IP Library Granted Patent US 12,012,211
Granted Patent B2
US 12,012,211 · App. 18/303,935 · Granted Jun 18, 2024

Carrier device, seating area divider and vehicle cabin

Inventors: Gary Lee Senechal (Lake Stevens, WA); Anthony Harcup (Surrey, GB)
Assignee: Adient Aerospace, LLC
B64D11/0627B64D11/0606
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,012,211
App. No.
18/303,935
Granted
Jun 18, 2024
Kind
B2
Abstract

A carrier device for a seating area divider provided within a vehicle cabin, in particular an aircraft cabin, comprising at least a base member and a fixation device which is coupled to the base member to support the base member on a cabin floor. The base member is configured to carry a privacy divider screen of the seating area divider. The fixation device comprises at least a seat track locking member protruding perpendicular from the base member.

Claims (29)

1. A carrier device for a seating area divider provided within an aircraft cabin, the carrier device comprising:

a base member including a vertical beam to support the seating area divider on a cabin floor, the vertical beam having a plurality of through holes; and

at least one connection device detachably mounted to the vertical beam to couple the base member to a seat furniture structure, the at least one connection device including a bracket mounted on the seat furniture structure, and at least one coupling element mounted to the base member in a releasable locking engagement with the bracket, wherein the coupling element has two free ends extending on opposite lateral sides of the vertical beam, and a tie rod portion coupling both free ends.

2. The carrier device of claim 1 , wherein the tie rod portion is guided through one of the through holes of the vertical beam.

3. The carrier device of claim 1 , wherein the free ends each comprise a bearing element.

4. The carrier device of claim 3 , wherein the bracket comprises a first bracket portion mounted to the seat furniture structure, and a second bracket portion configured as a clamp to receive one of the bearing elements.

5. The carrier device of claim 4 , wherein the connection device further includes a locking pin to releasable attach the bracket to the coupling element.

6. The carrier device of claim 5 , wherein the locking pin is guided through holes formed through the clamp and an opening arranged centric in the bearing element.

7. The carrier device of claim 6 , wherein the connection device further includes a locking bolt arranged in the opening to secure the locking pin against the clamp.

8. A seating area divider for an aircraft cabin, the seating area divider comprising:

a privacy divider screen; and

a carrier device including a base member including a vertical beam to support the privacy divider screen on a cabin floor, the vertical beam having a plurality of through holes, and at least one connection device detachably mounted to the vertical beam to couple the base member to a seat furniture structure, the at least one connection device including a bracket mounted on the seat furniture structure, and at least one coupling element mounted to the base member in a releasable locking engagement with the bracket, wherein the coupling element has two free ends extending on opposite lateral sides of the vertical beam, and a tie rod portion coupling both free ends.

9. The seating area divider of claim 8 , wherein the tie rod portion is guided through one of the through holes of the vertical beam.

10. The seating area divider of claim 8 , wherein the free ends each comprise a bearing element.

11. The seating area divider of claim 10 , wherein the bracket comprises a first bracket portion mounted to the seat furniture structure, and a second bracket portion configured as a clamp to receive one of the bearing elements.

12. The seating area divider of claim 11 , wherein the connection device further includes a locking pin to releasable attach the bracket to the coupling element.

13. The seating area divider of claim 12 , wherein the locking pin is guided through holes formed through the clamp and an opening arranged centric in the bearing element.

14. The seating area divider of claim 13 , wherein the connection device further includes a locking bolt arranged in the opening to secure the locking pin against the clamp.

15. An aircraft cabin, comprising:

a cabin floor;

a plurality of seat units; and

a seating area divider comprising:

a privacy divider screen; and

a carrier device including a base member including a vertical beam to support the privacy divider screen on the cabin floor, the vertical beam having a plurality of through holes, and at least one connection device detachably mounted to the vertical beam to couple the base member to a seat furniture structure, the at least one connection device including a bracket mounted on the seat furniture structure, and at least one coupling element mounted to the base member in a releasable locking engagement with the bracket, wherein the coupling element has two free ends extending on opposite lateral sides of the vertical beam, and a tie rod portion coupling both free ends.

16. The aircraft cabin of claim 15 , wherein the tie rod portion is guided through one of the through holes of the vertical beam.

17. The aircraft cabin of claim 15 , wherein the free ends each comprise a bearing element.

18. The aircraft cabin of claim 17 , wherein the bracket comprises a first bracket portion mounted to the seat furniture structure, and a second bracket portion configured as a clamp to receive one of the bearing elements.

19. The aircraft cabin of claim 18 , wherein the connection device further includes a locking pin to releasable attach the bracket to the coupling element.

20. The aircraft cabin of claim 19 , wherein the locking pin is guided through holes formed through the clamp and an opening arranged centric in the bearing element.

Assignments (2)
CHANGE OF NAME Recorded Jul 2, 2025
From: ADIENT AEROSPACE, LLC
To: ELEVATE AIRCRAFT SEATING LLC
Reel/Frame 071786/0571 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 21, 2023
From: SENECHAL, GARY LEE; HARCUP, ANTHONY
To: ADIENT AEROSPACE, LLC
Reel/Frame 063397/0772 →
Continuity (3)
Continuation 17120994 · Dec 14, 2020
Provisional Application 62947895 · Dec 13, 2019
Related Publication 20230249830A1 · Aug 10, 2023