US20170081845A1 - Brace member - Google Patents
Brace member Download PDFInfo
- Publication number
- US20170081845A1 US20170081845A1 US15/310,631 US201515310631A US2017081845A1 US 20170081845 A1 US20170081845 A1 US 20170081845A1 US 201515310631 A US201515310631 A US 201515310631A US 2017081845 A1 US2017081845 A1 US 2017081845A1
- Authority
- US
- United States
- Prior art keywords
- reinforcing
- buckling restraining
- core member
- longitudinal direction
- disposed
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 230000000452 restraining effect Effects 0.000 claims abstract description 94
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 79
- 230000007423 decrease Effects 0.000 claims description 7
- 238000005452 bending Methods 0.000 description 10
- 230000000052 comparative effect Effects 0.000 description 10
- 229910000831 Steel Inorganic materials 0.000 description 8
- 239000010959 steel Substances 0.000 description 8
- 238000003466 welding Methods 0.000 description 6
- 125000004122 cyclic group Chemical group 0.000 description 5
- 230000000694 effects Effects 0.000 description 5
- 238000005304 joining Methods 0.000 description 5
- 238000005266 casting Methods 0.000 description 4
- 239000008186 active pharmaceutical agent Substances 0.000 description 3
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000004570 mortar (masonry) Substances 0.000 description 2
- 239000013585 weight reducing agent Substances 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 229920003002 synthetic resin Polymers 0.000 description 1
- 239000000057 synthetic resin Substances 0.000 description 1
Images
Classifications
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- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H9/00—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate
- E04H9/02—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate withstanding earthquake or sinking of ground
- E04H9/021—Bearing, supporting or connecting constructions specially adapted for such buildings
- E04H9/0215—Bearing, supporting or connecting constructions specially adapted for such buildings involving active or passive dynamic mass damping systems
-
- E04B1/985—
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H9/00—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate
- E04H9/02—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate withstanding earthquake or sinking of ground
- E04H9/021—Bearing, supporting or connecting constructions specially adapted for such buildings
- E04H9/0237—Structural braces with damping devices
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04B—GENERAL BUILDING CONSTRUCTIONS; WALLS, e.g. PARTITIONS; ROOFS; FLOORS; CEILINGS; INSULATION OR OTHER PROTECTION OF BUILDINGS
- E04B1/00—Constructions in general; Structures which are not restricted either to walls, e.g. partitions, or floors or ceilings or roofs
- E04B1/62—Insulation or other protection; Elements or use of specified material therefor
- E04B1/92—Protection against other undesired influences or dangers
- E04B1/98—Protection against other undesired influences or dangers against vibrations or shocks; against mechanical destruction, e.g. by air-raids
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/30—Columns; Pillars; Struts
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H9/00—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate
- E04H9/02—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate withstanding earthquake or sinking of ground
- E04H9/021—Bearing, supporting or connecting constructions specially adapted for such buildings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/02—Springs made of steel or other material having low internal friction; Wound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant
- F16F1/025—Springs made of steel or other material having low internal friction; Wound, torsion, leaf, cup, ring or the like springs, the material of the spring not being relevant characterised by having a particular shape
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/12—Vibration-dampers; Shock-absorbers using plastic deformation of members
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04C—STRUCTURAL ELEMENTS; BUILDING MATERIALS
- E04C3/00—Structural elongated elements designed for load-supporting
- E04C3/02—Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
- E04C2003/026—Braces
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04H—BUILDINGS OR LIKE STRUCTURES FOR PARTICULAR PURPOSES; SWIMMING OR SPLASH BATHS OR POOLS; MASTS; FENCING; TENTS OR CANOPIES, IN GENERAL
- E04H9/00—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate
- E04H9/02—Buildings, groups of buildings or shelters adapted to withstand or provide protection against abnormal external influences, e.g. war-like action, earthquake or extreme climate withstanding earthquake or sinking of ground
- E04H9/028—Earthquake withstanding shelters
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2230/00—Purpose; Design features
- F16F2230/0023—Purpose; Design features protective
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2230/00—Purpose; Design features
- F16F2230/16—Purpose; Design features used in a strut, basically rigid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2236/00—Mode of stressing of basic spring or damper elements or devices incorporating such elements
- F16F2236/04—Compression
- F16F2236/045—Compression the spring material being generally enclosed
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2238/00—Type of springs or dampers
- F16F2238/04—Damper
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F7/00—Vibration-dampers; Shock-absorbers
- F16F7/12—Vibration-dampers; Shock-absorbers using plastic deformation of members
- F16F7/125—Units with a telescopic-like action as one member moves into, or out of a second member
Definitions
- the present invention relates to brace members, and particularly to a brace member that includes a core member, which absorbs the seismic energy in occurrences of earthquakes, and a buckling restraining member, which stiffens the core member.
- brace members installed in architectural structures to deal with occurrences of earthquakes include a core member, which absorbs seismic energy, and a stiffening member, which restricts out-of-plane (direction perpendicular to longitudinal direction) deformation that occurs when compressive force acts in the longitudinal direction of the core member.
- the brace members prevent or retard an occurrence of buckling of the entirety of the core member even when the compressive axial force acts to cause stable deformation in the axial direction and enhance the ability to absorb seismic energy.
- Patent Literature 1 The applicant of patent has disclosed a brace member (for example, see Patent Literature 1) that is easily manufacturable and that can prevent a weight increase as a result of eliminating a welding operation for disposing a core member and a stiffening member in a predetermined form and an operation of filling a space between the core member and the stiffening member with mortar.
- crevices are connected, with screw threads, to both end portions of the core member that extends through the buckling restraining member and that is made of a steel bar.
- a first end portion of the buckling restraining member is secured with screw threads to a first end portion of the core member with a retaining ring interposed therebetween, the retaining ring being screwed on the buckling restraining member and the core member.
- a sleeve made of a steel pipe is secured, with a screw thread, to a second end portion of the core member.
- the thickness of the sleeve is required to be smaller than half the difference between the inner diameter of the stiffening member and the outer diameter of the core member.
- the inner surface of the stiffening member is preferably located near the outer surface of the core member to deliver its stiffening performance.
- the thickness of the sleeve naturally has its limit. If the sleeve has a small bending strength due to this limit, the sleeve may be yielded due to bending in a range of the sleeve exposed beyond the buckling restraining member. In this case, the core member may be buckled within this range since no buckling restraining member is originally disposed between the second end surface of the buckling restraining member and the end portion of the crevice secured with a screw to the second end portion of the core member and the sleeve has been yielded.
- a brace member includes a core member, a buckling restraining member through which the core member extends and that restricts out-of-plane deformation of the core member, a cap sleeve in which a first end portion of the core member on a first side in a longitudinal direction and a first end portion of the buckling restraining member on the first side in the longitudinal direction are disposed, a cap-sleeve crevice disposed on the cap sleeve so as to protrude toward a side opposite to a side on which the core member and the buckling restraining member are disposed, the cap-sleeve crevice serving as a joint for installing the brace member on an architectural structure, a reinforcing member in which a second end portion of the core member on a second side in the longitudinal direction is disposed, and a reinforcing-member crevice disposed on the reinforcing member so as to protrude toward a side opposite to
- a brace member includes a core member, a buckling restraining member through which the core member extends and that restricts out-of-plane deformation of the core member, reinforcing members disposed individually on two ends of the core member in a longitudinal direction, and reinforcing-member crevices disposed individually on the reinforcing members so as to each protrude toward a side opposite to a side on which the core member is disposed, the reinforcing-member crevices serving as joints for installing the brace member on an architectural structure.
- Each of the reinforcing members surrounds a predetermined area of the buckling restraining member extending from a corresponding one of end portions of the buckling restraining member in the longitudinal direction.
- an inner diameter of the reinforcing member(s) in the range in which the reinforcing member(s) surrounds the buckling restraining member is constant in the longitudinal direction, and an outer diameter of the reinforcing member(s) in the range decreases toward a center of the buckling restraining member in the longitudinal direction.
- the first end portion of the buckling restraining member on the first side in the longitudinal direction is disposed in the cap sleeve and a predetermined area of the buckling restraining member extending from the second end surface on the second side in the longitudinal direction is surrounded by the reinforcing member.
- the reinforcing member surrounds the external circumferential surface of the buckling restraining member and the thickness of the reinforcing member is not limited.
- the outer diameter (and the inner diameter) and the thickness can be increased, whereby the stiffness can be enhanced.
- the brace member according to aspects of the present invention is a brace member having high (great) bending strength.
- FIG. 1 illustrates a brace member according to a first embodiment of the present invention.
- FIG. 1( a ) is a side view of the brace member and
- FIG. 1( b ) is a sectional view of a main portion of the brace member viewed sideways.
- FIG. 2 illustrates a specimen that undergoes a loading test to evaluate the performances of the brace member according to the first embodiment of the present invention and is a sectional view viewed sideways to define the length of each component.
- FIG. 3 illustrates a specimen that undergoes a loading test to evaluate the performances of an existing brace member for use as a comparative example and is a sectional view viewed sideways to define the length of each component.
- FIG. 4 has axial force-axial strain chart(s) showing the results of the loading test conducted to clarify the performances of the brace member according to the first embodiment of the present invention.
- FIG. 4( a ) is a chart for a specimen No. 1
- FIG. 4( b ) is a chart for a specimen No. 2.
- FIG. 5 is an axial force-axial strain chart showing the results of the loading test conducted to clarify the performances of an existing brace member of a comparative example.
- FIG. 6 illustrates a brace member according to a second embodiment of the present invention.
- FIG. 6( a ) is a side view of the brace member and
- FIG. 6( b ) is a sectional view of a main portion of the brace member viewed sideways.
- FIG. 7 illustrates a brace member according to a third embodiment of the present invention.
- FIG. 7( a ) is a side view of the brace member and
- FIG. 7( b ) is a sectional view of a main portion of the brace member viewed sideways.
- FIG. 1 illustrates a brace member according to a first embodiment of the present invention.
- FIG. 1( a ) is a side view of the brace member and
- FIG. 1( b ) is a sectional view of a main portion of the brace member viewed sideways.
- Each of the diagrams is schematically drawn and the dimensions such as the relative size or thickness of each component are not limited to those illustrated in the drawings.
- the left side is referred to as “a first side in the longitudinal direction” and the right side is referred to as “a second side in the longitudinal direction”.
- a brace member 100 includes a core member 10 , a buckling restraining member 20 through which the core member 10 extends and that surrounds the core member 10 to restrict out-of-plane deformation of the core member 10 , a cap sleeve 30 in which a first end portion 11 a of the core member 10 on the first side in the longitudinal direction and a first end portion 21 a of the buckling restraining member 20 on the first side in the longitudinal direction are disposed, a cap-sleeve crevice 40 disposed on the cap sleeve 30 so as to protrude toward a side opposite to a side on which the core member 10 and the buckling restraining member 20 are disposed, the cap-sleeve crevice 40 serving as a joint for installing the brace member 100 on an architectural structure (not illustrated), a reinforcing member 50 in which a second end portion 11 b of the core member 10 on the second side in the longitudinal direction is disposed, and
- the core member 10 is a long member formed from a steel bar having a circular cross section.
- a male screw thread 12 a is formed at the first end portion 11 a on the first side in the longitudinal direction and a male screw thread 12 b is formed at the second end portion 11 b on the second side in the longitudinal direction.
- the core member 10 made of a steel bar having a circular cross section is illustrated.
- the core member 10 is not limited to the one having this cross section and may be formed from, for example, a steel pipe or may be formed by joining flat boards so as to have a cross-shaped cross section.
- the core member 10 When the core member 10 is made of a plastically deformable material, the core member 10 has a higher effect. In order to prevent noises and an excessive increase in axial force due to friction that occur when the external circumferential surface of the core member 10 and the internal circumferential surface of the buckling restraining member 20 slide over each other, a liner made of a material such as a synthetic resin may be disposed on the external circumferential surface of the core member 10 .
- the buckling restraining member 20 is a steel pipe having a circular cross section and shorter than the core member 10 .
- a male screw thread 22 a is formed at the first end portion 21 a on the first side in the longitudinal direction (a male screw thread or the like is not formed at a second end portion 21 b on the second side in the longitudinal direction).
- the buckling restraining member 20 may have a rectangular cross section.
- the cap sleeve 30 includes a cylindrical portion 33 low in height.
- a female screw thread 34 is formed in a first end surface 30 a
- a female screw thread 32 is formed in a second end surface 30 b
- a female screw thread 31 is formed through the center of the cylindrical portion 33 .
- the female screw thread 34 , the female screw thread 32 , and the female screw thread 31 are concentric with one another.
- the male screw thread 12 a of the core member 10 is screwed on the female screw thread 31 .
- the male screw thread 22 a of the buckling restraining member 20 is screwed on the female screw thread 32 .
- a male screw thread 43 (described below) of the cap-sleeve crevice 40 is screwed on the female screw thread 34 .
- a tapered portion 30 c whose outer diameter decreases toward the second end surface 30 b , is formed in a range of the external circumferential surface near the second end surface 30 b .
- the corner portion may be chamfered as in the case of the first end surface 30 a.
- the cap-sleeve crevice 40 serves as a joint for installing the brace member 100 in an architectural structure (not illustrated).
- the cap-sleeve crevice 40 includes a disk-shaped portion 41 , a plate-shaped portion 42 disposed on the first end surface of the disk-shaped portion 41 , an attachment hole 44 that extends through the plate-shaped portion 42 , and a male screw thread 43 disposed on the external circumferential surface of the disk-shaped portion 41 .
- the central axis of the attachment hole 44 and the central axis of the disk-shaped portion 41 perpendicularly cross each other (not geometrically accurately but industrially accurately cross each other).
- the cap sleeve 30 and the cap-sleeve crevice 40 are separately manufactured and are integrated together with screw connection.
- the present invention is not limited to this configuration.
- the cap sleeve 30 and the cap-sleeve crevice 40 may be integrated together by mechanical joining such as shrinkage fit or metallurgic joining such as welding.
- the cap sleeve 30 and the cap-sleeve crevice 40 may be originally manufactured as an integrated unit by, for example, casting.
- the reinforcing member 50 includes a tubular portion 52 and a disk-shaped portion 55 .
- a female screw thread 56 is formed in a second end surface 50 b of the disk-shaped portion 55 and a female screw thread 51 is formed through the center of the disk-shaped portion 55 .
- the male screw thread 12 b of the core member 10 is screwed on the female screw thread 51 and a male screw thread 65 (described below) of the reinforcing-member crevice 60 is screwed on the female screw thread 56 .
- the inner diameter of the tubular portion 52 is constant in the longitudinal direction.
- the central axis of the tubular portion 52 , the central axis of the female screw thread 51 , and the central axis of the female screw thread 56 coincide with one another.
- the tubular portion 52 surrounds the second end portion 21 b (an area extending a predetermined distance from an end surface 20 b ) of the buckling restraining member 20 on the second side in the longitudinal direction (an area of the buckling restraining member 20 extending a predetermined distance from the second end surface 20 b on the second side in the longitudinal direction is inserted into the tubular portion 52 ).
- a tapered portion 50 c whose outer diameter decreases toward the first end surface (corresponding to the tip end) 50 a on the first side in the longitudinal direction, is formed on the outer surface of the tubular portion 52 .
- This configuration gives the impression of smoothly reinforcing the buckling restraining member 20 , thereby improving the design.
- the reinforcing-member crevice 60 serves as a joint for installing the brace member 100 on an architectural structure (not illustrated).
- the reinforcing-member crevice 60 includes a disk-shaped portion 61 , a plate-shaped portion 62 disposed on the second end surface of the disk-shaped portion 61 , an attachment hole 66 that extends through the plate-shaped portion 62 , and a male screw thread 65 formed on the external circumferential surface of the disk-shaped portion 61 .
- the center line of the attachment hole 66 and the center line of the male screw thread 65 perpendicularly cross each other (not geometrically accurately but industrially accurately cross each other).
- the reinforcing-member crevice 60 has the same shape as the cap-sleeve crevice 40 .
- the reinforcing member 50 and the reinforcing-member crevice 60 are separately manufactured and are integrated together with screw connection.
- the present invention is not limited to this configuration.
- the reinforcing member 50 and the reinforcing-member crevice 60 may be integrated together by mechanical joining such as shrinkage fit or metallurgic joining such as welding.
- the reinforcing member 50 and the reinforcing-member crevice 60 may be originally manufactured as an integrated unit by, for example, casting.
- the first end portion 21 a of the buckling restraining member 20 on the first side in the longitudinal direction is disposed in the cap sleeve 30 .
- a predetermined area of the buckling restraining member 20 extending from the second end surface 20 b in the longitudinal direction is surrounded with the tubular portion 52 of the reinforcing member 50 .
- the tubular portion 52 surrounds the external circumferential surface of the buckling restraining member 20 and the thickness of the tubular portion 52 is not limited.
- the outer diameter (and the inner diameter) and the thickness can be increased compared with an existing sleeve (disposed in a gap between the core member and the buckling restraining member), whereby the stiffness can be enhanced.
- a length l k for which the buckling restraining member 20 is surrounded by the tubular portion 52 and a difference e k between the outer diameter of the buckling restraining member 20 (corresponding to a “bucking restraining member”) and the inner diameter of the reinforcing member 50 has a relationship of e k /l k ⁇ 0.05.
- the outer diameter of the reinforcing member 50 decreases toward the first end surface 50 a (tip end) on the first side in the longitudinal direction (toward the center of the buckling restraining member 20 in the longitudinal direction).
- the weight reduction can be enhanced and the design can be improved while the strength at each position in the longitudinal direction is secured.
- Both end portions of the core member 10 are respectively connected with screw threads to the cap sleeve 30 and the reinforcing member 50 .
- these screw threads in opposite handedness (for example, the male screw thread 12 a and the female screw thread 31 are right-handed screws and the male screw thread 12 b and the female screw thread 51 are left-handed screws)
- the distance between the attachment hole 44 and the attachment hole 66 can be adjusted, whereby installation of the brace member 100 can be facilitated.
- FIG. 2 illustrates a specimen that undergoes a loading test to evaluate the performances of the brace member according to the first embodiment of the present invention and is a sectional view viewed sideways to define the length of each component. Some reference signs are not shown. Table 1 shows the dimensions or the like of each portion of the specimens (No. 1 and No. 2).
- the outer diameter of the core member 10 of each of the specimen No. 1 and the specimen No. 2 is denoted with “D S ”.
- the yield point of the core member 10 is denoted with “ ⁇ y ”
- the product of the cross section of the core member 10 and the yield point ⁇ y is denoted with “N y ”.
- the outer diameter of the buckling restraining member 20 (corresponding to the “buckling restraining member”) is denoted with “D B ”, the thickness of the buckling restraining member 20 is denoted with “t B ”, the distance between the second end surface 20 b of the buckling restraining member 20 on the second side in the longitudinal direction and the center of the attachment hole 66 of the reinforcing-member crevice 60 is denoted with “l c ”, and the distance between the second end surface 20 b of the buckling restraining member 20 on the second side in the longitudinal direction and the first end surface 50 a of the reinforcing member 50 on the first side in the longitudinal direction is denoted with “l k ”.
- l k has been described above.
- the distance between the center of the attachment hole 44 of the cap-sleeve crevice 40 and the second end surface 30 b of the cap sleeve 30 is denoted with “FlJ”
- the distance between the second end surface 30 b of the cap sleeve 30 and the first end surface 50 a of the reinforcing member 50 is denoted with “l B ”
- the distance between the first end surface 50 a of the reinforcing member 50 and the attachment hole 66 of the reinforcing-member crevice 60 is denoted with “MlJ”.
- the distance between the center of the attachment hole 44 of the cap-sleeve crevice 40 and the center of the attachment hole 66 of the reinforcing-member crevice 60 is denoted with “l”.
- e S the difference between the outer diameter of the core member 10 and the inner diameter of the buckling restraining member 20
- e k the difference between the outer diameter of the buckling restraining member 20 and the inner diameter of the reinforcing member 50
- the thickness of the reinforcing member 50 at the first end surface 50 a (tip end) on the first side in the longitudinal direction is denoted with “t K ”.
- FIG. 3 illustrates a specimen that undergoes a loading test to evaluate the performances of an existing brace member of a comparative example and is a sectional view viewed sideways to define the length of each component.
- Table 2 shows the dimensions or the like of each component of a comparative example (No. 3).
- the outer diameter of a core member 910 of a comparative example (No. 3) 900 is denoted with “D 5 ”
- the outer diameter of a buckling restraining member 20 is denoted with “D B ”
- the thickness of the buckling restraining member 920 is denoted with “t B ”.
- the yield point of the core member 910 is denoted with “ ⁇ y ”
- the product of the cross section of the core member 10 and the yield point ⁇ y is denoted with “N y ”.
- Integrated crevices 940 and 960 are disposed on end portions 911 a and 911 b (at which male screw threads 912 a and 912 b are respectively formed) of the core member 910 .
- the distance between the center of a connection hole 944 of the first integrated crevice 940 and the center of a connection hole 966 of the second integrated crevice 960 is denoted with “l”.
- the first end portion 911 a (at which the male screw thread 912 a is formed) of the core member 910 and a first end portion 921 a (at which a female screw thread 922 a is formed) of the buckling restraining member 920 are connected together with a cap sleeve 930 (at which a female screw thread 931 and a male screw thread 932 are formed).
- a tubular sleeve 970 is disposed at a position near the second end portion 911 b of the core member 910 .
- the sleeve 970 is inserted into the buckling restraining member 920 by a distance “L” from a second end surface 920 b of the buckling restraining member 920 .
- the difference between the outer diameter of the sleeve 970 and the inner diameter of a second end portion 921 b of the buckling restraining member 920 is denoted with “e S ”.
- the geometrical moment of inertia is greater than or equal to “ten millions (mm 4 )”.
- the geometrical moment of inertia is smaller than or equal to 0.62 millions (mm 4 ).
- the geometrical moment of inertia of the reinforcing member 50 of aspects of the present invention is approximately 17 times as high (great) as the geometrical moment of inertia of the existing sleeve 970 of a comparative example.
- the reinforcing member 50 having such high stiffness restricts out-of-plane deformation of the buckling restraining member 20 .
- FIG. 4 has axial force-axial strain charts showing the results of the loading test conducted to evaluate the performances of the brace member according to the first embodiment of the present invention.
- FIG. 4( a ) is a chart for a specimen No. 1
- FIG. 4( b ) is a chart for a specimen No. 2.
- the loading test is a reversed cyclic loading test in which the core member 10 is repeatedly and alternately compressed and stretched.
- the core member 10 is compressed by 0.25% (the “distance l” between the center of the attachment hole 44 of the cap-sleeve crevice 40 and the center of the attachment hole 66 of the reinforcing-member crevice 60 is reduced by 6.25 mm).
- the compressive load and the compressive strain are shown in a first quadrant.
- the core member 10 is stretched by 0.25% (the distance l is increased by 6.25 mm). At this time, the tensile load and the tensile strain are shown in a third quadrant.
- the core member 10 is compressed by 0.5% (the distance l is reduced by 12.5 mm) and then the core member 10 is stretched by 0.5% (the distance l is increased by 12.5 mm).
- the core member 10 is compressed by 1.0% (the distance l is reduced by 25 mm) and then the core member 10 is stretched by 1.0% (the distance l is increased by 25 mm). This loading is regarded as one cycle and this cycle is repeated five times.
- the core member 10 is compressed by 2.0% (the distance l is reduced by 50 mm) and then the core member 10 is stretched by 2.0% (the distance l is increased by 50 mm).
- This loading is regarded as one cycle (or referred to as a “final cycle”, below). This cycle is repeated until the core member 10 is buckled or broken.
- the core member 10 of the specimen No. 1 was broken at the fourth stretch after the final cycle had been repeated three times.
- the core member 10 of neither the specimen No. 1 nor the specimen No. 2 was buckled. This result reveals that the buckling restraining member 20 and the reinforcing member 50 restrict out-of-plane deformation of the core member 10 .
- FIG. 5 is an axial force-axial strain chart showing the results of the cyclic loading test conducted to evaluate the performances of an existing brace member of a comparative example.
- the cyclic loading test is a reversed cyclic loading test in which the core member 10 is repeatedly and alternately compressed and stretched.
- the core member 910 of the specimen No. 3 was subjected to one cycle of compression and stretch by 0.1%, two cycles of compression and stretch by 0.25%, and two cycles of compression and stretch by 0.5%. Then, when the core member 910 was compressed by 1.0%, the core member 910 was buckled.
- the brace member of aspects of the present invention has been proved to be a brace member in which the reinforcing member 50 has high (great) bending strength.
- FIG. 6 illustrates a brace member according to a second embodiment of the present invention.
- FIG. 6( a ) is a side view of the brace member and
- FIG. 6( b ) is a sectional view of a main portion of the brace member viewed sideways.
- Portions the same as or corresponding to the portions of the first embodiment are denoted with the same reference signs and some of them are not described herein.
- the dimensions such as the relative size or thickness of each component are not limited to those illustrated in the drawings.
- a brace member 200 includes a core member 10 , a buckling restraining member 20 through which the core member 10 extends and that surrounds the core member 10 to restrict out-of-plane deformation of the core member 10 , a cap sleeve 230 in which a first end portion 11 a of the core member 10 on the first side in the longitudinal direction and a first end portion 21 a of the buckling restraining member 20 on the first side in the longitudinal direction are disposed, a cap-sleeve crevice 40 disposed on the cap sleeve 230 so as to protrude toward a side opposite to a side on which the core member 10 and the buckling restraining member 20 are disposed, the cap-sleeve crevice 40 serving as a joint for installing the brace member 200 on an architectural structure (not illustrated), a reinforcing member 250 in which a second end portion 11 b of the core member 10 on the second side in the longitudinal direction is disposed,
- the cap sleeve 230 and the reinforcing member 250 of the brace member 200 do not respectively have the tapered portion 30 c and the tapered portion 50 c , which are respectively formed on the outer surface of the cap sleeve 30 and the outer surface of the reinforcing member 50 of the brace member 100 (first embodiment). Except for this point, the brace member 200 is similar to the brace member 100 .
- the brace member 200 has high (great) bending strength and is manufactured at low costs.
- the brace member 200 can be manufactured at low costs by performing welding connection between steel pipes or welding connection between a steel pipe and a circular plate (or a disk having a center hole).
- FIG. 7 illustrates a brace member according to a third embodiment of the present invention.
- FIG. 7( a ) is a side view of the brace member and
- FIG. 7( b ) is a sectional view of a main portion of the brace member viewed sideways.
- Portions the same as or corresponding to the portions of the first embodiment are denoted with the same reference signs and some of them are not described.
- the dimensions such as the relative size or thickness of each component are not limited to those illustrated in the drawings.
- a brace member 300 includes a core member 10 , a buckling restraining member 20 through which the core member 10 extends and that surrounds the core member 10 to restrict out-of-plane deformation of the core member 10 , a first-side reinforcing member 350 a in which a first end portion 11 a of the core member 10 on the first side in the longitudinal direction and a first end portion 21 a of the buckling restraining member 20 on the first side in the longitudinal direction are disposed, a reinforcing-member crevice 60 disposed on the first-side reinforcing member 350 a so as to protrude toward a side opposite to a side on which the core member 10 and the buckling restraining member 20 are disposed, the reinforcing-member crevice 60 serving as a joint for installing the brace member 300 on an architectural structure (not illustrated), a second-side reinforcing member 350 b in which a second end portion 11 b of the core member 10 on
- the brace member 300 includes a first-side reinforcing member 350 a instead of the cap sleeve 30 of the brace member 100 (first embodiment).
- the first-side reinforcing member 350 a and the second-side reinforcing member 350 b correspond to the reinforcing member 50 .
- the first end portion 21 a of the buckling restraining member 20 is reinforced with the first-side reinforcing member 350 a , in the same manner as the second end portion 21 b reinforced with the second-side reinforcing member 350 b .
- the brace member 300 is the same as the brace member 100 .
- the brace member 300 has high (great) bending strength and is manufactured at low costs.
- this configuration eliminates the need to manufacture the cap sleeve 30 .
- the die set for casting the cap sleeve 30 is not needed and the number of types of components constituting the brace member 300 is reduced, whereby stock control is facilitated.
- the brace member 300 includes a pair of reinforcing members 50 , but may include a pair of reinforcing members 250 instead of the reinforcing members 50 .
- aspects of the present invention achieve a brace member having a high (great) bending strength with a simple structure.
- the brace member is also usable for core members having cross-sections of various different shapes.
- the brace member according to aspects of the present invention is widely usable as a brace member for dealing with various different demands of architectural structures.
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Abstract
Description
- This application is the U.S. National Phase application of PCT/JP2015/002421, filed May 13, 2015, and claims priority to Japanese Patent Application No. 2014-103271, May 19, 2014, the disclosures of each of these applications being incorporated herein by reference in their entireties for all purposes.
- The present invention relates to brace members, and particularly to a brace member that includes a core member, which absorbs the seismic energy in occurrences of earthquakes, and a buckling restraining member, which stiffens the core member.
- Existing brace members installed in architectural structures to deal with occurrences of earthquakes include a core member, which absorbs seismic energy, and a stiffening member, which restricts out-of-plane (direction perpendicular to longitudinal direction) deformation that occurs when compressive force acts in the longitudinal direction of the core member. The brace members prevent or retard an occurrence of buckling of the entirety of the core member even when the compressive axial force acts to cause stable deformation in the axial direction and enhance the ability to absorb seismic energy.
- The applicant of patent has disclosed a brace member (for example, see Patent Literature 1) that is easily manufacturable and that can prevent a weight increase as a result of eliminating a welding operation for disposing a core member and a stiffening member in a predetermined form and an operation of filling a space between the core member and the stiffening member with mortar.
- [PTL 1] Japanese Unexamined Patent Application Publication No. 2013-112949 (pages 4 to 5 and FIG. 1)
- In the brace member disclosed in
Patent Literature 1, crevices are connected, with screw threads, to both end portions of the core member that extends through the buckling restraining member and that is made of a steel bar. A first end portion of the buckling restraining member is secured with screw threads to a first end portion of the core member with a retaining ring interposed therebetween, the retaining ring being screwed on the buckling restraining member and the core member. On the other hand, a sleeve made of a steel pipe is secured, with a screw thread, to a second end portion of the core member. Substantially half the sleeve in the longitudinal direction is inserted into the buckling restraining member and the remaining substantially half the sleeve is exposed beyond the buckling restraining member. Here, a gap having a predetermined size is formed between the external circumference of the sleeve and the internal circumference of the buckling restraining member. Such a brace member thus has a remarkable effect that allows the core member to be disposed at a predetermined position relative to the buckling restraining member without performing a welding operation and a remarkable effect that allows elimination of an operation of filling a space between the core member and the stiffening member with mortar. - However, the thickness of the sleeve is required to be smaller than half the difference between the inner diameter of the stiffening member and the outer diameter of the core member. On the other hand, the inner surface of the stiffening member is preferably located near the outer surface of the core member to deliver its stiffening performance.
- Thus, the thickness of the sleeve naturally has its limit. If the sleeve has a small bending strength due to this limit, the sleeve may be yielded due to bending in a range of the sleeve exposed beyond the buckling restraining member. In this case, the core member may be buckled within this range since no buckling restraining member is originally disposed between the second end surface of the buckling restraining member and the end portion of the crevice secured with a screw to the second end portion of the core member and the sleeve has been yielded.
- To address this, a brace member having bending strength enhanced (increased) by a mechanism substitute for the sleeve has been demanded.
- Aspects of the present invention were made to respond to the above-described demand and aims to provide a brace member having high (great) bending strength.
- (1) A brace member according to aspects of the present invention includes a core member, a buckling restraining member through which the core member extends and that restricts out-of-plane deformation of the core member, a cap sleeve in which a first end portion of the core member on a first side in a longitudinal direction and a first end portion of the buckling restraining member on the first side in the longitudinal direction are disposed, a cap-sleeve crevice disposed on the cap sleeve so as to protrude toward a side opposite to a side on which the core member and the buckling restraining member are disposed, the cap-sleeve crevice serving as a joint for installing the brace member on an architectural structure, a reinforcing member in which a second end portion of the core member on a second side in the longitudinal direction is disposed, and a reinforcing-member crevice disposed on the reinforcing member so as to protrude toward a side opposite to a side on which the core member is disposed, the reinforcing-member crevice serving as a joint for installing the brace member on the architectural structure. The reinforcing member surrounds a predetermined area of the buckling restraining member extending from a second end surface on the second side in the longitudinal direction.
- (2) A brace member according to aspects of the present invention includes a core member, a buckling restraining member through which the core member extends and that restricts out-of-plane deformation of the core member, reinforcing members disposed individually on two ends of the core member in a longitudinal direction, and reinforcing-member crevices disposed individually on the reinforcing members so as to each protrude toward a side opposite to a side on which the core member is disposed, the reinforcing-member crevices serving as joints for installing the brace member on an architectural structure. Each of the reinforcing members surrounds a predetermined area of the buckling restraining member extending from a corresponding one of end portions of the buckling restraining member in the longitudinal direction.
- (3) Further, in the above-described paragraph (1) or (2), an inner diameter of the reinforcing member(s) in the range in which the reinforcing member(s) surrounds the buckling restraining member is constant in the longitudinal direction, and an outer diameter of the reinforcing member(s) in the range decreases toward a center of the buckling restraining member in the longitudinal direction.
- (i) In the brace member according to aspects of the present invention, the first end portion of the buckling restraining member on the first side in the longitudinal direction is disposed in the cap sleeve and a predetermined area of the buckling restraining member extending from the second end surface on the second side in the longitudinal direction is surrounded by the reinforcing member. In other words, the reinforcing member surrounds the external circumferential surface of the buckling restraining member and the thickness of the reinforcing member is not limited. Thus, compared with an existing sleeve (disposed between the core member and the buckling restraining member), the outer diameter (and the inner diameter) and the thickness can be increased, whereby the stiffness can be enhanced.
- Here, deformation of the predetermined area of the buckling restraining member extending from the second end surface on the second side in the longitudinal direction is restricted by the reinforcing member having high stiffness and the core member is prevented from being buckled. Thus, the brace member according to aspects of the present invention is a brace member having high (great) bending strength.
- (ii) When predetermined areas of the buckling restraining member extending from both end portions of the buckling restraining member in the longitudinal direction are surrounded by respective reinforcing members, the above-described effect is obtained. Moreover, the elimination of the need for the cap sleeve enables reduction of the number of types of components, whereby manufacturing costs or inventory costs can be kept low.
- (iii) In addition, since the outer diameter of the reinforcing member decreases toward the tip end (toward the center of the buckling restraining member in the longitudinal direction), the weight reduction can be enhanced and the design can be improved while the strength at each position in the longitudinal direction is secured.
-
FIG. 1 illustrates a brace member according to a first embodiment of the present invention.FIG. 1(a) is a side view of the brace member andFIG. 1(b) is a sectional view of a main portion of the brace member viewed sideways. -
FIG. 2 illustrates a specimen that undergoes a loading test to evaluate the performances of the brace member according to the first embodiment of the present invention and is a sectional view viewed sideways to define the length of each component. -
FIG. 3 illustrates a specimen that undergoes a loading test to evaluate the performances of an existing brace member for use as a comparative example and is a sectional view viewed sideways to define the length of each component. -
FIG. 4 has axial force-axial strain chart(s) showing the results of the loading test conducted to clarify the performances of the brace member according to the first embodiment of the present invention.FIG. 4(a) is a chart for a specimen No. 1 andFIG. 4(b) is a chart for a specimen No. 2. -
FIG. 5 is an axial force-axial strain chart showing the results of the loading test conducted to clarify the performances of an existing brace member of a comparative example. -
FIG. 6 illustrates a brace member according to a second embodiment of the present invention.FIG. 6(a) is a side view of the brace member andFIG. 6(b) is a sectional view of a main portion of the brace member viewed sideways. -
FIG. 7 illustrates a brace member according to a third embodiment of the present invention.FIG. 7(a) is a side view of the brace member andFIG. 7(b) is a sectional view of a main portion of the brace member viewed sideways. -
FIG. 1 illustrates a brace member according to a first embodiment of the present invention.FIG. 1(a) is a side view of the brace member andFIG. 1(b) is a sectional view of a main portion of the brace member viewed sideways. Each of the diagrams is schematically drawn and the dimensions such as the relative size or thickness of each component are not limited to those illustrated in the drawings. InFIG. 1 , the left side is referred to as “a first side in the longitudinal direction” and the right side is referred to as “a second side in the longitudinal direction”. - In
FIG. 1 , abrace member 100 includes acore member 10, abuckling restraining member 20 through which thecore member 10 extends and that surrounds thecore member 10 to restrict out-of-plane deformation of thecore member 10, acap sleeve 30 in which afirst end portion 11 a of thecore member 10 on the first side in the longitudinal direction and afirst end portion 21 a of thebuckling restraining member 20 on the first side in the longitudinal direction are disposed, a cap-sleeve crevice 40 disposed on thecap sleeve 30 so as to protrude toward a side opposite to a side on which thecore member 10 and thebuckling restraining member 20 are disposed, the cap-sleeve crevice 40 serving as a joint for installing thebrace member 100 on an architectural structure (not illustrated), a reinforcingmember 50 in which asecond end portion 11 b of thecore member 10 on the second side in the longitudinal direction is disposed, and a reinforcing-member crevice 60 disposed on the reinforcingmember 50 so as to protrude toward a side opposite to a side on which thecore member 10 is disposed, the reinforcing-member crevice 60 serving as a joint for installing thebrace member 100 on an architectural structure (not illustrated). - The
core member 10 is a long member formed from a steel bar having a circular cross section. Amale screw thread 12 a is formed at thefirst end portion 11 a on the first side in the longitudinal direction and amale screw thread 12 b is formed at thesecond end portion 11 b on the second side in the longitudinal direction. For convenience of illustration, thecore member 10 made of a steel bar having a circular cross section is illustrated. However, thecore member 10 is not limited to the one having this cross section and may be formed from, for example, a steel pipe or may be formed by joining flat boards so as to have a cross-shaped cross section. - When the
core member 10 is made of a plastically deformable material, thecore member 10 has a higher effect. In order to prevent noises and an excessive increase in axial force due to friction that occur when the external circumferential surface of thecore member 10 and the internal circumferential surface of thebuckling restraining member 20 slide over each other, a liner made of a material such as a synthetic resin may be disposed on the external circumferential surface of thecore member 10. - The buckling
restraining member 20 is a steel pipe having a circular cross section and shorter than thecore member 10. Amale screw thread 22 a is formed at thefirst end portion 21 a on the first side in the longitudinal direction (a male screw thread or the like is not formed at asecond end portion 21 b on the second side in the longitudinal direction). - Here, the buckling restraining
member 20 may have a rectangular cross section. - The
cap sleeve 30 includes acylindrical portion 33 low in height. Afemale screw thread 34 is formed in afirst end surface 30 a, afemale screw thread 32 is formed in asecond end surface 30 b, and afemale screw thread 31 is formed through the center of thecylindrical portion 33. Thefemale screw thread 34, thefemale screw thread 32, and thefemale screw thread 31 are concentric with one another. - The
male screw thread 12 a of thecore member 10 is screwed on thefemale screw thread 31. Themale screw thread 22 a of the buckling restrainingmember 20 is screwed on thefemale screw thread 32. A male screw thread 43 (described below) of the cap-sleeve crevice 40 is screwed on thefemale screw thread 34. - A tapered
portion 30 c, whose outer diameter decreases toward thesecond end surface 30 b, is formed in a range of the external circumferential surface near thesecond end surface 30 b. However, instead of forming the taperedportion 30 c, the corner portion may be chamfered as in the case of thefirst end surface 30 a. - The cap-
sleeve crevice 40 serves as a joint for installing thebrace member 100 in an architectural structure (not illustrated). The cap-sleeve crevice 40 includes a disk-shaped portion 41, a plate-shapedportion 42 disposed on the first end surface of the disk-shaped portion 41, anattachment hole 44 that extends through the plate-shapedportion 42, and a male screw thread 43 disposed on the external circumferential surface of the disk-shaped portion 41. Here, the central axis of theattachment hole 44 and the central axis of the disk-shaped portion 41 perpendicularly cross each other (not geometrically accurately but industrially accurately cross each other). - In the above-described configuration, the
cap sleeve 30 and the cap-sleeve crevice 40 are separately manufactured and are integrated together with screw connection. However, the present invention is not limited to this configuration. Thecap sleeve 30 and the cap-sleeve crevice 40 may be integrated together by mechanical joining such as shrinkage fit or metallurgic joining such as welding. Alternatively, thecap sleeve 30 and the cap-sleeve crevice 40 may be originally manufactured as an integrated unit by, for example, casting. - The reinforcing
member 50 includes atubular portion 52 and a disk-shapedportion 55. Afemale screw thread 56 is formed in asecond end surface 50 b of the disk-shapedportion 55 and afemale screw thread 51 is formed through the center of the disk-shapedportion 55. - The
male screw thread 12 b of thecore member 10 is screwed on thefemale screw thread 51 and a male screw thread 65 (described below) of the reinforcing-member crevice 60 is screwed on thefemale screw thread 56. - The inner diameter of the
tubular portion 52 is constant in the longitudinal direction. The central axis of thetubular portion 52, the central axis of thefemale screw thread 51, and the central axis of thefemale screw thread 56 coincide with one another. Thetubular portion 52 surrounds thesecond end portion 21 b (an area extending a predetermined distance from anend surface 20 b) of the buckling restrainingmember 20 on the second side in the longitudinal direction (an area of the buckling restrainingmember 20 extending a predetermined distance from thesecond end surface 20 b on the second side in the longitudinal direction is inserted into the tubular portion 52). - A tapered
portion 50 c, whose outer diameter decreases toward the first end surface (corresponding to the tip end) 50 a on the first side in the longitudinal direction, is formed on the outer surface of thetubular portion 52. This configuration gives the impression of smoothly reinforcing the buckling restrainingmember 20, thereby improving the design. - Similar to the cap-
sleeve crevice 40, the reinforcing-member crevice 60 serves as a joint for installing thebrace member 100 on an architectural structure (not illustrated). The reinforcing-member crevice 60 includes a disk-shaped portion 61, a plate-shapedportion 62 disposed on the second end surface of the disk-shaped portion 61, anattachment hole 66 that extends through the plate-shapedportion 62, and a male screw thread 65 formed on the external circumferential surface of the disk-shaped portion 61. Here, the center line of theattachment hole 66 and the center line of the male screw thread 65 perpendicularly cross each other (not geometrically accurately but industrially accurately cross each other). - The reinforcing-
member crevice 60 has the same shape as the cap-sleeve crevice 40. - In the above-described configuration, the reinforcing
member 50 and the reinforcing-member crevice 60 are separately manufactured and are integrated together with screw connection. However, the present invention is not limited to this configuration. The reinforcingmember 50 and the reinforcing-member crevice 60 may be integrated together by mechanical joining such as shrinkage fit or metallurgic joining such as welding. Alternatively, the reinforcingmember 50 and the reinforcing-member crevice 60 may be originally manufactured as an integrated unit by, for example, casting. - In the
brace member 100, thefirst end portion 21 a of the buckling restrainingmember 20 on the first side in the longitudinal direction is disposed in thecap sleeve 30. A predetermined area of the buckling restrainingmember 20 extending from thesecond end surface 20 b in the longitudinal direction is surrounded with thetubular portion 52 of the reinforcingmember 50. Specifically, thetubular portion 52 surrounds the external circumferential surface of the buckling restrainingmember 20 and the thickness of thetubular portion 52 is not limited. Thus, the outer diameter (and the inner diameter) and the thickness can be increased compared with an existing sleeve (disposed in a gap between the core member and the buckling restraining member), whereby the stiffness can be enhanced. In order to prevent a bending moment from affecting the buckling restrainingmember 20 to a large extent as a result of the reinforcing-member crevice 60 being eccentrically located due to excessive rotation and deformation, preferably, a length lk for which the buckling restrainingmember 20 is surrounded by thetubular portion 52 and a difference ek between the outer diameter of the buckling restraining member 20 (corresponding to a “bucking restraining member”) and the inner diameter of the reinforcingmember 50 has a relationship of ek/lk≦0.05. - Here, deformation of a predetermined area of the buckling restraining
member 20 extending from thesecond end surface 20 b on the second side in the longitudinal direction is restricted by thetubular portion 52 of the reinforcingmember 50 having high stiffness, whereby thecore member 10 is prevented from being buckled (this is separately described in detail). - The outer diameter of the reinforcing
member 50 decreases toward thefirst end surface 50 a (tip end) on the first side in the longitudinal direction (toward the center of the buckling restrainingmember 20 in the longitudinal direction). Thus, the weight reduction can be enhanced and the design can be improved while the strength at each position in the longitudinal direction is secured. - Both end portions of the
core member 10 are respectively connected with screw threads to thecap sleeve 30 and the reinforcingmember 50. Thus, by having these screw threads in opposite handedness (for example, themale screw thread 12 a and thefemale screw thread 31 are right-handed screws and themale screw thread 12 b and thefemale screw thread 51 are left-handed screws), the distance between theattachment hole 44 and theattachment hole 66 can be adjusted, whereby installation of thebrace member 100 can be facilitated. -
TABLE 1 Buckling Restraining Reinforcing Core Member Member Member Full Length DS σy Ny DB tB lK tK Crevice Gap eS l Ref. mm N/mm2 kN mm mm mm mm lC mm ek mm mm mm No. 1 48.50 622 1149 120.0 28 250 12 326.5 4.0 15.5 2500 No. 2 1149 114.3 25 15.8 -
FIG. 2 illustrates a specimen that undergoes a loading test to evaluate the performances of the brace member according to the first embodiment of the present invention and is a sectional view viewed sideways to define the length of each component. Some reference signs are not shown. Table 1 shows the dimensions or the like of each portion of the specimens (No. 1 and No. 2). - In
FIG. 2 , the outer diameter of thecore member 10 of each of the specimen No. 1 and the specimen No. 2 is denoted with “DS”. The yield point of thecore member 10 is denoted with “σy”, the product of the cross section of thecore member 10 and the yield point σy is denoted with “Ny”. - The outer diameter of the buckling restraining member 20 (corresponding to the “buckling restraining member”) is denoted with “DB”, the thickness of the buckling restraining
member 20 is denoted with “tB”, the distance between thesecond end surface 20 b of the buckling restrainingmember 20 on the second side in the longitudinal direction and the center of theattachment hole 66 of the reinforcing-member crevice 60 is denoted with “lc”, and the distance between thesecond end surface 20 b of the buckling restrainingmember 20 on the second side in the longitudinal direction and thefirst end surface 50 a of the reinforcingmember 50 on the first side in the longitudinal direction is denoted with “lk”. Here, lk has been described above. - The distance between the center of the
attachment hole 44 of the cap-sleeve crevice 40 and thesecond end surface 30 b of thecap sleeve 30 is denoted with “FlJ”, the distance between thesecond end surface 30 b of thecap sleeve 30 and thefirst end surface 50 a of the reinforcingmember 50 is denoted with “lB”, and the distance between thefirst end surface 50 a of the reinforcingmember 50 and theattachment hole 66 of the reinforcing-member crevice 60 is denoted with “MlJ”. - The distance between the center of the
attachment hole 44 of the cap-sleeve crevice 40 and the center of theattachment hole 66 of the reinforcing-member crevice 60 is denoted with “l”. - Furthermore, the difference between the outer diameter of the
core member 10 and the inner diameter of the buckling restrainingmember 20 is denoted with “eS”, and the difference between the outer diameter of the buckling restrainingmember 20 and the inner diameter of the reinforcingmember 50 is denoted with “ek”. Here, ek has been described above. - Moreover, the thickness of the reinforcing
member 50 at thefirst end surface 50 a (tip end) on the first side in the longitudinal direction is denoted with “tK”. -
TABLE 2 Buckling Restraining Core Member Member Full Length DS σy Ny DB tB eS l Ref. mm N/mm2 kN mm mm mm mm No. 3 46.00 635 1055 114.3 25 18.3 2500 -
FIG. 3 illustrates a specimen that undergoes a loading test to evaluate the performances of an existing brace member of a comparative example and is a sectional view viewed sideways to define the length of each component. Table 2 shows the dimensions or the like of each component of a comparative example (No. 3). - In
FIG. 3 , the outer diameter of acore member 910 of a comparative example (No. 3) 900 is denoted with “D5”, the outer diameter of a buckling restrainingmember 20 is denoted with “DB”, and the thickness of the buckling restrainingmember 920 is denoted with “tB”. The yield point of thecore member 910 is denoted with “σy”, and the product of the cross section of thecore member 10 and the yield point σy is denoted with “Ny”. -
Integrated crevices 940 and 960 (at which 941 and 961 are respectively formed) are disposed onfemale screw threads end portions 911 a and 911 b (at whichmale screw threads 912 a and 912 b are respectively formed) of thecore member 910. The distance between the center of aconnection hole 944 of the firstintegrated crevice 940 and the center of aconnection hole 966 of the secondintegrated crevice 960 is denoted with “l”. - The first end portion 911 a (at which the male screw thread 912 a is formed) of the
core member 910 and afirst end portion 921 a (at which afemale screw thread 922 a is formed) of the buckling restrainingmember 920 are connected together with a cap sleeve 930 (at which afemale screw thread 931 and amale screw thread 932 are formed). - Furthermore, a
tubular sleeve 970 is disposed at a position near thesecond end portion 911 b of thecore member 910. Thesleeve 970 is inserted into the buckling restrainingmember 920 by a distance “L” from asecond end surface 920 b of the buckling restrainingmember 920. Here, the difference between the outer diameter of thesleeve 970 and the inner diameter of asecond end portion 921 b of the buckling restrainingmember 920 is denoted with “eS”. - From the description given above, the reinforcing
member 50 of the specimen No. 2 has an inner diameter of “114.3+4.0=118.3 (mm)” and an outer diameter of greater than or equal to “118.3+2×12=142.3 (mm)”. Thus, the geometrical moment of inertia is greater than or equal to “ten millions (mm4)”. - On the other hand, the
sleeve 970 of the specimen No. 3, which is a comparative example, has an inner diameter of “46.0 (mm)” and an outer diameter of smaller than or equal to “114.3−2×25=64.3 (mm)”. Thus, the geometrical moment of inertia is smaller than or equal to 0.62 millions (mm4). - Specifically, the geometrical moment of inertia of the reinforcing
member 50 of aspects of the present invention is approximately 17 times as high (great) as the geometrical moment of inertia of the existingsleeve 970 of a comparative example. Thus, the reinforcingmember 50 having such high stiffness restricts out-of-plane deformation of the buckling restrainingmember 20. -
FIG. 4 has axial force-axial strain charts showing the results of the loading test conducted to evaluate the performances of the brace member according to the first embodiment of the present invention.FIG. 4(a) is a chart for a specimen No. 1 andFIG. 4(b) is a chart for a specimen No. 2. The loading test is a reversed cyclic loading test in which thecore member 10 is repeatedly and alternately compressed and stretched. - In
FIG. 4(a) , firstly, thecore member 10 is compressed by 0.25% (the “distance l” between the center of theattachment hole 44 of the cap-sleeve crevice 40 and the center of theattachment hole 66 of the reinforcing-member crevice 60 is reduced by 6.25 mm). At this time, the compressive load and the compressive strain are shown in a first quadrant. - Thereafter, the
core member 10 is stretched by 0.25% (the distance l is increased by 6.25 mm). At this time, the tensile load and the tensile strain are shown in a third quadrant. - Furthermore, the
core member 10 is compressed by 0.5% (the distance l is reduced by 12.5 mm) and then thecore member 10 is stretched by 0.5% (the distance l is increased by 12.5 mm). - Moreover, the
core member 10 is compressed by 1.0% (the distance l is reduced by 25 mm) and then thecore member 10 is stretched by 1.0% (the distance l is increased by 25 mm). This loading is regarded as one cycle and this cycle is repeated five times. - Finally, the
core member 10 is compressed by 2.0% (the distance l is reduced by 50 mm) and then thecore member 10 is stretched by 2.0% (the distance l is increased by 50 mm). This loading is regarded as one cycle (or referred to as a “final cycle”, below). This cycle is repeated until thecore member 10 is buckled or broken. - The
core member 10 of the specimen No. 1 was broken at the fourth stretch after the final cycle had been repeated three times. - In
FIG. 4(b) , as in the case of the specimen No. 1, thecore member 10 of the specimen No. 2 was broken at the fourth stretch after the final cycle had been repeated three times. - Specifically, the
core member 10 of neither the specimen No. 1 nor the specimen No. 2 was buckled. This result reveals that the buckling restrainingmember 20 and the reinforcingmember 50 restrict out-of-plane deformation of thecore member 10. -
FIG. 5 is an axial force-axial strain chart showing the results of the cyclic loading test conducted to evaluate the performances of an existing brace member of a comparative example. As in the case of the specimens No. 1 and No. 2, the cyclic loading test is a reversed cyclic loading test in which thecore member 10 is repeatedly and alternately compressed and stretched. - In
FIG. 5 , thecore member 910 of the specimen No. 3 was subjected to one cycle of compression and stretch by 0.1%, two cycles of compression and stretch by 0.25%, and two cycles of compression and stretch by 0.5%. Then, when thecore member 910 was compressed by 1.0%, thecore member 910 was buckled. - Thus, also through the comparison with the
sleeve 970 of an existingbrace member 900, the brace member of aspects of the present invention has been proved to be a brace member in which the reinforcingmember 50 has high (great) bending strength. -
FIG. 6 illustrates a brace member according to a second embodiment of the present invention.FIG. 6(a) is a side view of the brace member andFIG. 6(b) is a sectional view of a main portion of the brace member viewed sideways. Portions the same as or corresponding to the portions of the first embodiment are denoted with the same reference signs and some of them are not described herein. The dimensions such as the relative size or thickness of each component are not limited to those illustrated in the drawings. - In
FIG. 6 , abrace member 200 includes acore member 10, a buckling restrainingmember 20 through which thecore member 10 extends and that surrounds thecore member 10 to restrict out-of-plane deformation of thecore member 10, acap sleeve 230 in which afirst end portion 11 a of thecore member 10 on the first side in the longitudinal direction and afirst end portion 21 a of the buckling restrainingmember 20 on the first side in the longitudinal direction are disposed, a cap-sleeve crevice 40 disposed on thecap sleeve 230 so as to protrude toward a side opposite to a side on which thecore member 10 and the buckling restrainingmember 20 are disposed, the cap-sleeve crevice 40 serving as a joint for installing thebrace member 200 on an architectural structure (not illustrated), a reinforcingmember 250 in which asecond end portion 11 b of thecore member 10 on the second side in the longitudinal direction is disposed, and a reinforcing-member crevice 60 disposed on the reinforcingmember 250 so as to protrude toward a side opposite to a side on which thecore member 10 is disposed, the reinforcing-member crevice 60 serving as a joint for installing thebrace member 200 on an architectural structure (not illustrated). - Specifically, the
cap sleeve 230 and the reinforcingmember 250 of thebrace member 200 do not respectively have the taperedportion 30 c and the taperedportion 50 c, which are respectively formed on the outer surface of thecap sleeve 30 and the outer surface of the reinforcingmember 50 of the brace member 100 (first embodiment). Except for this point, thebrace member 200 is similar to thebrace member 100. - Thus, as in the case of the
brace member 100, in thebrace member 200, the buckling restrainingmember 20 reinforced with the reinforcingmember 250 restricts out-of-plane deformation of thecore member 10. Thus, thebrace member 200 has high (great) bending strength and is manufactured at low costs. - Specifically, when the
cap sleeve 230 and the reinforcingmember 250 are manufactured by casting, the die sets are simplified. In addition, thebrace member 200 can be manufactured at low costs by performing welding connection between steel pipes or welding connection between a steel pipe and a circular plate (or a disk having a center hole). -
FIG. 7 illustrates a brace member according to a third embodiment of the present invention.FIG. 7(a) is a side view of the brace member andFIG. 7(b) is a sectional view of a main portion of the brace member viewed sideways. Portions the same as or corresponding to the portions of the first embodiment are denoted with the same reference signs and some of them are not described. The dimensions such as the relative size or thickness of each component are not limited to those illustrated in the drawings. - In
FIG. 7 , a brace member 300 includes a core member 10, a buckling restraining member 20 through which the core member 10 extends and that surrounds the core member 10 to restrict out-of-plane deformation of the core member 10, a first-side reinforcing member 350 a in which a first end portion 11 a of the core member 10 on the first side in the longitudinal direction and a first end portion 21 a of the buckling restraining member 20 on the first side in the longitudinal direction are disposed, a reinforcing-member crevice 60 disposed on the first-side reinforcing member 350 a so as to protrude toward a side opposite to a side on which the core member 10 and the buckling restraining member 20 are disposed, the reinforcing-member crevice 60 serving as a joint for installing the brace member 300 on an architectural structure (not illustrated), a second-side reinforcing member 350 b in which a second end portion 11 b of the core member 10 on the second side in the longitudinal direction and a second end portion 21 b of the buckling restraining member 20 on the second side in the longitudinal direction are disposed, and a reinforcing-member crevice 60 disposed on the second-side reinforcing member 350 b so as to protrude toward a side opposite to a side on which the core member 10 and the buckling restraining member 20 are disposed, the reinforcing-member crevice 60 serving as a joint for installing the brace member 300 on an architectural structure (not illustrated). - Specifically, the
brace member 300 includes a first-side reinforcing member 350 a instead of thecap sleeve 30 of the brace member 100 (first embodiment). The first-side reinforcing member 350 a and the second-side reinforcing member 350 b correspond to the reinforcingmember 50. - Thus, the
first end portion 21 a of the buckling restrainingmember 20 is reinforced with the first-side reinforcing member 350 a, in the same manner as thesecond end portion 21 b reinforced with the second-side reinforcing member 350 b. Except for this point, thebrace member 300 is the same as thebrace member 100. - Thus, in the
brace member 300, the buckling restrainingmember 20 reinforced with the first-side reinforcing member 350 a and the second-side reinforcing member 350 b restricts out-of-plane deformation of thecore member 10. Thus, thebrace member 300 has high (great) bending strength and is manufactured at low costs. - Specifically, this configuration eliminates the need to manufacture the
cap sleeve 30. Thus, the die set for casting thecap sleeve 30 is not needed and the number of types of components constituting thebrace member 300 is reduced, whereby stock control is facilitated. - The
brace member 300 includes a pair of reinforcingmembers 50, but may include a pair of reinforcingmembers 250 instead of the reinforcingmembers 50. - Aspects of the present invention achieve a brace member having a high (great) bending strength with a simple structure. The brace member is also usable for core members having cross-sections of various different shapes. Thus, the brace member according to aspects of the present invention is widely usable as a brace member for dealing with various different demands of architectural structures.
-
-
- 10 core member
- 11 a first end portion
- 11 b second end portion
- 12 a male screw thread
- 12 b male screw thread
- 20 buckling restraining member
- 20 b second end surface
- 21 a first end portion
- 21 b second end portion
- 22 a male screw thread
- 30 cap sleeve
- 30 a first end surface
- 30 b second end surface
- 30 c tapered portion
- 31 female screw thread
- 32 female screw thread
- 33 cylindrical portion
- 34 female screw thread
- 40 cap-sleeve crevice
- 41 disk-shaped portion
- 42 plate-shaped portion
- 43 male screw thread
- 44 attachment hole
- 50 reinforcing member
- 50 a first end surface (tip end)
- 50 b second end surface
- 50 c tapered portion
- 51 female screw thread
- 52 tubular portion
- 53 disk-shaped portion
- 56 female screw thread
- 60 reinforcing-member crevice
- 61 disk-shaped portion
- 62 plate-shaped portion
- 65 male screw thread
- 66 attachment hole
- 100 brace member (first embodiment)
- 200 brace member (second embodiment)
- 230 cap sleeve
- 250 reinforcing member
- 300 brace member (third embodiment)
- 350 a first-side reinforcing member
- 350 b second-side reinforcing member
- 900 brace member (comparative example)
- 910 core member
- 911 a end portion
- 911 b end portion
- 912 a male screw thread
- 912 b male screw thread
- 920 buckling restraining member
- 920 b end surface
- 921 a end portion
- 921 b end portion
- 922 a female screw thread
- 922 b inner surface
- 930 cap sleeve
- 931 female screw thread
- 932 male screw thread
- 940 integrated crevice
- 941 female screw thread
- 944 connection hole
- 960 integrated crevice
- 961 female screw thread
- 966 connection hole
- 970 sleeve
Claims (4)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2014103271A JP6204263B2 (en) | 2014-05-19 | 2014-05-19 | Brace material |
| JP2014-103271 | 2014-05-19 | ||
| PCT/JP2015/002421 WO2015177987A1 (en) | 2014-05-19 | 2015-05-13 | Brace member |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20170081845A1 true US20170081845A1 (en) | 2017-03-23 |
Family
ID=54553672
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US15/310,631 Abandoned US20170081845A1 (en) | 2014-05-19 | 2015-05-13 | Brace member |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US20170081845A1 (en) |
| JP (1) | JP6204263B2 (en) |
| KR (2) | KR102025055B1 (en) |
| CN (1) | CN106414871A (en) |
| TW (1) | TWI615535B (en) |
| WO (1) | WO2015177987A1 (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170030701A1 (en) * | 2015-07-29 | 2017-02-02 | Corebrace, Llc | Displacement measurement systems and methods |
| US11299901B2 (en) * | 2017-02-16 | 2022-04-12 | John Damian Allen | Control structure |
| US11828083B2 (en) | 2017-02-16 | 2023-11-28 | John Damian Allen | Control structure with rotary force limiter and energy dissipater |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105735507B (en) * | 2016-03-10 | 2018-01-30 | 苏州科技学院 | A kind of tension and compression type magnetic shape memory alloy Multimode Intelligent damper |
| CN106639027B (en) * | 2017-01-22 | 2022-04-22 | 西安交通大学 | Self-stressing anti-buckling support for threaded connection and assembling method thereof |
| CN112554361A (en) * | 2020-11-30 | 2021-03-26 | 中原工学院 | Assembled replaceable two-stage buckling-restrained energy-dissipation supporting component |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090260304A1 (en) * | 2002-02-21 | 2009-10-22 | Oiles Corporation | Damper and vibration damping structure using the same |
| US20140305048A1 (en) * | 2011-11-25 | 2014-10-16 | Jfe Steel Corporation | Brace member |
| US20150159361A1 (en) * | 2012-07-30 | 2015-06-11 | Jfe Civil Engineering & Construction Corp. | Pin joint type structural member made of double steel pipe for restraining buckling thereof |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0811891B2 (en) * | 1992-09-11 | 1996-02-07 | 川鉄建材工業株式会社 | Structural material for double steel tube truss structure and joining method thereof |
| JP3702818B2 (en) * | 2001-07-26 | 2005-10-05 | Jfeシビル株式会社 | Double steel pipe type earthquake-resistant structural material |
| US6837010B2 (en) * | 2002-12-05 | 2005-01-04 | Star Seismic, Llc | Pin and collar connection apparatus for use with seismic braces, seismic braces including the pin and collar connection, and methods |
| JP4816091B2 (en) * | 2006-01-13 | 2011-11-16 | Jfeスチール株式会社 | Double steel pipe brace material |
| CN100451259C (en) * | 2007-01-12 | 2009-01-14 | 清华大学 | Steel tube anti-flex energy dissipation support |
| TWI429811B (en) * | 2008-08-30 | 2014-03-11 | Yu Guang Lai | The energy dissipation and vibration reduction structure element |
| JP5409472B2 (en) * | 2010-03-24 | 2014-02-05 | 株式会社ブリヂストン | Bracing and seismic structure |
| CN203034634U (en) * | 2013-01-16 | 2013-07-03 | 财团法人国家实验研究院 | Pinned Buckling Restraint Brace |
| JP2015017371A (en) * | 2013-07-09 | 2015-01-29 | 株式会社竹中工務店 | Buckling stiffening brace |
-
2014
- 2014-05-19 JP JP2014103271A patent/JP6204263B2/en active Active
-
2015
- 2015-05-13 KR KR1020197006754A patent/KR102025055B1/en active Active
- 2015-05-13 US US15/310,631 patent/US20170081845A1/en not_active Abandoned
- 2015-05-13 KR KR1020167031207A patent/KR20170007282A/en not_active Ceased
- 2015-05-13 WO PCT/JP2015/002421 patent/WO2015177987A1/en active Application Filing
- 2015-05-13 CN CN201580025754.5A patent/CN106414871A/en active Pending
- 2015-05-19 TW TW104115816A patent/TWI615535B/en active
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090260304A1 (en) * | 2002-02-21 | 2009-10-22 | Oiles Corporation | Damper and vibration damping structure using the same |
| US20140305048A1 (en) * | 2011-11-25 | 2014-10-16 | Jfe Steel Corporation | Brace member |
| US9045913B2 (en) * | 2011-11-25 | 2015-06-02 | Jfe Steel Corporation | Brace member |
| US20150159361A1 (en) * | 2012-07-30 | 2015-06-11 | Jfe Civil Engineering & Construction Corp. | Pin joint type structural member made of double steel pipe for restraining buckling thereof |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20170030701A1 (en) * | 2015-07-29 | 2017-02-02 | Corebrace, Llc | Displacement measurement systems and methods |
| US9989349B2 (en) * | 2015-07-29 | 2018-06-05 | Corebrace, Llc | Displacement measurement systems and methods |
| US11299901B2 (en) * | 2017-02-16 | 2022-04-12 | John Damian Allen | Control structure |
| US11828083B2 (en) | 2017-02-16 | 2023-11-28 | John Damian Allen | Control structure with rotary force limiter and energy dissipater |
| US11866956B2 (en) | 2017-02-16 | 2024-01-09 | John Damian Allen | Force limiter and energy dissipater |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106414871A (en) | 2017-02-15 |
| JP2015218498A (en) | 2015-12-07 |
| JP6204263B2 (en) | 2017-09-27 |
| WO2015177987A1 (en) | 2015-11-26 |
| KR20190026982A (en) | 2019-03-13 |
| TW201600691A (en) | 2016-01-01 |
| KR102025055B1 (en) | 2019-09-24 |
| TWI615535B (en) | 2018-02-21 |
| KR20170007282A (en) | 2017-01-18 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: JFE CIVIL ENGINEERING & CONSTRUCTION CORPORATION, Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:KINOSHITA, TOMOHIRO;ISHII, TAKUMI;MIYAGAWA, KAZUAKI;AND OTHERS;SIGNING DATES FROM 20160728 TO 20160802;REEL/FRAME:040899/0752 Owner name: JFE STEEL CORPORATION, JAPAN Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:KINOSHITA, TOMOHIRO;ISHII, TAKUMI;MIYAGAWA, KAZUAKI;AND OTHERS;SIGNING DATES FROM 20160728 TO 20160802;REEL/FRAME:040899/0752 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |