Synchronous seat recline mechanism

• US 9,061,766 B2
• Filed: 11/30/2012
• Issued: 06/23/2015
• Est. Priority Date: 11/30/2011
• Status: Active Grant

• Current Assignee: Burkley U. Kladde
• Original Assignee: Burkley U. Kladde
• Inventors: Kladde, Burkley U.
• Primary Examiner(s): MCPARTLIN, SARAH BURNHAM
• Application Number:
  US13/691,119
• Publication Number:
  US 20130134758A1
• Time in Patent Office: 935 Days
• Field of Search: 297/341, 297/342
• US Class Current: 1/1
• CPC Class Codes: A47C 1/024 the parts, being the back-rest, or the back-rest and seat unit, having adjustable and lockable inclination
• 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 11/0601 Arrangement of seats for non-standard seating layouts, e.g. seats staggered horizontally or vertically, arranged in an angled or fishbone layout, or facing in other directions than the direction of flight
• CPC Class Codes: B64D 11/064 Adjustable inclination or position of seats
• CPC Class Codes: B64D 11/0648 Lower frame constructions
• CPC Class Codes: B64D 11/0696 Means for fastening seats to floors, e.g. to floor rails

Abstract

A seat for use in an aircraft having a floor is provided. The seat has a support assembly, a seat, a seat back pivotably coupled to the support assembly for movement between an upright position and a reclined position relative to the support assembly, and an occupant back support having an upper portion and lower portion pivotally coupled to the seat back at the upper portion. A pivot link pivotally couples to the rear portion of the seat at a first end and pivotally couples to the lower portion of the occupant back support at a second end. The pivot link causes the lower portion of the occupant back support to move downwardly and forward relative to the seat as the seat back moves from the upright position to the reclined position.

Claims

1. An aircraft seat for use in an aircraft having a floor comprising a support assembly coupleable to an aircraft floor, a seat bottom having a seat bottom frame pivotably coupled to the support assembly, a seat back beam supporting a seat back frame, the seat back beam pivotably coupled to the support assembly, wherein the seat back frame defines an occupant back support having:

an upper portion and lower portion pivotally coupled by a non-translational pivot connection to the seat back beam at the upper portion; and

a pivot link pivotally coupled to a rear portion of the seat bottom frame at a first end and pivotally coupled to the lower portion of the occupant back support at a second end;

such that the lower portion of the occupant back support moves downwardly and forward relative to the seat bottom frame and the seat bottom frame is drawn toward the seat back frame and tilts downward as the seat back frame moves from an upright position to a reclined position.

2. The aircraft seat of claim 1, wherein the support assembly includes a mid-support beam element.

3. The aircraft seat of claim 2, wherein a bottom frame link pivotably couples the seat bottom frame to the mid-support beam element.

4. The aircraft seat of claim 1, wherein the seat bottom frame is pivotably coupled to a lower portion of the seat back beam.

5. The aircraft seat of claim 1, further comprising a vertical adjustment assembly for movement of the seat bottom frame and the seat back beam between an upper position and a lower position.

6. The aircraft seat of claim 1, further comprising a recline adjustment assembly for movement of the seat back frame and seat bottom frame between the upright position and the reclined position.

7. The aircraft seat of claim 1, further comprising a seat angle adjustment assembly for adjustment of the angle of the seat bottom frame relative to the support assembly.

8. A aircraft seat for use in an aircraft, comprising a support assembly coupleable to an aircraft floor having a mid-support beam element, a seat having a seat bottom frame, a seat back including a seat back beam pivotably coupled to the support assembly which is horizontally and rotationally moveable and moveable between an upright position and a reclined position relative to the support assembly, an occupant back support having an upper portion and lower portion pivotally coupled by a non-translational pivot connection to the seat back beam at the upper portion, and a pivot link pivotally coupled to a rear portion of the seat bottom frame at a first end and pivotally coupled to the lower portion of the occupant back support at a second end, such that:

the lower portion of the occupant back support moves downwardly and forward relative to the seat bottom and the seat bottom frame tilts back and moves toward the seat back as the seat back moves from the upright position to the reclined position; and

a front edge of the seat bottom frame moves downward as the aircraft seat horizontally rotates.

9. The aircraft seat of claim 8, wherein a bottom frame link pivotably couples the seat bottom frame to the mid-support beam element.

10. The aircraft seat of claim 8, wherein the seat bottom frame is pivotably coupled to a lower portion of the seat back beam.

11. The aircraft seat of claim 8, further comprising a vertical adjustment assembly for movement of the seat bottom frame and the seat back beam between an upper position and a lower position.

12. The aircraft seat of claim 8, further comprising a recline adjustment assembly for movement of the seat back and seat bottom frame between the upright position and the recline position.

13. The aircraft seat of claim 8, further comprising a seat angle adjustment assembly for adjustment of the angle of the seat bottom frame relative to the support assembly.

14. The aircraft seat of claim 8, wherein the mid-support beam, seat bottom frame, and seat back frame have pivot points allowing for rotational movement of the seat bottom frame about a point in space located approximately below a front edge of the seat bottom frame.

15. An aircraft seat for use in an aircraft comprising:

a support assembly coupleable to an aircraft floor having a mid-support beam element;

a seat bottom having a seat bottom frame and a bottom frame link pivotably coupling the seat bottom frame to the mid-support beam element;

a seat back having a seat back beam pivotably coupled to the support assembly for movement between an upright position and a reclined position relative to the support assembly, a pivotal connection between the seat bottom and the seat back, and an occupant back support having an upper portion and a lower portion pivotally coupled by non-translational pivot connection to the seat back beam at the upper portion; and

a pivot link pivotally coupled to a rear portion of the seat bottom at a first end and pivotally coupled to the lower portion of the occupant back support at a second end for causing the lower portion of the occupant back support to move downwardly and forward relative to the seat bottom as the seat back moves from the upright position to the reclined position.

16. The aircraft seat of claim 15, further comprising a vertical adjustment assembly for movement of the seat bottom frame and the seat back beam between an upper position and a lower position.

17. The aircraft seat of claim 16, wherein the support assembly includes a support assembly bottom frame coupled to the vertical adjustment assembly.

18. The aircraft seat of claim 15, further comprising a recline adjustment assembly for the movement of the seat back and seat bottom frame between the upright position and the recline position.

19. The aircraft seat of claim 15, wherein the seat bottom frame is pivotably coupled to a lower portion of the seat back beam.

20. The aircraft seat of claim 15, wherein a bottom frame link pivotably couples the seat bottom frame to the mid-support beam element.