Detection device based on total station
Through the combination of the total station, reflector and clamping structure, the problem of low measurement accuracy of truss steel beams and abdominal rods is solved, and efficient and accurate truss assembly is achieved, which improves construction efficiency and quality.
Patent Information
- Application Number
- CN202422024295.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-20
- Publication Date
- 2025-08-05
- Estimated Expiration
- 2034-08-20
AI Technical Summary
In the prior art, the accuracy of the steel ruler is low and inconvenient when measuring the truss steel beams and the belly rods, resulting in deviations from the target size after the truss welding, affecting the splicing quality and efficiency.
The total station is used to cooperate with four detection components to measure the three-dimensional coordinates of the four top angles at the top angle of the truss through the reflector and clamping structure, and automatically measure the length and spacing of the steel beams to improve the measurement accuracy and speed.
High-precision measurement of the spacing and length of truss steel beams is achieved, reducing the difficulty and deformation of truss splicing, and improving the splicing speed and quality.
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Figure CN223192350U_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the technical field of truss installation, and in particular to a detection device based on a total station. Background Art
[0002] The total length of the truss in construction scenarios such as factories is relatively long, and multiple truss sections need to be spliced and assembled. When each truss section is welded on the ground, the steel beam chord and web members need to be assembled. After measuring the length of the upper and lower chords with a steel ruler, the steel beam chord and web members are welded together, and multiple truss sections are then spliced together to form the entire truss.
[0003] However, when assembling the steel beam chords and web members, the measurement accuracy of the steel ruler is low and the measurement is not convenient enough, resulting in deviations in the length and width of each truss section compared to the envisioned target size after welding. Summary of the Invention
[0004] In order to solve the above technical problems or at least partially solve the above technical problems, the present application provides a detection device based on a total station.
[0005] The present application provides a detection device based on a total station, comprising a total station and four detection components. The truss has four vertex angles, each of which is connected to a detection component. The total station cooperates with the four detection components to measure the three-dimensional coordinates of the four vertex angles.
[0006] The detection assembly includes a reflective plate and a clamping structure connected to each other, and the reflective plate is detachably connected to the truss through the clamping structure.
[0007] The clamping structure includes a bottom plate connected to the reflector, the bottom plate is provided with a slot, and the truss includes a steel beam, and the wing plate of the steel beam is plugged into the slot.
[0008] Optionally, the clamping structure further includes a first movable portion connected to the base plate, the first movable portion being capable of approaching or moving away from the wing plate, the wing plate having a first surface and a second surface opposite to each other along a thickness direction thereof, and one end of the wing plate having a third end surface along a length direction thereof;
[0009] The clamping structure has a clamping state, in which the first surface and the third end surface are both in contact with the inner wall of the slot, and the second surface is in contact with the first movable portion.
[0010] Optionally, the clamping structure further includes a second movable portion connected to the base plate, the base plate is fixedly connected to the reflective plate, and the second movable portion can move toward the third end surface to abut against the third end surface.
[0011] Optionally, the reflective plate is movably connected to the base plate, and the clamping structure further includes a second movable portion connected to the base plate, and the second movable portion can move toward the third end surface to abut against the reflective plate. At this time, the reflective plate is clamped between the second movable portion and the third end surface.
[0012] Optionally, the first movable part is a first screw, a first threaded hole is formed on the base plate, and the first screw and the first threaded hole form a threaded fit.
[0013] Optionally, a first nut is connected to the base plate, the first movable part is a first screw, and the first screw and the first nut form a bolt connection pair.
[0014] Optionally, a second nut is connected to the base plate, the second movable part is a second screw, and the second screw and the second nut form a bolt connection pair.
[0015] Optionally, the wing plate is gap-matched with the slot.
[0016] Optionally, one end of the first screw toward the wing plate extends radially along the first screw to form a first limiting portion, and a cross-sectional area of the first limiting portion is larger than a cross-sectional area of the first threaded hole or the threaded hole of the first nut.
[0017] The technical solution provided by the embodiments of the present application has the following advantages compared with the prior art:
[0018] In the detection device based on a total station provided in an embodiment of the present application, a reflector is clamped at the measured point corresponding to the top corner of the truss by a clamping structure. The total station and the reflector cooperate to measure the three-dimensional coordinates of the four measured points. By providing reflectors at the four top corners of the truss, the three-dimensional coordinates of the four top corners can be obtained, and the measured data can be used to automatically measure the length of the steel beams on both sides of the truss and the distance between the two steel beams through simple calculations or in conjunction with programming algorithms.
[0019] The total station-based inspection device facilitates rapid, accurate, and convenient testing, minimizing the error between the spacing between the truss beams and the target spacing. This reduces the difficulty of joining two adjacent truss sections and minimizes deformation. Furthermore, the error between the truss beam lengths and the target lengths is minimized, making assembly of multiple trusses easier and minimizing deformation. This improves the speed and quality of truss splicing. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the present application and, together with the description, serve to explain the principles of the present application.
[0021] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, for ordinary technicians in this field, other drawings can be obtained based on these drawings without any creative work.
[0022] Figure 1 This is a schematic structural diagram of a total station-based detection device according to an embodiment of the present application;
[0023] Figure 2 This is a schematic diagram of the three-dimensional structure of the detection component described in an embodiment of the present application;
[0024] Figure 3 This is a schematic diagram of the structure of the detection component described in an embodiment of the present application;
[0025] Figure 4 for Figure 3 AA section view in the figure;
[0026] Figure 5 A schematic structural diagram of a detection component according to another embodiment of the present application.
[0027] Among them, 1. detection component; 2. truss; 21. wing plate; 211. first surface; 212. second surface; 213. third end surface; 3. reflector; 4. bottom plate; 5. first movable part; 6. second movable part. DETAILED DESCRIPTION
[0028] In order to more clearly understand the above-mentioned objectives, features and advantages of the present application, the scheme of the present application will be further described below. It should be noted that, in the absence of conflict, the embodiments of the present application and the features therein can be combined with each other.
[0029] In the following description, many specific details are set forth to facilitate a full understanding of the present application, but the present application can also be implemented in other ways different from those described herein; it is obvious that the embodiments in the specification are only part of the embodiments of the present application, not all of the embodiments.
[0030] Reference Figures 1 to 5 As shown, this embodiment provides a total station-based detection device, comprising a total station and four detection assemblies 1. A truss 2 has four corners, each of which is connected to a detection assembly 1. The total station and the four detection assemblies 1 work together to measure the three-dimensional coordinates of the four corners. The detection assembly 1 includes a reflector 3 and a clamping structure, which are detachably connected to the truss 2 via the clamping structure. In a specific implementation, the reflector 3 may include a plate body and reflective stickers affixed to the plate body.
[0031] The detection device based on the total station provided in this embodiment, when in use, the reflector 3 is clamped at the measurement points corresponding to the top corners of the truss 2, and the total station and the reflector 3 cooperate to measure the three-dimensional coordinates of the four measurement points. By providing reflectors 3 at the four top corners of the truss 2, the three-dimensional coordinates of the four top corners can be obtained, and the measured data is used to automatically measure the length L of the steel beams on both sides of the truss 2 and the distance D between the two steel beams through calculation or in cooperation with programming algorithms. The steel beams on both sides of the truss 2 are the upper chord and the lower chord generally referred to in the art, and the steel beam can be an I-beam. The reflector 3 is detachably connected to the truss 2 through a clamping structure to detect the lengths of multiple sections of the truss 2.
[0032] The detection device based on the total station is convenient, fast and accurate in detection, making the error between the distance D between the upper chord and the lower chord of the truss 2 and the target distance small, and the connection difficulty low and the deformation amount small when adjacent two sections of the truss 2 are spliced. Moreover, the error between the lengths L of the upper chord and the lower chord of the truss 2 and the target length is small, making the assembly difficulty low and the deformation amount small when multiple sections of the truss 2 are assembled. The speed and quality of the splicing of the truss 2 are improved.
[0033] In some embodiments, as Figures 2 to 4 shown, the clamping structure includes a bottom plate 4 connected to the reflector 3. A slot is provided on the bottom plate 4. The truss 2 includes a steel beam, and one end of the wing plate 21 of the steel beam is inserted into the slot. The wing plate 21 of the steel beam is in interference fit with the slot. The clamping structure is simple and convenient to implement in the construction working condition. The reflector 3 can be welded to the bottom plate 4. The reflector 3 can be a plate body of the same material as the bottom plate 4, and a reflective sticker can be pasted on the plate body, with low cost and easy to implement.
[0034] In some embodiments, along the thickness direction of the bottom plate 4, that is, the height direction of the steel beam, the slot on the bottom plate 4 penetrates through the bottom plate 4. The slot penetrating through the bottom plate 4 is easy to process and form. Of course, the projection shape of the slot in the thickness direction of the bottom plate 4 can be an inverted "U", that is, the slot has a bottom wall (not shown in the figure) in the thickness direction of the bottom plate 4. When the bottom plate 4 is inserted into one end of the wing plate 21, the bottom wall abuts against the top surface of the wing plate 21. One end of the wing plate 21 along its length direction has a third end face 213, and the third end face 213 abuts against the side wall of the slot. The wing plate 21 has opposite first face 211 and second face 212 along its thickness direction, and the first face 211 and the second face 212 abut against the two side walls of the slot. The side wall and the bottom wall are both inner walls of the slot, and the three side walls and the bottom wall of the slot abut against the four sides (upper side, front side and left and right sides) of the wing plate 21 respectively, increasing the connection strength between the bottom plate 4 and the wing plate 21 and making the connection between the bottom plate 4 and the wing plate 21 more stable.
[0035] In some embodiments, the clamping structure further includes a first movable portion 5 connected to the bottom plate 4. The first movable portion 5 can move closer to or farther from the wing plate 21. The wing plate 21 has a first surface 211 and a second surface 212 opposite to each other along its thickness direction. The wing plate 21 has a third end surface 213 at one end along its length direction. The state when the clamping structure clamps the wing plate 21 is a clamping state. Figure 2 and Figure 3 As shown, in the clamped state, the first surface 211 and the third end surface 213 both abut the inner wall of the slot, while the second surface 212 abuts the first movable portion 5. At this point, if the slot and the wing plate 21 form an interference fit, the second surface 212 also abuts the inner wall of the slot. Alternatively, the slot and the wing plate 21 can form a clearance fit—that is, if the slot width is greater than the thickness of the wing plate 21, the wing plate 21 and the clamping structure are more easily disassembled, and the clamping structure is adaptable to wing plates 21 of varying thicknesses.
[0036] In a specific implementation, the first movable portion 5 can be a first screw, with a first threaded hole formed in the base plate 4, and the first screw and the first threaded hole forming a threaded engagement. Alternatively, a first nut is connected to the base plate 4, and the first movable portion 5 is a first screw, with the first screw and the first nut forming a bolted connection pair. The first nut can be directly welded to the base plate 4, and the first screw and the nut can cooperate to move the first screw closer to, or further away from, the wing plate 21. The screw and nut achieve movement of the first movable portion 5, making it easy to implement on-site, cost-effective, and practical.
[0037] In some embodiments, as Figure 2 and Figure 3 As shown, the base plate 4 is fixedly connected to the reflector 3. The clamping structure further includes a second movable portion 6 connected to the base plate 4. The second movable portion 6 can move toward the third end surface 213 until it abuts against the third end surface 213, further strengthening the connection strength between the clamping structure and the wing plate 21. The base plate 4 and the reflector 3 can be fixedly connected by welding, bonding, or integral molding.
[0038] In some embodiments, as Figure 5 As shown, the reflector 3 is movably connected to the base plate 4. The clamping structure also includes a second movable portion 6 connected to the base plate 4. The second movable portion 6 can move toward the third end surface 213 until it abuts the reflector 3. At this point, the reflector 3 is clamped between the second movable portion 6 and the third end surface 213. The position of the reflector 3 relative to the wing plate 21 along the thickness direction of the wing plate 21 is adjustable. Because the ends of the wing plate 21 are inclined, the longest end of the wing plate 21 aligns with the middle of the reflector 3 (the location where the reflective tape is affixed, preferably the center of the tape). This is the most accurate measurement of the steel beam length, so the position of the reflector 3 needs to be adjusted. The reflector 3 is clamped between the second movable portion 6 and the third end surface 213 to maintain a vertical position relative to the base plate 4.
[0039] In a specific implementation, a second nut is connected to the base plate 4, and the second movable portion 6 is a second screw. The second screw and the second nut form a bolted connection pair. When the reflector 3 is fixedly connected to the base plate 4, the second nut can be located above or below the base plate 4. When the reflector 3 is movably connected to the base plate 4, the second nut is located above the base plate 4. The second screw and the second nut form a bolted connection pair, which is easy to implement on site, low-cost, and practical.
[0040] In some embodiments, the wing plate 21 is clearance-matched with the slot, that is, the width of the slot is greater than the thickness of the wing plate 21 , and the wing plate 21 and the clamping structure are easier to disassemble. At the same time, the clamping structure is adapted to wing plates 21 of different thicknesses.
[0041] In some embodiments, one end of the first screw toward the wing plate 21 extends radially along the first screw to form a first limiting portion, and the cross-sectional area of the first limiting portion is larger than the cross-sectional area of the first threaded hole or the threaded hole of the first nut. One end of the second screw toward the wing plate 21 extends radially along the second screw to form a second limiting portion, and the cross-sectional area of the second limiting portion is larger than the cross-sectional area of the threaded hole of the second nut. The first limiting portion / the second limiting portion can increase the connection area when the first screw / the second screw abuts the wing plate 21, so as to make the connection between the clamping structure and the wing plate 21 more stable; at the same time, the first limiting portion / the second limiting portion can also prevent the first screw / the second screw from being separated from the first nut / the second nut, thereby preventing the first screw and the second screw from being lost during practical use of the detection device based on the total station.
[0042] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprises," "comprising," or any other variations thereof are intended to cover non-exclusive inclusion, so that a process, method, article, or device comprising a series of elements includes not only those elements, but also other elements not explicitly listed, or elements inherent to such process, method, article, or device. In the absence of further limitations, an element defined by the phrase "comprising a ..." does not exclude the presence of other identical elements in the process, method, article, or device comprising the element.
[0043] The foregoing is merely a list of specific embodiments of the present application, intended to enable those skilled in the art to understand and implement the present application. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of the present application. Therefore, the present application is not limited to the embodiments described herein, but is intended to conform to the broadest scope consistent with the principles and novel features of the present application.
Claims
1. A detection device based on a total station for measuring a truss (2), characterized in that: The truss (2) comprises a total station and four detection assemblies (1), wherein the truss (2) has four vertex angles, each of the vertex angles is connected to a detection assembly (1), and the total station cooperates with the four detection assemblies (1) to measure the three-dimensional coordinates of the four vertex angles; The detection assembly (1) comprises a reflective plate (3) and a clamping structure connected to each other, and the reflective plate (3) is detachably connected to the truss (2) via the clamping structure; The clamping structure comprises a bottom plate (4) connected to the reflective plate (3), the bottom plate (4) being provided with a slot, and the truss (2) comprising a steel beam, the wing plate (21) of the steel beam being plugged into the slot.
2. The detection device based on the total station according to claim 1, characterized in that: The clamping structure further comprises a first movable portion (5) connected to the bottom plate (4), the first movable portion (5) being capable of moving closer to or farther from the wing plate (21), the wing plate (21) having a first surface (211) and a second surface (212) opposite to each other along its thickness direction, and the wing plate (21) having a third end surface (213) at one end along its length direction; The clamping structure has a clamping state, wherein the first surface (211) and the third end surface (213) are both in contact with the inner wall of the slot, and the second surface (212) is in contact with the first movable portion (5).
3. The detection device based on the total station according to claim 2, characterized in that: The clamping structure further comprises a second movable portion (6) connected to the base plate (4), the base plate (4) being fixedly connected to the reflective plate (3), and the second movable portion (6) being capable of moving toward the third end surface (213) to abut against the third end surface (213).
4. The detection device based on the total station according to claim 2, characterized in that: The reflective plate (3) is movably connected to the base plate (4), and the clamping structure further comprises a second movable portion (6) connected to the base plate (4). The second movable portion (6) can move toward the third end surface (213) to abut against the reflective plate (3). At this time, the reflective plate (3) is clamped between the second movable portion (6) and the third end surface (213).
5. The detection device based on the total station according to claim 2, characterized in that: The first movable part (5) is a first screw, a first threaded hole is formed on the bottom plate (4), and the first screw and the first threaded hole form a threaded fit.
6. The detection device based on the total station according to claim 2, characterized in that: The base plate (4) is connected to a first nut, the first movable part (5) is a first screw, and the first screw and the first nut form a bolt connection pair.
7. The detection device based on the total station according to claim 3, characterized in that: A second nut is connected to the bottom plate (4), the second movable part (6) is a second screw, and the second screw and the second nut form a bolt connection pair.
8. The detection device based on a total station according to any one of claims 2 to 7, characterized in that: The wing plate (21) is clearance-matched with the slot.
9. The detection device based on a total station according to claim 5, characterized in that: One end of the first screw toward the wing plate (21) extends radially along the first screw to form a first limiting portion, and the cross-sectional area of the first limiting portion is larger than the cross-sectional area of the first threaded hole.