Main wing 10 has multiple ejection openings II, some of them being arranged side by side in direction HS of main wing span and communicated via air line 13 with outlet device P2 located on main wing 10 or spoiler 30 of flow feed drive device P. Spoiler 30 comprises multiple outlet air inlet openings communicated via air line 40, 50 with inlet P1 of flow delivery drive device P. Said device P incorporates receiver of command signals for control over flow delivery drive device P. Flow influencing device comprises control devoice 101 to control drive P connected with flight control device 100.
EFFECT: higher aerodynamic efficiency of wing.
13 cl, 9 dwg
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