Passenger seat headrest

Patent metadata

Field	Value
Publication number	US-10202196-B2
Application number	US-201715471855-A
Country	US
Kind code	B2
Filing date	Mar 28, 2017
Priority date	Mar 20, 2015
Publication date	Feb 12, 2019
Grant date	Feb 12, 2019

Abstract

Apparatus and associated methods relate to an adjustable passenger seat headrest which includes articulating side wings, provides a more acute angle of support, and fits the width of a standard economy seat when stowed. In some embodiments, fabric may be stretched across the extreme ends of the wings to a center headrest, forming a hammock in which a passenger may rest their head. In an illustrative example, passengers may be provided with improved head support and comfort by employment of a mechanism that enables the side wings of the headrest to be articulated further apart, and/or extend out further from the back of the seat. These features may offer a more acute angle of passenger head support.

First claim

What is claimed is:

1. A headrest apparatus for a seated passenger, the apparatus comprising:
a base frame;
a center section mounted to the base frame;
a first wing section and a second wing section, each being coupled to the base frame and disposed laterally of the center section; and
a flexible fabric extending between each wing section and the center section;
wherein each of the first and second wing sections articulate between an undeployed position and a deployed position, wherein
in the undeployed position, an inner edge of the respective wing section is adjacent to the center section and the respective wing section is generally coplanar with the center section, and
in the deployed position, an inner edge of the respective wing section is laterally spaced apart from the center section relative to the undeployed position and an outer edge of the wing section is positioned forward and laterally outward relative to the undeployed position to the center section, such that the wing section is not generally coplanar with the center section,

wherein the flexible fabric extending between each wing when in the deployed position is sufficient to support five pounds of the weight of a passenger's head, the remaining weight of the passenger's head being borne by the center section and one of the first wing section and the second wing section.

2. The apparatus of claim 1 , wherein each of the first and second wing sections is adapted to be articulated between the deployed position to the undeployed position solely by force applied by a passenger and without the articulation of a button, latch or lock.

3. The apparatus of claim 1 , wherein each of the right wing section and the left wing section is individually articulable between the undeployed position and the deployed position.

4. The apparatus of claim 1 , wherein, in the undeployed position, a cushion of each wing section abuts a center base cushion connected to the center section.

5. The apparatus of claim 1 , wherein in the deployed position, a plane containing the respective wing section and a plane containing the center section intersect to form a deployment angle between about 60 and about 80 degrees.

6. The apparatus of claim 1 , wherein the inner edge of the respective wing section is positioned forward and laterally outward relative to the undeployed position to the center section.

7. The apparatus of claim 1 , wherein the flexible fabric extending between each wing when in the deployed position is sufficient to support at least 6 pounds of the weight of a passenger's head, the remaining weight of the passenger's head being borne by the center section and one of the first wing section and the second wing section.

8. The apparatus of claim 1 , wherein the flexible fabric extending between each wing when in the deployed position is sufficient to support at least 7 pounds of the weight of a passenger's head, the remaining weight of the passenger's head being borne by the center section and one of the first wing section and the second wing section.

9. The apparatus of claim 1 , wherein the flexible fabric extending between each wing when in the deployed position is sufficient to support at least 8 pounds of the weight of a passenger's head, the remaining weight of the passenger's head being borne by the center section and one of the first wing section and the second wing section.

10. A headrest apparatus for a seated passenger, the apparatus comprising:
a base frame;
a center section;
a first wing section and a second wing section, each being coupled to the base frame and disposed laterally of the center section;
a first means for pivotably coupling the first wing section to the base frame, and a second means for pivotably coupling the second wing section to the base frame, wherein each of the first means for pivotably coupling and the second means for pivotably coupling enables the respective wing section to articulate between an undeployed position and a deployed position, wherein
in the undeployed position, the respective wing section is generally coplanar with the center section, and
in the deployed position, the respective wing portion is positioned forward and laterally outward relative to the undeployed position, such that the wing section is not generally coplanar with the center section; and

a flexible fabric extending between each wing section and across the center section wherein,
in the undeployed position, the flexible fabric is substantially aligned with and proximate to the first wing section, the second wing section, and the center section, and
in the deployed position, the flexible fabric moves to a hammock position, creating a gap for receiving a portion of the passenger's head;

wherein, in the deployed position,
the flexible fabric is configured to support at least about five pounds of the weight of the passenger's head, and
an elasticity of the flexible fabric is sufficient to permit the fabric to provide a hammock for the passenger's head.

11. The headrest apparatus of claim 10 , wherein, in the deployed position, a lower portion of the respective wing section is positioned closer to a center of the passenger seat than an upper portion of the respective wing section.

12. The headrest apparatus of claim 11 , wherein a cushion of the respective wing section has a taper angle of at least 15 degrees.

13. The headrest apparatus of claim 10 , further comprising a means for retaining each of the first wing section and the second wing section in the deployed position.

14. The headrest apparatus of claim 10 , further comprising a means for preventing access to the first means for pivotably coupling and the second means for pivotably coupling from at least a top trajectory.

15. A passenger seat headrest, comprising:
a mounting frame for mounting the headrest to a passenger seat of an aircraft;
a center section comprising a center cushion;
a first wing section and a second wing section, each being pivotably coupled to the mounting frame at opposing sides of the center section; and
a flexible fabric releasably mounted between each wing section and the center section;
wherein each of the first and second wing sections is configured to pivotably articulate between an undeployed position and a deployed position, wherein
in the undeployed position, an inner edge of the respective wing section is adjacent to the center section and the respective wing section is generally coplanar with the center section, and
in the deployed position, an inner edge of the respective wing section is laterally spaced apart from the center section relative to the undeployed position and an outer edge of the wing section is positioned forward and laterally outward relative to the undeployed position to the center section, such that the wing section is not generally coplanar with the center section, and the flexible fabric is disposed such that a gap is provided for receiving a portion of a head of a passenger.

16. The headrest of claim 15 , wherein each of the first and second wing sections are configured to pivotably articulate to a narrow spaced-apart position between the undeployed position and the deployed position, and releasably lock into the partially deployed position.

17. The headrest of claim 16 , wherein, in the partially deployed position, the inner edge of the respective wing section is laterally closer to the center section relative to the deployed position.

18. The headrest of claim 16 , wherein, in both the deployed position and the partially deployed position, the lower porti

Assignees

• Be Aerospace Inc

Inventors

• Hontz Jeff
• Baker Cameron
• Darbyshire Martin

Classifications

• B64D11/0646

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

• B60N2/58

  Seat coverings · CPC title

• B60N2/885

  provided with side-rests · CPC title

• B64D11/0642 Primary

  Adjustable headrests · CPC title

• B60N2/879

  with additional features not related to head-rest positioning, e.g. heating or cooling devices or loudspeakers · CPC title