System and a method of operation of the system incorporating a graphical user interface in a bulkhead of a vehicle cabin

• US 9,650,141 B2
• Filed: 01/27/2014
• Issued: 05/16/2017
• Est. Priority Date: 01/31/2013
• Status: Active Grant

• Current Assignee: Bombardier Incorporated
• Original Assignee: Bombardier Incorporated
• Inventors: Fagan, Tim Michael, Conner, Brian, Bartenbach, Jeff, Nancarrow, Linsey, Hobbs, Tom, Waldman, Erick, Petry, Sebastian
• Primary Examiner(s): Badii, Behrang
• Assistant Examiner(s): TESTARDI, DAVID A
• Application Number:
  US14/164,932
• Publication Number:
  US 20160059953A1
• Time in Patent Office: 1,205 Days
• Field of Search: 701 3
• CPC Class Codes: B60K 2360/143 Touch sensitive instrument input devices
• CPC Class Codes: B60K 35/10 Input arrangements, i.e. from user to vehicle, associated with vehicle functions or specially adapted therefor
• CPC Class Codes: B64D 11/0015 Arrangements for entertainment or communications, e.g. radio, television
• CPC Class Codes: B64D 2013/0655 with zone or personal climate controls

Abstract

A method of operation for a system incorporating a graphical user interface disposed in a bulkhead within a cabin of an aircraft. The method includes displaying a menu for at least one controllable parameter, receiving a selection of the controllable parameter, displaying at least one control for the selected controllable parameter, receiving a control input for the selected controllable parameter, and adjusting the selected controllable parameter consistent with the control input. The controllable parameter may be one from a plurality of controllable parameters selected from a group that includes cabin light intensity, cabin light color, temperature, and the degree of openness of at least one window shade. A system and an executable computer program product also are provided.

Claims

1. A method of operation for a system incorporating a bulkhead graphical user interface disposed in a bulkhead within a cabin of an aircraft, the bulkhead dividing the cabin lengthwise into cabin zones, wherein the system comprises a processor, a controller operatively connected to the processor, and the bulkhead graphical user interface connected to the controller, the method comprising:

displaying a menu of at least one controllable parameter on the bulkhead graphical user interface, wherein the bulkhead graphical user interface is disposed within the bulkhead adjacent to a first cabin zone;

receiving, by the controller, a selected controllable parameter from the menu of at least one controllable parameter on the bulkhead graphical user interface;

displaying at least one control for the selected controllable parameter on the bulkhead graphical user interface;

receiving, by the controller, a control input for the selected controllable parameter from the bulkhead graphical user interface;

adjusting, by the controller, the selected controllable parameter within the first cabin zone, independently from a second cabin zone, consistent with the control input, wherein the selected controllable parameter comprises at least one of cabin light intensity, cabin light color, temperature, and the degree of openness of at least one window shade;

prioritizing, by the controller, the control input received from the bulkhead graphical user interface in relation to control inputs received from another input device, thereby avoiding conflicts between the control inputs,

wherein the first cabin zone extends between two bulkheads in the cabin of the aircraft.

2. The method of claim 1, further comprising:

placing the bulkhead graphical user interface into a sleep mode if the selected controllable parameter is not received.

3. The method of claim 1, wherein cabin light intensity, temperature, and degree of openness of the at least one window shade are adjustable between a predetermined minimum and a predetermined maximum.

4. The method of claim 3, wherein cabin light intensity, temperature, and degree of openness of the at least one window shade are adjustable in response to a sliding motion across a touch-sensitive surface of the bulkhead graphical user interface.

5. The method of claim 1, wherein the light color is adjustable between a predetermined warm color and a predetermined cool color.

6. The method of claim 1, wherein the displaying of the menu of the at least one controllable parameter includes displaying a cabin light icon, a thermostat icon, and a window shade icon.

7. The method of claim 1, wherein the first cabin zone comprises at least one of a crew seating area, a passenger seating area, a bedroom, and a conference room between the two bulkheads in the cabin of the aircraft.

8. A system incorporating a bulkhead graphical user interface disposed in a bulkhead within a cabin of an aircraft, the bulkhead dividing the cabin lengthwise into cabin zones, comprising:

a processor;

a controller being operatively connected to the processor,

wherein the bulkhead graphical user interface is connected operatively to the processor and the bulkhead graphical user interface is disposed within the bulkhead adjacent to a first cabin zone;

a first display for displaying on the bulkhead graphical user interface a menu for at least one controllable parameter;

an input on the bulkhead graphical user interface for receiving a selected controllable parameter from the menu of the at least one controllable parameter; and

a second display for displaying on the bulkhead graphical user interface at least one control for the selected controllable parameter, wherein the input receives a control input for the selected controllable parameter;

wherein, consistent with the control input, the controller adjusts the selected controllable parameter from at least one of cabin light intensity, cabin light color, temperature, and the degree of openness of at least one window shade within the first cabin zone independently from the second cabin zone, and

wherein the first cabin zone extends between two bulkheads in the cabin of the aircraft, and

wherein the controller prioritizes the control input received from the bulkhead graphical user interface in relation to control inputs received from another input device, thereby avoiding conflicts between the control inputs.

9. The system of claim 8, wherein the bulkhead comprises at least one interior wall within the cabin of the aircraft.

10. The system of claim 8, wherein the bulkhead graphical user interface is touch sensitive.

11. The system of claim 8, wherein the first display comprises a cabin light icon, a thermostat icon, and a window shade icon.

12. The system of claim 8, wherein the second display comprises a slider that responds to a sliding motion across a touch-sensitive surface of the bulkhead graphical user interface.

13. The system of claim 8, wherein the first cabin zone comprises at least one of a crew seating area, a passenger seating area, a bedroom, and a conference room between the two bulkheads in the cabin of the aircraft.

14. A non-transitory, executable, computer program product providing instructions for a method of operation of a system incorporating a bulkhead graphical user interface disposed in a bulkhead within a cabin of an aircraft, the bulkhead dividing the cabin lengthwise into cabin zones, wherein the system comprises a processor, a controller operatively connected to the processor, and the bulkhead graphical user interface connected to the controller, wherein the instructions comprise:

displaying a menu of at least one controllable parameter on the bulkhead graphical user interface, wherein the bulkhead graphical user interface is disposed within the bulkhead adjacent to a first cabin zone;

receiving, by the controller, a selected controllable parameter from the menu of the at least one controllable parameter on the bulkhead graphical user interface;

displaying at least one control for the selected controllable parameter on the bulkhead graphical user interface;

receiving, by the controller, a control input for the selected controllable parameter from the bulkhead graphical user interface;

adjusting, by the controller, the selected controllable parameter within the first cabin zone, independently from a second cabin zone, consistent with the control input, wherein the selected controllable parameter comprises at least one of cabin light intensity, cabin light color, temperature, and the degree of openness of at least one window shade; and

prioritizing, by the controller, the control input received from the bulkhead graphical user interface in relation to control inputs received from another input device, thereby avoiding conflicts between the control inputs,

wherein the first cabin zone extends between two bulkheads in the cabin of the aircraft.

15. The non-transitory, executable, computer program product of claim 14, wherein the bulkhead comprises at least one interior wall within the cabin of the aircraft.

16. The non-transitory, executable, computer program product of claim 14, wherein the instructions further comprise:

placing the bulkhead graphical user interface into a sleep mode if the selected controllable parameter is not received.

17. The non-transitory, executable, computer program product of claim 14, wherein the first cabin zone comprises at least one of a crew seating area, a passenger seating area, a bedroom, and a conference room between the two bulkheads in the cabin of the aircraft.

18. An aircraft, comprising:

a cabin;

a first cabin zone located between a first bulkhead and a second bulkhead;

a second cabin zone located between the second bulkhead and a third bulkhead, wherein the first, second, and third bulkheads divide the cabin lengthwise into the first and second cabin zones;

a processor;

a controller operatively connected to the processor;

a first bulkhead graphical user interface operatively connected to the controller, the first bulkhead graphical user interface being disposed in the first bulkhead adjacent to the first cabin zone, wherein the first bulkhead graphical user interface is operative for receiving a control input associated with at least one controllable parameter selected from a group consisting of cabin light intensity, cabin light color, temperature, and the degree of openness of at least one window shade, and wherein, consistent with the control input, the controller adjusts the at least one controllable parameter selected within the first cabin zone, independently from the second cabin zone, and

a second bulkhead graphical user interface operatively connected to the controller, the second bulkhead graphical user interface being disposed in the second bulkhead adjacent to the second cabin zone, wherein the second bulkhead graphical user interface is operative for receiving the control input associated with the at least one controllable parameter, and wherein, consistent with the control input, the controller adjusts the at least one controllable parameter selected within the second cabin zone, independently from the first cabin zone.

19. The aircraft of claim 18, wherein the bulkhead graphical user interface is touch sensitive.

20. The aircraft of claim 18, wherein the controller prioritizes the control input received from the first and second bulkhead graphical user interfaces in relation to control inputs received from another input device, thereby avoiding conflicts between the control inputs.

21. The aircraft of claim 18, wherein each bulkhead graphical interface comprises a first display comprising a cabin light icon, a thermostat icon, and a window shade icon.

22. The aircraft of claim 21, wherein each bulkhead graphical user interface comprises a second display comprising a slider that responds to a sliding motion across a touch-sensitive surface of the bulkhead graphical user interface.

23. The aircraft of claim 18, wherein the first cabin zone and the second cabin zone comprises at least one of a crew seating area, a passenger seating area, a bedroom, and a conference room between the two bulkheads in the cabin of the aircraft.

24. The aircraft of claim 18, wherein the first bulkhead and the second bulkhead each comprise at least one interior wall within the cabin of the aircraft.

25. The aircraft of claim 18, wherein the first and second bulkhead graphical user interfaces are placed into a sleep mode if the control input is not received.

26. The aircraft of claim 18, wherein cabin light intensity, temperature, and degree of openness of the at least one window shade are adjustable between a predetermined minimum and a predetermined maximum.