Automatic detector for buildings and structures
By designing an automated detector and using the cooperation of the drone and suction cup components, the problems of low detection accuracy and efficiency in the prior art are solved, and efficient and accurate detection of the building is achieved.
Patent Information
- Application Number
- CN202411411392.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-10
- Publication Date
- 2024-12-27
AI Technical Summary
The existing building inspection technology has insufficient accuracy and efficiency, especially the appearance camera inspection of drones cannot fully detect hollowing and material performance, and the climbing inspection efficiency of the inspectors is low, making it difficult to quickly complete the inspection of a large number of buildings.
Design an automated detector for building structures, including drone components, installation frames, camera components, infrared components, pressure gauge, sampling components and suction cup components. Through the cooperation of drone flight and suction cup components, the comprehensive construction of the building is achieved. Detection, improve detection accuracy and efficiency.
High-precision detection of buildings is realized, the inspection of a large number of buildings can be completed quickly and effectively, the detection efficiency is improved, and the detection is carried out on corners and complex terrain through the movement function of the suction cup assembly.
Smart Images

Figure CN119198745A_ABST
Abstract
Description
Technical Field
[0001] The invention relates to the technical field of building structure detection, and in particular to an automatic detection instrument for building structures. Background Art
[0003] Buildings and structures have a certain service life. During the use of buildings and structures, they need to be inspected regularly to understand the health of the buildings and prevent property losses and harm to people’s lives due to poor local quality or damage.
[0004] When inspecting buildings, the main focus is on checking whether there are cracks, whether there are cracks, deformation or other damage in the main load-bearing components, such as beams, columns, slabs, walls, etc., and evaluating the performance of various materials that make up the building, including the aging, corrosion or degradation of concrete, steel, masonry, wood, etc., and checking whether there are leakage, water accumulation or moisture problems, which may cause structural damage or mildew, as well as hollowing. At present, the inspection of buildings is mainly carried out by drone appearance camera inspection, or inspection personnel climb on the buildings to conduct inspections using various instruments. When using drone appearance camera inspection, the inspection of hollowing, material performance, etc. is not thorough. When using inspection personnel to climb on the building for inspection, the inspection accuracy is high, but the inspection efficiency is too low. When a large number of buildings need to be inspected, it is difficult to complete the inspection quickly and effectively.
[0005] Therefore, those skilled in the art are committed to developing an automated building detection instrument that can not only improve the detection accuracy of buildings, but also improve the detection efficiency of buildings. Summary of the invention
[0007] The technical problem to be solved by the present invention is to provide an automatic building detection instrument, which can not only improve the detection accuracy of buildings, but also improve the detection efficiency of buildings. The technical solution of the present invention to solve the above technical problems is as follows: An automatic detector for building structures, comprising UAV components; A mounting frame, the mounting frame is located at the lower side of the drone assembly, a camera assembly and an infrared assembly are mounted on the mounting frame, and a pressure gauge and a sampling assembly are also mounted in the mounting frame; A first suction cup assembly, the first suction cup assembly on both sides being mounted on both sides of the mounting frame; A second suction cup assembly, wherein two of the second suction cup assemblies are located on both sides of the mounting frame, and a lifting assembly is installed between the second suction cup assembly and the mounting frame; A control component, wherein the control component has a storage module, and the control component is electrically connected to the camera component, the infrared component, the pressure gauge, the sampling component, the first suction cup component, the second suction cup component and the lifting component.
[0008] The beneficial effects of adopting the above scheme are: during the flight of the installation frame driven by the drone component, the camera component and the infrared component detect the appearance and infrared information of the building, and transmit the detection information to the storage module; After reaching the set position, the control component controls the first suction cup component and the second suction cup component to extend and adsorb on the structure, so that the pressure gauge can detect the structure, and the sampling component can also take samples from the surface of the structure for further analysis; At corners or places that are inconvenient for drone components to reach, the cooperation of the first suction cup assembly, the second suction cup assembly and the lifting assembly allows the installation frame to crawl and move on the surface of the building, thereby facilitating the detection of various positions of the building and improving the detection accuracy and efficiency.
[0009] Based on the above technical solution, the present invention can also be improved as follows.
[0010] Furthermore, the adsorption ends of the first suction cup assembly and the second suction cup assembly are both connected to a vacuum assembly, and the vacuum assembly is electrically connected to the control assembly.
[0011] The beneficial effect of adopting the above further scheme is that the vacuum assembly is connected to the adsorption ends of the first suction cup assembly and the second suction cup assembly, so that the suction cup assembly has sufficient adsorption force to keep the drone assembly and the mounting frame stable.
[0012] Furthermore, the sampling assembly includes a sampling drill bit, a support block, a thrust assembly and a power assembly. The sampling drill bit has a sampling cavity, and the end of the sampling drill bit has drill teeth. The sampling drill bit is installed on the support block through a mounting bearing. The sampling drill bit is also connected to the thrust assembly and the power assembly.
[0013] The beneficial effect of adopting the above further scheme is that the rotation of the power component drives the sampling drill bit to rotate, and the thrust component pushes the drill bit to move, so that the drill teeth drill samples on the surface of the building and temporarily store them in the sampling cavity.
[0014] Further, the thrust assembly includes a first electromagnet, a second electromagnet and a return spring, the first electromagnet is installed on the support block, the second electromagnet is installed on the sampling drill bit, the return spring is sleeved on the outer layer of the sampling drill bit and the two ends of the return spring are respectively abutted against the first electromagnet and the second electromagnet, and the first electromagnet and the second electromagnet are electrically connected to the control assembly.
[0015] The beneficial effect of adopting the above further scheme is that when the control component controls the power component to rotate, it simultaneously controls the first electromagnet and the second electromagnet to be energized, so that the first electromagnet and the second electromagnet attract each other and compress the reset spring, thereby pushing the drill bit to move along the axial direction of the mounting bearing to drill samples on the surface of the building.
[0016] Furthermore, a transmission groove is provided on the outer wall of the sampling drill bit and on a side opposite to the drill teeth, a rotating shaft is installed at the output end of the power component, a transmission pin is provided on the rotating shaft, and the transmission pin is located in the transmission groove.
[0017] The beneficial effect of adopting the above further solution is that the rotation of the power assembly drives the rotation shaft and the transmission pin to rotate, thereby driving the sampling drill bit to rotate, ensuring that the power assembly and the sampling drill bit rotate synchronously when the sampling drill bit moves horizontally.
[0018] Further, the first suction cup assembly includes a first suction cup, the first suction cup is installed at the output end of the first telescopic assembly, and the first telescopic assembly is connected to the control assembly; The second suction cup assembly includes a second suction cup, the second suction cup is installed at the output end of the second telescopic assembly, and the second telescopic assembly is connected to the control assembly.
[0019] The beneficial effect of adopting the above further solution is that the telescopic component drives the suction cup component to move, which is conducive to the suction cup component being adsorbed on the surface of the building, and is conducive to subsequent sampling or pressure gauge detection.
[0020] Furthermore, the first suction cup and the second suction cup each have a through hole, and the through hole is connected to the suction end of the vacuum assembly.
[0021] The beneficial effect of adopting the above further solution is that the vacuum pumping component continuously draws a vacuum so that the suction cup component always has a suitable vacuum degree, which helps the suction cup to be adsorbed on the building to avoid falling off.
[0022] Further, the lifting assembly includes a lifting screw, a lifting motor, a lifting plate and a guide block, the lifting screw is installed in the installation frame through a screw mounting seat, one end of the lifting screw is connected to the lifting motor, the lifting motor drives the lifting screw to rotate, the lifting screw outer sleeve is provided with the lifting plate, the lifting plate has a threaded hole matched with the lifting screw, and the lifting plate is connected to the second suction cup assembly; The guide blocks are also installed at both ends of the lifting plate, and the inner side wall of the installation frame is also provided with a guide groove that cooperates with the guide blocks.
[0023] The beneficial effect of adopting the above further solution is that the control component controls the lifting motor to rotate so that the second suction cup component moves up and down, which is beneficial for the installation frame to crawl and move on the surface of the building.
[0024] Furthermore, the camera component includes a high-speed camera, the infrared component includes an infrared detector, and the high-speed camera and the infrared detector are both electrically connected to the control component.
[0025] The beneficial effect of adopting the above further scheme is: the high-speed camera collects the surface information of the building, the infrared detector collects the infrared information of the building, and transmits the various information to the storage module for storage, which is conducive to further analysis and detection later.
[0026] Furthermore, the pressure gauge is a concrete pressure gauge, and the concrete pressure gauge is electrically connected to the control component.
[0027] The beneficial effect of adopting the above further solution is that the concrete pressure gauge is used to detect the internal pressure of the building structure. BRIEF DESCRIPTION OF THE DRAWINGS
[0028] Figure 1 It is a structural schematic diagram of a specific embodiment of the present invention; Figure 2 This is a schematic diagram of the internal plane layout structure of the installation frame of a specific embodiment of the present invention; Figure 3 This is a schematic diagram of the structure of a sampling component according to a specific embodiment of the present invention; Figure 4 It is a schematic diagram of the structure of a lifting assembly according to a specific embodiment of the present invention.
[0029] In the accompanying drawings, the components represented by the reference numerals are listed as follows: 1. UAV assembly; 2. Mounting frame; 3. Camera assembly; 4. Infrared assembly; 5. Pressure gauge; 6. Sampling assembly; 7. First suction cup assembly; 8. Second suction cup assembly; 9. Lifting assembly; 10. Control assembly; 11. Vacuum assembly; 12. Sampling drill bit; 13. Support block; 14. Thrust assembly; 15. Power assembly; 16. Sampling chamber; 17. Drill teeth; 18. Mounting bearing; 19. First electromagnet; 20. Second electromagnet; 21. Return spring; 22. Transmission groove; 23. Transmission pin; 24. First suction cup; 25. First telescopic assembly; 26. Second suction cup; 27. Second telescopic assembly; 28. Through hole; 29. Lifting screw; 30. Lifting motor; 31. Lifting plate; 32. Guide block; 33. Screw mounting seat; 34. Guide groove; 35. High-speed camera; 36. Concrete pressure gauge; 37. Infrared detector; 38. Battery. DETAILED DESCRIPTION
[0031] The principles and features of the present invention are described below in conjunction with the accompanying drawings. The examples given are only used to explain the present invention and are not used to limit the scope of the present invention.
[0032] In the description of the present invention, it is necessary to understand that the terms "center", "length", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "inside", "outside", "peripheral", "circumferential" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, and do not indicate or imply that the referred system or element must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be understood as a limitation on the present invention.
[0033] In the description of the present invention, “plurality” means at least two, for example, two, three, etc., unless otherwise clearly and specifically defined.
[0034] In the present invention, unless otherwise clearly specified and limited, the terms "installed", "connected", "connected", "fixed" and the like should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium, it can be the internal connection of two elements or the interaction relationship between two elements, unless otherwise clearly defined. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.
[0035] like Figure 1 , Figure 2 , Figure 3 and Figure 4 As shown, an automatic detector for building structures includes: UAV component 1; An installation frame 2, the installation frame 2 is located at the lower side of the drone component 1, a camera component 3 and an infrared component 4 are installed on the installation frame 2, and a pressure gauge 5 and a sampling component 6 are also installed in the installation frame 2; The first suction cup assembly 7, the first suction cup assembly 7 on both sides is installed on both sides of the mounting frame 2; A second suction cup assembly 8, wherein two second suction cup assemblies 8 are located on both sides of the mounting frame 2, and a lifting assembly 9 is installed between the second suction cup assembly 8 and the mounting frame 2; The control component 10 has a storage module, and the control component 10 is electrically connected to the camera component 3, the infrared component 4, the pressure gauge 5, the sampling component 6, the first suction cup component 7, the second suction cup component 8 and the lifting component 9.
[0036] In the present invention, when the drone component 1 drives the mounting frame 2 to fly, the camera component 3 and the infrared component 4 detect the appearance and infrared information of the building, and transmit the detection information to the storage module; After reaching the set position, the control component 10 controls the first suction cup component 7 and the second suction cup component 8 to extend and adsorb on the structure, so that the pressure gauge 5 can detect the structure, and it is also convenient for the sampling component 6 to sample the surface of the structure for further analysis; At corners or places that are inconvenient for the drone assembly 1 to reach, the first suction cup assembly 7, the second suction cup assembly 8 and the lifting assembly 9 cooperate to enable the mounting frame 2 to crawl on the surface of the building, thereby facilitating the detection of various positions of the building and improving the detection accuracy and efficiency.
[0037] like Figure 1 , Figure 2 As shown, in some embodiments, the suction ends of the first suction cup assembly 7 and the second suction cup assembly 8 are both connected to the vacuum assembly 11, and the vacuum assembly 11 is electrically connected to the control assembly 10. Specifically, the first suction cup assembly 7 includes a first suction cup 24, which is installed at the output end of the first telescopic assembly 25, and the first telescopic assembly 25 is connected to the control assembly 10. The second suction cup assembly 8 includes a second suction cup 26, and the first suction cup 24 and the second suction cup 26 can both be rubber suction cups, and the second suction cup 26 is installed at the output end of the second telescopic assembly 27, and the second telescopic assembly 27 is connected to the control assembly 10. The control assembly 10 controls the first telescopic assembly 25 and the second telescopic assembly 27 to extend or retract, thereby facilitating the suction cups to be adsorbed on the surface of the building. In order to ensure that the suction cups always have sufficient adsorption force, the first suction cup 24 and the second suction cup 26 are each provided with a through hole 28, and the through hole 28 is connected to the suction end of the vacuum assembly 11.
[0038] like Figure 1 , Figure 2 and Figure 4 As shown, in the embodiment, the lifting assembly 9 includes a lifting screw 29, a lifting motor 30, a lifting plate 31 and a guide block 32. Both ends of the lifting screw 29 are installed in the mounting frame 2 through a screw mounting seat 33. One end of the lifting screw 29 is connected to the lifting motor 30. The lifting motor 30 can be a servo motor. The lifting motor 30 drives the lifting screw 29 to rotate. The lifting screw 29 is provided with a lifting plate 31 on its outer sleeve. The lifting plate 31 has a threaded hole that matches the lifting screw 29. The lifting motor 30 rotates to drive the lifting screw 29 to rotate, thereby driving the lifting plate 31 to move up and down. The lifting plate 31 is connected to the second suction cup assembly 8. In order to make the lifting plate 31 move up and down smoothly, guide blocks 32 are also installed at both ends of the lifting plate 31, and the inner side wall of the mounting frame 2 is also provided with a guide groove 34 that matches the guide block 32.
[0039] like Figure 1 , Figure 2 and Figure 3 As shown, in another embodiment, the sampling assembly 6 includes a sampling drill bit 12, a support block 13, a thrust assembly 14 and a power assembly 15. The sampling drill bit 12 has a sampling cavity 16. The diameter of the front end of the sampling drill bit 12 is smaller than the diameter of the rear end, so that the rear sampling cavity 16 can store an appropriate amount of sample. The end of the sampling drill bit 12 has a drill tooth 17. The sampling drill bit 12 is installed on the support block 13 through a mounting bearing 18. The support block 13 is installed in the mounting frame 2. The sampling drill bit 12 is also connected to the thrust assembly 14 and the power assembly 15.
[0040] In the embodiment, the thrust assembly 14 includes a first electromagnet 19, a second electromagnet 20 and a return spring 21, the first electromagnet 19 is in a circular ring shape and is installed on the support block 13, the sampling drill bit 12 passes through the circular ring and abuts against the mounting bearing 18, the second electromagnet 20 is installed on the sampling drill bit 12, the return spring 21 is sleeved on the outer layer of the sampling drill bit 12 and the two ends of the return spring 21 are respectively abutted against the first electromagnet 19 and the second electromagnet 20, the first electromagnet 19 and the second electromagnet 20 are electrically connected to the control assembly 10, the control assembly 10 controls the first electromagnet 19 and the second electromagnet 20 to be energized, so that the first electromagnet 19 and the second electromagnet 20 attract each other and compress the return spring 21, because the sampling drill bit 12 is fixedly connected to the second electromagnet 20, the second electromagnet 20 moves toward the first electromagnet 19 under the magnetic force of the first electromagnet 19, and drives the sampling drill bit 12 to move axially downward toward the mounting bearing 18.
[0041] When the sampling drill bit 12 moves horizontally to drill samples on the surface of the building, the power assembly 15 can drive the sampling drill bit 12 to rotate continuously. Specifically, the outer wall of the sampling drill bit 12 and the side opposite to the drill teeth 17 have a transmission groove 22, and a plurality of transmission grooves 22 can be provided. A rotating shaft is installed at the output end of the power assembly 15, and a transmission pin 23 is provided on the rotating shaft. The transmission pin 23 is located in the transmission groove 22. When the transmission pin 24 drives the sampling drill bit 12 to rotate, the transmission pin 24 can move along the transmission groove 22.
[0042] like Figure 1 , Figure 2 As shown, in the embodiment, the camera assembly 3 includes a high-speed camera 35, the infrared assembly 4 includes an infrared detector 37, the high-speed camera 35 and the infrared detector 37 are both electrically connected to the control assembly 10, and the pressure gauge 5 is a concrete pressure gauge 36, which is electrically connected to the control assembly 10. The high-speed camera 35, the concrete pressure gauge 36 and the infrared detector 37 transmit the detection information to the storage module, which is conducive to further analysis and judgment later. The control assembly 10 is also connected to a battery 38, and the battery 38 is installed in the installation frame 2.
[0043] In the description of this specification, the description with reference to the terms "one embodiment", "some embodiments", "example", "specific example", or "some examples" etc. means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present invention. In this specification, the schematic representations of the above terms do not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described may be combined in any one or more embodiments or examples in a suitable manner. In addition, those skilled in the art may combine and combine the different embodiments or examples described in this specification and the features of the different embodiments or examples, without contradiction.
[0044] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims
1. An automatic detector for building structures, characterized in that: include Drone components (1); A mounting frame (2), the mounting frame (2) being located at the lower side of the drone component (1), the mounting frame (2) being provided with a camera component (3) and an infrared component (4), and the mounting frame (2) being provided with a pressure gauge (5) and a sampling component (6); A first suction cup assembly (7), the first suction cup assembly (7) being mounted on both sides of the mounting frame (2); A second suction cup assembly (8), wherein two second suction cup assemblies (8) are located on both sides of the mounting frame (2), and a lifting assembly (9) is installed between the second suction cup assembly (8) and the mounting frame (2); A control component (10), the control component (10) having a storage module, the control component (10) being electrically connected to the camera component (3), the infrared component (4), the pressure gauge (5), the sampling component (6), the first suction cup component (7), the second suction cup component (8) and the lifting component (9).
2. The automatic detector for building structures according to claim 1, characterized in that: The suction ends of the first suction cup assembly (7) and the second suction cup assembly (8) are both connected to a vacuum assembly (11), and the vacuum assembly (11) is electrically connected to the control assembly (10).
3. The automatic detector for building structures according to claim 1, characterized in that: The sampling assembly (6) comprises a sampling drill bit (12), a support block (13), a thrust assembly (14) and a power assembly (15); the sampling drill bit (12) has a sampling cavity (16), and the end of the sampling drill bit (12) has a drill tooth (17); the sampling drill bit (12) is mounted on the support block (13) via a mounting bearing (18); and the sampling drill bit (12) is also connected to the thrust assembly (14) and the power assembly (15).
4. The automatic detector for building structures according to claim 3 is characterized in that: The thrust assembly (14) comprises a first electromagnet (19), a second electromagnet (20) and a return spring (21), wherein the first electromagnet (19) is mounted on the support block (13), the second electromagnet (20) is mounted on the sampling drill bit (12), the return spring (21) is sleeved on the outer layer of the sampling drill bit (12), and two ends of the return spring (21) are respectively in contact with the first electromagnet (19) and the second electromagnet (20), and the first electromagnet (19) and the second electromagnet (20) are both electrically connected to the control assembly (10).
5. The automatic detector for building structures according to claim 4 is characterized in that: The outer wall of the sampling drill bit (12) and the side opposite to the drill teeth (17) has a transmission groove (22), and the output end of the power assembly (15) is equipped with a rotating shaft, and the rotating shaft has a transmission pin (23), and the transmission pin (23) is located in the transmission groove (22).
6. The automatic detector for building structures according to claim 2, characterized in that: The first suction cup assembly (7) comprises a first suction cup (24), the first suction cup (24) being mounted at the output end of a first telescopic assembly (25), the first telescopic assembly (25) being connected to the control assembly (10); The second suction cup assembly (8) comprises a second suction cup (26), the second suction cup (26) being mounted at the output end of a second telescopic assembly (27), the second telescopic assembly (27) being connected to the control assembly (10).
7. The automatic detector for building structures according to claim 6, characterized in that: The first suction cup (24) and the second suction cup (26) are both provided with a through hole (28), and the through hole (28) is connected to the suction end of the vacuum assembly (11).
8. The automatic detector for building structures according to claim 3 is characterized in that: The lifting assembly (9) comprises a lifting screw (29), a lifting motor (30), a lifting plate (31) and a guide block (32); the lifting screw (29) is installed in the installation frame (2) via a screw mounting seat (33); one end of the lifting screw (29) is connected to the lifting motor (30); the lifting motor (30) drives the lifting screw (29) to rotate; the lifting plate (31) is provided on the outer sleeve of the lifting screw (29); the lifting plate (31) has a threaded hole that matches the lifting screw (29); and the lifting plate (31) is connected to the second suction cup assembly (8); The guide blocks (32) are also installed at both ends of the lifting plate (31), and the inner side wall of the installation frame (2) is also provided with a guide groove (34) that cooperates with the guide block (32).
9. The automatic detector for building structures according to claim 1, characterized in that: The camera assembly (3) comprises a high-speed camera (35), the infrared assembly (4) comprises an infrared detector (37), and both the high-speed camera (35) and the infrared detector (37) are electrically connected to the control assembly (10).
10. The automatic building structure detector according to claim 1, characterized in that: The pressure gauge (5) is a concrete pressure gauge (36), and the concrete pressure gauge (36) is electrically connected to the control component (10).
Citation Information
Patent Citations
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CN114802514A
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CN118549197A
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