Carpet display systems and methods

Patent metadata

Field	Value
Publication number	US-10822087-B2
Application number	US-201715468166-A
Country	US
Kind code	B2
Filing date	Mar 24, 2017
Priority date	Mar 24, 2017
Publication date	Nov 3, 2020
Grant date	Nov 3, 2020

Abstract

A carpet display system includes a plurality of carpet modules. Each of the plurality of carpet modules includes a translucent support panel, a carpet layer secured to the support panel, and a light-emitting element coupled to the support panel. The light-emitting element is configured to emit light through the support panel to provide lighting effects through the carpet layer.

First claim

What is claimed is:

1. An aircraft comprising:
an interior cabin; and
a carpet display system within the interior cabin, the carpet display comprising a plurality of carpet modules, wherein each of the plurality of carpet modules includes:
a translucent support panel;
a carpet layer secured to the support panel; and
one or more display screens coupled to the support panel, wherein the one or more display screens are configured to emit light through the support panel to provide lighting effects through the carpet layer.

2. The aircraft of claim 1 , wherein each of the plurality of carpet modules further comprises an associated controller that is configured to control operation of the one or more display screens.

3. The aircraft of claim 1 , wherein the plurality of carpet modules comprises:
a master system carpet module having an associated master system controller within a first zone of an interior cabin of a vehicle;
at least one column-controlling carpet module having an associated column controller within the first zone, wherein the column controller is communicatively coupled to the master system controller; and
at least one slave carpet module having an associated slave controller within the first zone, wherein the slave controller is communicatively coupled to the column controller,
wherein the master system controller distributes operational control of the carpet display system among the master system controller, the column controller, and the slave controller.

4. The aircraft of claim 3 , wherein the plurality of carpet modules further comprises at least one other slave carpet module having an associated other slave controller within the first zone, wherein the associated other slave controller is communicatively coupled to the master system controller, wherein the master system controller further distributes operational control of the carpet display system to the associated other slave controller.

5. The aircraft of claim 3 , wherein the plurality of carpet modules further comprises a zone-controlling carpet module having an associated zone controller within a second zone of the interior cabin that differs from the first zone, wherein the zone controller is communicatively coupled to the master system controller, wherein the master system controller further distributes operational control of the carpet display system to the zone controller.

6. The aircraft of claim 5 , wherein the zone controller is communicatively coupled to another column controller associated with at least one other column-controlling carpet module within the second zone.

7. The aircraft of claim 6 , wherein the another column controller is communicatively coupled to another slave controller associated with at least one other slave carpet module within the second zone.

8. The aircraft of claim 1 , wherein the plurality of carpet modules are secured to one or more of a floor, wall, ceiling, or monument within the interior cabin.

9. The aircraft of claim 1 , wherein the one or more display screens comprises one or more light emitting diodes (LEDs), or one or more organic light emitting diodes (OLEDs).

10. The aircraft of claim 1 , wherein the support panel comprises at least one channel formed through a surface.

11. The aircraft of claim 10 , wherein at least a portion of the one or more display screens is secured to the support panel within the at least one channel.

12. The aircraft of claim 10 , wherein at least a portion of the one or more display screens is configured to emit light through the at least one channel.

13. The aircraft of claim 10 , wherein the one or more display screens is embedded within the support panel.

14. The aircraft of claim 1 , wherein the carpet display system further comprises at least one electrical distribution system within the interior cabin, wherein the one or more display screens receives one or both of power and data signals through the at least one electrical distribution system.

15. A method of providing lighting effects through a carpet display system within an interior cabin of an aircraft, the method comprising:
providing a plurality of carpet modules within the interior cabin of the aircraft; and
emitting light energy from display screens of the plurality of carpet modules through support panels to provide lighting effects through carpet layers.

16. The method of claim 15 , further comprising associating a controller that is configured to control operation of the one or more display with each of the plurality of carpet modules.

17. The method of claim 15 , wherein the providing comprises:
providing a master system carpet module having an associated master system controller within a first zone of the interior cabin;
providing at least one column-controlling carpet module having an associated column controller within the first zone;
communicatively coupling the column controller to the master system controller;
providing at least one slave carpet module having an associated slave controller within the first zone;
communicatively coupling the slave controller to the column controller;
providing at least one other slave carpet module having an associated other slave controller within the first zone;
communicatively coupling the associated other slave controller to the master system controller, wherein the master system controller further distributes operational control of the carpet display system to the associated other slave controller;
providing a zone-controlling carpet module having an associated zone controller within a second zone of the interior cabin that differs from the first zone;
communicatively coupling the zone controller to the master system controller; and
distributing operational control of the carpet display system among the master system controller, the column controller, the slave controller, the other slave controller, and the zone controller.

18. The method of claim 17 , further comprising:
communicatively coupling the zone controller to another column controller associated with at least one other column-controlling carpet module within the second zone;
communicatively coupling the another column controller to another slave controller associated with at least one other slave carpet module within the second zone.

19. An aircraft comprising:
an interior cabin; and
a carpet display system within the interior cabin, wherein the carpet display system comprises a plurality of carpet modules within the interior cabin, wherein the plurality of carpet modules are secured to one or more of a floor, wall, ceiling, or monument within the interior cabin, wherein each of the plurality of carpet modules includes:
a translucent support panel;
a carpet layer secured to the support panel; and
one more display screens coupled to the support panel, wherein the one or more display screens are configured to emit light through the support panel to provide lighting effects through the carpet layer,

wherein the plurality of carpet modules comprises:
a master system carpet module having an associated master system controller within a first zone of the interior cabin;
at least one column-controlling carpet module having an associated column controller within the first zone, wherein the column controller is communicatively coupled to the master system controller;
at least one slave carpet module having an associated slave controller within the first zone, wherein the slave controller is communicatively coupled to the column controller;
at least one other slave carpet module having an as

Assignees

• Boeing Co

Inventors

• Ibrahim Yakentim
• Hills Karen L
• Babunovic Richard

Classifications

• G09F13/0418

  Constructional details · CPC title

• G09F13/044

  Signs, boards or panels mounted on vehicles · CPC title

• B64D25/00

  Emergency apparatus or devices, not otherwise provided for · CPC title

• B64D2203/00

  Aircraft or airfield lights using LEDs · CPC title

• B64D47/02

  Arrangements or adaptations of signal or lighting devices · CPC title