Patents by Inventor Robert Arthur Williams

Robert Arthur Williams has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 8463096
    Abstract: Described are track-resistant all dielectric self-supporting (TR-ADSS) cables with improved cable jackets. A typical TR-ADSS optical fiber cable comprises an optical fiber sub-assembly, and a cable jacket system. The cable jacket system comprises an inner jacket, an aramid strength layer and an outer jacket. The improvement in the cable jacket system results from the addition of a friction layer between the aramid strength layer and the outer jacket. The friction layer prevents unwanted slippage of the outer jacket with respect to the inner portions of the cable.
    Type: Grant
    Filed: September 26, 2011
    Date of Patent: June 11, 2013
    Assignee: OFS Fitel, LLC
    Inventors: Peter A. Weimann, Robert Arthur Williams
  • Publication number: 20130077922
    Abstract: Described are track-resistant all dielectric self-supporting (TR-ADSS) cables with improved cable jackets. A typical TR-ADSS optical fiber cable comprises an optical fiber sub-assembly, and a cable jacket system. The cable jacket system comprises an inner jacket, an aramid strength layer and an outer jacket. The improvement in the cable jacket system results from the addition of a friction layer between the aramid strength layer and the outer jacket. The friction layer prevents unwanted slippage of the outer jacket with respect to the inner portions of the cable.
    Type: Application
    Filed: September 26, 2011
    Publication date: March 28, 2013
    Inventors: Peter A. Weimann, Robert Arthur Williams
  • Patent number: 6917908
    Abstract: The present invention relates to software for training an aircraft pilot to respond to the failure of one or more engines of a multi-engine aircraft during flight. The software simulates engine failure through the use of software imposed power output limits on the one or more engines for which failure is simulated. In certain embodiments, the software of the present invention sets one or more of the engine condition gauges to a fictitious readings corresponding to readings that would be displayed in the event of an actual engine failure.
    Type: Grant
    Filed: March 16, 2001
    Date of Patent: July 12, 2005
    Assignee: Bell Helicopter Textron Inc.
    Inventor: Robert Arthur Williams
  • Publication number: 20020133322
    Abstract: The present invention relates to software for training an aircraft pilot to respond to the failure of one or more engines of a multi-engine aircraft during flight. The software simulates engine failure through the use of software imposed power output limits on the one or more engines for which failure is simulated. In certain embodiments, the software of the present invention sets one or more of the engine condition gauges to a fictitious readings corresponding to readings that would be displayed in the event of an actual engine failure.
    Type: Application
    Filed: March 16, 2001
    Publication date: September 19, 2002
    Inventor: Robert Arthur Williams