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
Vacuum cleaner
Methods and compositions for improved F-18 labeling of proteins, peptides and other molecules
Cardiac function management integrating cardiac contractility modulation
Automatic search system and method
Methods, systems, and products for providing communications services
Inhibitors of human immunodeficiency virus replication
Method and apparatus for monitoring for a radio link failure
  Randomly Featured Patents
Record drive system for rotary electrical stylus device
Garbage can
Percussion instrument
Door lock
Organic electroluminescence display panel and method for sealing the same
Output circuit of semiconductor memory device
Apparatus for controlling spindle motor of compact disc utilizing appliance
Method and cosmetic composition for reducing sebum secretion
Translation of object queries involving inheritence