User-defined pages for aircraft

• US 8,981,968 B2
• Filed: 11/22/2011
• Issued: 03/17/2015
• Est. Priority Date: 07/22/2011
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Huang, Cindy Chi-Lan, Cajavilca, Eduardo Raul
• Primary Examiner(s): Swarthout, Brent
• Application Number:
  US13/302,177
• Publication Number:
  US 20130021173A1
• Time in Patent Office: 1,211 Days
• Field of Search: 340/945, 340/971, 340/461, 340/439, 340973-975, 701/14
• US Class Current: 340/971
• CPC Class Codes: G01D 7/08 using a common indicating element for two or more variables
• CPC Class Codes: G06F 3/14 Digital output to display device ; Cooperation and interconnection of the display device with other functional units
• CPC Class Codes: G06F 3/1423 controlling a plurality of local displays, e.g. CRT and flat panel display
• CPC Class Codes: G09G 2340/0464 Positioning
• CPC Class Codes: G09G 2340/14 Solving problems related to the presentation of information to be displayed
• CPC Class Codes: G09G 2370/20 Details of the management of multiple sources of image data
• CPC Class Codes: G09G 2380/12 Avionics applications
• CPC Class Codes: G09G 5/14 Display of multiple viewports

Abstract

A method and apparatus for displaying aircraft information. A selection of a piece of dynamic information is detected about an aircraft on a first display on a user interface. The piece of dynamic information is used to operate the aircraft and changes during operation of the aircraft. The piece of dynamic information selected from the first display is added to a custom display on the user interface. The custom display is displayed on the user interface on a display system for the aircraft.

Claims

1. A method for displaying aircraft information, the method comprising:

detecting, by a processor unit, a plurality of selections of pieces of dynamic information about an aircraft on a plurality of displays on a user interface, wherein the pieces of dynamic information are used to operate the aircraft and change during operation of the aircraft;

adding, by the processor unit, the pieces of dynamic information selected from the plurality of displays to a custom display on the user interface;

displaying the custom display on the user interface on a display system for the aircraft;

determining, by the processor unit, whether a number of selected events have occurred during the operation of the aircraft, wherein the number of selected events include at least one of a selected speed for the aircraft, a beginning of a selected phase of flight for the aircraft, an alert being generated, a notification being received from a ground station, and landing gear being deployed; and

storing, by the processor unit, screenshots of the custom display during the operation of the aircraft in response to a determination that any of the number of selected events has occurred.

2. The method of claim 1 further comprising:

identifying a set of functions for the pieces of dynamic information selected; and

adding the set of functions to the custom display.

3. The method of claim 1 further comprising:

displaying values for the pieces of dynamic information on the custom display, wherein the values were stored during the operation of the aircraft.

4. The method of claim 1, wherein a number of pieces of dynamic information about the aircraft from a number of different displays is present in the custom display in addition to the pieces of dynamic information from the plurality of displays.

5. The method of claim 1, wherein the display system is located on at least one of the aircraft and a location remote to the aircraft.

6. The method of claim 1 further comprising:

storing values for the pieces of dynamic information during the operation of the aircraft.

7. The method of claim 1, wherein displaying the custom display on the user interface on the display system for the aircraft comprises:

displaying the custom display on the user interface on the display system for the aircraft during the operation of the aircraft, wherein the plurality of selections are made by an operator via a number of user input devices during the operation of the aircraft.

8. The method of claim 1 further comprising:

storing the custom display for use at a subsequent time.

9. The method of claim 1, wherein the pieces of dynamic information about the aircraft are selected from one of an engine temperature, a fuel use, an altitude, a position of a control surface, cabin temperature, hydraulic pressure, and a fuel level.

10. The method of claim 1, wherein the plurality of displays are for systems in the aircraft selected from a hydraulic system, a fuel system, an electrical system, a landing gear system, a control surface system, a sensor system, and an environmental system.

11. An apparatus comprising:

a display system for an aircraft; and

a computer system configured to detect a plurality of selections of pieces of dynamic information about the aircraft on a plurality of displays on a user interface, wherein the pieces of dynamic information are used to operate the aircraft and change during operation of the aircraft;

add the pieces of dynamic information selected from the plurality of displays to a custom display on the user interface;

display the custom display on the user interface on the display system for the aircraft;

determine whether a number of selected events have occurred during the operation of the aircraft, wherein the number of selected events include at least one of a selected speed for the aircraft, a beginning of a selected phase of flight for the aircraft, an alert being generated, a notification being received from a ground station, and landing gear being deployed; and

store screenshots of the custom display during the operation of the aircraft in response to a determination that any of the number of selected events has occurred.

12. The apparatus of claim 11, wherein the computer system is further configured to identify a set of functions for the pieces of dynamic information;

and add the set of functions to the custom display.

13. The apparatus of claim 11, wherein the computer system is further configured to display values for the pieces of dynamic information on the custom display, wherein the values were stored during the operation of the aircraft.

14. The apparatus of claim 11, wherein a number of pieces of dynamic information about the aircraft from a number of different displays is present in the custom display in addition to the pieces of dynamic information from the plurality of displays.

15. The apparatus of claim 11, wherein the display system is located on at least one of the aircraft and a location remote to the aircraft.

16. The apparatus of claim 11, wherein the computer system is further configured to store values for the pieces of dynamic information during the operation of the aircraft.

17. The apparatus of claim 11, wherein in being configured to display the custom display on the user interface on the display system for the aircraft, the computer system is configured to display the custom display on the user interface on the display system for the aircraft during the operation of the aircraft, wherein the plurality of selections are made by an operator via a number of user input devices during the operation of the aircraft.

18. A custom display system for an aircraft, the custom display system comprising:

a display system for the aircraft; and

a computer system configured to detect a plurality of selections of pieces of dynamic information about the aircraft on a plurality of displays on a user interface, wherein the pieces of dynamic information are used to operate the aircraft and change during operation of the aircraft;

add the pieces of dynamic information selected from the plurality of displays to a custom display on the user interface, wherein a number of pieces of dynamic information about the aircraft from a number of different displays is present in the custom display in addition to the pieces of dynamic information from the plurality of displays;

identify a set of functions for the pieces of dynamic information;

add the set of functions to the custom display;

display the custom display on the user interface on the display system for the aircraft;

determine whether a number of selected events have occurred during the operation of the aircraft, wherein the number of selected events include at least one of a selected speed for the aircraft, a beginning of a selected phase of flight for the aircraft, an alert being generated, a notification being received from a ground station, and landing gear being deployed; and

store screenshots of the custom display during the operation of the aircraft in response to a determination that any of the number of selected events has occurred.