Inertial breakover mechanism
There is provided a seat break over device. The seat break over device features linkage members that connect the seat back to the quadrant arm. In the static condition, the linkage member acts as a rigid member, constraining rotation of the seat back relative to the quadrant arm. Upon impact of a certain inertial force, the linkage member interacts with a weighted member. The weighted member may include a suspended weight or mass that pivots about a horizontal axis. During a gravity load of a certain amount (e.g., a 16 g event), inertial loads act on the weighted member/hammer, which transfers a force onto the linkage member. This force moves the linkage member into an unstable mode, allowing forward rotation of the seat back with respect to the quadrant arm.
1. A seat break over device, comprising:
a linkage member comprising first and second arms configured to hinge with respect one another; the first arm secured to a seat back and the second arm secured to a stable quadrant arm of a seat assembly;
a weighted member configured to move upon application of an identified force load;
wherein movement of the weighted member causes hinged movement of the linkage member,
wherein hinged movement of the linkage member causes movement of the seat back with respect to the stable quadrant arm.
2. The device of claim 1 , wherein the weighted member comprises a push arm and a roller.
3. The device of claim 1 , wherein the weighted member comprises one or more disk weight members.
4. The device of claim 1 , wherein the seat back comprises an extension and wherein the weighted member pivotably cooperates with the extension.
5. The device of claim 1 , wherein the linkage member comprises a hinge between the first arm and the second arm.
6. The device of claim 1 , further comprising an extension spring extending between the first arm and the second arm.
7. The device of claim 1 , further comprising a support bar for securing the linkage member to the seat back and the stable quadrant arm.
8. The device of claim 1 , further comprising a securement plate and an intermediate bracket securing the first arm of the linkage member to the seat back assembly.
9. The device of claim 1 , further comprising a lower securement feature securing the second arm of the linkage member to the stable quadrant arm.
10. The device of claim 1 , wherein the first arm and the second arm comprise profiles that interface with one another when the linkage member is in a stable configuration.
11. A seat back assembly, comprising:
a seat back assembly comprising first and second ends, the seat back assembly configured to be pivotally mounted with respect to a quadrant arm;
a break over device, comprising first and second linkage members positioned at or near first and second ends of the seat back assembly;
each linkage member comprising first and second arms, the first arm secured to the seat back assembly, the second arm secured to the quadrant arm;
a pivot point between the first and second arms;
a weighted member configured to move upon application of an identified force load;
wherein movement of the weighted member causes hinged movement of the linkage member at the pivot point,
wherein hinged movement of each of the first and second linkage members causes hinged movement of the seat back with respect to the quadrant arm.
12. The seat back assembly of claim 11 , wherein the weighted member comprises a push arm and a roller.
13. The seat back assembly of claim 11 , wherein the weighted member comprises one or more disk weight members.
14. The seat back assembly of claim 11 , wherein the seat back comprises an extension and wherein the weighted member pivotably cooperates with the extension.
15. The seat back assembly of claim 11 , further comprising a support bar for securing each linkage member to the seat back and the stable quadrant arm.
16. The seat back assembly of claim 11 , further comprising a securement plate and an intermediate bracket securing the first arm of each linkage member to the seat back assembly.
17. The seat back assembly of claim 11 , further comprising a lower securement feature securing the second arm of the linkage member to the stable quadrant arm.
18. The device of claim 11 , wherein the first arm and the second arm comprise profiles that interface with one another when the linkage member is in a stable configuration.
19. A method for causing seat break over upon application of a specified force, comprising:
providing a seat back assembly pivotally mounted with respect to a quadrant arm;
providing a break over device comprising first and second linkage members positioned at or near first and second ends of the seat back assembly, the first and second linkage members comprising hinged arms; and a weighted member configured to move upon application of an identified force load;
wherein movement of the weighted member causes hinged movement of the hinged arms of the linkage member; and
wherein hinged movement of each of the first and second linkage members causes hinged movement of the seat back with respect to the quadrant arm.
20. A seat break over device, comprising:
a first gear member associated with a gear housing secured to a seat back and a weighted member that articulates with respect to the seat back;
a second gear member associated with a link and a support bar secured to a stable quadrant arm;
the weighted member configured to move upon application of an identified force load;
wherein movement of the weighted member causes geared movement between the first and second gears which causes hinged movement between the gear housing and the link, creating movement of the seat back with respect to the stable quadrant arm.