Patents by Inventor Chad L. Cundiff

Chad L. Cundiff 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: 6907324
    Abstract: The invention provides a primary flight display instrument in which a symbol—such as a small star or triangle—indicates the bearing to the current waypoint in the flight navigation plan. The display may also show a bearing indication symbol showing a follow-on waypoint in the flight plan. These symbols are preferably located on the horizon line of the primary flight display (or the attitude indicator) providing bearing to the current waypoint in the flight plan and/or to the following waypoint. An image processing unit generates the display, including earth ground and horizon, in a view substantially conformal with a VMC view from the aircraft.
    Type: Grant
    Filed: October 11, 2001
    Date of Patent: June 14, 2005
    Assignee: Honeywell International Inc.
    Inventor: Chad L. Cundiff
  • Publication number: 20030132860
    Abstract: An apparatus, method and computer program product for an integrated display presentation for tactical flight path management that simplifies instrument flight by replicating many of the cues basic to visual flight using spatial flow, integrating navigation information conformal symbology, and improving instrumentation using an enhanced “T” instrument display.
    Type: Application
    Filed: September 20, 2002
    Publication date: July 17, 2003
    Applicant: Honeywell International, Inc.
    Inventors: Thea L. Feyereisen, Chad L. Cundiff, Ou Zhao
  • Publication number: 20020123830
    Abstract: The invention provides a primary flight display instrument in which a symbol—such as a small star or triangle—indicates the bearing to the current waypoint in the flight navigation plan. The display may also show a bearing indication symbol showing a follow-on waypoint in the flight plan. These symbols are preferably located on the horizon line of the primary flight display (or the attitude indicator) providing bearing to the current waypoint in the flight plan and/or to the following waypoint. An image processing unit generates the display, including earth ground and horizon, in a view substantially conformal with a VMC view from the aircraft.
    Type: Application
    Filed: October 11, 2001
    Publication date: September 5, 2002
    Applicant: Honeywell International, Inc.
    Inventor: Chad L. Cundiff