Aircraft passenger seat assembly including a backrest tilt apparatus

Patent metadata

Field	Value
Publication number	US-10450070-B2
Application number	US-201715718602-A
Country	US
Kind code	B2
Filing date	Sep 28, 2017
Priority date	Sep 28, 2016
Publication date	Oct 22, 2019
Grant date	Oct 22, 2019

Abstract

An aircraft passenger seat has a seat back including a lower portion pivotably mounted to a seat bottom and an upper portion rotatably coupled to the lower portion. The upper portion may rotate in a forward direction relative to the lower portion during articulation of the seat. An inner diaphragm may be positioned between a headrest and a set of side frame members of the upper portion and is rotatably coupled to the upper portion and lower portion to provide support for an upper back and shoulders of a seated passenger. An actuating assembly may coordinate articulation of the lower portion, the upper portion, and the inner diaphragm to permit articulation of the seat between an upright taxi takeoff and landing (TTOL) position and a reclined position and to enable the seated passenger to achieve more ergonomic postures.

First claim

What is claimed is:

1. An aircraft passenger seat comprising:
a seat bottom frame;
a seat back frame pivotably mounted to the seat bottom frame for permitting the angle of the seat back frame relative to the seat bottom frame to be varied at least from an upright taxi takeoff and landing (TTOL) position to a reclined position, wherein the seat back frame further includes
a lower portion pivotably mounted to the seat bottom frame such that the seat back and the seat bottom frame cooperatively pivot between the upright TTOL position and the reclined position about a first pivot point, and
an upper portion rotatably coupled to the lower portion, the upper portion including a set of side frame members,
wherein the upper portion is configured to articulate in a forward direction relative to the lower portion about a second pivot point between the upper portion and the lower portion, and
an inner diaphragm positioned between the set of side frame members of the upper portion and rotatably coupled to the upper portion and lower portion at the second pivot point, wherein
the inner diaphragm is configured to articulate about the second pivot point independently of articulation of the upper portion to provide support for an upper back and shoulders of a seated passenger; and
an actuating assembly configured to cause simultaneous articulation of each of the upper portion, the lower portion, and the inner diaphragm between the upright TTOL position and the reclined position.

2. The aircraft passenger seat of claim 1 , wherein the actuating assembly comprises a motor-driven linear actuator.

3. The aircraft passenger seat of claim 1 , wherein the actuating assembly includes an output arm coupled to the upper portion of the seat back frame at a receiving flange such that extension of the output arm causes the upper portion to articulate forward relative to the lower portion.

4. The aircraft passenger seat of claim 3 , wherein the extension of the output arm of the actuating assembly when the seat is in the upright, TTOL position is configured to cause the lower portion of the seat back frame to articulate toward the reclined position.

5. The aircraft passenger seat of claim 1 , further comprising: a seat base comprising a main guide track; and a main roller pivotably connected to the lower portion of the seat back frame and the seat bottom frame at a main pivot point, the main roller configured to slideably engage the main guide track as the aircraft passenger seat articulates between the upright TTOL position and the reclined position.

6. The aircraft passenger seat of claim 1 , wherein the actuating assembly is configured to cause articulation of the seat back frame to a partially reclined position, wherein, in the partially reclined position, each of the lower portion, upper portion, and inner diaphragm is positioned at a different articulation angle relative to a horizontal plane.

7. The aircraft passenger seat of claim 1 , wherein the actuating assembly is further configured to cause simultaneous articulation of each of the upper portion, the lower portion, and the inner diaphragm between the reclined position and a lie-flat bed position.

8. The aircraft passenger seat of claim 7 , wherein, in the lie-flat bed position, the lower portion, the upper portion, and the inner diaphragm are substantially aligned with a horizontal plane.

9. The aircraft passenger seat of claim 1 , further comprising a respective curved slot disposed on each side of the lower portion of the seat back frame, the curved slot configured to define a travel path for the upper portion relative to the lower portion.

10. The aircraft passenger seat of claim 9 , further comprising a respective upper guide roller mounted to an inner surface of each of the set of side frame members of the upper portion, wherein the guide roller is configured to slideably translate within the curved slot as the upper portion articulates relative to the lower portion.

11. The aircraft passenger seat of claim 1 , further comprising a linkage pivotably connecting a third pivot point on the seat back frame to a fourth pivot point on a base of the seat, wherein the linkage is configured to maintain a substantially constant relative distance between the third pivot point and the fourth pivot point as the seat articulates between the upright TTOL position and the reclined position.

12. The aircraft passenger seat of claim 11 , wherein the fourth pivot point is disposed on a rear frame member pivotably mounted to the base of the seat such that pivoting of the linkage caused by articulation of the seat toward the reclined position causes upward rotation of the rear frame member to maintain the constant relative distance between the third pivot point and the fourth pivot point.

13. The aircraft passenger seat of claim 1 , further comprising a set side panels pivotably mounted on each side of the seat bottom frame and seat back frame at the first pivot point, wherein the set of side panels are configured to cooperatively articulate with the seat bottom frame and seat back frame between the upright TTOL position and the reclined position.

14. The aircraft passenger seat of claim 1 , further comprising a headrest mounted to an upper end of the side frame members such that the headrest is positioned forward of the first set of side frame members and above the inner diaphragm.

15. The aircraft passenger seat of claim 1 , wherein the upper portion is configured to rotate forward about the first pivot point to provide additional head clearance for an aft-seated passenger in a rapid deceleration event.

Assignees

• Rockwell Collins Inc

Inventors

• Beroth Michael

Classifications

• B64D11/0644

  Adjustable arm rests · CPC title

• B60N2/995

  Lower-leg-rests, e.g. calf-rests · CPC title

• B60N2/34

  into a bed · CPC title

• B60N2/23

  by {linear actuators, e.g.} linear screw mechanisms · CPC title

• B60N2/2222

  the back-rest having two or more parts · CPC title