Reconfigurable seatback for in-seat entertainment

Patent metadata

Field	Value
Publication number	US-9469400-B1
Application number	US-201414480197-A
Country	US
Kind code	B1
Filing date	Sep 8, 2014
Priority date	Sep 8, 2014
Publication date	Oct 18, 2016
Grant date	Oct 18, 2016

Abstract

A reconfigurable seatback system and methods are described. The reconfigurable seatback system includes a display configured to provide in-flight entertainment to a passenger of an aircraft, a receptacle area and a cover panel. The receptacle area is positioned in a seatback of the aircraft and is configured to releasably receive and hold the display. The cover panel is configured to cover the receptacle area when the display is not positioned within the receptacle area.

First claim

What is claimed is:

1. A reconfigurable seatback system comprising:
a display configured to provide in-flight entertainment to a passenger of an aircraft;
a receptacle area positioned in a seatback of the aircraft, the receptacle area configured to releasably receive and hold the display via a first connection; and
a cover panel configured to cover the receptacle area via the first connection when the display is not positioned within the receptacle area and to cover the receptacle area via a second connection when the display is positioned within the receptacle area.

2. The system of claim 1 , further comprising a quick release mechanism configured to release at least one of the display and the cover panel from the receptacle area when engaged by a tool.

3. The system of claim 1 , wherein the receptacle area comprises a slam latch configured to securely lock the cover panel into the receptacle area.

4. The system of claim 1 , further comprising a tool configured to remove the display from the receptacle area, the tool having an elongated keyed portion.

5. The system of claim 4 , wherein the display is bordered by a frame, the frame having an access opening configured to receive the elongated keyed portion of the tool therein.

6. The system of claim 1 , further comprising a tool configured to remove the cover panel from the receptacle area, the tool having an elongated keyed portion.

7. The system of claim 6 , wherein the cover panel comprises an access opening configured to receive the elongated keyed portion of the tool therein.

8. The system of claim 1 , further comprising a tool having an elongated keyed portion configured to be inserted into an access opening in the cover panel and a frame of the display to release the cover panel and the display from the receptacle area.

9. The system of claim 1 , wherein the cover panel comprises a hard plastic backed with fabric.

10. The system of claim 1 , wherein the display comprises a liquid crystal display.

11. A reconfigurable seatback compatible with an in-seat entertainment system, the reconfigurable seatback comprising:
a front surface configured to support the back of a passenger sitting in an attached seat;
a back surface facing away from the front surface; and
a receptacle area positioned within the back surface of the reconfigurable seatback,
wherein the receptacle area is configured to securely hold a display releasably positioned therein via a first connection, the display being a part of the in-seat entertainment system on an aircraft;
wherein the receptacle area is configured to receive a cover panel via the first connection when the display is not positioned within the receptacle area; and
wherein the receptacle area is configured to receive the cover panel via a second connection when the display is positioned within the receptacle area.

12. The reconfigurable seatback of claim 11 , wherein the display has a bordering frame with a first tool receiving structure within the frame and the cover panel has a second tool receiving structure therein, the first tool receiving structure and the second tool receiving structure configured to receive a common tool to detach the display and the cover panel from the receptacle area.

13. The reconfigurable seatback of claim 12 , wherein the first tool receiving structure and the second tool receiving structure substantially align such that the common tool may be inserted into both the first tool receiving structure and the second tool receiving structure at the same time.

14. The reconfigurable seatback of claim 11 , wherein the display is a liquid crystal display.

15. The reconfigurable seatback of claim 11 , wherein the cover panel comprises a hard material backed with a fabric material configured to blend with the back surface of the seatback.

16. A method of reconfiguring a seatback of a passenger aircraft seat with a receptacle area positioned in the seatback, the receptacle area having a display positioned therein by a quick release mechanism, the method comprising:
engaging the quick release mechanism through an access opening in a frame of the display with a tool;
removing the display from the receptacle area; and
attaching a cover panel to the receptacle area of the seatback by the quick release mechanism after the display is removed from the receptacle area and attaching the cover panel to the receptacle area of the seatback by a second connection when the display is positioned within the receptacle area, the cover panel being substantially flush with a back surface of the seat.

17. The method claim 16 , further comprising:
inserting the tool into the access opening on the cover panel to engage the quick release mechanism;
removing the cover panel from the receptacle area; and
replacing the display within the receptacle area.

18. The method of claim 17 , further comprising inserting a different display into the receptacle area than was removed.

19. The method of claim 16 , wherein the cover panel comprises a first tool receiving structure configured to receive a first tool configured to lock and unlock the cover panel from the frame;
wherein the display comprises a second tool receiving structure configured to receive a second tool configured to unlock the display from the frame; and
wherein the first tool is different from the second tool.

20. The method of claim 19 , wherein the cover panel extends from a back surface of the seat to accommodate the display in the receptacle area.

Assignees

• Irmen Greg A
• Rockwell Collins Inc

Inventors

• Irmen Greg A

Classifications

• B64D11/06

  Arrangements of seats, or adaptations or details specially adapted for aircraft seats (crew seat constructions for emergency purposes B64D25/04) · CPC title

• B64D11/00155

  Individual entertainment or communication system remote controls therefor, located in or connected to seat components, e.g. to seat back or arm rest · CPC title

• B64D11/00152 Primary

  Seat back fixtures for removable monitors, e.g. tablet computers · CPC title

• B64D11/00153

  Monitors mounted on or in the seat other than the seat back · CPC title

• B64D11/0015 Primary

  Arrangements for entertainment or communications, e.g. radio, television · CPC title