Honeywell International Inc.

Trent C Reusser

Thea Lynn Feyereisen

Stephen D Whitlow

Robert E De Mers

Jeffrey Mathew Rye

Jan Flasar

Methods and apparatus are provided for context sensitive notifications of incoming digital communications on an aircraft. The method comprises receiving a new datalink message from a sender on a device, the datalink message including a unique identifier associated with the sender, and determining if the sender is a new sender based on the unique identifier. The method comprises determining if the device is involved in an active exchange of datalink messages based on activity data associated with the device and outputting a first alert that the new datalink message has been received at an alert level below a current alert level if the sender is not a new sender and the device is engaged in the active exchange of datalink messages.

Systems and methods for context sensitive notification

Avionics display system is provided for deployment onboard an aircraft and includes an air traffic data source that provides the avionics display system with data indicative of at least position and velocity of a neighboring aircraft. The system comprises a cockpit display system, and a monitor included within the cockpit display system. The cockpit display system receives and displays position and velocity data pertaining to the neighboring aircraft on the cockpit monitor as a position symbol and a velocity vector graphic. A processor operatively coupled to the monitor is configured to generate an air traffic display on the monitor including symbology indicative of (1) the current position of the neighboring aircraft (2) a velocity of the neighboring aircraft, and (3) the rate-of-change of the velocity of the neighboring aircraft.

System and method for displaying a velocity rate-of-change indicator

An aircraft display system () includes a first device () providing () flight data of a selected flight path of an aircraft (), a device () providing () a plurality of data points representative of the terrain () below the selected flight path, a processor () generating () display commands from the flight data and the plurality of data points, and a display () coupled to receive the display commands and operable to render () in a perspective view an icon representative of the aircraft () and the terrain () near the aircraft ().

Apparatus and method of displaying an aircraft's position

A method of removing synthetic vision terrain and objects from a graphical display when unsafe to rely on the synthetic vision terrain and objects is provided. The method comprises receiving current position data from at least one sensor, determining when to fade out synthetic vision terrain and objects based on the position data received, and fading out synthetic vision terrain and objects gradually when determined.

Synthetic vision final approach terrain fading

A method for displaying attitude, heading, and navigation data on a single display is described. The method comprises configuring the display with terrain data, overlaying the terrain display with a compass rose display, and superimposing an attitude direction indicator with the compass rose display, the attitude direction indicator referenced to a center of the compass rose.

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Robbinsdale, MN, United States of America

Trent C Reusser