Flight deck touch screen interface for interactive displays

Patent metadata

Field	Value
Publication number	US-9352848-B2
Application number	US-201314073288-A
Country	US
Kind code	B2
Filing date	Nov 6, 2013
Priority date	Nov 6, 2013
Publication date	May 31, 2016
Grant date	May 31, 2016

Abstract

A system and method for controlling a display on an aircraft. An operator interaction with an edge area of a touch screen is identified by a processor unit when a first format of the display is displayed on the touch screen. The edge area extends along an edge of the touch screen. A second format of the display is displayed on the touch screen by the processor unit in response to identifying the operator interaction with the edge area of the touch screen. The second format of the display is different from the first format of the display.

First claim

What is claimed is:

1. A method of controlling a display on an aircraft, comprising:
identifying, by a processor unit, while displaying on a touch screen a first format other than a format select page, an interaction with an edge area of the touch screen, such that the edge area extends along an edge of the touch screen; and
displaying, in response to identifying the interaction, by the processor unit, a second format of the display on the touch screen, the second format of the display differing from the first format of the display and comprising the format select page, in response to the interaction the edge area extending along one of: a left edge, and a right edge, of the touch screen, such that the format select page comprises a plurality of buttons corresponding to a plurality of formats for the display.

2. The method of claim 1 , further comprising the interaction with the edge area of the touch screen comprising one of: a touch in the edge area of the touch screen, and a slide action in the edge area of the touch screen.

3. The method of claim 1 , further comprising the edge of the touch screen comprising a bottom edge of the touch screen.

4. The method of claim 1 , wherein the edge area extends approximately one inch from the edge of the touch screen in a direction perpendicular to the edge of the touch screen.

5. The method of claim 1 , wherein displaying the second format of the display on the touch screen comprises displaying the first format of the display on a first portion of the touch screen and simultaneously displaying the second format of the display on a second portion of the touch screen.

6. The method of claim 1 further comprising:
displaying the first format of the display on another display device on the aircraft in response to identifying the interaction with the edge area of the touch screen, wherein the first format of the display comprises an engine-indicating and crew-alerting system display.

7. The method of claim 1 further comprising:
displaying the first format of the display on another display device on the aircraft in response to identifying the interaction with the edge area of the touch screen, wherein the interaction with the edge area of the touch screen comprises a slide action in the edge area of the touch screen along a bottom edge of the touch screen.

8. The method of claim 1 , wherein:
the first format of the display comprises a partial format in which two formats are displayed simultaneously on the touch screen and the second format of the display comprises a full format in which only one of the two formats is displayed on the touch screen; and
displaying the second format of the display comprises changing between displaying the partial format on the touch screen and displaying the full format on the touch screen in response to identifying a slide action in the edge area along a bottom edge of the touch screen.

9. An apparatus, comprising:
a touch screen on a flight deck on an aircraft; and
a controller configured such that in operation, based upon a first format displayed on the touch screen, the controller:
identifies an interaction with an edge area of the touch screen, such that the edge area extends along one of a left edge and a right edge of the touch screen, and the first format comprises a format other than a format select page and the edge area extends along an edge of the touch screen; and
displays, in response to identifying the interaction with the edge area of the touch screen, a second format of the display on the touch screen such that the second format of the display differs from the first format of the display and comprises the format select page for the display, such that the format select page comprises a plurality of buttons corresponding to a plurality of formats for the display.

10. The apparatus of claim 9 , further comprising the interaction with the edge area of the touch screen comprising one of: a touch in the edge area of the touch screen, and a slide action in the edge area of the touch screen.

11. The apparatus of claim 9 , wherein the edge of the touch screen further comprises a bottom edge of the touch screen.

12. The apparatus of claim 9 , wherein the edge area extends approximately one inch from the edge of the touch screen in a direction perpendicular to the edge of the touch screen.

13. The apparatus of claim 9 , wherein the controller is configured to display simultaneously the first format of the display on a first portion of the touch screen and the second format of the display on a second portion of the touch screen in response to identifying the interaction with the edge area of the touch screen.

14. The apparatus of claim 9 , wherein:
the first format of the display comprises an engine-indicating and crew-alerting system display; and
the controller is configured to display the first format of the display on another display device on the aircraft in response to identifying the interaction with the edge area of the touch screen.

15. The apparatus of claim 9 , wherein the controller is configured to display the first format of the display on another display device on the aircraft in response to identifying a slide action in the edge area along a bottom edge of the touch screen.

16. The apparatus of claim 9 , wherein:
the first format of the display comprises a partial format in which two formats are displayed simultaneously on the touch screen and the second format of the display comprises a full format in which only one of the two formats is displayed on the touch screen; and
the controller is configured to change between displaying the partial format on the touch screen and displaying the full format on the touch screen in response to a slide action in the edge area along a bottom edge of the touch screen.

17. A method of controlling a display on an aircraft, comprising:
displaying, by a processor unit, a navigation display on a touch screen on the aircraft;
identifying, by the processor unit, an interaction with the navigation display displayed on the touch screen, the interaction comprising a slide action in a center area along a bottom edge of the navigation display, such that the center area is positioned at a horizontal center of the navigation display; and
changing, by the processor unit in response to the identifying the slide action, the navigation display via one of: displaying a vertical situation display, and ceasing displaying the vertical situation display.

18. The method of claim 17 , wherein changing the navigation display comprises changing a range of the navigation display by an amount corresponding to a length of the slide action.

19. The method of claim 17 , wherein:
the navigation display comprises a map display comprising a track line indicating a direction of travel of the aircraft;
identifying the interaction with the navigation display further comprises identifying a slide action along the track line in the map display; and
changing the navigation display further comprises changing a range of the navigation display in response to the slide action along the track line.

20. The method of claim 17 , wherein:
the navigation display further comprises the vertical situation display comprising: distance markers indicating a distance from the aircraft, and a representation of an altitude of the aircraft with respect to the distance markers;
identifying the interaction with the navigation display further comprises identifying a slide action along the distance markers in the vertical situation

Assignees

• Boeing Co

Inventors

• Nikolic Mark Ivan
• Gilbert Brian David
• Bowen Jayson Jean

Classifications

• G08G5/55

  for a single aircraft · CPC title

• G08G5/50

  Navigation or guidance aids · CPC title

• G01C23/00

  Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration · CPC title

• B64D43/00 Primary

  Arrangements or adaptations of instruments · CPC title

• G08G5/0047

  Physics · mapped topic