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
Architectural panel with bamboo rings light density embossed surface
Media processing method and device
Cooling structure and cooling method for control rod drive mechanism and nuclear reactor
Products for animal use including humans having a certificate verifying at least one of efficacy or safety, and methods of providing such certificates
Flat display panel and method for forming the same
Method of modified facies proportions upon history matching of a geological model
Irreversible thermochromic ink compositions
  Randomly Featured Patents
Apparatus for suspending goods for display
Automatic focusing camera system and photographing lens structure therefor
Device for continuous separation of solid particles from a liquid suspension
Hydrogel constructs using stereolithography
Low pressure shutoff valve for fluid operated tool
Guitar hanger
Color conversion device and color conversion method
Disk for cleaning magnetic head of disk drive
Cheat preventing OMR cardcheat preventing OMR card
Versatile toy capable of activating electronics and launching components thereof