IP Library Granted Patent US 12,486,034
Granted Patent B2
US 12,486,034 · App. 18/216,265 · Granted Dec 2, 2025

Reclining seat with coordinated lowering motion and sliding monitor

Inventors: Christopher M. Wilson (Clemmons, NC); Javier Valdes de la Garza (Winston-Salem, NC); Jeremy R. Loman (Lexington, NC); David J. Poole (Winston-Salem, NC); John R. Kuyper (Winston Salem, NC)
Assignee: B/E Aerospace, Inc.
B64D11/00151B60R11/0235B64D11/064
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Quick Facts
Patent No.
US 12,486,034
App. No.
18/216,265
Granted
Dec 2, 2025
Kind
B2
Abstract

A passenger seat assembly includes features to mitigate privacy and use concerns that accompany backrest recline. In embodiments, the assembly includes a seat frame, a seat pan coupled to the seat frame, a backrest coupled to the seat frame, a backrest extension movably coupled to the backrest, the backrest extension configured to move between a retracted position within the backrest and an extended position above a top of the backrest, and a monitor rotatably mounted to the backrest extension and movable with the backrest extension. In use, backrest extension movement and/or monitor movement may be coordinated with backrest rotation motion.

Claims (38)

1 . A passenger seat assembly, comprising:

a seat frame;

a seat pan coupled to the seat frame;

a backrest coupled to the seat frame;

a backrest extension movably coupled to the backrest, the backrest extension configured to move between a retracted position within the backrest and an extended position above a top of the backrest;

a monitor rotatably mounted to the backrest extension and movable with the backrest extension;

a first actuator coupled to the backrest and to the backrest extension;

a second actuator coupled to the backrest extension and to the monitor; and

a controller, including a processor, configured to:

operate the first actuator to move the backrest extension toward the extended position as the backrest reclines and lowers, wherein the amount of movement of the backrest extension is determined by the amount of backrest recline and lowering; and

operate the second actuator to rotate the monitor, wherein the amount of rotation of the monitor is determined by the amount of backrest recline and lowering.

2 . The passenger seat assembly according to claim 1 , wherein the operation of the first actuator and the operation of the second actuator are coordinated.

3 . The passenger seat assembly according to claim 1 , further comprising a third actuator coupled to the seat frame and to the backrest, wherein the controller is further configured to operate the third actuator to rotate the backrest.

4 . The passenger seat assembly according to claim 3 , wherein the controller is configured to coordinate operation of the first actuator, the second actuator, and the third actuator.

5 . The passenger seat assembly according to claim 1 , wherein the seat pan is configured to lower as the backrest reclines and lowers.

6 . The passenger seat assembly according to claim 1 , wherein the backrest is configured with more than 5 degrees of recline.

7 . The passenger seat assembly according to claim 1 , wherein the backrest is configured with more than 10 degrees of recline.

8 . The passenger seat assembly according to claim 1 , wherein the backrest comprises a fixed headrest portion, and the backrest extension is positioned behind the fixed headrest portion.

9 . The passenger seat assembly according to claim 1 , wherein the backrest extension and the backrest have substantially equal widths.

10 . An aircraft passenger seat assembly, comprising:

a seat frame;

a seat pan coupled to the seat frame;

a backrest coupled to the seat frame, the backrest having an axis of rotation configured to lower as the backrest reclines;

a backrest extension movably coupled to the backrest, the backrest extension configured to move between a retracted position within the backrest and an extended position above a top of the backrest;

a monitor rotatably mounted to the backrest extension and movable with the backrest extension;

a first actuator coupled to the backrest and to the backrest extension;

a second actuator coupled to the backrest extension and to the monitor; and

a controller, including a processor, configured to:

operate the first actuator to move the backrest extension toward the extended position as the backrest reclines, wherein the amount of movement of the backrest extension is determined by the amount of backrest recline; and

operate the second actuator to rotate the monitor, wherein the amount of rotation of the monitor is determined by the amount of backrest recline;

wherein the operations of the first and second actuators are coordinated.

11 . The aircraft passenger seat assembly according to claim 10 , further comprising a third actuator coupled to the seat frame and to the backrest, wherein the controller is further configured to operate the third actuator to rotate the backrest.

12 . The aircraft passenger seat assembly according to claim 11 , wherein the controller is configured to coordinate operation of the first actuator, the second actuator, and the third actuator.

13 . The aircraft passenger seat assembly according to claim 10 , wherein the backrest is rotatably coupled the seat pan about the axis of rotation of the backrest, and wherein the seat pan is configured to lower as the backrest reclines.

14 . The aircraft passenger seat assembly according to claim 10 , wherein the backrest is configured with more than 5 degrees of recline.

15 . The aircraft passenger seat assembly according to claim 10 , wherein the backrest is configured with more than 10 degrees of recline.

16 . The aircraft passenger seat assembly according to claim 10 , wherein the backrest comprises a fixed upper portion, and the backrest extension is positioned behind the fixed upper portion.

17 . The aircraft passenger seat assembly according to claim 1 , wherein the backrest extension and the backrest have substantially equal widths.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 29, 2023
From: WILSON, CHRISTOPHER M.; VALDES DE LA GARZA, JAVIER; LOMAN, JEREMY R.; POOLE, DAVID J.; KUYPER, JOHN R.
To: B/E AEROSPACE, INC.
Reel/Frame 064116/0524 →
Continuity (1)
Related Publication 20250002151A1 · Jan 2, 2025
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