Patents by Inventor David J. Weiler

David J. Weiler 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: 9858824
    Abstract: A system for determining a flight plan based on internet connectivity includes at least one processor coupled with a non-transitory processor-readable medium storing processor-executable code for causing the at least one processor to receive internet connectivity data for a plurality of airspace regions, where the internet connectivity data is indicative of an internet connectivity characteristic; and determine a flight plan for an aircraft through at least one region of the plurality of airspace regions based on the internet connectivity characteristic.
    Type: Grant
    Filed: July 14, 2015
    Date of Patent: January 2, 2018
    Assignee: Rockwell Collins, Inc.
    Inventors: Scott J. Zogg, Steven D. Acheson, Kevin M. Kronfeld, Jaclyn A. Hoke, Kevin J. Delaney, David J. Weiler
  • Patent number: 7689324
    Abstract: A vehicle operator interface is disclosed. The vehicle operator interface comprises a visual display device. A first indicator which is representative of a vehicle energy target, a second indicator representative of a vehicle energy vector and a third indicator representative of a vehicle capability zone are on the display.
    Type: Grant
    Filed: June 21, 2004
    Date of Patent: March 30, 2010
    Assignee: Rockwell Collins, Inc.
    Inventors: Michael J. Krenz, David J. Weiler
  • Patent number: 6285926
    Abstract: A selected hover altitude deviation display and method for displaying the difference between the current altitude of an aircraft and a selected hover altitude on a multi-functional display unit that includes a compass rose and an aircraft symbol. An altitude sensor generates current altitude data, which is transmitted to a computer processing unit together with a selected hover altitude. The selected hover altitude is determined by the pilot of the aircraft. The selected hover altitude is displayed as a static, analog symbolic representation on the multi-functional display unit. The hover altitude deviation is displayed as a dynamic, analog symbolic representation of the difference between the current altitude of the aircraft and the selected hover altitude. With the selected hover altitude deviation display, the pilot can readily see if his aircraft is above or below a selected hover altitude without relying on external visual reference cues.
    Type: Grant
    Filed: April 28, 2000
    Date of Patent: September 4, 2001
    Assignee: Rockwell Collins
    Inventors: David J. Weiler, Michael J. Marks