This invention relates generally as indicated to a reinforcing bar connection, and more particularly to a high strength reinforcing bar splice which provides not only high tensile and compressive strengths, but also has the dynamic and fatigue characteristics to qualify as a Type 2 coupler approved for all United States earthquake zones. The invention also relates to a method of making the connection.
In steel reinforced concrete construction, there are generally three types of splices or connections; namely lap splices; mechanical splices; and welding. Probably the most common is the lap splice where two bar ends are lapped side-by-side and wire tied together. The bar ends are of course axially offset which creates design problems, and eccentric loading whether compressive or tensile from bar-to-bar. Welding is suitable for some bar steels but not for others and the heat may actually weaken some bars. Done correctly, it requires great skill and is expensive. Mechanical splices normally require a bar end preparation or treatment such as threading, upsetting or both. They also may require careful torquing. Such mechanical splices don't necessarily have high compressive and tensile strength, nor can they necessarily qualify as a Type 2 mechanical connection where a minimum of five couplers must pass the cyclic testing procedure to qualify as a Type 2 splice in all United States earthquake zones.
Accordingly, it would be desirable to have a high strength coupler which will qualify as a Type 2 coupler and yet which is easy to assemble and join in the field and which does not require bar end preparation or torquing in the assembly process. It would also be desirable to have a coupler which could be assembled initially simply by sticking a bar end in an end of a coupler sleeve or by placing a coupler sleeve on a bar end.
A reinforcing bar connection for concrete construction utilizes a contractible jaw or assembly which is closed around aligned bar ends to form the joint and tightly grip the bars. The jaw assembly is closed from each axial end to constrict around and bridge the ends of end-to-end reinforcing bars. The jaws of the assembly have teeth which bite into the ends of the bar. The assembly is constricted by forcing self-locking taper sleeves or collars over each end which hold the jaw constricted locking the bars together. The teeth are designed to bite into the ribs or projecting deformations on the surface of the bar which forms the overall diameter, but not bite into the core or nominal diameter of the bar. In this manner, the splice does not affect the fatigue or ultimate strength properties of the bar while providing a low slip connection. The jaw segments may be held assembled by a frangible plastic frame. The configuration of the jaws limits the contraction and precludes undue penetration of the bar by the teeth. The connection or splice has high tensile and compressive strength and will pass the dynamic cycling and/or fatigue requirements to qualify as a Type 2 coupler. No bar end preparation or torque application is required to make the coupling. In the method, the closing and locking occur concurrently with a simplified tool to enable the splice to be formed easily and quickly.
According to an aspect of the invention, a reinforcing bar splice includes at least two contractible jaw elements configured to engage ends of generally axially aligned reinforcing bars, wherein the jaw elements each have tapered outer surfaces sloping up from both ends of the jaw element; and tapered collars for engaging the tapered outer surfaces of the jaw elements to force the jaw elements, inward to grip ends of the reinforcing bars.
According to another aspect of the invention, a method of joining ends of substantially axially aligned reinforcing bars, the method comprising: placing jaw elements having tapered outer surfaces over ends of the reinforcing bars; and forcing the jaw elements inward to grip the ends of the reinforcing bars, wherein the forcing includes exerting an axial force on tapered lock collars placed on ends of the jaw elements.
According to still another aspect of the invention, a jaw element section for engaging reinforcing bars includes a wall; and teeth attached to an inner surface of the wall. The wall has a tapered outer surface. The wall has wall notches therein that define hinge points or reduced thickness. The jaw element section includes jaw elements hingedly coupled to one another at the hinge points.
According to yet another aspect of the invention, a reinforcing bar splice includes a jaw element section configured to engage ends of generally axially aligned reinforcing bars, wherein the jaw element section includes multiple jaw elements physically coupled together; and tapered collars for engaging tapered outer surfaces of the jaw element sections to force the jaw elements inward to grip ends of the reinforcing bars.
According to a further aspect of the invention, a method of joining ends of substantially axially aligned reinforcing bars includes the steps of: placing jaw elements having tapered outer surfaces over ends of the reinforcing bars; and forcing the jaw elements inward to grip the ends of the reinforcing bars, wherein the forcing includes exerting an axial force on tapered lock collars placed on ends of the jaw elements. The forcing includes driving teeth of the jaw elements into protrusions on a surface the reinforcing bars, without encroaching upon an underlying core of the reinforcing bars.
According to a still further aspect of the invention, a jaw element section for splicing ends of reinforcing bars, includes: a flexible web; and plural jaw elements coupled to the web. The jaw elements each include tapered outer surfaces and a toothed inner surface.
To the accomplishment of the foregoing and related ends the invention, then, comprises the features hereinafter fully described and particularly pointed out in the claims, the following description and the annexed drawings setting forth in detail certain illustrative embodiments of the invention, these being indicative, however, of but a few of the various ways in which the principles of the invention may be employed.
Referring initially to
As seen more clearly in
Referring now to
As seen more clearly in
As seen more clearly in
The taper exterior of the opposite ends of the jaw elements as well as the jaw assembly not only enables the matching lock collars to be driven on the splice, contracting the jaw elements with great force but locking them in contracted position. The configuration of the connection also enhances the dynamic and fatigue characteristics of the splice. This not only enhances the fatigue characteristics of the splice, but also enables the splice to qualify as a Type 2 coupler which may be used anywhere in a structure in any of the four earthquake zones of the United States.
Referring now to
As seen in comparing the left and right hand side of
As indicated, the inward projection of the teeth is designed to bite into the projecting deformations on the bar, but not into the core 38. As the teeth 35 press into the deformation, they provide additional cold working of the bar, resulting in better performance of the connection. By not pressing the teeth 35 into the core 38 of the bar, fatigue cracks and/or stress concentrations may thereby be avoided.
The three jaw elements are shown in
It will be appreciated that a transition splice may be formed with the present invention simply by reducing the interior diameter of one end of the splice so that the teeth on that end will bite into the projecting deformations on a smaller bar. The exterior configuration of the jaw elements may also change or remain the same with different size or identical locking collars driven on each end.
It will be appreciated that alternatively other means may be utilized for contracting internally-toothed jaw elements to clamp ends of reinforcing bars, for example by use of a radially-contracting collar or band.
Referring now to
The three axially extending or longitudinal elements are held in place with respect to each other by the center three-legged triangular connection shown generally at 68, which also acts as a bar end stop. In this manner, the three jaw elements are held assembled and circumferentially spaced. Each locking collar may be positioned on the end of the assembled jaw elements as seen at 32 and 33 and held in place by a shrink wrap, for example, as seen at 70 and 71, in
Referring now to
The opposite end of the lever 79 is provided with a C-shape termination pivoted at 96 to a C-shape tubular member 97 having an open side 98. A wedge driving collar shown generally at 100 is mounted on the lower end of the open tube 97. The collar is formed of hinged semi-circular halves 101 and 102. When closed and locked, the wedge collar has an interior taper matching that of the taper collars 32 or 33.
The lower arm 80 similarly is provided with a C-termination 105 pivoted at 106 to open tube 107 supporting wedge collar 108 formed of pivotally connected semicircular halves 109 and 110.
In order to make a splice, the coupler or splice assembly 59 seen more clearly in
The tool 78 shown in
Turning now to
The wall 124 of the jaw element section 120 has tapering shallow angle outer surfaces 152 and 154, which may be similar to the shallow angle surfaces 29 and 30 of the jaw element 25 (
The jaw element section 120 may have an extent of greater than 120 degrees and less than 180 degrees. The illustrated jaw element section 120 has an extent of about 134 degrees, although will be appreciated that the jaw element may have a greater or lesser extent. More broadly, the jaw element section 120 may have an extent from about 125 to about 140 degrees or to about 150 degrees.
It will appreciated that symmetric teeth may in addition be utilized with other embodiments described above, such as with the jaw 26 shown in
Thus, as shown in
Taper lock collars 182 and 184 may be used to press the jaw element sections 120 and 170 against the reinforcing bars 172 and 174. Under force, as when taper lock collars 182 and 184 are driven onto the jaw element sections 120 and 170, jaw element sections (such as the jaw element 134–140 of the jaw element section 120) can pivot relative to one another about hinge points (such as the hinge points 144–148 of the jaw element section 120). This allows the jaw element sections 120 and 170 to conform better to and/or to better grip the reinforcing bars 172 and 174. This may allow compensation for difference in sizes of the reinforcing bars 172 and 174, and/or for slight misalignments of the reinforcing bars 172 and 174 relative to one another. Also, misalignments of the jaw element sections 120 and 170 may be compensated for by relative movement of the jaw element sections of the jaw element sections 120 and 170. Further, as with other embodiments described above, the pressure of the taper lock collars 182 and 184 against the outer surfaces 152 and 154 of the wall 124 may cause the annular teeth 122 to bite into or otherwise deform protrusions on the reinforcing bars 172 and 174. Alternatively or in addition, the annular teeth 122 may deform as the jaw element sections 120 and 170 are pressed by the taper lock collars 182 and 184 against the reinforcing bars 172 and 174.
It will be appreciated that the embodiment shown in
The ribs 202 have rounded corners 242 and 244. The troughs 220 also have rounded corners 246 and 248 at the transition to the adjacent of the ribs 202.
The extent of the jaw element section 200 may be about the same as that of the jaw element section 120 (
The jaw element section 200 may be made of a softer material than that of reinforcing bars which the jaw element section 200 couples together. Thus the ribs 202 may deform as the jaw element section 200 is pressed against deformations on the outside of reinforcing bar ends to be coupled together.
As shown in
The jaw element sections 200 and 260 may be substantially identical to one another, and may be placed substantially diametrically opposed on opposite sides of the reinforcing bars 252 and 254. The gaps 264 and 266 therefore may each have an extent of at least 40 degrees.
It will be appreciated that the jaw element sections 120 (
The taper lock collars 182 and 184 (
Alternatively, taper lock collars such as a taper lock collar 300, shown in
It will be appreciated that driving force may be directly applied to a pair of the taper lock collars 300 to drive them onto jaw element sections to secure a pair of reinforcing bars together, for example avoiding the need to use installation collars.
The various taper lock collars described herein may have an inner surface coated with synthetic polymer material, such as a material sold under the trademark TEFLON, or with another suitable lubricant material, in order to reduce friction between the lock collars and the jaw elements or jaw element sections.
The tapered shell 330 has tapered outer surfaces 332 and 334, similar to the tapered surfaces of the other jaw element sections described above. However, rather than teeth or ribs on its inner surface, the tapered shell 330 has a smooth (non-toothed) inner surface 338. The inner surface 338 may be curved, as is shown in
The depressions 326 and 328 in the tapered shell 330 receive and secure the toothed elements 322 and 324. The toothed elements 322 and 324 have teeth 344, which may be either symmetrical or asymmetrical teeth. The toothed elements 322 and 324 may be shaped roughly as a parallelepiped, having a flat back and sides, and having a substantially rectangular cross-section in any direction. The teeth 344 may be flat, without curvature. Alternatively, the teeth 344 may have curvature, for example having a curvature corresponding to the reinforcing bars to be joined.
Two or more of the multi-part jaw element sections 320 may be used to join together reinforcing bars, using tapered lock collars to press the teeth 344 of the toothed inserts 322 and 324 into protrusions of the reinforcing bars. As the tapered collars are pressed or driven onto the tapered outer surfaces 332 and 334 of the tapered shell 330. The tapered shell 330 presses inward against the toothed inserts 332 and 324, which are located in the depressions 326 and 328 of the tapered shell 330. The inward pressure against the toothed inserts 322 and 324 drive the teeth 344 into protrusions on the reinforcing bars.
The tooth inserts 322 and 324 and the depressions 326 and 328 may have any of a large variety of suitable shapes. For example, the inserts and depressions may sloped shapes, preferentially orienting one end of the tooth inserts 322 and 324 toward the middle of the tapered shell 330. Such a feature for orienting the toothed inserts 322 and 324 may be desirable when the teeth 344 are asymmetric teeth with a preferred orientation direction.
Referring now to
The toothed inserts 374, 376, 384, and 386 may have a shape substantially that of a parallelepiped. Alternatively, the toothed inserts may have some curvature.
The depressions 364, 366, 378, and 380 may be oriented so as to direct the teeth of each of the toothed inserts 374, 376, 384, and 386 directly toward the reinforcing bars.
A smooth (non-toothed) inner surface 390 of the tapered shell 362 may be curved (as shown in
It will be appreciated that multi-piece jaw element sections may have other configurations than those shown and described above. For example, each side of the jaw element may have three or more inserts. As another example, the toothed inserts could extend across both sides of the tapered shell, for engaging both reinforcing bars to be joined.
It will be appreciated that alternatives to depressions may be used for locating and securing the toothed insert(s). For example, suitable protrusions on the inner surface of the tapered shells may be used. As another alternative, the tapered shell may have a suitably tapered or otherwise shaped inner surface for engaging and securing the toothed insert(s).
The multi-part jaw element sections 320 and 360 may be easier to manufacture than the single-piece jaw elements and jaw element sections of other embodiments. Thus used of multi-part jaw element sections may reduce costs.
Turning now to
As best seen in
The web 402 may include any of a variety of flexible materials, such as suitable flexible plastics, flexible sheet metal, and/or wire.
The web 402 and the jaw elements 400 may be a part of a belt or roll having many such elements 400, linked by the web 402. In use, an appropriate number of the jaw elements 400, with the web 402 connecting them, are separated from a belt or roll of jaw elements. As illustrated in
The number of jaw elements 400 in the jaw element section 404 utilized may be varied for various sizes of reinforcing bars. The jaw elements 400 may be narrow, such that 5, 7, 9, 11, or more jaw elements 400 may be used to coupled the ends of the reinforcing bars 430 and 432. An odd or even number of the jaw elements 400 may be used, although it may be advantageous to employ an odd number of jaw elements, for example to reduce the likelihood of deforming and/or pressing into the core of reinforcing bars 430 and 432.
The web 402 may be positioned such that the collars 436 and 438 do not touch or otherwise encounter the web 402, as the collars are pressed onto the tapered surfaces 410 of the jaw elements 400.
The web 402 alternatively may be located elsewhere with respect to the jaw elements 400. For example, the web 402 may alternatively run along an inside surface of the jaw elements 400, for example between the teeth 406 and 408, to be located between the ends of the reinforcing bars 430 and 432.
The jaw elements 400 may be substantially evenly spaced along the web 402. Alternatively, there may be some variation in the spacing of the jaw elements 400.
Due to the flexibility of the web 402, the jaw elements 400 are free to move relative to one another, allowing the jaw elements to individually shift to compensate for misalignments of the ends of the reinforcing bars 430 and 432, and/or to compensate for other misalignments or irregularities.
The jaw elements 400 may be formed by such processes as blanking, stamping, or forging. It will be appreciated that the relatively simple shape of the jaw elements 400 may make them inexpensive to manufacture.
It will be appreciated that coupling the jaw elements 400 to the web 402 simplifies installation of the splice 446. In addition, the use of multiple jaw elements 400 on the web 402, as part of the jaw element section 404, advantageously may allow use with various sizes of reinforcing bars, with the number of jaw elements 400 used varying with the size of the bars, as described above.
The jaw elements 502 fit into the spacer notches 514, and have jaw element notches 524 that fit onto edges 526 of the potions 520 of the spacer 504.
A tapered collar 530 engages tapered outer surfaces 532 of the jaw elements 532, driving the jaw elements 502 radially inward such that teeth 536 of the jaw elements 502 bite into and engage the ends of the reinforcing bars 510 and 512.
The spacer 504 may be made of a rigid material. Alternatively, the spacer 504 may be made of a flexible material, such as a suitable plastic, that allows it to deform inward as the jaw elements 502 are pressed radially inward.
It will be seen that the present invention provides a high strength coupler or splice which will qualify as a Type 2 coupler and yet which is easy to assemble and join in the field and which does not require bar end preparation or torquing in the assembly process.
Although the invention has been shown and described with respect to certain preferred embodiments, it is obvious that equivalent alterations and modifications will occur to others skilled in the art upon the reading and understanding of this specification. It will be appreciated that suitable features in one of the embodiments may be incorporated in another of the embodiments, if desired. The present invention includes all such equivalent alterations and modifications, and is limited only be the scope of the claims.
This application is a continuation in part of U.S. application Ser. No. 10/055,551, filed Jan. 23, 2002, now U.S. Pat. No. 6,719,478 which claims priority under 35 USC 119(e) of U.S. Provisional Application No. 60/263,860, filed Jan. 23, 2001. Both of the preceding applications are hereby incorporated by reference in their entireties.
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Number | Date | Country | |
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Number | Date | Country | |
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Parent | 10055551 | Jan 2002 | US |
Child | 10697509 | US |