Aircraft seat with segmented seatback for achieving in-bed lounge sitting position

Patent metadata

Field	Value
Publication number	US-10266271-B2
Application number	US-201615282352-A
Country	US
Kind code	B2
Filing date	Sep 30, 2016
Priority date	Mar 28, 2014
Publication date	Apr 23, 2019
Grant date	Apr 23, 2019

Abstract

In a preferred embodiment, an adjustable aircraft passenger seat includes a seat bottom; a legrest moveably connected to the seat bottom that articulates between a legrest vertical and a legrest horizontal positions; a lower seatback moveably connected to the seat bottom to be articulated between a lower seatback vertical and a lower seatback horizontal positions; and an upper seatback moveably connected to the lower seatback to be articulated between an upper seatback vertical and an upper seatback horizontal positions. The articulation of the legrest, the articulation of the lower seat back, and the articulation of the upper seatback may be configured to articulate the adjustable aircraft passenger seat from an upright sitting to a horizontal sleeping position, through an in-bed lounge sitting position.

First claim

The invention claimed is:

1. An adjustable aircraft passenger seat comprising:
a seat bottom;
a legrest moveably connected to the seat bottom that articulates between a legrest vertical position and a legrest horizontal position via a legrest actuation system;
a lower seatback moveably connected to the seat bottom to be articulated between a lower seatback vertical position and a lower seatback horizontal position via a lower seatback actuation system;
an upper seatback moveably connected to the lower seatback to be articulated between an upper seatback vertical position and an upper seatback horizontal position via an upper seatback actuation system; and
a headrest connected to the upper seatback;
wherein the articulation of the legrest, the articulation of the lower seatback, and the articulation of the upper seatback, are configured to articulate the adjustable aircraft passenger seat from an upright sitting position to a horizontal sleeping position, through an in-bed lounge sitting position, wherein, in the in-bed lounge sitting position, an angle between the lower seatback and the seat bottom is greater than 90, the seat bottom is substantially horizontal and substantially planar with the legrest, and an angle of the upper seatback relative to the seat bottom is smaller than the angle between the lower seatback and the seat bottom such that a lower body of a passenger in the passenger seat would be in a lie flat position while an upper torso of the passenger would be in a raised position; and
wherein the legrest actuation system, the lower seatback actuation system, and the upper seatback actuation system are communicatively coupled to articulate the adjustable aircraft passenger seat from any of the upright sitting position, the in-bed lounge sitting position, and the horizontal sleeping position to any other of the upright sitting position, the in-bed lounge sitting position, and the horizontal sleeping position by way of a single passenger-operated control actuation.

2. The adjustable aircraft passenger seat of claim 1 , wherein each of the legrest actuation system, the lower seatback actuation system, and the upper seatback actuation system is articulated via a respective electromechanical actuator.

3. The adjustable aircraft passenger seat of claim 2 , wherein each of the electromechanical actuators is configured to be selectively coupled for simultaneous repositioning, wherein the coupling is performed by a primary control device that electrically connects the electromechanical actuators.

4. The adjustable aircraft passenger seat of claim 1 , wherein the headrest is moveably connected to the upper seatback to be articulated between a contracted position and a deployed position.

5. The adjustable aircraft passenger seat of claim 4 , wherein the articulation of the headrest follows at least one of a rectilinear course, a curvilinear course, and a circular course.

6. The adjustable aircraft passenger seat of claim 1 , further including a middle seatback moveably connected to the lower seatback and to the upper seatback to be articulated from a middle seatback vertical position to a middle seatback horizontal position.

7. An aircraft passenger suite comprising:
a plurality of privacy walls defining boundaries of the passenger suite;
a passenger seat including
a seat bottom;
a legrest moveably connected to the seat bottom and configured to articulate between a legrest vertical position and a legrest horizontal position via a legrest actuation system;
a headrest; and
at least two seatback sections including a lower seatback section connected to the seat bottom and an upper seatback section connected to the headrest, wherein each seatback section of the at least two seatback sections is configured to be articulated between an upright seating position and a lie flat position via at least a lower seatback actuation system and an upper seatback actuation system;
wherein the articulation of the legrest and the articulation of the at least two seatback sections are configured to articulate to at least an upright sitting position, a horizontal sleeping position, and an in-bed lounge sitting position, wherein the in-bed lounge sitting position is characterized by a lie-flat lower body position and a raised upper body position; and
wherein the legrest actuation system, the lower seatback actuation system, and the upper seatback actuation system, are communicatively coupled to articulate the passenger seat from any of the upright sitting position, the in-bed lounge sitting position, and the horizontal sleeping position to any other of the upright sitting position, the in-bed lounge sitting position, and the horizontal sleeping position by way of a single passenger-operated control actuation.

8. The aircraft passenger suite of claim 7 , further comprising an ottoman positioned directly forward of the passenger seat to form a substantially horizontal surface with the legrest when the legrest is in a horizontal position.

9. The aircraft passenger suite of claim 7 , wherein the at least two seatback sections further comprise a middle seatback section moveably connected on a lower end to the lower seatback section and movably connected on an upper end to the upper seatback section.

10. The aircraft passenger suite of claim 7 , wherein the at least two seatback sections comprise a series of at least five seatback sections having a spatial configuration to follow a general anatomy of a spine.

11. A method for providing multiple adjustable positions in an airplane passenger seat with a segmented seatback, comprising:
providing a first means for articulating a legrest of the airplane passenger seat, a second means for articulating a lower seatback segment of the airplane passenger seat, and a third means for articulating an upper seatback segment of the airplane passenger seat;
providing a means for coupling the first means for articulating, the second means for articulating, and the third means for articulating to enable simultaneous articulation of the legrest, the lower seatback segment, and the upper seatback segment; and
providing a means for controlling coupled articulation of the legrest, the lower seatback segment, and a upper seatback segment;
wherein the means for controlling is configured, upon input from a passenger of the airplane passenger seat, to cause actuation of the airplane passenger seat to one of at least three default positions, wherein the at least three default positions comprise an upright position, a lie-flat position, and an in-bed lounge position, wherein the in-bed lounge position is characterized by a lie-flat lower body position and a raised upper body position, and
wherein the means for controlling further comprises at least one passenger-actuable convenience control configured, upon selection, to cause actuation of the airplane passenger seat between the seat positions including the lie-flat position, the in-bed lounge position, and the upright position.

12. The method of claim 11 , wherein at least one of the first means for articulating, the second means for articulating, and the third means for articulating comprises a linear actuator.

13. The method of claim 11 , wherein the means for controlling comprises a coupler configured to couple signals to the first means for articulating, the second means for articulating, and the third means for articulating.

14. The method of claim 11 , wherein the means for controlling comprises a set of user controls for individually customizing angles of the legrest, the lower seatback segment, and the upper seatback segment.

15. The method of claim 1

Assignees

• Be Aerospace Inc

Inventors

• Udriste Daniel
• De La Garza Javier Valdes
• Beroth Michael

Classifications

• B60N2/34

  into a bed · CPC title

• B60N2/995

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

• B60N2/643

  shape of the back-rests (B60N2/66 takes precedence) · CPC title

• B64D11/0646

  Seats characterised by special features of stationary arms, foot or head rests · CPC title

• B64D11/0642

  Adjustable headrests · CPC title