Resources Contact Us Home
Browse by: INVENTOR PATENT HOLDER PATENT NUMBER DATE
 
 
Rotatable non-circular forebody flow controller










Image Number 2 for United States Patent #5050819.

The invention is a rotatable, non-circular forebody flow controller. The apparatus comprises a small geometric device located at a nose of a forebody of an aircraft or missile. The geometric device has a circular base that fits flush upon the remaining forebody of the aircraft and a non-circular cross-sectional area that extends toward the apex of the aircraft. The device is symmetrical about a reference plane and preferably attaches to an axle which in turn attaches to a rotating motor. The motor rotates the device about an axis of rotation. Preferably, a control unit connected to an aircraft flight control computer signals to the rotating motor the proper rotational positioning of the geometric device.








 
 
  Recently Added Patents
Infant bodysuit
Cysteine protease inhibitors for the treatment of parasitic diseases
Comparison selection, ranking, and anti-cheating methods in an online contest environment
Cable tie
Method of manufacturing semiconductor device with offset sidewall structure
Balancing usage of hardware devices among clients
Composite crystal colloidal array with photochromic member
  Randomly Featured Patents
Instant photographic apparatus
Glass refrigerator shelf
Methods and systems for adjusting a scoring measure based on query breadth
Pet console seat
Cis or trans-6-substituted-11-aminoalkylidenemorphanthridines
DC power source device with timer controlled synchronous rectifiers in the secondary
Composition and methods for promoting wound healing and tissue regeneration
Semiconductor device package
Adhesive bonding of strings of pocketed coil springs
Clause counter map inference engine