Aircraft passenger seat mechanism

• US 10,450,071 B2
• Filed: 06/29/2016
• Issued: 10/22/2019
• Est. Priority Date: 06/30/2015
• Status: Active Grant

• Current Assignee: British Airways PLC (International Consolidated Airlines Group SA)
• Original Assignee: British Airways PLC (International Consolidated Airlines Group SA)
• Inventors: Jones, Gareth Evan Lyn
• Primary Examiner(s): White, Rodney B
• Application Number:
  US15/741,040
• Publication Number:
  US 20180194474A1
• Time in Patent Office: 1,210 Days
• Field of Search: 297118, 297317, 297322, 297341, 297342, 29735412, 29735413
• CPC Class Codes: B64D 11/06395 characterised by the arrangement of electric motors for adjustment
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats

Abstract

An aircraft passenger seat comprises a seat back and a seat pan, the seat pan being pivotally connected at or around a forward end thereof to a seat frame at a first pivot point, and at or around a rearward end thereof to a lower end of the seat back at a second pivot point. The seat back has an extension extending beyond the second pivot point and engaging a guide track in or connected to the seat frame, and a reclining actuator for driving the extension along the guide track so as to adjust the reclining of the seat.

Claims

1. An aircraft passenger seat comprising a seat back and a seat pan, the seat pan being pivotally connected at or around a forward end thereof to a seat frame at a first pivot point, and at or around a rearward end thereof to a lower end of the seat back at a second pivot point;

the seat back having an extension extending beyond the second pivot point and engaging a guide track in or connected to the seat frame, and a reclining actuator for driving the extension along the guide track so as to adjust the reclining of the seat;

wherein the extension is driven by a linear drive mechanism aligned with the guide track, the linear drive mechanism comprising a pinion driven by the reclining actuator and engaging a rack arranged along the guide track.

2. The aircraft passenger seat of claim 1, wherein the rack is arranged along an upper side of the guide track.

5. The aircraft passenger seat of claim 1, wherein the guide track is located in the seat frame, below the lower end of the seat back.

10. The aircraft passenger seat of claim 1, wherein the guide track is removably attached to the seat frame.

11. The aircraft passenger seat of claim 1, including a support attached to the seat frame and arranged to support the seat back in a reclined position.

12. The aircraft passenger seat of claim 11, wherein the support is arranged to slide against the seat back as the seat back reclines.

13. The aircraft passenger seat of claim 1, wherein the seat frame is slidably supported on a mounting bracket for fixing the seat to a cabin floor.

14. The aircraft passenger seat of claim 13, including a translation actuator for driving the seat frame relative to the mounting bracket.

15. The aircraft passenger seat of claim 13, including a seat controller for controlling the reclining actuator and the translation actuator.

16. The aircraft passenger seat of claim 15, wherein the seat controller is arranged to move the seat forward as the seat back is reclined.

17. The aircraft passenger seat of claim 15, wherein the seat controller is arranged to move the seat forward when the seat back is upright, independently of movement of the reclining actuator.

3. An aircraft passenger seat comprising a seat back and a seat pan, the seat pan being pivotally connected at or around a forward end thereof to a seat frame at a first pivot point, and at or around a rearward end thereof to a lower end of the seat back at a second pivot point;

the seat back having an extension extending beyond the second pivot point and engaging a guide track in or connected to the seat frame, and a reclining actuator for driving the extension along the guide track so as to adjust the reclining of the seat;

wherein the extension is driven by a linear drive mechanism aligned with the guide track, the seat including a clutch for releasing the linear drive mechanism from the reclining actuator.

4. An aircraft passenger seat comprising a seat back and a seat pan, the seat pan being pivotally connected at or around a forward end thereof to a seat frame at a first pivot point, and at or around a rearward end thereof to a lower end of the seat back at a second pivot point;

the seat back having an extension extending beyond the second pivot point and engaging a guide track in or connected to the seat frame, and a reclining actuator for driving the extension along the guide track so as to adjust the reclining of the seat;

wherein the extension carries a bearing moveable along the guide track;

wherein the extension is driven by a linear drive mechanism aligned with the guide track, and wherein the bearing is arranged to reduce loading on the linear drive mechanism.

6. An aircraft passenger seat comprising a seat back and a seat pan, the seat pan being pivotally connected at or around a forward end thereof to a seat frame at a first pivot point, and at or around a rearward end thereof to a lower end of the seat back at a second pivot point;

the seat back having an extension extending beyond the second pivot point and engaging a guide track in or connected to the seat frame, and a reclining actuator for driving the extension along the guide track so as to adjust the reclining of the seat;

wherein the guide track has a first section extending downwardly and forwardly from a first end, such that the seat back reclines as the part moves along the first section away from the first end.

7. The aircraft passenger seat of claim 6, wherein the first section is arcuate.

8. The aircraft passenger seat of claim 6, wherein the guide track has a second section extending upwardly and forwardly towards a second end, such that the seat back reclines and the rearward end of the seat pan is raised as the part moves along the second section towards the second end.

9. The aircraft passenger seat of claim 8, wherein the second section is substantially straight.