Load-limiting seat

• US 5,730,492 A
• Filed: 02/09/1996
• Issued: 03/24/1998
• Est. Priority Date: 02/09/1996
• Status: Expired due to Term

• Current Assignee: Weber Aircraft LP (Safran SA)
• Original Assignee: BAE Systems Simula, Inc. (Safariland LLC)
• Inventors: Yuhas, James, Warrick, James C., Lou, Ken-An, Yaniv, Gershon
• Primary Examiner(s): Nelson, Jr., Milton
• Application Number:
  US08/598,927
• Time in Patent Office: 774 Days
• Field of Search: 297/216.1, 297/216.16, 297/216.19, 297/216.2, 297/232, 297/325, 297/326, 297/331, 297/335, 297/248, 248/501, 248/502, 248/503.1, 248/188.1, 248/188.8, 244/122 R, 244/118.5, 244/118.6
• US Class Current: 297/216.2
• CPC Class Codes: B60N 2/4221 due to impact coming from the front
• CPC Class Codes: B60N 2/42736 of the whole seat
• CPC Class Codes: B64D 25/04 Seat modifications

Abstract

A leg assembly for mounting passenger seats in transport vehicles especially configured to absorb energy, in the event of a survivable crash or other sudden deceleration. The seat legs deform in a controlled manner to prevent loads at its floor attachment points from exceeding the magnitude of allowable floor strength. The leg assembly includes a base member whose forward and rear ends attach to the floor, and a V-leg whose lower vertex pivots about an axis passing through the front of the base member in the event of a forward crash. The V-leg has a vertical member and a diagonal member. A load-limiting strut connects the rear end of the base member to an intermediate area on the diagonal member of the V-leg. A tension link connects the intermediate area of the V-leg and to the upper end of the vertical member of the V-leg. Elongation of the load-limiting strut allows the seat and legs to pitch forward at a predetermined inertial loading which, if exceeded substantially, would rip the seat loose from the floor. The tension link elongates at a predetermined load to distribute the loads within the seat.

Claims

1. A seat for a passenger vehicle comprising:

(a) a base member having a rear end and a forward end;

(b) a V-leg having a vertex, a vertical member and a diagonal member, said vertical member extending vertically up from the vertex of the V-leg, and said diagonal member extending rearwards diagonally up from the vertex of the V-leg, wherein the diagonal member has a central region and a top end, and wherein the vertical member has a top end;

(c) a load-limiting strut attached at its bottom end to rear end of the base member and attached at its top end to the central region of the diagonal member;

(d) a tension link attached at its top end to the top end of the vertical member and at its bottom end to the central region of the diagonal member; and

(e) a pivot bolt pivotally connecting the vertex of the V-leg to the forward end of the base member.

2. The seat of claim 1, wherein the load-limiting strut is an energy-absorbing strut which absorbs energy by elongating in the event of a forward crash.

3. The seat of claim 1, wherein the load-limiting strut comprises a tubular member and a die, and wherein the load-limiting strut is designed to absorb energy in the event that it is placed under a tensile load exceeding a predetermined value by pulling the tubular member through the die, constricting the tubular member to a smaller diameter.

4. The seat of claim 3, wherein the tubular member is cylindrical.

5. The seat of claim 4, wherein the tubular member comprises an end having an enlarged diameter, such that the end of the tubular member cannot be drawn through the die.

6. The seat of claim 3, wherein the tubular member is tapered.

7. The seat of claim 6, wherein the tubular member comprises an end having an enlarged diameter, such that the end of the tubular member cannot be drawn through the die.

8. The seat of claim 5 or claim 7, wherein the die includes means to allow the tubular member to slide back into load-limiting strut after the load-limiting strut is no longer under the tensile load.

9. The seat of claim 8, wherein the tension link is fabricated from aluminum.

10. The seat of claim 9, wherein the tension link is fabricated from wrought aluminum.

11. The seat of claim 9, wherein the tension link comprises a channel extending along a greater length of the tension link.

12. The seat of claim 1, wherein the dimensions of the tension link are selected such that the tension link stretches at a load equal approximately two-thirds of the limiting load of the load-limiting strut.

13. The seat of claim 1, wherein the seat comprises a seat pan having a front stretcher beam and a rear stretcher beam, and wherein the top end of the vertical member of the V-leg is attached to the front stretcher beam and the top end of the diagonal member of the V-leg is attached to the rear stretcher beam.

14. The seat of claim 1, wherein the ends of the load-limiting strut are configured to deform under loads from floor warpage.

15. The seat of claim 1, wherein the pivot bolt connects the base member to the vertex of the V-leg through an almost spherical bearing installed in the forward end of the base member, said almost spherical bearing being a spherical ball with a flat circumferential band.

16. A leg assembly for a passenger vehicle seat comprising:

(a) a base member having a rear end and a forward end;

(b) a V-leg having a vertex, a vertical member and a diagonal member, said vertical member extending vertically up from the vertex of the V-leg, and said diagonal member extending rearwards diagonally up from the vertex of the V-leg, wherein the diagonal member has a central region and a top end, and wherein the vertical member has a top end;

(c) a load-limiting strut having a deformable top end and a deformable bottom end attached at its bottom end to the rear end of the base member by a lateral bolt and attached at its top end to the central region of the diagonal member;

(d) a tension link attached at its top end to the top end of the vertical member and at its bottom end to the central region of the diagonal member;

(e) a pivot bolt pivotally connecting the vertex of the V-leg to the forward end of the base member;

(f) two rear studs extending down from the rear end of the base member on either side of the lateral bolt; and

(g) a front stud extending down from the front end of the base member below the pivot bolt.

17. The leg assembly of claim 16, wherein the heads of the front and rear studs are circular discs dimensioned to fit into vehicle floor tracks having an inverted T-slot cross-section.

18. The leg assembly of claim 16, wherein the load-limiting strut comprises a tubular member and a die, and wherein the load-limiting strut is designed to absorb energy if placed under a tensile load exceeding a predetermined value by pulling the tubular member through the die, constricting the tubular member to a smaller diameter.

19. The leg assembly of claim 18, wherein the tubular member comprises an end having an enlarged diameter, such that the end of the tubular member cannot be drawn through the die.

20. The leg assembly of claim 18, wherein the die is configured to allow the tubular member to slide back into the load-limiting strut after the load-limiting strut is no longer under the tensile load.

21. The leg assembly of claim 18, wherein the tension link is fabricated from aluminum.

22. The leg assembly of claim 21, wherein the tension link comprises a channel extending along the greater length of the tension link.

23. The leg assembly of claim 22, wherein the dimensions of the tension link are selected such that the tension link stretches at a load equal to approximately two-thirds of the limiting load of the load-limiting strut.

24. The leg assembly of claim 18, wherein the die is a lightweight ring, and wherein the load-limiting strut further comprises a cone-shaped die holder.

25. The leg assembly of claim 18, wherein the load-limiting strut is designed to retract back towards its original length, after it has been subjected to a tensile load and after it is no longer subjected to a tensile load, when a compressive load is applied to the load-limiting strut.

26. The leg assembly of claim 16, wherein the leg assembly is configured to reduce floor reaction to a forward load from a 16 g dynamic forward load to a 9 g static forward load.

27. The leg assembly of claim 26, wherein the load-limiting strut comprises a tubular member and a die, and wherein the load-limiting strut is designed to absorb energy if placed under a tensile load exceeding a predetermined value by pulling the tubular member through the die, constricting the tubular member to a smaller diameter.

28. The leg assembly of claim 27, wherein the tubular member comprises an end having an enlarged diameter, such that the end of the tubular member cannot be drawn through the die.

29. The leg assembly of claim 27, wherein the die is configured to allow the tubular member to slide back into the load-limiting strut after the load-limiting strut is no longer under the tensile load.

30. The leg assembly of claim 26, wherein the dimensions of the tension link are selected such that the tension link stretches at a load equal to approximately two-thirds of the limiting load of the load-limiting strut.

31. A seat assembly for a passenger vehicle comprising:

(a) a plurality of upper seat portions, comprising longitudinal members, a front stretcher, a rear stretcher and a seat pan, said seat pan being attached to the front stretcher at its front end and to the rear stretcher at its rear end;

(b) a plurality of base members, each base member having a rear end and a forward end, and each base member corresponding to one of the plurality of upper seat portions;

(c) a plurality of V-legs, each V-leg corresponding to one of the plurality of upper seat portions and having a vertex, a vertical member and a diagonal member, said vertical member extending vertically up from the vertex of the V-leg, and said diagonal member extending rearwards diagonally up from the vertex of the V-leg, wherein the diagonal member has a central region and a top end, wherein the vertical member has a top end, and wherein the top end of the diagonal member is attached to the rear stretcher and the top end of the vertical member is attached to the front stretcher;

(d) a plurality of load-limiting struts, each load-limiting strut corresponding to one of the plurality of upper seat portions, each load-limiting strut being attached at its bottom end to the rear end of the base member and attached at its top end to the central region of the diagonal member;

(e) a plurality of tension links, each tension link corresponding to one of the V-legs, each tension link being attached at its top end to the top end of the corresponding vertical member and at its bottom end to the central region of the corresponding diagonal member; and

(f) a plurality of pivot bolts, wherein each pivot bolt pivotally connects the vertex of each V-leg to the forward end of the corresponding base member.

32. The seat assembly of claim 31, wherein each load-limiting strut comprises a tubular member and a die, and wherein the load-limiting strut is designed to absorb energy in the event that it is placed under a tensile load exceeding a predetermined value by pulling the tubular member through the die, constricting the tubular member to a smaller diameter.

33. The seat assembly of claim 32, wherein each tubular member comprises an end having an enlarged diameter, such that the end of the tubular member cannot be drawn through the die.

34. The seat assembly of claim 32, wherein the die is configured to allow the tubular member to slide back into the load-limiting strut after the load-limiting strut is no longer under the tensile load.

35. The seat assembly of claim 32, wherein the die is a lightweight ring, and wherein the load-limiting strut further comprises a cone-shaped die holder designed to support the die as the tubular member is drawn through the die.

36. The seat assembly of claim 31, wherein the tension link comprises a channel extending along a greater length of the tension link.

37. The seat assembly of claim 31, wherein the dimensions of the tension link are selected such that the tension link stretches at a load equal to approximately two-thirds of the limiting load of the load-limiting strut.

38. The seat assembly of claim 31, wherein the ends of the load-limiting struts are configured to deform under loads from floor warpage.

39. The seat assembly of claim 31, further comprising two mushroom-shaped rear studs extending downwardly from the rear end of each base member, and one mushroom-shaped stud extending downwardly from the front end of each base member.

40. The seat assembly of claim 31, wherein each pivot bolt connects the base member to the vertex of the V-leg corresponding to that base member through an almost spherical bearing installed in the forward end of the base member, said almost spherical bearing being a spherical ball with a flat circumferential band.

41. A leg assembly for a vehicle seat comprising:

(a) a base member having a rear end and a forward end;

(b) a V-leg having a vertex, a vertical member and a diagonal member, said vertical member extending vertically up from the vertex of the V-leg, and said diagonal member extending rearwards diagonally up from the vertex of the V-leg, wherein the diagonal member has a central region and a top end, and wherein the vertical member has a top end;

(c) a load-limiting strut attached at its bottom end to the rear end of the base member and attached at its top end to the central region of the diagonal member;

(d) a pivot bolt pivotally connecting the vertex of the V-leg to the forward end of the base member;

(e) two rear studs extending down from the rear end of the base member on either side of a lateral bolt; and

(f) a front stud extending down from the front end of the base member below the pivot bolt,

wherein the load-limiting strut provides the only vertical force applied to the rear studs as the leg assembly pivots forward around the pivot bolt.

42. The leg assembly of claim 41, wherein the load-limiting strut comprises a tubular member and a die, and wherein the load-limiting strut is designed to absorb energy if placed under a tensile load exceeding a predetermined value by pulling the tubular member through the die, constricting the tubular member to a smaller diameter.

43. The leg assembly of claim 42, wherein the tubular member comprises an end having an enlarged diameter, such that the end of the tubular member cannot be drawn through the die.

44. The leg assembly of claim 42, wherein the die is configured to allow the tubular member to slide back into the load-limiting strut after the load-limiting strut is no longer under the tensile load.

45. The leg assembly of claim 41, further comprising a tension link attached at its top end to the top end of the vertical member, and at its bottom end to the central region of the diagonal member.

46. The leg assembly of claim 45, wherein the tension link is fabricated from aluminum.

47. The leg assembly of claim 45, wherein the tension link comprises a channel extending along a greater length of the tension link.

48. The leg assembly of claim 45, wherein the dimensions of the tension link are selected such that the tension link stretches at a load equal to approximately two-thirds of the limiting load of the load-limiting strut.

49. The leg assembly of claim 41, wherein the load-limiting strut comprises a structural member and a die, and wherein the load-limiting strut is designed to absorb energy if placed under a tensile load exceeding a predetermined value by extruding the structural member through the die, reducing the outer dimension of the structural member.

50. The leg assembly of claim 41, wherein the load-limiting strut is designed to retract back towards its original length, after it has been subjected to a tensile load and after it is no longer subjected to a tensile load, when a compressive load is applied to the load-limiting strut.

51. The leg assembly of claim 41, wherein the leg assembly is configured to reduce floor reaction to a forward load from a 16 g dynamic forward load to a 9 g static forward load.