The present invention relates to hysteretic damping for structures used in light-framed constructions, and in particular to a lateral bracing system constructed to provide a high degree of energy dissipation through hysteretic damping along with high initial stiffness so that energy is dissipated at low displacement thresholds within a light-framed construction.
Shear stresses due to natural phenomena such as seismic activity and high winds can have devastating effects on the structural integrity of light-framed constructions. Lateral forces generated during such natural phenomena may cause the top portion of a wall to move laterally with respect to the bottom portion of the wall, which movement can result in damage or structural failure of the wall and, in some instances, collapse of the building.
In constructions such as residences and small buildings, lateral bracing systems were developed to counteract the potentially devastating effects of shear stress on the structural integrity of light-framed constructions. Although various designs are known, one type of lateral bracing system includes vertical studs spaced from each other and horizontal beams affixed to and extending between the studs. The beams are affixed to the studs in a manner aimed at increasing structural performance of the connection under lateral loads.
Many conventional lateral bracing systems perform well initially under lateral loads, but yield and fail upon the repetitive lateral loads which often occur during significant seismic activity and high winds. Upon appreciable yield or failure of the lateral bracing system, the entire system must be replaced.
Another consideration relates to clearances of components with respect to each other as the beam rotates relative to the column under lateral loads.
The present invention will now be described with reference to the figures, which in embodiments relate to a lateral bracing system having high initial stiffness and including yield links capable of effectively dissipating energy generated within the lateral bracing system under lateral loads. It is understood that the present invention may be embodied in many different forms and should not be construed as being limited to the embodiments set forth herein. Rather these embodiments are provided so that this disclosure will be thorough and complete and will fully convey the invention to those skilled in the art. Indeed, the invention is intended to cover alternatives, modifications and equivalents of these embodiments, which are included within the scope and spirit of the invention as defined by the appended claims. Furthermore, in the following detailed description of the present invention, numerous specific details are set forth in order to provide a thorough understanding of the present invention. However, it will be clear to those of ordinary skill in the art that the present invention may be practiced without such specific details.
Referring now for example to
The beam 102 is affixed to the column 104 by means of a lateral bracing system 300. The lateral bracing system is comprised of a pair of buckling-restrained braced devices 302, one on each of the top and bottom flanges 110 of beam 102. Each buckling-restrained braced device 302 may include a flat, “dog-bone” shaped yield member 304 (
A shear tab 222 may further be provided between the beam 102 and column 104. The shear tab 222 may be affixed as by bolting, welding or gluing to a flange of column 104 and as by bolting to the central diaphragm 112 of beam 102. As shown, the shear tab 222 may include bolt holes 228 comprising a central bolt hole 228a and a pair of edge bolt holes 228b. The central bolt hole 228a may be circular, while the edge bolt holes 228b may be oblong, with a length dimension oriented parallel to the flanges 110 of beam 102 when assembled. As explained below, upon lateral loads of sufficient magnitude, the beam 102 may rotate about an axis through central bolt hole 228a. The oblong edge bolt holes 228b allow translation of the bolts affixed to the central diaphragm of the beam 102 within the edge bolt holes upon rotation of the beam 102 relative to column 104.
In operation, the pair of buckling-restrained braced devices 302 operate in tandem to oppose rotation of the beam relative to the column (i.e., rotation about the central hole 228a of shear tab 222) under a lateral loads. Attempted rotation in a first direction will place the first of the devices 302 in tension and the second of the devices in compression. Attempted rotation in the opposite direction will place the first of the devices in compression and the second in tension.
The yield member 304 of the respective devices 302 provides high initial stiffness and tensile resistance to relative movement between the column 104 and the beam 102 under lateral loads, but provides stable yielding and energy dissipation under lateral loads above a predictable and controlled level. In particular, the bending strength of the column and beam could be designed to exceed the moment capacity of the yield members 304, and in particular, the thinner center portions of yield members 304. Thus, the yield members 304 yield under lateral loads before yielding or failure of the column or beam, and any damage is limited to the yield links which may be easily removed and replaced. The buckling restraint blocks 316 prevent buckling of the yield members under a compressive load. The shear tab 222 is provided to oppose vertical shear (i.e., along the length of column 104) under a vertical load or as created during lateral loading of the bracing system. The shear tab 222 is also provided to oppose axial force (i.e., along the length of beam 102) under a lateral load in the bracing system.
As noted in the Background, it is one advantage of the present technology to avoid interferences and binding of components as the beam 102 pivots relative to column 104 under lateral loads. For example, in one embodiment, the beam 102 is coped at its end adjacent the column 104 to include angled sections 114 (as numbered for example in
The angle sections 114 define an extended web section 112a to which the shear tab 222 is bolted. Each angled section 114 may form an angle, θ, with the flange 110 which may vary between 80° and 40°, such as for example 60°, those the angle θ may be lesser or greater than that in further embodiments. In embodiments, the flanges may be coped so that each flange 110 may end (and the angled section 114 begins) at an endpoint 110a that is, for example, 3 inches from the distal edge of the extended web section 112a. This position is aligned along a transverse (vertical) axis, t, orthogonal to the surface of flanges 110, which passes through a center point of the center bolt hole 228a. However, it is possible that the endpoint 110a of each flange 110 may end at a point that is spaced forward or back from the transverse axis t. For example, each flange may end at a point that is ⅛th inch or 1/16th inch forward or back from the transverse axis t. The endpoints 110a of flanges 110 may end at points that are spaced other distances from the transverse axis tin further embodiments.
Coping the beam 102 in this manner provides advantages in that, without coping the beam 102 as described above, the flanges 110 can bear against, interfere with or bind against the column-mounted plate 308. Since the plate 308 can offer a fair amount of resistance to this action, forces build within the beam which create additional unwanted shear forces in the bolts on the shear tab 222. Additionally, by bearing against the column-mounted plate 308, unwanted forces are generated on the column-mounted plate 308 and yield member 304, as well as the bolts, weld or glue fastening the column-mounted plate 308 to column 104.
However, by coping the beam 102 as described herein, these problems are avoided.
The horizontal portion 308b may be formed of a flat, unitary construction with beam-mounted plate 310 and yield plate 312. The horizontal portion 308b and plates 308, 310 and 312 may for example be formed from a single piece of ¼ inch steel. The horizontal portion 308b and plates 308, 310 and 312 may for example be formed to other thicknesses in further embodiments.
The column-mounted plate 308 and beam-mounted plate 310 may each have a width (across the width of the flanges of beam 102) approximately equal to the width of the flanges of beam 102, such as for example 7.00 inches. The yield plate 312 may have a width (across the width of the flanges of beam 102) that is less than the width of the plates 308, 312. The width of plate 312 may be between 1 and 6 inches in an embodiment, between 1 and 3 inches in a further embodiment, and between 2 and 3 inches in a further embodiment. The width of yield plate 312 may be other dimensions, with the provision that the yield plate have a smaller width than the column and beam-mounted plates 308, 310.
The buckling-retrained assembly 302 further includes a buckling restraint member 316 and a pair of spacer blocks 318 (one of which is omitted from
The spacer blocks 318 are sized to fit in between the horizontal portion 308b of column-mounted plate 308 and beam-mounted plate 310, on either side of yield plate 312, when the buckling-retrained assembly 302 is assembled together as explained below. The spacer blocks 318 may have the same thickness as the yield member 304.
The yield member 304 including column-mounted plate 308, beam-mounted plate 310, and yield plate 312 may be affixed to the column 104, either at the jobsite or remote from the jobsite. In one embodiment, the vertical portion 308a includes holes 320 (
Thereafter, at the jobsite, the beam-mounted plate 310 may be bolted to the beam 102 via a plurality of bolts 326. While the figures show six bolts 326, there may be more or less than that in further embodiments. At this point, the yield member 304 is affixed to both the beam 102 and column 104. The beam and column may also be attached to each other by a shear tab 222 as described above. Shear tab 222 may be affixed to the column 104 as by welding, gluing or bolting to a flange of column 104 and to the web of beam 102 as by bolts.
In embodiments, the buckling restraint assemblies 302 and shear tab 222 may affix beam 102 to column 104 at the jobsite with bolts only, thus simplifying construction by omitting welding. However, in further embodiments, the beam-mounted plate 310 and/or shear tab 222 may be affixed to beam 102 by welding or gluing. In further embodiments, the yield member 304 may be affixed to the beam 102 first, either before or at the jobsite, and then affixed to the column 104.
Although the invention has been described in detail herein, it should be understood that the invention is not limited to the embodiments herein disclosed. Various changes, substitutions and modifications may be made thereto by those skilled in the art without departing from the spirit or scope of the invention as described and defined by the appended claims.
This application claims priority to U.S. Provisional Patent Application No. 62/743,176, entitled “MOMENT FRAME INCLUDING LATERAL BRACING SYSTEM AND COPED BEAM”, filed Oct. 9, 2018, which application is incorporated herein by reference in its entirety.
Number | Name | Date | Kind |
---|---|---|---|
4696137 | Schleich | Sep 1987 | A |
6474902 | Beauvoir | Nov 2002 | B1 |
6739099 | Takeuchi | May 2004 | B2 |
7497054 | Takeuchi | Mar 2009 | B2 |
8074359 | Bong | Dec 2011 | B2 |
10669718 | Pryor | Jun 2020 | B2 |
10697192 | Richard | Jun 2020 | B2 |
20020184836 | Takeuchi | Dec 2002 | A1 |
20040187430 | Takeuchi | Sep 2004 | A1 |
20040244330 | Takeuchi | Dec 2004 | A1 |
20050257451 | Pryor | Nov 2005 | A1 |
20060144006 | Suzuki | Jul 2006 | A1 |
20100205891 | Bong | Aug 2010 | A1 |
20190292783 | Pryor | Sep 2019 | A1 |
20190330873 | Richard | Oct 2019 | A1 |
20200291653 | Pryor | Sep 2020 | A1 |
Number | Date | Country |
---|---|---|
103114733 | May 2013 | CN |
2468986 | Jun 2012 | EP |
2002371626 | Dec 2002 | JP |
2004278293 | Oct 2004 | JP |
Entry |
---|
International Search Report and Written Opinion dated Jan. 16, 2020 in International Patent Application No. PCT/US2019/055344. |
Number | Date | Country | |
---|---|---|---|
20200109556 A1 | Apr 2020 | US |
Number | Date | Country | |
---|---|---|---|
62743176 | Oct 2018 | US |