Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift

Wing for an aircraft, aircraft and method for reducing aerodynamic drag and improving maximum lift

  • CN 103,419,929 A
  • Filed: 03/28/2013
  • Published: 12/04/2013
  • Est. Priority Date: 03/29/2012
  • Status: Active Application
First Claim
Patent Images

1. the wing for aircraft (2) comprising:

  • Leading edge (4), andWingtip extension (8), described wingtip extension (8) extends to wingtip (26) from the end in host wing zone,Wherein, described wingtip extension (8) comprises along described leading edge (8) at least to be arranged from described end to the opening (22) of described wingtip (26) in described host wing zone, described opening (22) is connected to air transport device (30,38,40,44), and described air transport device (30,38,40,44) passes through described opening (22) for delivery of air.

View all claims
    ×
    ×

    Thank you for your feedback

    ×
    ×