Control structure

Abstract

A control structure device for racks or buildings. The device is able to limit forces developed within itself or a structure (e.g. building or storage rack) it connects with and is seismically supportive of as it endures ground or base motion input from a seismic event. The control structure may comprise a relatively inflexible rocker frame which is pivotably connected to a foundation. Rotation of the rocker frame causes a flexural member to flexurally displace to limit force and energy in the system.

Claims

1. A force limiting and energy dissipating seismic control structure comprising: a pivotable rocker frame having a pivot connection to a structural member; a yield connector comprising a resistively and resiliently deformable, elastoplastically yielding yield element, the yield connector being directly or indirectly connected between the rocker frame and the structural member wherein the yield connector comprises a first anchor for direct or indirect connection to a first end region of the yield element, and a second anchor for direct or indirect connection to a second end region of the yield element, and wherein the second anchor and second end region are configured with at least one of a free translational boundary condition or a free translational and rotational boundary condition wherein the second end region is able to translate or translate and rotate relative to a reaction surface or reaction point at the second anchor, whereby the yield connector is able to elastoplastically displace while maintaining a constant resistive yield force, and control and limit a dynamic response of the control structure and a mass seismically supported by the control structure, during a seismic event.

2. The force limiting and energy dissipating seismic control structure of claim 1 wherein the structural member comprises a structural base or foundation, and the yield connector is directly connected between the rocker frame and the structural base or foundation.

3. The force limiting and energy dissipating seismic control structure of claim 1 wherein the structural member comprises a structural base or foundation, and the yield connector is connected between the rocker frame and a further structural member, the further structural member being pivotably connected to the structural base or foundation.

4. The force limiting and energy dissipating seismic control structure of claim 3 wherein the further structural member comprises a chord.

5. The force limiting and energy dissipating seismic control structure of claim 1 wherein the structural member is pivotably connected to a structural base or foundation.

6. The force limiting and energy dissipating seismic control structure of claim 1 further comprising a secondary flexural member provided between the yield connector and the structural member.

7. The force limiting and energy dissipating seismic control structure of claim 1 wherein the yield connector further comprises a flexural deflection limiter configured to stop flexure of a yielding element at a prescribed limit.

8. The force limiting and energy dissipating seismic control structure of claim 7 further comprising a secondary flexural member configured to yield upon the prescribed limit being reached.

9. The force limiting and energy dissipating seismic control structure of claim 1 wherein the yield connector comprises a pivot connector to connect to either the rocker frame or the structural member.

10. The force limiting and energy dissipating seismic control structure of claim 1 wherein the yield connector comprises a guide configured to receive and guide a connector configured to connect to either the rocker frame or the structural member.

11. The force limiting and energy dissipating seismic control structure of claim 10 wherein the yield connector comprises a pivot connector to connect to either the rocker frame or the structural member and the pivot connector is configured to maintain the connector orthogonal to the yield element.

12. The force limiting and energy dissipating seismic control structure of claim 10 wherein the connector comprises a part of one of: the structural member; the rocker frame; a further structural member.

13. The force limiting and energy dissipating seismic control structure of claim 1 wherein the yield element comprises a plate or a plurality of plates.

14. The force limiting and energy dissipating seismic control structure of claim 1 wherein the first anchor is configured for connection to the rocker frame and a second anchor for connection to the structural member.

15. The force limiting and energy dissipating seismic control structure of claim 1 wherein the yield element is displaced and increases in length between the first and second anchors during a seismic event.

16. The force limiting and energy dissipating seismic control structure of claim 15 wherein no membrane forces are generated in the yield element during displacement.

17. The force limiting and energy dissipating seismic control structure of claim 1 wherein the yield element undergoes plastic deformation at a yield zone intermediate the first anchor and second anchor during a seismic event as a result of relative oscillatory movement between the rocker frame and the structural member.

18. The force limiting and energy dissipating seismic control structure of claim 1 wherein the rocker frame comprises a vertical aspect and the structural member comprises a horizontal structural base or foundation.

19. The force limiting and energy dissipating seismic control structure of claim 1 wherein the rocker frame has a horizontal aspect and is pivotably connected at each end to vertical chords which are pivotably connected to a horizontal base or foundation.

20. The force limiting and energy dissipating seismic control structure of claim 1 wherein the rocker frame comprises part of, or is connected to, a shelving or racking or building structure.

21. A force limiting and energy dissipating seismic control structure comprising: a pivotable rocker frame having a pivot connection to a structural member and being configured to be connected to a shelving, racking or building structure, the pivotable rocker frame being configured to rotate about the pivot connection as the shelving, racking or building structure moves relative to the structural member in response to a seismic event, a yield connector comprising a resistively and resiliently deformable, elastoplastically yielding yield element, wherein the yield connector comprises a first anchor for direct or indirect connection to the rocker frame distal from the pivot connection and a second anchor for direct or indirect connection to the structural member, and wherein one of the first or second anchors is configured with a free translational and rotational boundary condition whereby the yield element is displaced and undergoes plastic deformation at a yield zone intermediate the first anchor and second anchor during a seismic event as a result of relative oscillatory movement between the rocker frame and the structural member, and wherein the yield connector maintains a constant resistive yield force to thereby control rotation of the rocker frame about the pivot connection, the constant resistive yield force limiting and controlling the magnitude of a dynamic response force developed within the control structure during the seismic event.

22. The force limiting and energy dissipating seismic control structure of claim 21 wherein the dynamic response force is independent of the magnitude of the seismic event.

23. A structure supported on a foundation, the structure comprising: a framework, the framework being connected to a pivotable rocker frame having a pivot connection to the foundation and being configured to rotate about the pivot connection as the framework moves relative to the structural member in response to a seismic event, a yield connector comprising a resistively and resiliently deformable, elastoplastically yielding yield element, and wherein the yield connector comprises a first anchor for direct or indirect connection to the rocker frame distal from the pivot connection and a second anchor for direct or indirect connection to the foundation, and wherein one of the first or second anchors is configured with a free translational and rotational boundary condition whereby the yield element is displaced and undergoes plastic deformation at a yield zone intermediate the first anchor and second anchor during a seismic event as a result of relative oscillatory movement between the rocker frame and the foundation, and wherein the yield connector maintains a constant resistive yield force to thereby control rotation of the rocker frame about the pivot connection, the constant resistive yield force limiting and controlling the magnitude of a dynamic response force developed within the framework during the seismic event.

24. The structure of claim 23 wherein a dynamic response force developed in the foundation during the seismic event is limited by the constant resistive yield force.

25. The structure of claim 23 wherein the framework has or supports a mass, and a dynamic response force developed in the mass during the seismic event is limited by the constant resistive yield force.

26. The structure of claim 23 wherein the dynamic response force is independent of the magnitude of the seismic event.

27. A force limiting and energy dissipating seismic control structure comprising: a pivotable rocker frame pivotably connected to a structural member, a yield connector located between and directly or indirectly connecting rocker frame to structural member, the yield connector comprising a resistively and resiliently deformable elastoplastically yielding yield element, the yield element having a first region connected to a first anchor and a second end region connected to a second anchor, the first and second anchor directly or indirectly connecting to the rocker frame or structural member, the yield connector configured with free translational or free translational and free rotational boundary conditions, wherein the second end, edge, or boundary region of the yield element, is able to translate or translate and rotate relative to the reaction surface or reaction point at its second anchor, and without generating membrane forces within the yield element, and wherein the resultant reaction force at the reaction surface or reaction point, is able to rotate as the yield element elastoplastically displaces, and remain orthogonal to the tangent plane at the reaction surface of the yield element, and wherein the horizontal component of the resultant reaction force acts in the same direction as the horizontal translation component of the displacing end region, the yield element able to elastoplastically displace while maintaining a constant resistive yield force, enabling the control structure to form an elastoplastic mechanism, able to cyclically displace and plastically flow, in response to a forcing event or in response to base motion input from a seismic event, with a constant resistive yield force, the seismic control structure able to control and limit its dynamic response and control and limit the response acceleration and dynamic response of a mass it is seismically supportive of.

28. The force limiting and energy dissipating seismic control structure as claimed in claim 1 wherein the yield connector is connected between the rocker frame and a further structural member, the further structural member and rocker frame being pivotably connected to the structural member.

29. The force limiting and energy dissipating seismic control structure as claimed in claim 28 wherein the structural member and further structural member comprise pivotably connected chords.

30. The force limiting and energy dissipating seismic control structure as claimed in claim 6 wherein the secondary flexural member enables independent adjustment of the natural elastic response frequency of the control structure.

31. The force limiting and energy dissipating seismic control structure as claimed in claim 7 further comprising a secondary flexural member, wherein the secondary flexural member and the flexural deflection limiter enable the control structure to provide a two tier, elastic stiffening, ductile response.

32. The force limiting and energy dissipating seismic control structure as claimed in claim 13 wherein the or each plate is configured to flex about a minor bending axis and flexurally yield at a specific yield zone and is displaced to high elastoplastic displacements and high ductility values while maintaining the constant resistive yield force.

33. The force limiting and energy dissipating seismic control structure as claimed in claim 1 wherein the yield element is displaced and freely increases and decreases in length between the first and second anchors during a seismic event.

34. The force limiting and energy dissipating seismic control structure as claimed in claim 33 wherein the length of the yield element along a flexing curve of the yield element is able to freely increase and decrease length between the first and second anchors and wherein reaction resultants rotate and remain orthogonal with a tangent plane of the yield element during a seismic event.

35. The force limiting and energy dissipating seismic control structure as claimed in claim 1, wherein the yield element has a spanning aspect and is configured with simply supported, flexurally continuous or flexurally restrained boundary conditions at the second end region.

36. The force limiting and energy dissipating seismic control structure as claimed in claim 29 wherein the yield connector is connected between the chords and wherein interlaminar displacement along and between the chords is resisted by a constant interlaminar shear force produced by flexural yielding of the yield element.

37. The force limiting and energy dissipating seismic control structure as claimed in claim 1 wherein the yield element is able to cyclically displace to plastic strain values within the yield element along a positive yield plateau and to and beyond plastic strain values at maximum stress values within a strain hardening region of the stress-strain curve of the yielding material from which the yield element is formed.

38. The force limiting and energy dissipating seismic control structure as claimed in claim 14 wherein the yield connector comprises a casing and a guided pushrod, the pushrod linking the yield connector to the rocker frame, and the casing being pivotably connected to the structural member, and wherein the guided pushrod is configured to connect to the yield element at the first anchor, and the casing is configured to connect to the yield element at the second anchor.

39. A force limiting and energy dissipating seismic control structure comprising a rocker frame which is pivotably connected to a structural base or structural member, wherein rotation of the rocker frame about the pivotal connection causes a pivotably anchored flexural yield member which is directly or indirectly connected to the rocker frame, but distal to the rocker frame pivot, to flexurally displace, wherein the yield member is configured with a (i) free translational or (ii) free translational and free rotational boundary condition to allow it to flex and yield about its minor bending axis to high elastoplastic displacements and high ductility values while maintaining a constant resistive yield force, and wherein the structure is able to dissipate energy and limit forces developed within itself or a structure it connects with and is seismically supportive of as it endures ground or base motion input from a seismic event.

40. The force limiting and energy dissipating seismic control structure as claimed in claim 39 wherein the yield member comprises: a first anchor secured directly or indirectly to the rocker frame, a second anchor secured to another structural member of the control structure or to a foundation base, the flexural yield member having a first region and a second region spaced from the first region and located respectively by the first anchor and second anchor, whereby the first anchor secures the first region to the rocker frame so that the first region is able to move with the rocker frame relative to the second region and second structural member being another member of the control structure or foundation base, during a seismic event, and the second anchor allowing translation or translation and rotation of the second region relative to the second anchor during rocking movement of the rocker frame relative to the second structural member allowing the flexural yield member to flexurally yield while maintaining a stable constant resistive yield force.

41. The force limiting and energy dissipating seismic control structure as claimed in claim 40 wherein at the second region the flexural member is able to translate or translate and rotate relative to its respective anchor and at the other of the first or second regions the flexural member is pinned or cantilevered to its respective anchor.

Description

FIGURE DESCRIPTIONS

(1) The invention will now be described by way of example only and with reference to the drawings in which:

(2) FIG. 1: shows a schematic front view of a control structure with inclined tension bracing.

(3) FIG. 1A: shows a schematic front view of a control structure with inclined and horizontaltension bracing.

(4) FIG. 2: shows a schematic front view of a control structure connecting to plan bracing.

(5) FIG. 3: shows a schematic front view of a control structure similar to that of FIG. 2 but with frame in tower form with vertical chords.

(6) FIG. 4A: shows control structures of FIG.s 1-3 within a rack structure or general building structure to which the control structure is seismically supportive.

(7) FIG. 4B: shows an end view of FIG. 4A showing location of control structures of FIG.s 1-3 located intermediate of two storage racks.

(8) FIG. 5A: shows a schematic front view of control structure with frame horizontally oriented and located between two vertical chords.

(9) FIG. 5B: shows displaced form of control structure of FIG. 5A in sway mode.

(10) FIG. 6A: shows a schematic front view of a simply spanning yield connector.

(11) FIG. 6B: shows a schematic front view of FIG. 6A with displaced form of flexing yield plate.

(12) FIG. 6C-6C-1: shows a simply supported plate/beam/

(13) FIG. 6D-6D-1: shows a cantilevered simply supported plated/beam.

(14) FIG. 7A: shows rocker frame pivot anchor to vertical chord connection. FIG. 7B: shows plan cross sectional view of FIG. 7A.

(15) FIG. 8A: shows a schematic front view of control structure of FIG. 3 with yield connectors set within sleeve guide motion-controlled rocker and pin ended push rods connecting yield plates to main rocker frame.

(16) FIG. 8B: shows control structure of FIG. 8A in sway mode.

(17) FIG. 8C: shows control structure of FIG. 3 with yield connectors set within stay motion-controlled rocker and pin ended push rods connecting yield plates to rocker frame.

(18) FIG. 8D: shows control structure of FIG. 8C in sway mode.

(19) FIG. 8E: shows schematic detail of yield plate rocker of FIG. 8A with multipleplates.

(20) FIG. 9A: shows schematic front view of control structure of FIG. 5A with yieldplates set within sleeve guide motion-controlled rockers and pin ended push rods connecting yield plates to main rocker frame.

(21) FIG. 9B: shows control structure of FIG. 9A in sway mode.

(22) FIG. 10A: shows a schematic front view of control structure of FIG. 9A in towerform.

(23) FIG. 10B: shows a schematic detail of sleeve guide motion-controlled yield platerocker of FIG. 10A.

(24) FIG. 10C: shows schematic detail of yield plate rocker of FIG. 10B but with rotation limiter blocks.

(25) FIG. 11A: shows a schematic front view of control structure with two pivot rockerframes located between top and bottom beam with anchor ties.

(26) FIG. 11B: shows a schematic front view of two framing control structures located between top and bottom beam.

(27) FIG. 11C: shows schematic end view of control structure :located at end of racks.

(28) FIG. 12A: shows a schematic view of control structure with inter-lamina shear yield connectors.

(29) FIG. 12B: shows control structure of FIG. 12A in sway mode.

(30) FIG. 13A: shows a front schematic view of the control structure of FIG. 12A horizontally orientated and located between two vertical chords.

(31) FIG. 13B: shows control structure of FIG. 13A in sway mode.

(32) FIG. 14A: shows a simple shear type plate for the control structures of FIGS. 12A and 13A fixed at the frame side and with rotatable and translatable connection to exterior chord at opposite end.

(33) FIG. 14B: shows shear plate of FIG. 14A in displaced form when control structure in sway mode.

(34) FIG. 15A-1: shows a continuous shear type plate fixed at frame side and with tworotatable and translatable supports at opposite connection to exteriorchord.

(35) FIG. 15B-1: shows shear plate of FIG. 14A in displaced form when control structure in sway mode.

(36) FIG. 16A: shows a rotationally restrained shear type plate fixed at frame side and with rotational restraint by rollers but free translation at opposite end connected to exterior chord.

(37) FIG. 16B: shows shear plate of FIG. 16A in displaced form when control structure in sway mode.

(38) FIG. 17: shows shear type connector of FIG. 14A with multiple plates.

(39) FIG. 18A: shows schematic front view of control structure of FIG. 12A inclusive of motion control ties.

(40) FIG. 18B: shows control structure of FIG. 18A in sway mode, inclusive of motioncontrol ties.

(41) FIG. 18C: shows control structure of FIG. 13B inclusive of motion control ties.

(42) FIG. 19A: shows schematic front view of control structure of FIG. 5A with secondary flexure member.

(43) FIG. 19B: shows schematic detail of rocker of FIG. 19A connected to secondaryflexure member.

(44) FIG. 19C: shows schematic detail of control structure in sway mode with inflexible secondary member.

(45) FIG. 19D: shows schematic detail of FIG. 19C with flexing secondary member.

(46) FIG. 19E: shows the force-displacement graph of a bilinear elastic stiffening system.

(47) FIG. 19F: shows a schematic detail of a rocker connected to a secondary flexural member.

(48) FIG. 20A: shows a side view of control structure within rack structure.

(49) FIG. 20B: shows plan view of FIG. 20A.

(50) FIG. 21A: shows a schematic view of control structure of finite dimensions withtension bracing yield connectors of FIG. 6A and base member.

(51) FIG. 21B: shows displaced form of FIG. 21A under action of bracing tension forceswith inflexible base.

(52) FIG. 21C: shows FIG. 21B type displacement with flexible base.

(53) FIG. 21D: shoes schematic view of control structure of finite dimensions with tension bracing and sleeve guided motion-controlled yield connector rockers.

(54) FIG. 21E: shows displaced form of FIG. 21D under action of bracing tensionforces.

(55) FIG. 21F: shows FIG. 21E type displacement with flexible base.

(56) FIG. 21G: shows schematic front view of control structure of FIG. 21D withrocker frame pivot elevated and supported by A-frame.

(57) FIG. 21H: shows displaced form of control structure of FIG. 21G with rigid basemember under action of bracing tension forces.

(58) FIG. 21I: shows FIG. 21H type displacement with flexible base.

(59) FIG. 21J: shows schematic front view of lamina shear type control structure of finite dimensions with tension bracing.

(60) FIG. 21K: shows displaced form of control structure of FIG. 21J under action ofbracing tension forces.

(61) FIG. 21L: shows FIG. 21K type displacement with flexible base.

(62) FIG. 22: shows control structure with tension bracing and hydraulic dampers.

(63) FIG. 23: shows single tension brace to control structure of FIG. 22.

(64) FIG. 24A: shows control structure of FIG. 8A with planar concrete rocker frame.

(65) FIG. 24B: shows shear type control structure of FIG. 12A with planar concrete rocker frame.

(66) Alpha1 Rocker Frame

(67) FIG. 25: Alpha1 Frame Elevation with beta1 yield plate rocker with eccentricpivot.

(68) FIG. 26: Alphal Frame sway mode (beta1 rocker/eccentric pivot).

(69) FIG. 27: Alpha1 Frame Elevation with beta1 yield plate rocker with concentricpivot.

(70) FIG. 28: Alpha1 Frame sway mode (beta1 rocker/concentric pivot).

(71) FIG. 29: Alpha1 Frame Elevation with beta2 yield plate rocker with eccentricpivot.

(72) FIG. 30: Alpha1 Frame sway mode (beta2 rocker/leccentric pivot).

(73) FIG. 31: Alpha1 Frame Elevation with beta2 yield plate rocker with concentricpivot.

(74) FIG. 32: Alpha1 Frame sway mode (beta2 rocker/concentric pivot).

(75) FIG. 33: Beta2 yield plate rocker elevation with motion control sleeve guide, multiple plates and concentric pivot.

(76) FIG. 34: elevation of FIG. 33.

(77) FIG. 35: Plan of rocker sleeve (beta2 rocker), plan of yield plate.

(78) FIG. 36: Beta2 yield plate rocker section.

(79) FIG. 37: Beta2 yield plate rocker elevation with motion control sleeve guide, and multiple yield plates and eccentric pivot.

(80) FIG. 38: Part Elevation of alpha1 Frame with beta2 yield plate rocker and eccentric pivot.

(81) FIG. 39: Plan of beta1, beta2 yield plate rocker with eccentric pivot and delta1 yield plate.

(82) FIG. 40: Beta2 yield plate rocker, with concentric pivot and flexing/yielding plate.

(83) FIG. 41: Plan of beta1, beta2 yield plate rocker with concentric pivot and delta1 yield plate.

(84) FIG. 42: Delta1 yield plates; simply spanning, no rotational or translationa restraints each end.

(85) FIG. 43: Delta2 yield plates; continuous with variable stiffness rotational restraint at each end. No translational restraints.

(86) FIG. 44: Delta3 yield plates; full rotational restraints and each end. No translational restraints.

(87) FIG. 45: Elevation of delta1 yield plate within beta1, beta2 rocker with eccentricpivot.

(88) FIG. 46: Elevation of delta2 yield plate within beta1 rocker with motion control stays and eccentric pivot.

(89) FIG. 47: Elevation of delta2 yield plate within beta1, beta2 rocker with eccentricpivot.

(90) FIG. 48: Plan of delta2 yield plate.

(91) FIG. 49: Elevation of beta1, beta2 rocker with slots for delta2 yield plate.

(92) FIG. 50: Elevation of delta3 yield plate within beta1, beta2 rocker with eccentricpivot.

(93) FIG. 51: Elevation of beta1 rocker with motion control stays, multiple plates and eccentric pivot.

(94) FIG. 52: Elevation of beta1 rocker ith motion control stays, multiple plates and concentric pivot.

(95) FIG. 53: Elevation of delta1 yield plate within beta1, beta2 rocker with concentricpivot.

(96) FIG. 54: Elevation of delta2 yield plate within beta1, beta2 rocker with concentricpivot.

(97) FIG. 55: Elevation of beta1 beta2 rocker with slots for delta2 yield plate.

(98) FIG. 56: Elevation of delta3 yield plate within beta1, BETA2 rocker with concentric pivot.

(99) FIG. 57: Part elevation of alphal1 Frame to column connection.

(100) FIG. 58: Plan of FIG. 57.

(101) FIG. 59: Part Elevation of alpha1 Frame base Pivot.

(102) FIG. 60: Plan of FIG. 59.

(103) FIG. 61-79: Various arrangements of alpha1 Frame.

(104) FIG. 80: Elevation of alpha1 Frame within two tier ductile system.

(105) FIG. 81: Detail of FIG. 80.

(106) FIG. 82: Two tier system sway mode.

(107) FIG. 83: Two tier system sway mode with yield plates at flexural limit and secondtier member flexing and yielding.

(108) FIG. 84: Plan of edge supported circular yield plate within beta1, beta2 rocker.

(109) FIG. 85: Elevation of FIG. 84.

(110) Alpha2 Rocker Frame

(111) FIG. 86: Alpha2 Frame Elevation.

(112) FIG. 87: Alpha2 Frame in sway mode.

(113) FIGS. 88 & 89: Motion control stays in sway mode.

(114) FIGS. 90 & 91: Delta4 yield plate; simple. No rotational or translational restraint one end; fixed opposite end.

(115) FIG. 92: Slot in connection plate for delta4 yield plate.

(116) FIG. 93: Delta4 yield plate; flexing / yielding in frame sway mode.

(117) FIG. 94: Delta5 yield plate; continuous variable stiffness rotational restraint with no translationalpha1 restraint one end; fixed opposite end.

(118) FIG. 95: Delta5 yield plate; flexing/yielding in frame sway mode.

(119) FIG. 96: Slots in connection plate for delta5 yield plate.

(120) FIG. 97: Delta6 yield plate; full rotationalpha1 restraints at each end. Notranslational restraints at one end.

(121) FIG. 98: Delta6 yield plate, flexing/yielding in frame sway mode.

(122) FIG. 99: Plan of delta6 yield plate.

(123) FIG. 100: Elevation of multiple delta4 yield plates (similar for delta5, delta6).

(124) FIG. 101: Plan of delta4 yield plate.

(125) FIG. 102: Elevation of motion control tie connection to exterior chord.

(126) FIG. 103: Plan of motion control tie between exterior chord and rocker frame centre line.

(127) FIG. 104: Elevation of motion control tie between exterior chord and rocker frame centre line.

(128) FIG. 105: Alpha2 Frame; Vertical Orientation (motion control ties excluded forclarity).

(129) FIG. 106: Alpha2 Frame; Vertical orientation in sway mode (motion control ties excluded for clarity).

(130) FIG. 107: Alpha2 Frame; Horizontal Orientation (motion control ties excluded for clarity).

(131) FIG. 108: Alpha2 Frame; Horizontal Orientation in sway mode (motion control ties excluded for clarity).

(132) FIG. 109: Alpha2 Frame; Vertical Orientation (motion control ties included).

(133) FIG. 110: Alpha2 Frame; Vertical Orientation in sway mode (motion control ties included).

(134) FIG. 111: Alpha2 Frame; Horizontal Orientation (motion control ties included).

(135) FIG. 112: Alpha2 Frame; Horizontal Orientation in sway mode (motion control ties included).

DETAILED DESCRIPTION

(136) The invention relates to a control structure which helps direct and control the motion of connected force limiting and energy dissipating structural members (preferably a plate or plates of a yield anchor), which are capable of stable cycling high displacement elasto-plastic flexure about their minor bending axis, or out of plane bending.

(137) The invention comprises a device and mechanism, or more specifically a control structure with a pivoting rocker frame, which directs and governs the motion of a connected force limiting and energy dissipating structural plate(s) with connector (yielding connector or yield connector) which by its form is capable of producing a stable, constant resistive yield force while flexurally yielding about its minor (or out of plane) bending axis to high elasto-plastic displacements. The plate(s) action enables the control structure, it is a part of, to form a stable elasto-plastic mechanism which is able to flow and cycle to high elasto-plastic displacements with constant resistive force, in resistive response to ground (base) motion input, while internal forces within it or any adjacent structure it may also be seismically supportive of, are maintained and limited to maximum values which are a function of the yield force of the structural plates which are part of it.

(138) The control structure by governing the motion of the yielding plates within it in a controlled manner is subsequently modifying its own natural response (displacement, velocity, acceleration) and response of masses or adjacent structures it may be directly or indirectly seismically supportive of.

(139) By flowing as a stable, high displacement capable, elasto-plastic mechanism with constant resistive yield force; the control structure is limiting the magnitude of accelerations and dynamic forces that can develop within its members as it endures the ground motion (displacement, velocity, acceleration) input.

(140) That is, the control structure directs and controls the motion of the yielding plates; while the plates, yielding at a constant resistive force, limit the forces generated within the structure(s).

(141) The plates are effectively cushioning the control structures response to ground motion or base excitation.

(142) Contingent on the plates to limit the forces within the control structure and any connected structure; is their ability to sustain potentially high cycling elasto-plastic displacements (deformation) in a stable manner while maintaining a constant resistive yield force.

(143) The magnitude of the peak elasto-plastic displacement demand on the plates is a function of a number of variables including; ground motion (acceleration) input, mass seismically supported by structure and its distribution, elastic natural frequency of structure(s) (inclusive of plates) and yield strength of plate(s).

(144) The ability of the plate(s) to sustain the cycling peak displacement demands on them, while maintaining a stable constant resistive yield force is further dependent on their material stress-strain characteristics, and structural form.

(145) For convenience, reference will herein predominantly be made to an energy absorbing system 1000 control structure for use in or incorporated in a storage rack 3. It will be appreciated that other applications of the present invention exist. Such include but are not limited to high rise buildings.

(146) During a seismic event, as described previously, storage racks can sway in a lengthwise and width-wise direction.

(147) During a seismic event the equivalent force applied to the structure can be approximated to be acting at say around 70% the height of the storage rack 3 or load supporting structure. This does, depend on the weight distribution of goods supported on the rack 3.

(148) The system of the current invention can be incorporated (and retrofitted) to a storage rack or structure to modify and control the displacement, velocity and acceleration response of both the structure and masses supported by it, to ground motion (earthquake acceleration) input and limit the forces generated within the members of the rack structure or building structure and the control structure seismically supportive of it during a seismic event.

(149) The present invention utilises a system as part of or incorporated into a structure to restrain (but not prevent) the structure against movement during a seismic event and dissipate energy during movement. The present invention incorporates a rocker 2000 as part of a substantially stiff control structure that incorporates at least one yield connector to (c) transfer movement induced forces from the upper region of a storage rack or building structure to the foundation, and (d) intermediate of the foundation and the upper region through plastic yielding of the yield members (plates) of the control structure, limit forces that could develop both within the control structure and any adjacent structure it is seismically supportive of (rack or building).

(150) The simple structural behaviour of the yield plate of the yield connector 230 allows for its performance to be both load tested and/or calculated accurately. Its design is such that its yield force and energy absorbing performance remains predictable during each movement cycle of the control structure and storage rack during a seismic event. The yield connector utilises a flexure member 100, that is able to deform. The flexure member 100 (also herein referred to as the plate) is designed or has its performance known for its intended purpose. As such the more accurate the analysis of it the more simplified the design of the overall structure can be and the more predictable the outcome will be during a seismic event. Further to this, it is important that the flexure member 100 (plate) is not able to develop tensile or compressive membrane forces within itself as it flexes to high transverse plastic displacements during yield. Membrane forces generated within a yielding member (plate) will both increase the (plate) stiffness and result in an increasing force resistance within the plate with increased deformation. This in turn will reduce its energy dissipating and force limiting ability, resulting in higher forces being developed in both the control structure and any adjacent structure the control structure may be seismically supportive of.

(151) FIGS. 1 to 3 show a variety of energy absorbing systems 1000 (also herein referred to as control structures) that can be included or that can form part of a storage rack or general building structure. Their incorporation in a storage rack or building is shown in FIG. 4A. Each system comprises a rocker 2000 that includes a frame 280 and a pivot anchor 240. In the examples shown in FIGS. 1 to 3 the pivot anchor 240 may be directly connected to the foundation 4. In other embodiments herein after described, the pivot anchor 240 may be connected to other structures or other component.

(152) The pivot anchor 240 provides a dedicated pivot for rotational movement of the frame 280 of the control structure it is part of. The movement is constrained at least in part by the yield connectors 230 that are disposed outwardly from each side of the pivot anchor 240 in the lengthwise direction. Preferably the pivot anchor 240 is located centrally and intermediate two spaced apart connectors 230A and 230B. Preferably the connectors 230A and 230B are the same.

(153) In some embodiments, the rocker 2000 comprises a frame 280 which engages the two spaced apart yield connectors 230 and the pivot anchor 240. The frame 280 may be part of the storage rack or be incorporated therewith preferably to extend and be secured (directly or indirectly) to an upper region 27 of the storage rack 3 or to each floor of a general building structure. The upwardly extending parts of the frame 280 connecting to the storage rack allow for some or all of the forces from the swaying of the rack 3 or structure to be transferred to the pivot anchor 240 and the yield plates of the connector 230. The motion of the frame 280 being compatible with the motion of the rack 3 or structure. The connection between the control structure and any other adjacent structures it is seismically supportive of must be compatible with the motion of the control structure. For example a vertically slotted pinned connection at the centrelines of the frame pivot 240 or chord base pivots 315. The frame 280 may be short as shown in FIG. 1 or tall as shown in FIGS. 2 & 3. A short frame 280 may be joined to an upper region by ties, struts or cables 270 to provide the force transfer during swaying, as shown in FIG. 1. The short frame embodiment as shown in FIG. 1 may be utilised where lower rack heights are encountered. Where higher rack 3 heights are encountered, a tall frame embodiment may be desirable.

(154) FIG. 1 shows an embodiment that may be best suited for a low storage rack height or where tie cables 270 may be used. Preferably the tie cables 270 do not exceed a 45 degree angle with the foundation. This helps them efficiently transfer lengthwise forces from the storage rack 3 to the rocker 2000 and yield connectors.

(155) The energy absorbing system 1000 (control structure) may be joined to an upper region 27 of a storage rack 3. This may be two thirds up the height of the storage rack 3. This is a typical approximation of where the equivalent applied forces from seismic activity may be focused. It is envisaged that a person skilled in the art will realise that the energy absorbing system 1000 may be engaged at any height to a storage rack depending on the characteristics of stiffness required for the rack.

(156) Preferably the energy absorbing system 1000 comprises a top attachment 250. The top attachment 250 is be configured to attach to a member such as bracing 26 (sometimes known in the industry as plan bracing) of the storage rack 3. If the bracing is a strut or other similar stiff member, preferably this top attachment can pivoted so it does not create any torque or moments in the frame 280 or rack 3.

(157) The bracing 26 is merely a method of connecting the top of the frame 280 or top attachment 250 to the storage rack 3. Where two racks are provided back to back, bracing is typically located intermediate of the racks as shown in FIG. 4B. Plan bracing and connections can also be located at beam levels below the top of the structure.

(158) The plan bracing 26 can span two or more racks. Intermediate the two racks is gap 23 where the energy absorbing system 1000 is located. In alternative embodiments the energy absorbing system 1000 is located at the front face of a storage rack or on both the front and back face.

(159) The frame 280 is preferably a relatively stiff structure compared to the flexible nature of the flexure member 100 (yield plates). Preferably the frame 280 is of a truss type configuration. The truss may be of a multitude of designs and configurations as appropriate for the construction and required functional characteristics of the energy absorbing system 1000. In applications to general building structures a stiff planar reinforced concrete element could also be used for frame 280 (FIGS. 24).

(160) As briefly described earlier, the energy absorbing system 1000 (control structure) is connected or able to be connected to the storage rack 3 or other structure at or near its upper region 27. It is retrofittable to the storage rack or other structure. Given that the stiff frame 280 has little internal displacement (distortion) under applied load, the stiff frame 280 gets rocked or rotated about the pivot anchor 240. The role of the frame 280 is to transfer forces during length wise movement from the upper region 27 to the pivot 240. The rocking movement about the pivot anchor 240 is transferred to the spaced apart yield connectors 230. The rocking movement is then at least partially absorbed by the flexure members 100 (yield plates) as these plastically flex. For example, as shown in FIGS. 1-3, a lengthwise movement of the storage rack 3 to the right cause clockwise rotation of the frame 280 about the pivot anchor 240. This will cause the flexure member 100 of the yield connector 230A to yield in an upwards manner and the flexure member 100 of the yield connectors 230B to move downwards. The lengthwise movement of the upper region 27 is transferred into substantially vertical movement (in one embodiment) into the yield connectors 230. The vertical displacement (motion) of the yield plates is directed and controlled by the control structure of which the yield plates are a part. The yield plates in deforming (flexing) beyond their yield deflection produce a constant resistive yield force which in turn limits the forces that could develop within the control structure and any adjacent structure it may be seismically supportive of.

(161) FIGS. 5A & 5B show another embodiment of the energy absorbing system 1000. FIG. 5A shows a rack 3 in its non-displaced condition, and FIG. 5B shows a rack 3 in a displaced condition.

(162) This embodiment is referenced by numerals 300. I.e. the frame 280, is referenced as the frame 280 and so forth. In this example, the energy absorbing system 1000 effectively comprises two pivot anchors connected by a frame 380. The frame 380 pivots about each pivot anchor 340 and also connects to yield plates which are set within their own rockers. The yield connectors 331-334 are comprised of yield plates supported within yield plate rockers.

(163) The energy absorbing system 1000 locates a rocker 2000 intermediate of two substantially stiff vertical chords 310 (also known as vertical chords) that can sway relative to the ground. The vertical chords 310 are pivotally connected by pivot anchors 315 to the foundation 4. The vertical chords 310 are shown schematically in FIG. 5. The rocker 2000 comprises a frame 380 and two pivot anchors 340. The four yield connectors 331-334 are engaged to the respective vertical chords 310. The yield connectors 331-334 are comprised of yield plates set within their own pivoting rockers which connect to vertical chords 310.

(164) The frame 380 is preferably a stiff truss like configuration, as described previously, to help transfer forces and movement between the two vertical chords 310. The functionality of the two pivot rocker 2000 is much the same as the rocker 2000 previously described. It comprises pivot anchors 240 that allow the frame to pivot relative the vertical chords 310. The yield connectors 331-334 and the frame pivots 240 in this embodiment are not anchoring the rocker 2000 or frame 380 directly to the foundation, but anchoring the frame 380 to each vertical chord 310 that in turn is pivotally anchored to the foundation 4. The foundation 4 is the floor of a structure, a foundation, or a beam or truss type system.

(165) The pivot anchor 315 is engaged to the foundation 4 and defines a rotational axis parallel to the foundation 4 and perpendicular to the lengthwise direction of the storage rack 3. In the preferred embodiment the upper regions 312 of the stiff vertical chords 310 may or may not be connected/engaged with the upper region of the storage rack 3 or building structure.

(166) In a preferred embodiment, there is a first upper yield connector 331 and a second upper yield connector 332 respectively connected to a first of said vertical chords 313 and a second of said vertical chords 314. Furthermore there is a lower first yield connector 333 and a lower second yield connector 334 connected to respective first vertical chord 313 and second vertical chord 314. The flexure members 100 (plates)of the upper yield connectors 331 and 332 deflect in the opposite direction of movement of the storage rack 3 during lengthwise movement of the storage rack 3, and the lower yield connectors 333 and 334 deflect in the direction of lateral movement of the storage rack 3 during seismic activity.

(167) The frame 380 stays substantially horizontal during motion and together with the yield connectors 331-334 allows, yet resists, the racking movement of the energy absorbing structure.

(168) One type of yield connector 230 that may be used for many embodiments (excluding FIGS. 5A and 5B) of the energy absorbing system 1000 herein described is shown in FIG. 6A-B.

(169) As discussed previously, it is ideal that tensile or compressive membrane forces do not develop in the flexure member 100 (plate). Briefly, the connector should allow for the flexure members 100 end regions 231, 232 to translate freely without impediment or restriction, or being encumbered, fettered or the like with the foundation 4 during a yielding condition. The ability of the end regions 231, 232 to translate relatively freely during yielding or lifting of the flexure member is preferred to allow the flexure member 100 to be pulled and deformed/deflected into a curve. In other words the yield member 100 plates are free to flex simply without generating any tensile or compressive membrane forces in the end regions 231, 232 and hence within themselves and for the simply spanning plate, shown in FIG. 6, also be free to rotate at its end regions so as not to develop any unintended end moments.

(170) In one embodiment the flexure member may be described as a simply supported beam. Where a simply supported beam is well known and defined in classical mechanics. A simply supported beam, in one embodiment has a pinned end end condition at one end of a beam or plate (herein the flexure member), and a translational and pinned end end condition at the other end of a beam plate as shown in FIG. 6C. The flexure plate described herein, alternatively may have a fixed/cantilever end condition instead of its pinned end as shown in FIG. 6D. 6C and 6D also show an example of a minor axis (or out of plane axis) 9 going into the page.

(171) The yield connector must also allow for relatively easy lateral translation of a flexure member 100 end region during yielding. This lateral translation during yielding, allows the flexure member 100 to be drawn up with the rocker 2000 or rack during yielding without stretching, or generating membrane tension in the flexure member, or prying at the end regions. And subsequently the substantially lateral translation of an end region allows the flexure member 100 to be driven in the opposite direction, during its operational yielding in the opposite direction, without the flexure member 100 crumpling or kinking.

(172) FIG. 6A shows the yield connector 230 in non-deflected condition stable condition, and FIG. 6B shows a yield connector 230, with the flexure members 100 are in an upwards deflected condition. FIGS. 6A and 6B utilise a pin 234 and slot 235 system to allow both translation and rotation at each end region 231, 232. There are many systems available that will allow both sliding, and/or translation.

(173) FIG. 6C shows a further embodiment of a yield connector 230, with a flexure member 100 shown in a dashed deflected condition. The embodiment of FIG. 6C uses as a retaining slot 236 which allows both translation and rotation of the flexure member 100.

(174) A detailed view of the pivot anchor 340 engaged to a vertical chord 310 as per the configuration of FIG. 5A is shown in a side view in FIG. 7A. A plan cross sectional view is shown in FIG. 7B. Preferably the pivot anchor 340 is pinned by a pin 342 to the vertical chord 310 through the centroid of the vertical chord. The pivot anchor 340 has a pivot axis 341, and the pin 342 allows the frame 280 to pivot about the pivot axis 341 on the vertical chord 310.

(175) The connection of the yielding member (plate) to the horizontal base 4 shown in FIGS. 6A and 6B may be through anchor rods. With this connection the end regions of the flexing member are free to translate and rotate without generating tensile or compressive membrane forces within the plate.

(176) A more ideal connection is shown schematically in FIGS. 5A and 5B. Here the yield plates (member) may be supported within a pivoting rocker. The rocker can be motion controlled through the use of sleeve guides or stays.

(177) The rockers function is to help maintain an orthogonal loading to the yield plate(s) supported and contained within its casing while the yield plate(s); loaded by the pin ended tension/compression ties (push rods) of the rocker frame, undergo high transverse elasto-plastic displacements.

(178) The rockers pivots may be either concentric with or eccentric to the yield plate(s) contained within it.

(179) FIG. 8A schematically shows a sleeve guided rocker with its pivot eccentric to the yield plate.

(180) FIG. 8B shows the same rocker in frame sway mode.

(181) FIG. 8C shows the same frame and similar yield plate rocker; but here the motion of the rocker is controlled by a stay.

(182) FIG. 8D shows the rocker of FIG. 8C in frame sway mode.

(183) FIG. 8E shows an extension of the principle to a sleeve guided rocker with multiple yield plates.

(184) In FIGS. 8A to 8E the rockers are fixed to a horizontal (foundation) structural base.

(185) In FIG. 9A the system shown in FIG. 8A is located between two vertical structural chords.

(186) FIG. 9B shows the frame of FIG. 9A in sway mode.

(187) FIG. 10A schematically shows the horizontally orientated system of FIG. 9A within a tower frame.

(188) FIG. 10B shows the towers yield plate rocker within which multiple yield plates are supported. Here the rockers motion is sleeve guide controlled.

(189) A similar but less ideal yield plate rocker is also shown in FIG. 10C. Here motion control guides or motion control stays are replaced with rocker rotation limiter blocks.

(190) Further arrangements and combinations of rocker frames, yield plate rockers and non-tensioning yield plates are presented in figures subtitled alpha1 rocker frame and alpha1 rocker frame

(191) Here rocker frames (e.g. frame 280), yield plates (e.g. flexure member 100) and yield plate rockers (e.g. yield plate connectors 230) are more specifically categorised; respectively as alpha frames (types alpha1 and alpha2), delta plates (types delta.sub.1 to delta.sub.6) and beta rockers (types beta.sub.1, beta.sub.2).

(192) FIGS. 11A-B show two embodiments of the energy absorbing system 1000. The system 1000 comprises a two pivot rocker 2000 as previously described. Instead of the system 1000 being engaged intermediate two vertical chords, it is engaged between a base (like a foundation 4 or floor) and a beam, roof, ceiling or upper region of a rack 2.

(193) In a further embodiment as shown in FIG. 11C, there may be multiple energy absorbing structures 1000. For example a very tall (and/or heavy) storage rack 2 or structure may have four to twenty energy absorbing structures 1000 spaced apart along its height. In typical embodiments, each energy absorbing structures 1000 is preferably identically configured and of a kind herein described.

(194) Alternatively the embodiment shown in FIGS. 11A and 11B may be used between a top hat 500, such as a stiff beam or truss, and a lower beam or foundation of a storage rack. In which case the top hat 500 may be connected to the plan bracing of the storage rack. The top hat 500 is connected to the upper pivot of rocker 2000. The top hat 500 both increases the elastic stiffness of the control structure, reducing its elasto-plastic displacement during a seismic event and increases the strength and energy absorbing capacity of the control structure. These lateral extensions of a system can be attached to plan bracing of a storage rack or structure and increases the amount of contact and leverage the energy absorbing structure 1000 has with the rack 2. Ties 501 may also be used where the system is used on the end of a storage rack, and not on the side of a rack. I.e. the system is used to prevent width-wise racking—one embodiment of this is shown in FIG. 7.

(195) FIG. 11B shows a further embodiment where a top hat joins to energy absorbing structure 1000. The energy absorbing structures 1000 is engaged at their upper and bottom regions so the effects of any lateral movement will be moved through into each yield connectors much like as described in FIG. 5.

(196) An example of an energy absorbing structure 1000 (control structure) in a general building structure form is shown in FIG. 10A where the stiff vertical chords are shown as trusses. A close-up view of the yield connectors 230, having multiple flexure members 100 (plates) joined to a frame 380, and the vertical chord 310 is shown in FIG. 10B. Flexural yielding in the plates is a co-reactive response to axial forces and displacements generated within the double pin links or push rods as the (alphas) control structure sways in response to ground motion input.

(197) A further embodiment of an energy absorbing system 1000—‘shear type’ embodiment, with ‘shear type’ yield connectors 230, is shown in FIGS. 12 and 13.

(198) Here flexural yielding in the plates is a co-reactive response to the inter-lamina shear forces and displacements generated between the exterior chord and interior frame chord as the (alpha.sub.2) control structure sways in response to ground motion input.

(199) FIG. 12 shows an energy absorbing system 1000 (control structure), having a frame 280 pivotable about a pivoting anchor 240. The frame 280, and pivot anchor 240 are as described previously. The yield connectors 230 are located on either side of the frame 280. Two stiff vertical chords 310 are located on either side of the frame 280, and are anchored to the foundation (or like, such as a floor or beam) preferably by a vertical chord pivot 315. Intermediate each vertical chord and the frame 280 are one or more yield connectors 430. In this embodiment the yield connectors 230 transfer inter-lamina shear force between the exterior chords 310 and the interior chords of the frame 280. This shear force produces flexing in the plates (flexure member 100). Their flexural yielding absorbs energy and limits forces within the control structure or any adjacent structure it may be seismically supportive of. The control structure produces a shearing motion between the frame 280 and a stiff vertical chord 310 when the system is rocked by an earthquake for example. This embodiment still shares the same concepts as the energy absorbing systems 1000 as previously described—where the rocker 2000, translates lateral movement from the upper region 27 about the pivot anchor 240, to thus influence the yield connectors 230 on each lateral side of the pivot anchor 240.

(200) The vertical chords 310 are preferably either tied at their top or upper region to the same rack 2, or they are not constrained and the frame 280 is constrained to the rack 2 or plan bracing. Alternatively, both the chords and the rocker are directly engaged with the rack 2.

(201) Examples of the shear transfer yield plates are shown in FIGS. 14-17, and described later.

(202) In a further embodiment as shown in FIG. 13, the ‘shear type’ energy absorbing system 1000 (control structure) may also be utilised in a horizontal configuration. In this embodiment the energy absorbing system 1000 is rotated horizontally. The two pivot 240 rocker 2000 is placed intermediate two stiff horizontal chords 510.

(203) Both the energy absorbing system 1000 and the horizontal chords 510 are retained and engaged intermediate two vertical chords 310 as previously described. In this embodiment, the energy absorbing system 1000 shares the same shear type yield connectors 230 as described earlier. The horizontal chords 510 are pivotally attached at each of their ends to the two spaced apart vertical chords 510.

(204) The relative movement of the vertical chords 310 and the rocker 2000, creates relative movement at the yield connectors 230. This produces flexure and yielding in the yield plates (yield members 100).

(205) The shear type yield connectors 230 as used in the vertical or horizontal shear embodiment are shown in detail in FIG. 14A—a non-displaced condition, and FIG. 14B—a displaced condition. FIGS. 15 and 16 respectively show the cases of continuous and rotationally restrained lamina shear transfer plates. Non displaced and displaced conditions are shown. FIG. 14 shows a simple embodiment with only one flexure member 100. In other embodiments there are multiple flexure members stacked adjacent one another (FIG. 17).

(206) As stated previously all yield plates within and part of a control structure (designated as delta plates in the figures) are detailed to be free to translate at, at least one end region so as to help avoid self-generate internal membrane forces when flexing to high elasto-plastic displacements.

(207) The flexure member 100 is preferably connected at its end regions 231 and 232. The end regions of each flexure member 100 are connected to, or engage with, a stiffened or reinforced structure of the yield connector. The yield connector 230 is engaged intermediate or is integral with a) the vertical chord 310 and rocker 2000, in the vertical embodiment, or b) the horizontal chord 510 and rocker 2000, in the horizontal embodiment.

(208) In one embodiment as shown in FIG. 14, each end region of the flexure member 100 has different engagement types. As shown in FIG. 14, one end region 232 of the flexure member 100 has a rigidly fixed connection which is rigidly constrained to the interior chord of the frame 280. The opposite end region 231 of the flexure member 100 has a sliding and pivoting engagement with the yield connector and respective structure. The sliding engagement helps prevents the flexure member 100 (plates) from developing direct tensile or compressive membrane forces within itself.

(209) Because the flexure member 100 is not translationally connected to the respective structure (i.e. it can slide relative to), the entire system must be tied together. For this reason, rigid but end pin connected ties 400 should be utilised to connect the vertical chords 310 to the rocker 2000. The ties 400 are preferably pin connected to the centrelines of the exterior chords 310 and the centreline of the frame 1000. The ties 400 are seen in FIGS. 18A and 18B, a non-displaced and displaced condition respectively. FIG. 18C shows the ties in a displaced condition for the horizontally orientated system.

(210) The flexure members 100 herein described are force limiting and energy dissipating structural plates which transfer inter-lamina shear forces from exterior chord to interior chord of rocker frame through minor axis flexure and shear, and dissipate energy by minor axis flexural yielding.

(211) Preferably the entire system is composed substantially of metal. Even more preferably, composed of steel. The pivotable anchors, chords, frame, trusses are substantially stiff and rigid so as not to yield during a seismic event. There are variations that are available to an engineer to design the trusses, body, chords et cetera so they can withstand appropriate forces. For example the frame 280 could comprise a stiff planar reinforced concrete element (FIGS. 24). This results in a composite concrete/steel control structure.

(212) In further embodiments, any of the embodiments above may utilise a secondary flexure member for added resilience (FIGS. 19A-19D). Where the secondary flexure member is intermediate a yield connectors and the equivalent foundation (i.e. the foundation 4 or a vertical chord, or ceiling). The secondary flexure members add in a second layer of safety. In this case the yield plates have flexural deflection (travel) limiters which stop plastic flexure in them at a prescribed limit. Only after these limiters engage is the second tier system able to yield.

(213) By adjusting the relative strengths and elastic stiffness's of the yield plates and secondary flexure member a bi-linear elastic stiffening system can be developed in which yield can occur in one member only (either plate or secondary member) or both.

(214) A further embodiment is where a spring or elastic structural component is added to the pin ended ties connecting the frame 280 to the yield connectors in the alphas frame or a spring added at the connection of the exterior chords to the horizontal or vertical bases of the shear action alpha.sub.2 frames. This allows an independent adjustment of the control structures natural elastic frequency.

(215) Where a ground 2 has been mentioned, it is envisaged that the ground could also be a floor or ceiling of a building or structure, a beam, or truss, or part of a structure that is engaged to the anti-racking system as described.

(216) It is appreciated that where all of these structures and systems herein described are symmetrical, the systems may be halved or doubled or so forth and still be effective. For example the energy absorbing system 1000, may only have one yield connector 232 on one side of the pivot anchor 240. In a similar fashion, the energy absorbing system 400 FIG. 18A may also be halved so there is only one set of yield connector 430 spaced between a frame 400 and one stiff column 310.

(217) The embodiments described above may be altered and combined together to form further embodiments. A person skilled in the art will realise that these configurations can be adapted to suit many different purposes and functional characteristics of a structure or storage rack. Such as the height of the structure or storage rack, the number of storage racks to restrain, the weight of the structure or storage rack, the weight of the goods or structure, the tendency and frequency and magnitude of seismic events where the structure or rack is installed. Furthermore these configurations may be adapted depending on the materials used and the factor of safety required.

(218) Further variations of a system 1000 (control structure) are shown in FIGS. 20 to 23 where an energy absorbing system 1000 may be used to both restrain storage racks 3 and dissipate racking energy during a seismic event. The energy absorbing system 1000 utilises restraining ties 300 to brace itself to the racks 3. These ties 300 are connected to a rocker 2000.

(219) During a seismic event the forces transferred through the ties 300 are tensile forces. More than one tie 300 can be attached to a rocker 2000. The rocker 2000 is preferably provided intermediate two ties 300. In alternative embodiments, the rocker 2000 may be at the end of a rack and only attached to a single tie 300.

(220) The ties 300 have a low elasticity and minimal deformation during seismic activity. Preferably the ties 300 are metal cables. However the ties 300 may be braided line, or solid bar or the like. Any material and geometry substantially strong enough to take the tensile forces with low deformation may be used for the ties 300.

(221) The rocker 2000 (FIG. 21A), in this embodiment, connects with the yield connectors. The flexure member 100 (plate) is part of the yield connector. The flexure member 100 (plates) are able to flex to high elasto-plastic displacements. Absorption of energy through elastic and plastic deformation at the constant yield force of the plate reduces and limits the internal forces that can be generated within the control structure or any adjacent structure it is seismically supportive of. Both structures are hence able to withstand seismic activity with damage confined to the replaceable yield members (plates).

(222) Preferably, the material variables of the rocker 2000, and more specifically the flexure member(s) 100, do not change significantly after each cycle. Importantly, the variables that stay substantially similar are the yield strength and elastic stiffness of the flexure member(s) 100. Preferably the flexure member(s) 100 has 1) a stable and constant cycling yield strength and 2) a stable and constant cycling elastic stiffness.

(223) Because the structural behaviour of the yield plates (flexure member 100) is simple to calculate or verify by load test their performance can be accurately assessed. This allows the performance of the control structure and any adjacent structure it seismically supports to also be accurately assessed. For example, the stiffness, deflection and deformation in operation, weaknesses, stress concentrations et cetera are able to be readily calculated. This allows the design of the rocker 2000 to be specifically designed. As such the more simplified the design can be, and the more accurate the analysis can be.

(224) The rocker 2000 of the present invention utilises the flexure member(s) 100 that throughout the oscillating forces does not significantly change its material properties. This is achieved by detailing the yielding members (plates) to be free to translate (slide) so as to simply flex without developing any membrane forces within themselves.

(225) FIGS. 21 are schematic figures of finite dimension, of four control structures.

(226) These control structures are seismically supportive of load carrying rack structures or general building structures. Connection of these structures to the control structures is through typically inclined tensile cables or rods.

(227) FIG. 21A shows an alphas control structure in which double pin links connect the flexure member 100 yield plates to the frame. The yield plate end connections are anchor rods as described for FIG. 6. The anchor rods connect to a base member whose flexibility is independently adjustable.

(228) FIG. 21B shows the displaced form of FIG. 21A under the action of a tensile force in the ties.

(229) FIG. 21B shows the displacement form for the case of a rigid (inflexible) base.

(230) FIG. 21C shows the similar but increased displacement form for the same case but with a flexible base member.

(231) FIG. 21D shows the case of an alphas frame with yield plates (flexure member 100) supported within sleeve guided rockers (defined as eccentrically pivoting beta.sub.2 rockers in the figures).

(232) FIG. 21E shows the displaced form of FIG. 21D when subject to tensile load from the ties.

(233) FIG. 21F shows the similar but increased displaced form for the same case but with a flexible base member.

(234) FIG. 21G shows a control structure similar to that of FIG. 21D but with a rocker frame supported on and pivotable about an elevating A-frame.

(235) FIG. 21H shows the displaced form of FIG. 21G in response to tensile forces in the ties; and with inflexible base member.

(236) FIG. 21I shows the similar but increased displaced form for the same case but with a flexible base member.

(237) In FIGS. 21H and 21I the pin ended tension/compression ties (push rods) connecting the elasto-plastically flexing yield plates to the rocker frame remain near vertical while the plates flex to high elasto-plastic displacements. As discussed previously the sleeve guided rockers maintain an orthogonal loading to the plates as they freely flex at a constant resistive yield force to high displacements without self generating any response changing membrane forces. As also discussed previously this being due to their free translation support details.

(238) FIG. 21J shows the case of an alpha.sub.2 frame with ‘shear type’ flexure member 100 yield plates as previously described.

(239) FIG. 21K shows the displaced form of FIG. 21J when subject to tensile loads from the ties.

(240) FIG. 21L shows the similar but increased displaced form for the same case but with a flexible base member.

(241) The base member allows i. the fixing (anchor) forces to the foundation (base) generated by the moment couple from the counter directional yield force in the yield plates to be reduced by leverage through the base member about its central pivot. ii. the natural elastic frequency and force/displacement characteristics of the control structure, in conjunction with any other structure it is seismically supportive of, to be adjusted independently. iii. As discussed previously from FIG. 19; the development of a two-tier ductile system.

(242) The rocker 2000 in most instances is intermediate two ties 300 of a racked system. In alternative embodiments, the tie anchor may be at the end of a rack system and only attached to a single tie 300 (not shown). The examples shown in FIG. 20 onwards show a tie anchor located intermediate to ties 300 as shown in detail A in FIG. 20A.

(243) The desirability of having two ties 300, acting in opposite directions, is due to the cycling response of the restrained structure during a seismic event.

(244) The ties are typically in cable or rod form and are only able to carry tensile loads. Hence at any time only one tie is engaged in load transfer from main structure to energy absorbing system 1000 (control structure). Load and motion reversal between both the main structure and ground results in switching tensile loads in the ties, the rocking of 2000 and the yield working of plates 401 and 402. With only one tie 300, after deformation in one direction, racking during the next cycle will incur slack in the tie 300 due to the previous deformation. However, one tie may be used albeit with less effectiveness than two tie, this could be at the ends of a rack where one tie is better than no ties to a tie anchor (FIG. 23).

(245) In an alternative embodiment as shown in FIG. 22 hydraulic energy absorbent means 800 may be utilised. This is used to absorb the energy of the lever 200. In this embodiment, the tie anchor is converting the substantially lateral forces of the ties into substantially vertical forces.

(246) Preferably the entire rocker 2000 is substantially composed of metal. Even more preferably, the rocker 2000 is composed of steel. The rocker, rocker arms, upstand, and anchors are substantially stiff and rigid so as not to yield during a seismic event. There are many alternatives in the design to fabricate a rigid rocker frame.

(247) Where a foundation 4 has been mentioned, it is envisaged that the ground could also be a floor or ceiling of a building or structure, a beam, or truss, or part of a structure that is engaged to the anti-racking system as described.

(248) It is appreciated that where all of these structures and systems herein described are symmetrical, the systems may be halved or double or so forth and still be effective. For example the energy absorbing system 1000 may only have one yield connector 230 on one side of the pivot anchor 240.

(249) The embodiments described above may be altered and combined together to form further embodiments. A person skilled in the art will realise that these configurations can be adapted to suit many different purposes and functional characteristics of a structure or storage rack. Such as the height of the structure or storage rack, the number of storage racks to restrain, the weight of the structure or storage rack, the weight of the goods or structure, the tendency and frequency and magnitude of seismic events where the structure or rack is installed. Furthermore these configurations may be adapted depending on the materials used and the factor of safety required.

(250) Where in the foregoing description reference has been made to elements or integers having known equivalents, then such equivalents are included as if they were individually set forth.

(251) Although the invention has been described by way of example and with reference to particular embodiments, it is to be understood that modifications and/or improvements may be made without departing from the scope or spirit of the invention.