Resources Contact Us Home
Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance

Image Number 17 for United States Patent #7475848.

A wing for use on a supersonic aircraft that includes an inboard section a central section of the wing outboard of the inboard portion, and an outboard section. The outboard section can be a winglet oriented anhedrally relative to a lateral axis of the supersonic aircraft. Leading edge segments on the inboard section, central section and outboard winglet may have mounted thereon leading-edge flaps. These flaps are adjusted by a control system operable to reposition the leading-edge flaps in order to improve the aerodynamic performance of the supersonic aircraft. This winglet promotes sonic boom minimization. Further, the wing tip anhedral allows greater inboard dihedral. This effectively pushes lift aft for sonic boom and control purposes while minimizing the movement of control surfaces.

  Recently Added Patents
Mobile device case with storage compartment
Software self-checking systems and methods
Systems and methods for printing images outside a normal color gamut in image forming devices
Toy ball
Vehicle front fender
Method of manufacturing touch panel
Data transfer device and data transfer method
  Randomly Featured Patents
Semiconductor light-emitting device and method for manufacturing the same
Connectable drive for a screwdriver spindle
Piezoelectric wire matrix printer head
Beverage case
Pneumatic horn
Spiral groove pattern refiner plates
Method and apparatus for encoding/decoding bus signal
Back pack for use with hunting bow and method
Tapered compressed powder charge for muzzleloader and black powder firearms
Label switched packet transfer device