Aircraft table system with rolling sled member

1. An aircraft table system, comprising:

a table member configured to move reversibly from an at least partially undeployed position to an at least partially deployed position;

a sled member coupled to the table member;

one or more rollers coupled to the sled member;

one or more guide rails,

wherein at least one of the one or more rollers is configured to roll along at least one of the one or more guide rails such as to allow relative translating motion between the sled member and at least one of the one or more guide rails; and

a spine member comprising one or more holes;

one or more bolts carried by the sled member;

one or more cables;

wherein at least a portion of at least one of the one or more cables is coupled between at least one of the bolts and the table member; and

wherein the at least one bolt is sized and located such that when the table member is adjusted to the at least partially deployed position, the at least one bolt is received by at least one of the one or more holes of the spine member such that the sled member and the table member are at least partially supported by the spine member on the at least one bolt, wherein engagement of the at least one bolt with the spine member in the hole of the spine member inhibits the sled member from moving relative to the spine member, and

wherein at least a portion of at least one of the one or more cables is coupled between the table member and the at least one bolt such that, when the table member is adjusted to the at least partially undeployed position, the at least one bolt is drawn out engagement in the at least one hole of the spine member, wherein removal of the bolt from engagement in the at least one hole of the spine member frees the sled member to move relative to the spine member.

2. The system of claim 1 , wherein the at least partially deployed position is substantially horizontal.

3. The system of claim 1 , further comprising a spine member, wherein the spine member comprises at least one pair of guide rails.

4. The system of claim 1 , wherein the table member is pivotally coupled to the sled member.

5. The system of claim 1 , wherein the table member is directly connected to the sled member.

6. The system of claim 1 , further comprising one or more hinges configured to pivotally couple the table member to the sled member, wherein at least one of the one or more hinges is a quick disconnect hinge comprising a male component and a female component.

7. The system of claim 1 , further comprising one or more hinges configured to pivotally couple the table member to the sled member, wherein the length of at least one of the one or more hinges is at least about one inch.

8. The system of claim 1 , further comprising a plurality of rollers, wherein the plurality of rollers comprises one or more sets of rollers.

9. The system of claim 8 , wherein at least one of the one or more sets of rollers comprises:

at least one roller configured to roll along a front surface of at least one of the guide rails; and

at least one roller configured to roll along a back surface of the at least one guide rail.

10. The system of claim 8 , wherein the at least one set of the one or more sets of rollers is configured support the load of the sled member and the table member.

11. The system of claim 8 , wherein at least one set of the one or more sets of rollers comprises at least one roller configured to roll along an edge surface of at least one of the guide rails.

12. The system of claim 8 , wherein the one or more sets of rollers comprise at least one upper set of rollers configured to roll on one portion of at least one of the guide rails and at least one lower set of rollers configured to roll on another portion of the at least one guide rail.

13. The system of claim 1 , further comprising:

a spine member coupled to and supporting at least one of the one or more rails;

one or more spring reel elements rotatably coupled to the sled member;

one or more cables, wherein at least one of the cables comprises a portion coupled to the spine member and at least one other portion coupled to at least one of the spring reel elements.

14. An aircraft table system, comprising:

a table member configured to move reversibly from an at least partially undeployed position to an at least partially deployed position;

a sled member coupled to the table member;

a plurality of rollers coupled to the sled member;

one or more pairs of guide rails configured to mount to a structure in an aircraft;

wherein the at least one roller is configured to roll along the guide rails such as to allow relative translating motion between the sled member and the at least one pair of guide rails,

a spine member comprising one or more holes;

two or more bolts carried by the sled member;

two or more cables;

wherein at least a portion of at least first one of the one or more cables is coupled between at least a first one of the bolts and the table member, wherein at least a portion of at least second one of the one or more cables is coupled between at least second one of the bolts and the table member; and

wherein at least one of the bolts is sized and located such that when the table member is adjusted to the at least partially deployed position, the at least one bolt is received by at least one of the one or more holes of the spine member such that the sled member and the table member are at least partially supported by the spine member on the at least one bolt, wherein engagement of the at least one bolt with the spine member in the hole of the spine member inhibits the sled member from moving relative to the spine member, and

wherein at least a portion of at least one of the one or more cables is coupled between the table member and the at least one bolt such that, when the table member is adjusted to the at least partially undeployed position, the at least one bolt is drawn out engagement in the at least one hole of the spine member, wherein removal of the bolt from engagement in the at least one hole of the spine member frees the sled member to move relative to the spine member.

15. The system of claim 14 , wherein, for at least one pair of the guide rails, one guide rail of the pair is substantially opposed to the other guide rail of the pair.

16. The system of claim 14 , wherein at least one of the two or more sets of rollers is configured to support the load of the sled member.

17. The system of claim 14 , wherein at least one of the two or more sets of rollers is configured to stabilize the sled member while the sled member is in relative motion.

18. The system of claim 14 , wherein the at least partially deployed position is substantially horizontal.