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
Maintenance tool of control systems
Model matching for trace link generation
Method to dynamically tune precision resistance
Vehicle inertial sensor systems
Semiconductor unit having a power semiconductor and semiconductor apparatus using the same
Backup and recovery of distributed storage areas
Apparatus and method for controlling semiconductor die warpage
  Randomly Featured Patents
Categorization of a mobile user profile based on browse behavior
Electronic connector with extension band
Geranium plant named `Fisrohot`
Display apparatus for eyewear
Clock
Passive biotelemetry
Method and apparatus for decreasing the cycle times of a data processing system
Protective shield for shoe heels
Systems and methods for monitoring conditions
Device for atomizing a liquid product, a spray-drying and conditioning device provided therewith, and a method for conditioning a liquid product