The Boeing Company

Jeffrey Lee Williams

Samantha Ann Schwartz

Aaron Daniel Pilcher

Jason William Clark

Susan Anne Foster

Theodore Bruce Thompson

Steven Curtis Spackman

Stephen Solomon Altus

Brian A Azcuenaga

Katie M Reid

Alexander V Korolev

Melissa Irene Blackstun

Theresa Ernsbach

Jeffrey J Buhl

Catherine Marie Barnes

Theresa Emsbach

An aircraft management system and method includes a flight plan diversion prediction system including a rerouting control unit that is configured to generate one or more reroute options for an aircraft based on an analysis of a current position of the aircraft, a predicted future position of the aircraft, a current position of an in-flight hazard, and a predicted future position of the in-flight hazard.

Aircraft flight management systems and methods

A runway exiting system is configured to determine a suitable exit off of a runway for an aircraft. The runway exiting system includes a housing, and one or more processors within the housing that are configured to determine a current position of the aircraft on the runway, determine a current rate of deceleration of the aircraft on the runway, and determine the suitable exit off of the runway for the aircraft based, at least in part, on the current position of the aircraft on the runway and the current rate of deceleration of the aircraft on the runway.

Runway exiting systems and methods for aircraft

A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures, retrieves flight condition information relating to phase of flight, and displays small amounts of contextually relevant flight condition information on a display screen.

Wearable electronic display and method for displaying information to a pilot

Electronic map display information is generated. A map display comprising mapping data for a geographic region is generated. The mapping data is rendered on a map display. A plurality of concentric rings are overlaid on the map display. Each of the rings are indicative of a scaling factor for the mapping data. The scaling factor is adjusted based in a context of the map display.

Enroute distance measuring tool

A method and apparatus for displaying navigation objects for managing operations of a vehicle. A number of navigation objects for managing the operations of the vehicle is displayed in a graphical user interface to form a display of the number of navigation objects. Responsive to a user input to the number of navigation objects, the display of the number of navigation objects in the graphical user interface is changed to include one or more navigation objects identified based on the user input. The navigation objects in the number of navigation objects have a number of associations with each other. The display of the number of navigation objects includes a number of graphical indicators providing a visualization of the number of associations for the number of navigation objects.

Management system for aeronautical information

A computing device for displaying procedures for an aircraft is provided. The computing device includes a presentation interface, a user input interface, and a processing device coupled to the presentation interface and to the user input interface. The processing device is configured to cause the presentation interface to display an initial procedure display, and in response to a triggering event, cause the presentation interface to display an adjusted procedure display that emphasizes a predetermined portion of a procedure.

Systems and methods for displaying in-flight navigation procedures

Concepts described herein may provide available RCO information that may be used when moving from one RCO to another RCO. Range rings for the available RCOs may be calculated and adjusted based on current flight conditions. The range rings may be prioritized to provide a prioritized list of available RCOs.

Calculated graphical frequency coverages based on aircraft position

An environment associated with at least one crew member is identified, and a line-of-sight associated with the at least one crew member is determined. An alarm is generated when the line-of-sight remains within a predetermined area for an elapsed time that exceeds a first predetermined temporal threshold associated with the identified environment.

Heads down warning system

A method and apparatus for displaying an aircraft fix. A fix for an aircraft is identified, wherein the fix is a location of the aircraft. A fix identifier is displayed in a plan view display, wherein the fix identifier indicates a location of the fix on a map background in the plan view display. A fix formation identifier is displayed in the plan view display, wherein the fix formation identifier indicates a direction from a navigational aid to the fix.

Airspace fix formation display

A method and apparatus for managing a touch screen system. Data generated by an acceleration detector about acceleration of the touch screen system is received. The acceleration detector is located within the touch screen system. An action is initiated by an input manager when the acceleration of the touch screen system reduces usability of the touch screen system.

Growing community of inventors

Parker, CO, United States of America

Jeffrey Lee Williams