DIVIDER SYSTEM FOR AN INTERNAL CABIN OF AN AIRCRAFT

1 . A divider system configured to separate a first section from a second section within an internal cabin of a vehicle, the divider system comprising:

one or more walls; and

one or more electronic screens secured to the one or more walls, wherein the one or more electronic screens are transparent and configured to show electronic content thereon.

2 . The divider system of claim 1 , wherein the one or more electronic screens comprise a transparent organic light-emitting diode (OLED) screen.

3 . The divider system of claim 1 , wherein the one or more walls comprise a first wall and a second wall, and wherein the one or more electronic screens comprise a first electronic screen coupled to the first wall, and a second electronic screen coupled to the second wall.

4 . The divider system of claim 3 , wherein each of the first electronic screen and the second electronic screens is a transparent organic light-emitting diode (OLED) screen.

5 . The divider system of claim 3 , wherein the first wall and the second wall are configured to be separated by an aisle within the internal cabin.

6 . The divider system of claim 1 , wherein the one or more electronic screens are selectively switchable between a transparent mode and an opaque mode.

7 . The divider system of claim 1 , wherein the first section is a first class section or a business class section, and the second section is the business class section or an economy section.

8 . The divider assembly of claim 1 , wherein the one or more walls are configured to extend to one or both of an overhead stowage bin or a ceiling within the internal cabin.

9 . The divider assembly of claim 1 , further comprising a control unit in communication with the one or more electronic screens, wherein the control unit is configured to control operation of the one or more electronic screens to display various types of the electronic content.

10 . The divider system of claim 9 , wherein the vehicle is an aircraft.

11 . The divider assembly of claim 10 , wherein the control unit is configured to control the one or more electronic screens based on phases of a flight of the aircraft.

12 . An aircraft comprising:

an internal cabin having a first section and a section; and

a divider system within the internal cabin, wherein the divider system separates the first section from the second section, the divider system comprising:

one or more walls; and

one or more electronic screens secured to the one or more walls, wherein the one or more electronic screens are transparent and configured to show electronic content thereon.

13 . The aircraft of claim 12 , wherein the one or more walls comprise a first wall and a second wall, and wherein the one or more electronic screens comprise a first electronic screen coupled to the first wall, and a second electronic screen coupled to the second wall.

14 . The aircraft of claim 13 , wherein each of the first electronic screen and the second electronic screens is a transparent organic light-emitting diode (OLED) screen.

15 . The aircraft of claim 13 , wherein the first wall and the second wall are separated by an aisle within the internal cabin.

16 . The aircraft of claim 12 , wherein the one or more electronic screens are selectively switchable between a transparent mode and an opaque mode, wherein the electronic screens in the transparent mode provide a clear line of sight therethrough.

17 . The aircraft of claim 12 , wherein the first section is a first class section or a business class section, and the second section is the business class section or an economy section.

18 . The aircraft of claim 12 , wherein the one or more walls extend to one or both of an overhead stowage bin or a ceiling within the internal cabin.

19 . The aircraft of claim 12 , further comprising a control unit in communication with the one or more electronic screens, wherein the control unit is configured to control operation of the one or more electronic screens to display various types of the electronic content, and wherein the control unit is configured to control the one or more electronic screens based on phases of a flight of the aircraft.

20 . An aircraft comprising:

an internal cabin having a first section and a section, wherein the first section is a first class section or a business class section, and the second section is the business class section or an economy section; and

a divider system within the internal cabin, wherein the divider system separates the first section from the second section, the divider system comprising:

a first wall extending to one or both of a first overhead stowage bin or a ceiling within the internal cabin;

a first transparent organic light-emitting diode (OLED) screen coupled to the first wall, wherein the first transparent OLED screen is configured to show first electronic content thereon, and wherein the first transparent OLED screen is selectively switchable between a first transparent mode and a first opaque mode;

a second wall separated from the first wall by an aisle, wherein the second wall extends to one or both of a second overhead stowage bin or the ceiling within the internal cabin;

a second transparent OLED screen coupled to the second wall, wherein the second transparent OLED screen is configured to show second electronic content thereon, and wherein the second transparent OLED screen is selectively switchable between a second transparent mode and a second opaque mode; and

a control unit in communication with the first transparent OLED screen and the second transparent OLED screen, wherein the control unit is configured to control operation of the first transparent OLED screen and the second transparent OLED screen to display various types of the first electronic content and the second electronic content, respectively, and wherein the control unit is configured to control the first transparent OLED screen and the second transparent OLED screen based on phases of a flight of the aircraft.