Zero intrusion kinematic and recline mechanism for commercial aircraft seats

Patent metadata

Field	Value
Publication number	US-12077303-B2
Application number	US-201917760700-A
Country	US
Kind code	B2
Filing date	Sep 30, 2019
Priority date	Sep 30, 2019
Publication date	Sep 3, 2024
Grant date	Sep 3, 2024

Abstract

Described are aircraft seats having a seat bottom coupled to a seat back and a linkage mechanism for reclining the seat. The reclining mechanism includes an actuator coupled to a recline lock linkage. The actuator is movable between positions and moves the recline lock linkage about a pivot point to facilitate movement of the seat between an upright position and a deployed position.

First claim

That which is claimed is:

1. An aircraft seat comprising:
a seat bottom coupled to a seat back;
a linkage mechanism coupled to the seat bottom, wherein the linkage mechanism comprises:
an actuator having a retracted position and a deployed position;
a recline lock linkage having a first end and a second end, wherein the second end is coupled to the actuator;

wherein, when the actuator moves from the deployed position to the retracted position, the recline lock linkage pivots between a first position and a second position;
wherein, in the first position, the recline lock linkage is positioned at an angle such that the first end is positioned rearward with respect to the second end;
wherein, in the second position, the recline lock linkage is positioned at an angle such that the first end is positioned forward with respect to the second end;
wherein movement of the recline lock linkage between the first position and the second position moves the seat between an upright position and a reclined position; and
wherein the linkage mechanism further comprises a recline lock mount pivotably coupled to the recline lock linkage at a pivot point between the first end and the second end.

2. The aircraft seat of claim 1 , wherein the linkage mechanism further comprises a seat pan mount coupled to a bottom surface of the seat bottom and pivotably coupled to the first end of the recline lock linkage.

3. The aircraft seat of claim 2 , wherein, when the actuator moves between the retracted and deployed positions, the first end of the recline lock linkage rotates with respect to the seat pan mount.

4. The aircraft seat of claim 1 , wherein the pivot point of the recline lock linkage is movable in an up and down direction when the recline lock linkage moves between the first and second positions.

5. The aircraft seat of claim 1 , wherein the actuator can be locked in any position between the retracted and deployed positions thereby locking the recline lock linkage in any position between the first and second positions.

6. The aircraft seat of claim 1 , further comprising a pair of sidewalls positioned on opposing sides of the seat bottom; and
wherein each of the sidewalls further comprises at least one track; and
wherein movement of the recline lock linkage between the first and second positions causes the seat bottom to translate along the at least one track on each of the sidewalls thereby moving the seat between the upright and reclined positions.

7. The aircraft seat of claim 6 , wherein a length of the at least one track is less than 8 inches.

8. The aircraft seat of claim 1 , wherein-comprising:
a seat angle is formed between the seat bottom and the seat back;
a vertical axis is positioned rearward of the seat back;
wherein, when the aircraft seat is in the upright position, the seat back forms a first angle with respect to the vertical axis; and
wherein, when the aircraft seat is in the reclined position, the seat back forms a second angle with respect to the vertical axis; and
wherein the second angle is greater than the first angle; and
wherein the seat angle remains approximately constant when the seat is moved between the upright position and the reclined position.

9. The aircraft seat of claim 1 ,
wherein the seat bottom comprises:
a first wall positioned adjacent a first side of the seat bottom;
a second wall positioned adjacent a second side of the seat bottom opposite the first side;
wherein each of the first wall and the second wall comprises a first seat track and a second seat track; and

wherein the seat bottom translates along the first seat track and the second seat track in each wall to move the seat between the upright position and the reclined position.

10. The aircraft seat of claim 9 , wherein the second track is positioned rearward with respect to the first seat track on each of the first and second walls.

11. The aircraft seat of claim 9 , wherein the first seat track is positioned so as to be substantially horizontal on each of the first and second walls.

12. The aircraft seat of claim 9 , wherein the second seat track is positioned at an angle on each of the first and second walls such that a forward portion of the second seat track is positioned lower with respect to a rearward portion of the second seat track.

13. The aircraft seat of claim 9 , wherein, when the seat moves between the upright and reclined positions, the seat bottom translates simultaneously along the first seat track and the second seat track.

14. The aircraft seat of claim 9 , wherein a length of each of the first seat track and the second seat track is less than 8 inches.

15. An aircraft seat comprising:
a seat bottom coupled to a seat back;
a linkage mechanism coupled to the seat bottom, wherein the linkage mechanism comprises:
an actuator having a retracted position and a deployed position;
a recline lock linkage having a first end and a second end, wherein the second end is coupled to the actuator;

wherein, when the actuator moves from the deployed position to the retracted position, the recline lock linkage pivots between a first position and a second position;
wherein, in the first position, the recline lock linkage is positioned at an angle such that the first end is positioned rearward with respect to the second end;
wherein, in the second position, the recline lock linkage is positioned at an angle such that the first end is positioned forward with respect to the second end;
wherein movement of the recline lock linkage between the first position and the second position moves the seat between an upright position and a reclined position; and
wherein the actuator can be locked in any position between the retracted and deployed positions thereby locking the recline lock linkage in any position between the first and second positions.

16. An aircraft seat comprising:
a seat bottom coupled to a seat back;
a linkage mechanism coupled to the seat bottom, wherein the linkage mechanism comprises:
an actuator having a retracted position and a deployed position;
a recline lock linkage having a first end and a second end, wherein the second end is coupled to the actuator;

wherein, when the actuator moves from the deployed position to the retracted position, the recline lock linkage pivots between a first position and a second position;
wherein, in the first position, the recline lock linkage is positioned at an angle such that the first end is positioned rearward with respect to the second end;
wherein, in the second position, the recline lock linkage is positioned at an angle such that the first end is positioned forward with respect to the second end;
wherein movement of the recline lock linkage between the first position and the second position moves the seat between an upright position and a reclined position; and
a pair of sidewalls positioned on opposing sides of the seat bottom, wherein each of the sidewalls further comprises at least one track, and wherein movement of the recline lock linkage between the first and second positions causes the seat bottom to translate along the at least one track on each of the sidewalls thereby moving the seat between the upright and reclined positions.

Assignees

• Safran Seats Usa Llc

Inventors

• Parker Charles Michael
• Tranier Romain
• Mansouri Reza
• Omoragbon Amen
• Ramarathnam Gokul

Classifications

• B60N2/2209

  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 title

• B60N2/12

  slidable and tiltable · CPC title

• B64D11/064 Primary

  Adjustable inclination or position of seats · CPC title