Universal Avionics Systems Corporation

Honeywell International Inc.

Patrick Glaze

Patrick Gerald Krohn

Hubert Naimer

John Russell Jorgensen

Peng Liu

Wei Cui

Lin Wang

Jing Song

In one example, this disclosure is directed to a system configured to detect inclement weather in the travel path of a vehicle, determine a recommended maneuver to avoid the inclement weather, and determine the feasibility of the recommended maneuver with respect to any nearby vehicles.

Connected weather radar

A display generation system that is able to generate display signals for an underlay image with at least one embedded safety pattern and display images for an overlay image. The display generation system and method are able to determine whether there are any anomalies or graphical errors when an overlay display generated by the system or generated by some other system is displayed simultaneously with the underlay image with the embedded safety pattern. The display generation system uses the embedded safety pattern to detect the occurrence of anomalies in the simultaneous display and uses information from its own generated overlay image to detect graphical errors in the simultaneous display. Flight display systems for aircraft can use the display generation system and method of the present invention to display an underlay image depicting geographical scenery in the vicinity of the aircraft while on the ground, during takeoff or in flight. The underlay image is displayed simultaneously with an overlay image depicting standard graphics of a flight display system.

Display generation system

Flight plan information is provided in the form of a series of waypoints having attributes which preferably include, among others, latitude, longitude, altitude constraint, and waypoint identifier. A flight path, defined by this information is modeled, and the flight plan model is checked against terrain information to locate any instances in which a potentially unsafe flight altitude exists. In flight, the flight path model is updated using aircraft position so that the path from the aircraft position to the next waypoint is reflected in the model. In the event that a potentially unsafe flight altitude is detected, an alert may be issued to the flight crew. The crew may then amend the flight plan or take other appropriate action.

Flight plan intent alert system and method

Growing community of inventors

Duvall, WA, United States of America

Patrick Glaze