AIRCRAFT SEAT WITH TRANSLATING SEATBACK LINKAGE PIVOT

• US 20140300161A1
• Filed: 04/08/2014
• Published: 10/09/2014
• Est. Priority Date: 04/08/2013
• Status: Active Grant

• Current Assignee: B/E Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Original Assignee: B/E Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Beroth, Michael, Udriste, Daniel, De La Garza, Javier Valdes
• Granted Patent: US 9,174,737 B2
• Time in Patent Office: Days
• US Class Current: 297/340
• CPC Class Codes: B60N 2/2209 by longitudinal displacement of the cushion, e.g. back-rest hinged on the bottom to the cushion and linked on the top to the vehicle frame
• CPC Class Codes: B60N 2/34 into a bed
• CPC Class Codes: B64D 11/06 Arrangements of seats, or adaptations or details specially adapted for aircraft seats crew seat constructions for emergency purposes B64D25/04
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats
• CPC Class Codes: B64D 11/0641 Seats convertible into beds

Abstract

An aircraft passenger seat configured to recline and including a seatpan pivotally attached to a seatback, a spreader defining a non-linear guide path controlling the seatpan angle as the seat reclines, translating seatback linkage defining a non-linear guide path controlling the seatback angle as the seat reclines, and a drive link arranged to translate horizontally relative to the spreader to drive seat recline motion.

Claims

1. An aircraft passenger seat configured to recline, comprising:

a seatpan pivotally attached to a seatback;

a fixed spreader defining a first non-linear guide path for controlling the angle of the seatpan as the aircraft passenger seat reclines;

seatback linkage arranged to move relative to the fixed spreader as the aircraft passenger seat reclines, the seatback linkage defining a second non-linear guide path for controlling the angle of the seatback as the passenger seat reclines; and

a drive link arranged to translate horizontally relative to the fixed spreader to recline the aircraft passenger seat.

2. The aircraft passenger seat of claim 1, wherein a first end of the drive link is attached to a forward end of the seatpan and a second end of the drive link travels along the second non-linear guide path of the seatback linkage, and wherein the drive link is arranged to move horizontally away from the fixed spreader to drive the seatback toward horizontal and move toward the fixed spreader to drive the seatback toward vertical.

3. The aircraft passenger seat of claim 1, further comprising a seatback link pivotally attached at a first end to the seatback and pivotally attached at a second end to the seatback linkage, the seatback link arranged to pivot in a direction of the seatback linkage as the seatback reclines, and in a direction apart from the seatback linkage as the seatback returns upright.

4. The aircraft passenger seat of claim 1, wherein a first end of the seatback linkage is pivotally attached to the fixed spreader such that a second end of the seatback linkage is free to pivot up and down as the drive link translates horizontally relative to the fixed spreader.

5. The aircraft passenger seat of claim 1, further comprising a linear actuator positioned beneath the seatpan for driving horizontal translation of the drive link.

6. The aircraft passenger seat of claim 1, wherein the first and second non-linear guide paths are shaped to control the relationship between the angles of the seatpan and the seatback as the aircraft passenger seat reclines and moves toward upright.

7. The aircraft passenger seat of claim 1, wherein the seatpan and the seatback translate forward relative to the fixed spreader as the aircraft passenger seat reclines.

8. The aircraft passenger seat of claim 1, wherein a first roller spaced in fixed relation from the pivot of the seatpan and the seatback travels along the first non-linear guide path of the fixed spreader to control seatpan movement, and a second roller fixed to the drive link travels along the second non-linear guide path of the seatback linkage to drive seatback linkage movement as the drive link translates horizontally relative to the fixed spreader.

9. The aircraft passenger seat of claim 1, further comprising spaced left and right fixed spreaders interconnected through transverse forward, center and rear beam tubes, and spaced legs connected to one or more of the transverse forward, center and rear beam tubes.

10. The aircraft passenger seat of claim 1, wherein the seatback linkage pivots relative to the fixed spreader as the drive link translates horizontally relative to the fixed spreader.

11. The aircraft passenger seat of claim 1, wherein the first non-linear guide path is shaped to control the seatpan angle and the second linear guide path is shaped to control the seatback angle as the aircraft passenger seat reclines.

12. An aircraft passenger seat configured to recline, comprising:

a seatpan pivotally attached to a seatback;

a spreader defining a non-linear guide path controlling the seatpan angle as the aircraft passenger seat reclines;

translating seatback linkage defining a non-linear guide path controlling the seatback angle as the aircraft passenger seat reclines; and

a drive link arranged to move the seatpan along the non-linear guide path of the spreader and the seatback along the non-linear guide path of the seatback linkage as the drive link translates horizontally relative to the spreader.

13. The aircraft passenger seat of claim 12, wherein the spreader is fixed, the seatback linkage is pivotally attached to the spreader, and the drive link is arranged to move horizontally away from the fixed spreader to drive the seatback toward horizontal and move toward the fixed spreader to drive the seatback toward vertical.

14. The aircraft passenger seat of claim 12, further comprising a seatback link pivotally attached at a first end to the seatback and pivotally attached at a second end to the seatback linkage, the seatback link arranged to pivot in a direction of the seatback linkage as the seatback reclines, and in a direction apart from the seatback linkage as the seatback returns upright.

15. The aircraft passenger seat of claim 12, further comprising an actuator positioned beneath the seatpan for driving horizontal translation of the drive link.

16. The aircraft passenger seat of claim 12, wherein the angle between the seatpan and the seatback increases as the seatback moves toward horizontal.

17. The aircraft passenger seat of claim 12, wherein the seatpan and the seatback translate forward relative to the spreader as the aircraft passenger seat reclines.

18. The aircraft passenger seat of claim 12, wherein a first roller spaced in fixed relation from the pivot of the seatpan and the seatback travels along the non-linear guide path of the spreader to control the seatpan movement, and a second roller fixed to the drive link travels along the non-linear guide path of the seatback linkage to drive seatback linkage movement as the drive link translates horizontally relative to the spreader.

19. The aircraft passenger seat of claim 12, further comprising spaced left and right spreaders interconnected through transverse forward, center and rear beam tubes, and spaced legs connected to one or more of the transverse forward, center and rear beam tubes.

20. The aircraft passenger seat of claim 12, wherein the seatback linkage pivots relative to the spreader as the drive link translates horizontally relative to the spreader.