Seat system having a rotary recline lever
A seat system for a passenger aircraft. The seat system includes a passenger seat frame having a backrest support assembly including a backrest and a spreader; and a seat bottom support assembly. The seat system further includes a rotary recline lever assembly including an armrest connected to the spreader; an offset rotary actuator positioned within the armrest; and a release cable attached between the rotary actuator and the backrest support assembly. The seat system may further include a seat back tray table attached to the back of the passenger seat frame.
1. A seat system for a passenger aircraft, said seat system comprising:
(a) a passenger seat frame having
(i) a backrest support assembly including a backrest and a spreader; and
(ii) a seat bottom support assembly; and
(b) a rotary recline lever assembly including
(i) an armrest connected to said spreader;
(ii) a rotary actuator positioned within said armrest, wherein said rotary actuator includes a bushing having a contact surface of between about 25% and about 75% with respect to a shaft of rotation to provide a reduced force requirement; and
(iii) a release cable attached between said rotary actuator and said backrest support assembly.
2. The seat system according to claim 1 , including a seat back tray table attached to the back of said passenger seat frame.
3. The seat system according to claim 2 , wherein said seat back tray table attached to the back of said passenger seat frame is movable between a first storage position and a second deployed position.
4. The seat system according to claim 3 , including a lock mechanism attached to the back of said passenger seat frame for retaining said seat back tray table in a secured position.
5. The seat system according to claim 1 , including a display is adjoined by the back of said passenger seat frame.
6. The seat system according to claim 1 , including a backrest cushion attached to the backrest support assembly and a headrest.
7. In a seat system for a passenger aircraft wherein the seat system includes a passenger seat frame having (i) a backrest support assembly including a backrest and a spreader and (ii) a seat bottom support assembly, the improvement comprising a rotary recline lever assembly, said rotary recline lever assembly comprising:
(a) an armrest connected to said spreader;
(b) an offset rotary actuator positioned within said armrest, wherein said rotary actuator includes a low friction, square wave bushing having a contact surface of between about 25% and about 75% with respect to a shaft of rotation; and
(c) a release cable attached between said rotary actuator and said backrest support assembly.
8. The rotary recline lever assembly according to claim 7 , wherein said armrest includes a lower body and an arm cap.
9. The rotary recline lever assembly of claim 8 , wherein the lower portion of said arm cap interlocks with the upper portion of said lower body.
10. The rotary recline lever assembly of claim 9 , wherein the said arm cap is removably attached to the upper portion of said lower body by a fastener.
11. The rotary recline lever assembly according to claim 7 , wherein said rotary actuator is offset to provide a mechanical advantage to the user.
12. The rotary recline lever assembly according to claim 7 , wherein said rotary actuator further includes a pair of curved tabs to retain the proximate end of said release cable when said rotary actuator is operated by the user.
13. The rotary recline lever assembly according to claim 12 , wherein said rotary actuator further includes a grooved slot adjacent to said pair of curved tabs to receive said release cable for crimped end movement to reduce side friction of said cable with its conduit when said rotary actuator is operated by the user.
14. The rotary recline lever assembly according to claim 12 wherein said rotary actuator further includes at least one mechanical stop to prevent over backwards rotation of said rotary actuator when the actuator is released by the user.
15. The rotary recline lever assembly according to claim 7 , wherein said release cable further includes an outer protective jacket and a crimp on the proximate end of said release cable for engagement with said rotary actuator.
16. A seat system for a passenger aircraft, said seat system comprising:
(a) a passenger seat frame having
(i) a backrest support assembly including a backrest and a spreader; and
(ii) a seat bottom support assembly;
(b) a rotary recline lever assembly including
(i) an armrest connected to said spreader;
(ii) an offset rotary actuator positioned within said armrest; and
(iii) a release cable attached between said rotary actuator and said backrest support assembly; and
(c) a seat back tray table attached to the back of said passenger seat frame, and wherein said rotary actuator includes a low friction bushing having a contact surface of between about 25% and about 75% with respect to a shaft of rotation to provide a reduced force requirement to said user.
17. The seat system according to claim 16 , including a seat back tray table attached to the back of said passenger seat frame, and a lock mechanism attached to the back of said passenger seat frame for retaining said seat back tray table in a secured position.