Spiral stirrup prefabricated T beam

Abstract

The spiral stirrup prefabricated T beam comprises a wing plate steel reinforcement framework, a beam rib steel reinforcement framework and connecting ribs, one end of the beam rib steel reinforcement framework is inserted into the wing plate steel reinforcement framework to form an overlapping area, and the connecting ribs are located in the overlapping area; the wing plate steel reinforcement framework and the beam rib steel reinforcement framework are bound to the connecting ribs through steel bars to form the prefabricated T beam, and the wing plate steel reinforcement framework comprises wing plate spiral stirrups and wing plate longitudinal main ribs connected to the wing plate spiral stirrups. The beam rib steel reinforcement framework comprises beam rib spiral stirrups and beam rib longitudinal main reinforcements connected to the beam rib spiral stirrups, and the beam rib spiral stirrups and the wing plate spiral stirrups are both formed by continuously bending a rib material. According to the spiral stirrup prefabricated T beam, the integrality of a prefabricated T beam steel reinforcement framework is enhanced, the hooping effect of stirrups on core area concrete is improved, the steel reinforcement cutting and bending times are reduced from the machining angle, the workload is reduced, and meanwhile the production efficiency is improved.

Description

Technical Field

[0001] The present invention particularly relates to a prefabricated T-beam with spiral stirrups. Background Art

[0002] The existing prefabricated T-beams include a flange steel frame and a beam rib steel frame. The manufacturing process of the flange steel frame is as follows: first, multiple single-piece separate stirrups are bent into a specific shape, and multiple single-piece separate stirrups are connected by longitudinal force-bearing steel bars to form a flange steel frame. Similarly, the beam rib steel frame is also made by tying multiple single-piece separate stirrups with longitudinal force-bearing steel bars. During construction, first tie the beam rib steel frame on the tire frame, hoist the flange steel frame into the mold, and insert the connecting bars at the connection between the flange steel frame and the beam rib steel frame. After installing the side mold, concrete can be poured. However, this traditional prefabricated T-beam will have the following problems:

[0003] First, the steel bars need to be cut into single-piece separate stirrups of corresponding lengths. Each single-piece separate stirrup can be bent before it can be tied with the longitudinal force-bearing steel bars. The number of bending times is large and the workload is large. Multiple separate single-piece separate stirrups are only tied with the longitudinal force-bearing steel bars, the integrity of the steel bar skeleton is poor, and the constraint force on the core area concrete of the wing plate steel bar skeleton and the beam rib steel bar skeleton is low. Summary of the invention

[0004] The present invention aims to solve at least one of the technical problems existing in the prior art. To this end, the present invention provides a prefabricated T-beam with spiral stirrups.

[0005] In order to solve the above-mentioned technical problems, the present invention adopts the following technical solutions:

[0006] A prefabricated T-beam with spiral stirrups comprises a wing plate steel bar skeleton, a beam rib steel bar skeleton and connecting bars, one end of the beam rib steel bar skeleton is inserted into the wing plate steel bar skeleton to form an overlapping area, the connecting bars are located in the overlapping area, the wing plate steel bar skeleton and the beam rib steel bar skeleton are respectively tied to the connecting bars by steel bars to form a prefabricated T-beam, the wing plate steel bar skeleton comprises wing plate spiral stirrups and wing plate longitudinal main bars connected to the wing plate spiral stirrups, the beam rib steel bar skeleton comprises beam rib spiral stirrups and beam rib longitudinal main bars connected to the beam rib spiral stirrups, the beam rib spiral stirrups and the wing plate spiral stirrups are both formed by continuously bending a single bar.

[0007] Preferably, the spiral stirrups of the wing panel are arranged to form a wing panel installation space, and all the longitudinal main reinforcements of the wing panel are placed in the wing panel installation space and tied to the spiral stirrups of the wing panel.

[0008] Preferably, one end of the beam-rib reinforcement skeleton extends into the wing panel installation space, and the overlapping portion of the beam-rib reinforcement skeleton and the wing panel installation space constitutes the overlap area.

[0009] Preferably, the beam-rib spiral stirrups are arranged to form a beam-rib installation space, and all the beam-rib longitudinal main reinforcements are placed in the beam-rib installation space and tied to the beam-rib spiral stirrups.

[0010] The beneficial effects of the present invention are:

[0011] Compared with the prior art, the spiral stirrups of the beam rib and the spiral stirrups of the wing plate of the present application are both formed by continuously bending a single reinforcement bar. The spiral stirrups of the beam rib and the longitudinal main reinforcement of the beam rib are tied together to form a beam rib steel bar skeleton, and the spiral stirrups of the wing plate and the longitudinal main reinforcement of the wing plate are tied together to form a wing plate steel bar skeleton. This not only enhances the integrity of the prefabricated T-beam steel bar skeleton and improves the hoop effect of the stirrups on the core area concrete, but also reduces the number of steel bar cuts and bending times from a processing perspective, reduces the workload and improves production efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0012] The above and / or additional aspects and advantages of the present invention will become apparent and easily understood from the description of the embodiments in conjunction with the following drawings, in which:

[0013] Figure 1 The structure of the wing plate steel frame of this application is shown in FIG. Figure 1 ;

[0014] Figure 2 The structure of the wing plate steel frame of this application is shown in FIG. Figure 2 ;

[0015] Figure 3 This is a schematic diagram of the structure of the spiral stirrups of the flange plate of the present application;

[0016] Figure 4 This is a schematic diagram of the structure of the beam rib reinforcement skeleton of this application Figure 1 ;

[0017] Figure 5 This is a schematic diagram of the structure of the beam rib reinforcement skeleton of this application Figure 2 ;

[0018] Figure 6 This is a schematic diagram of the structure of the spiral stirrups of the beam rib of this application;

[0019] Figure 7 This is a schematic diagram of the structure of the new prefabricated T-beam of this application Figure 1 ;

[0020] Figure 8 This is a schematic diagram of the structure of the new prefabricated T-beam of this application Figure 2 ;

[0021] Fig. 9 This is a schematic diagram of the structure of the new prefabricated T-beam of this application Figure 3 . DETAILED DESCRIPTION

[0022] Embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions.

[0023] The orientation shown in the drawings cannot be understood as limiting the specific protection scope of the present invention, but is only provided for reference and understanding of the preferred embodiments. The product components shown in the drawings may be changed in position, increased in number, or simplified in structure.

[0024] The "connection" described in the specification and the mutual "connection" relationship of the components shown in the drawings can be understood as a fixed connection or a detachable connection or an integral connection; it can be a direct connection or a connection through an intermediate medium. Ordinary technicians in this field can understand the connection relationship according to the specific circumstances and can derive different implementation methods in an appropriate manner such as screwing, riveting, welding, clamping or embedding.

[0025] With respect to the directional words such as up, down, left, right, top, bottom, etc. described in the specification and the directions shown in the drawings, the components may be in direct contact or in contact through other features between them; for example, "above" may mean directly above or obliquely above, or it simply means higher than other objects; other directions may be understood by analogy.

[0026] The materials for making parts with solid shapes shown in the specification and the drawings may be metal materials, non-metal materials or other synthetic materials; the mechanical processing techniques used for parts with solid shapes may be stamping, forging, casting, wire cutting, laser cutting, injection molding, CNC milling, 3D printing, machining, etc.; ordinary technicians in this field can adaptively select or combine them according to different processing conditions, costs, and precisions, but are not limited to the above-mentioned materials and manufacturing processes.

[0027] A prefabricated T-beam with spiral stirrups, comprising a wing plate steel bar skeleton, a beam rib steel bar skeleton and connecting bars 3, one end of the beam rib steel bar skeleton is inserted into the wing plate steel bar skeleton to form an overlapping area, the connecting bars 3 are located in the overlapping area, the wing plate steel bar skeleton and the beam rib steel bar skeleton are respectively tied to the connecting bars 3 through steel bars to form a prefabricated T-beam, the wing plate steel bar skeleton comprises a wing plate spiral stirrup 1 and a wing plate longitudinal main bar 11 connected to the wing plate spiral stirrup 1, the beam rib steel bar skeleton comprises a beam rib spiral stirrup 2 and a beam rib longitudinal main bar 21 connected to the beam rib spiral stirrup 2, the beam rib spiral stirrup 2 and the wing plate spiral stirrup 1 are both formed by continuously bending a single bar.

[0028] Furthermore, the wing panel spiral stirrups 1 are arranged to form a wing panel installation space 10 , and all the wing panel longitudinal main reinforcements 11 are placed in the wing panel installation space 10 and tied to the wing panel spiral stirrups 1 .

[0029] Furthermore, one end of the beam-rib reinforcement skeleton extends into the wing panel installation space 10, and the overlapping portion of the beam-rib reinforcement skeleton and the wing panel installation space 10 constitutes the overlapped area.

[0030] Furthermore, the beam-rib spiral stirrups 2 are arranged to form a beam-rib installation space 20 , and all beam-rib longitudinal main reinforcements 21 are placed in the beam-rib installation space 20 and tied to the beam-rib spiral stirrups 2 .

[0031] The working principle of the present invention is:

[0032] Fabrication of wing plate reinforcement frame: Figure 3 As shown, the reinforcement material is pulled by a winding machine and a polygonal mold corresponding to the wing plate to form a spiral stirrup 1 for the wing plate, and the spiral stirrup 1 for the wing plate is surrounded to form a wing plate installation space 10 for installing the longitudinal main reinforcement 11 of the wing plate; Figure 1-2 As shown, the flange longitudinal main reinforcement 11 is tied to the flange spiral stirrup 1 by steel bars to form a flange reinforcement skeleton.

[0033] Production of beam rib reinforcement skeleton: Figure 6 As shown, the reinforcement material is pulled by a winding machine and a polygonal mold corresponding to the beam rib to form a beam rib spiral stirrup 2, and the beam rib spiral stirrup 2 is surrounded to form a beam rib installation space 20 for installing the beam rib longitudinal main reinforcement 21, as shown in FIG. Figure 4-5 As shown, the longitudinal main reinforcement 21 of the beam rib is tied to the beam rib spiral stirrup 2 by steel bars to form a beam rib steel bar skeleton.

[0034] Production of prefabricated T beams: Figure 7 As shown, the upper end of the beam rib reinforcement skeleton is inserted into the flange installation space 10, and the connecting rib 3 is placed in the flange installation space 10. The connecting rib 3 is respectively tied to the beam rib reinforcement skeleton and the flange reinforcement skeleton through steel bars to form a prefabricated T-beam.

[0035] In the above technical solution, it is preferred that the flange plate reinforcement skeleton is arranged perpendicularly to the beam rib reinforcement skeleton.

[0036] In the above technical solution, a connecting rib 3 is connected by binding at the middle section along the length direction of the wing plate steel bar skeleton, and then the upper end of the beam rib steel bar skeleton is extended into the wing plate steel bar skeleton, that is, the overlapping area of ​​the wing plate steel bar skeleton and the beam rib steel bar skeleton is installed with a connecting rib 3, and then the connecting rib 3 is respectively bound with the wing plate steel bar skeleton and the beam rib steel bar skeleton to form a prefabricated T-beam as a whole.

[0037] Compared with the prior art, the beam rib spiral stirrups 2 and the wing plate spiral stirrups 1 of the present application are both formed by continuously bending a single reinforcement bar. The beam rib spiral stirrups 2 and the beam rib longitudinal main reinforcement 21 are tied together to form a beam rib steel bar skeleton, and the wing plate spiral stirrups 1 and the wing plate longitudinal main reinforcement 11 are tied together to form a wing plate steel bar skeleton. This not only enhances the integrity of the prefabricated T-beam steel bar skeleton and improves the hoop effect of the stirrups on the core area concrete, but also reduces the number of steel bar cuts and bending times from a processing perspective, reduces the workload and improves production efficiency.

[0038] Although the present invention is described in detail with reference to the above embodiments, it is obvious to those skilled in the art through this disclosure that various changes or modifications may be made to the present invention without departing from the principle and spirit of the present invention defined by the claims. Therefore, the detailed description of the embodiments of the present disclosure is only used to explain, not to limit the present invention, but the scope of protection is limited by the content of the claims.

Claims

1. A prefabricated T-beam with spiral stirrups, characterized in that: The invention comprises a wing plate steel bar skeleton, a beam rib steel bar skeleton and connecting bars (3), one end of the beam rib steel bar skeleton is inserted into the wing plate steel bar skeleton to form an overlapping area, the connecting bars (3) are located in the overlapping area, the wing plate steel bar skeleton and the beam rib steel bar skeleton are respectively tied to the connecting bars (3) by steel bars to form a prefabricated T-beam, the wing plate steel bar skeleton comprises a wing plate spiral stirrup (1) and a wing plate longitudinal main bar (11) connected to the wing plate spiral stirrup (1), the beam rib steel bar skeleton comprises a beam rib spiral stirrup (2) and a beam rib longitudinal main bar (21) connected to the beam rib spiral stirrup (2), the beam rib spiral stirrup (2) and the wing plate spiral stirrup (1) are both formed by continuously bending a single bar material.

2. The prefabricated T-beam with spiral stirrups according to claim 1, characterized in that: The wing plate spiral stirrups (1) are arranged to form a wing plate installation space (10), and all wing plate longitudinal main reinforcements (11) are placed in the wing plate installation space (10) and tied to the wing plate spiral stirrups (1).

3. The prefabricated T-beam with spiral stirrups according to claim 2, characterized in that: One end of the beam-rib steel bar skeleton extends into the wing plate installation space (10), and the overlapping portion of the beam-rib steel bar skeleton and the wing plate installation space (10) constitutes the overlap area.

4. The prefabricated T-beam with spiral stirrups according to claim 1, characterized in that: The beam-rib spiral stirrups (2) are arranged to form a beam-rib installation space (20), and all beam-rib longitudinal main reinforcements (21) are placed in the beam-rib installation space (20) and tied to the beam-rib spiral stirrups (2).

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