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
Method for producing (meth)acrylic anhydride, method for storing (meth)acrylic anhydride, and method for producing (meth)acrylate
Quaternary chalcogenide wafers
Combined imaging and radiation therapy
Deposited conductive layers for leads of implantable electric stimulation systems and methods of making and using
Apparatus and method for information processing, program, and recording medium
Wireless device and communication control method
Over the counter medicinal container with surface ornamentation
  Randomly Featured Patents
Charge restore circuit for semiconductor memories
Method and apparatus for steering a vehicle
Cord restraint
Polypeptides having beta-glucosidase activity and beta-xylosidase activity and polynucleotides encoding same
Flow restraining elements in the headbox of a paper machine
Uploading TCP frame data to user buffers and buffers in system memory
Electric heater
Internal command generation circuit
Two channel compatible high definition television broadcast system
Cigarette making machine hopper