The Boeing Company

Sherwin S Chen

John Wiedemann

Peter D Gunn

Jason L Hammack

Michael Jefferie Tucker

Brian David Gilbert

Alireza Majd

Julianne M Fox

Neal D Molloy

Jean Marie Crane

David Paul Eggold

Sean J Flannigan

William Milo Bresley

Wayne R Jones

Steven L Fleiger-Holmes

Bechara J Mallouk

Bruce P Samuels

Jeffery S Harrigan

Kyle Gardner

Michael J Tucker

A method and apparatus for displaying information for an aircraft on display devices in a flight deck of the aircraft. A computer system in the aircraft identifies information used to operate the aircraft. The computer system selects a display configuration from a plurality of display configurations for the display devices. The computer system displays the information in windows on display devices in the flight deck of the aircraft in the display configuration. The display configuration simplifies access to the information used to operate the aircraft.

Flight deck display management

A method, apparatus, and system for displaying information for an aircraft on display devices in a flight deck of the aircraft. A computer system in the aircraft identifies information used to operate the aircraft. The computer system selects a display configuration from a plurality of display configurations for the display devices based on a first set of tasks assigned to a pilot for a current flight and a second set of tasks assigned to a copilot for the current flight of the aircraft. The computer system displays the information in windows on display devices in the flight deck of the aircraft in the display configuration. The display configuration simplifies access to the information used by the pilot to perform the first set of tasks and the copilot to perform the second set of tasks.

Flight deck display management system

A vertical situation display system for use in a vehicle such as, for example, an aircraft, is provided. A side view of an intended route of flight may be shown with altitude restrictions, airspace and instrument approach information, a projected flight path and range to airspeed symbol. The system may show terrain, weather, and traffic information along the intended route of flight. The system may be used in conjunction with a navigational display to enhance situational awareness. The system includes a computer, an electronic display device, an electronic entry device, a memory and a database. The database may contain terrain, airspace and flight planning data and may be updatable.

Enhanced vertical situation display

A flight information system may include a plan vertical situation display. The plan vertical situation display may display a vertical view of a flight path of an aircraft. The plan vertical situation display may display at least one path symbol showing at least one of a current path of the aircraft, a modified but not executed route of the aircraft, and an inactive route of the aircraft. The at least one path symbol may be adapted to display each of the current path of the aircraft, the modified but not executed route of the aircraft, and the inactive route of the aircraft. The plan vertical situation display may further display at least one terrain symbol showing a vertical terrain in the flight path along the at least one path symbol.

Method and system for plan map vertical situation display

A method, apparatus, and computer program product for displaying information about runways. A runway for an aircraft is identified when the aircraft is within a selected distance of the runway. A number of graphical indicators are displayed on a display in a flight deck. The number of graphical indicators corresponds to a number of features of the runway present in a field of view for an eye reference point in the flight deck.

Perspective runway system

Methods and systems for handling aircraft control information are disclosed. A system in accordance with one embodiment of the invention includes a display medium coupleable to a flight manager, with the flight manager configured to receive and direct instructions for automatically controlling aircraft functions at a future time during flight of the aircraft. The system can further include a display controller coupled to the display medium to present at least one operator activatable element at the display medium and update information presented at the display medium when the operator activates the operator activatable element. For example, the operator activatable element can include an icon presented at a computer display screen, and can be activated by a keystroke.

Systems and methods for handling the display and receipt of aircraft control information

A navigation system takes a graphical input and translates it into an alpha-numeric entry generally including latitude and longitude information. The system interprets the graphical entry, determines if a waypoint already exists or is depicted at the geographical location identified by the graphical entry and creates a new waypoint if no waypoint already exists or is depicted at the geographical location.

Navigational system with a graphical scratchpad filler

A flight information display for the flight deck of an aircraft showing a pictorial side view of the flight path or the area directly in front of the aircraft area having a selected distance of at least 0.5 nautical miles, comprising (a) a pictorial representation to scale of the profile of the highest elevations of a swath of terrain along said path or area, (b) an icon positioned on the left or right side of the display representing the aircraft, the altitude of which is to scale with the height of the terrain, and (c) an altitude reference scale; wherein the width of the swath is at least 0.1 nautical miles and no greater than the distance of the minimum accuracy of the means for determining the aircraft's location.

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Bellevue, WA, United States of America

Sherwin S Chen