This application is the national phase entry of International Application No. PCT/TR2017/050253, filed on Jun. 7, 2017, which is based upon and claims priority to Turkish Application No. 2016/07751, filed on Jun. 8, 2016, the entire contents of which are incorporated herein by reference.
The invention subject to the application is related to a torsional hysteretic damper that has been designed for braced frames. The aim of the torsional hysteretic damper is to reduce displacement and the associated damage on structural elements, by dampening (dissipating) earthquake energy that impacts structures.
Dampers dampen (dissipate) the kinetic energy that has been loaded on them. If explanation needs to be made in terms of force and displacement instead of energy, it can be said that, the force applied to the structure by the damper between two mounting points of the damper opposes the relative displacement between two mounting points of the device and hence leads to reduced displacement and thus reduced damage in the structure to which it is mounted. This force is referred to as the reaction force of the damper. Damping in hysteretic dampers is obtained by using a metal that will yield, develop plastic strain and act as a hysteretic energy-dissipating element.
Deployment of energy dissipation devices in building frames is a well-known practice. These devices include viscous dampers, hysteretic dampers, friction-based energy dissipaters and buckling-restraint braces (BRB). Among the steel dampers developed for use in braced frames, the most well-known is the added damping and stiffness (ADAS) elements and its variation, triangular-plate added damping and stiffness (TADAS). ADAS is composed of a series of X-shaped plates clamped and fixed at top and bottom through a bolted connection. Full-scale tests have shown advantages of incorporation of ADAS dampers in terms of reduction of damage in primary structural members, reduction of inter-story deformations at minor and moderate level earthquakes and stable hysteretic behavior of the bracing system. E-shaped and C-shaped elements are another type of plate-bending metallic dampers for Chevron-type bracing systems. Round-hole and double X-shaped dampers also belong to this class of dissipating elements. These two dampers also are of plate-bending type. Another type of plate-bending based damper is the Steel Slit Damper, fabricated from a standard structural wide-flange section with a number of slits cut from the web. Bucking-restraint brace (BRB) is another type of energy dissipation element used in braced frames. In a BRB the brace is encased in a mortar-filled steel tube, while being detached from the mortar using some ‘un-bonding’ agent. The overall assembly is an element in which the inner steel core is free to slide and thus free to deform axially independent of the outer section, while in bending their flexural resistance is added, producing a section stiff in flexure and thus strong against buckling. The subject of the present invention, torsional hysteretic damper, is a mechanical device designed to utilize torsional yielding of cylindrical energy dissipaters (EDs) made of ductile steel to dissipate the imposed energy through seismic movements in a structure. Torsional hysteretic damper converts the translational motion imposed on it at its two connection points into twisting at the energy dissipaters which are designed to yield in torsion and dissipate energy.
The invention subject to the application is related to a torsional hysteretic damper that has been designed for braced frames. The purpose of the torsional hysteretic damping device is to realize energy dissipation in steel cylindrical energy dissipaters under torsion through converting the translational movement at the mounting points of the device into twisting at the cylindrical energy dissipaters. The energy dissipater must not be bent while the translational motion is converted into twisting, so that the cylindrical energy dissipaters yield smoothly. Lateral supports are provided to prevent the energy dissipaters from bending.
The figures are described below.
The parts in the figures which have been drawn, so as to better explain the torsional hysteretic damper designed for braced frames developed with this invention have each been numbered and the references of each number have been explained below.
The invention subject to the application is related to a hysteretic torsion damper that has been designed for cross frames. The torsional hysteretic damper comprises:
The purpose of the torsional hysteretic damper (1) is to translate the translational movement at the end points of the arms (2) into a twisting at the cylindrical energy dissipaters. (
As it has been mentioned above, the guide strips (11) enable the connection plate (9) to move laterally and prevent out-of-plane bending. The guide strips (11) are screwed on one side to the torsional restraint plate (4) and on the other side to the cover plate (10). Shaped stainless steel plates (12) screwed to the connection plate (9) that is in contact with the guide strips (11) via the low friction slider bands (16) have been provided to allow for low-friction sliding. connection plate. The torsional restraint plate (4) and the cover plate (10) that is shown in
As shown in
In order to summarize, the torsional hysteretic damper has been designed to provide a hysteretic damping force via the rotation and yielding of the cylindrical energy dissipater (1) due to the differential motion of the mounting points. The bending moments are transferred from the from the support to the frame beam.
Number | Date | Country | Kind |
---|---|---|---|
2016/07751 | Jun 2016 | TR | national |
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/TR2017/050253 | 6/7/2017 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2018/056933 | 3/29/2018 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
5005326 | Ishimaru | Apr 1991 | A |
5245807 | Ishimaru | Sep 1993 | A |
5533307 | Tsai | Jul 1996 | A |
5630298 | Tsai | May 1997 | A |
5806250 | Medeot | Sep 1998 | A |
5842312 | Krumme et al. | Dec 1998 | A |
5875589 | Lai | Mar 1999 | A |
6141919 | Robinson | Nov 2000 | A |
6223483 | Tsukagoshi | May 2001 | B1 |
6247275 | Taylor | Jun 2001 | B1 |
7797886 | Su | Sep 2010 | B2 |
9447915 | Morgan | Sep 2016 | B1 |
9580924 | Taylor | Feb 2017 | B1 |
9885175 | Izumi | Feb 2018 | B1 |
20020020122 | Mueller | Feb 2002 | A1 |
20050050810 | Shimazaki | Mar 2005 | A1 |
20050138870 | Ishimura | Jun 2005 | A1 |
20050257451 | Pryor | Nov 2005 | A1 |
20080295420 | Simmons | Dec 2008 | A1 |
20110283653 | Christopoulos et al. | Nov 2011 | A1 |
20120038091 | Tagawa | Feb 2012 | A1 |
20120066986 | Dicleli | Mar 2012 | A1 |
20120138402 | Choi | Jun 2012 | A1 |
20130283709 | Christopoulos | Oct 2013 | A1 |
20150048234 | Almazan Campillay | Feb 2015 | A1 |
20170067249 | Matteson | Mar 2017 | A1 |
20180142489 | Becci | May 2018 | A1 |
Number | Date | Country |
---|---|---|
103572856 | Feb 2014 | CN |
H03103509 | Apr 1991 | JP |
Number | Date | Country | |
---|---|---|---|
20190257107 A1 | Aug 2019 | US |