Retractable passenger seat

1. A passenger seat assembly comprising:

(a) an overhead support structure comprising a first pivot location and a second pivot location;

(b) a first seat comprising a first seat back support pivotally coupled to the first pivot location in a forward-facing direction; and

(c) a second seat comprising a second seat back support pivotally coupled to the second pivot location in an aft-facing direction;

wherein the first pivot location is longitudinally offset from the second pivot location by an amount that is approximately the same as a length of the first seat back support or the second seat back support and is laterally offset from the second pivot location by an amount that is approximately the same as a width of the first seat back support or the second seat back support so that the first seat and the second seat each comprises a retracted position adjacent the overhead support structure and a deployed position facing in a direction of the other seat,

wherein the first seat and the second seat each rotate between the retracted position and the deployed position independently from the other seat.

2. The passenger seat assembly of claim 1 , wherein at least one of the first seat back support and the second seat back support comprises a recess configured to receive a seat back, wherein sides of the recess surround at least a portion of the seat back when the seat back is in a reclined position.

3. The passenger seat assembly of claim 2 , wherein the recess comprises speakers.

4. The passenger seat assembly of claim 2 , further comprising a tray table that is configured to stow in a location adjacent a portion of an outer profile of the recess.

5. The passenger seat assembly of claim 1 , further comprising a passenger belt, wherein the passenger belt comprises a pair of straps, wherein each strap is coupled to a mounting structure within a seat pan pivotally coupled to at least one of the first and second seat back supports and extends through an aperture in the seat pan.

6. The passenger seat assembly of claim 5 , wherein an end of each of the pair of straps is coupled to a latching projection or a latching receptacle, wherein the latching projection and the latching receptacle are configured not to fit within the aperture so that the end of the strap remains outside the seat pan when the strap is in a retracted position within the seat pan.

7. The passenger seat assembly of claim 1 , further comprising arm rests, each arm rest having a stowed position that is configured to be positioned approximately flush with a seat pan pivotally coupled to at least one of the first and second seat back supports.

8. The passenger seat assembly of claim 1 , further comprising a stowage compartment positioned adjacent at least one of the first and second seat back supports and coupled to a lower support structure.

9. The passenger seat assembly of claim 1 , further comprising an in-flight entertainment display positioned in a rear surface of at least one of the first and second seat back supports.

10. The passenger seat assembly of claim 1 , further comprising a foot rest support pivotally coupled to a seat pan, wherein the seat pan is pivotally coupled to at least one of the first and second seat back supports.

11. The passenger seat assembly of claim 10 , further comprising a foot rest pivotally coupled to the at least one-foot rest support and configured to rotate between a stowed position and a deployed position.

12. A passenger seat assembly comprising:

(a) an overhead support structure comprising a first pivot location and a second pivot location;

(b) a first seat comprising a first seat back support pivotally coupled to the first pivot location in a forward-facing direction; and

(c) a second seat comprising a second seat back support pivotally coupled to the second pivot location in an aft-facing direction;

wherein the first pivot location is longitudinally and laterally offset from the second pivot location, wherein the magnitude of the longitudinal offset between the first pivot location and the second pivot location is approximately the same as a length of the first seat back support or the second seat back support, so that the first seat and the second seat each comprises a refracted position adjacent the overhead support structure and a deployed position facing in a direction of the other seat,

wherein the first seat and the second seat each rotate between the retracted position and the deployed position independently from the other seat.

13. The passenger seat assembly of claim 12 , wherein at least one of the first and second seat back supports is pivotally coupled to a seat pan.

14. The passenger seat assembly of claim 13 , wherein the seat pan is pivotally coupled to a foot rest support.

15. The passenger seat assembly of claim 14 , wherein the foot rest support is configured to rotate into a retracted position adjacent the seat pan.

16. The passenger seat assembly of claim 15 , wherein the seat pan is configured to rotate into a retracted position adjacent the at least one first and second seat back supports.

17. A method of stowing a passenger seat assembly, the passenger seat assembly comprising (i) an overhead support structure comprising a first pivot location and a second pivot location; (ii) a first seat comprising a first seat back support pivotally coupled to the first pivot location in a forward-facing direction; and (iii) a second seat comprising a second seat back support pivotally coupled to the second pivot location in an aft-facing direction, wherein the first pivot location is longitudinally and laterally offset from the second pivot location, wherein the magnitude of the longitudinal offset between the first pivot location and the second pivot location is approximately the same as a length of the first seat back support or the second seat back support, the method comprising:

(a) rotating the first seat into a retracted position adjacent the overhead support structure; and

(b) independently rotating the second seat into a retracted position adjacent the overhead support structure.

18. The method of claim 17 , further comprising:

(c) rotating the first seat into a deployed position, wherein the first seat faces in a direction of the second seat; and

(d) independently rotating the second seat into a deployed position, wherein the second seat faces in a direction of the first seat.

19. The method of claim 17 , further comprising:

(c) unlocking the first seat prior to rotating into the retracted position; and

(d) unlocking the second seat prior to rotating into the retracted position.