Passenger seat with neck support
View Patent ↗Described are passenger seats comprising a seat back support and a neck support structure comprising a headrest coupled to the seat back support and at least one wing pivotally coupled to the headrest, wherein the at least one wing is configured to rotate downwardly from a stowed position to a first deployed position and the at least one wing is also configured to rotate laterally from the stowed position to a second deployed position. The neck support structure may comprise a first wing and a second wing. A cover may be removably coupled to the at least one wing. The at least one wing may be formed from a flexible material.
1. A passenger seat comprising:
(a) a seat back support; and
(b) a neck support structure comprising:
(i) a headrest fixedly coupled to the seat back support and configured to provide support for a passenger's head;
(ii) planar connecting member pivotally coupled to a lower end of the headrest so that the connecting member pivots downwardly from a stowed position to a deployed position adjacent a passenger's neck, wherein the connecting member is configured to allow contact between the passenger's head and the headrest when the connecting member is in the stowed position and the deployed position; and
(iii) a pair of wings pivotally coupled to opposing lateral ends of the connecting member via friction hinges so that each wing pivots from a stowed position to a deployed position relative to an adjacent lateral end of the connecting member, wherein the pair of wings are configured to provide lateral support for the passenger's neck in the deployed position.
2. The passenger seat of claim 1 , wherein each wing of the pair of wings independently pivots relative to the adjacent lateral end of the connecting member.
3. The passenger seat of claim 1 , wherein the pair of wings are formed from a flexible material.
4. The passenger seat of claim 1 , wherein each wing pivots up to 90 degrees from the stowed position to the deployed position relative to the adjacent lateral end of the connecting member.
5. The passenger seat of claim 1 , wherein each wing manually pivots from the stowed position to the deployed position relative to the adjacent lateral end of the connecting member.
6. The passenger seat of claim 1 , wherein a cushion is coupled to each wing.
7. The passenger seat of claim 1 , wherein the headrest is integrally formed with the seat back support.
8. The passenger seat of claim 1 , wherein a cushion is coupled to the headrest.
9. A passenger seat comprising:
(a) a seat back support; and
(b) a neck support structure comprising:
(i) a headrest fixedly coupled to the seat back support and configured to provide support for a passenger's head, the headrest comprising a recess proximate a lower end;
(ii) a planar connecting member shaped to fit within the recess in a stowed position and pivotally coupled to the lower end of the headrest so that the connecting member rotates downwardly from the stowed position within the recess to a deployed position adjacent a passenger's neck, wherein the connecting member is configured to allow contact between the passenger's head and the headrest when the connecting member is in the stowed position and the deployed position; and
(iii) a pair of wings pivotally coupled to opposing lateral ends of the connecting member so that each wing pivots from a stowed position to a deployed position relative to an adjacent lateral end of the connecting member, wherein the pair of wings are configured to provide lateral support for the passenger's neck in the deployed position.
10. The passenger seat of claim 9 , wherein the pair of wings are pivotally coupled to the opposing lateral ends of the connecting member via friction hinges.
11. A method of operating a neck support structure for a passenger seat, the neck support structure comprising a headrest fixedly coupled to a seat back support of the passenger seat and configured to provide support for a passenger's head, a planar connecting member pivotally coupled to a lower end of the headrest, and a pair of wings pivotally coupled to opposing lateral ends of the connecting member, the steps comprising:
(a) pivoting the connecting member downwardly from a stowed position to a deployed position adjacent a passenger's neck, wherein the connecting member is configured to allow contact between the passenger's head and the headrest when the connecting member is in the stowed position and the deployed position;
(b) pivoting a first wing of the pair of wings from a stowed position to a deployed position relative to an adjacent lateral end of the connecting member, wherein the first wing is configured to provide lateral support for the passenger's neck in the deployed position.
12. The method of claim 11 , further comprising pivoting a second wing of the pair of wings from a stowed position to a deployed position relative to the adjacent lateral end of the connecting member, wherein the second wing is configured to provide lateral support for the passenger's neck in the deployed position.
13. The method of claim 11 , wherein each wing of the pair of wings independently rotates relative to the adjacent lateral end of the connecting member.
14. The method of claim 11 , wherein the pair of wings are pivotally coupled to the opposing lateral ends of the connecting member via friction hinges.
15. The method of claim 11 , wherein each wing pivots up to 90 degrees from the stowed position to the deployed position relative to the adjacent lateral end of the connecting member.