Unmanned aerial vehicle detects bridge crack scanning device
Patent Information
- Application Number
- CN202521557853.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-07-24
- Publication Date
- 2026-10-27
- Estimated Expiration
- 2035-07-24
AI Technical Summary
无人机检测桥梁裂缝的扫描装置在使用时通过相机捕捉裂缝细节,但是箱梁内部、桥墩背面、伸缩缝下方等无人机无法直接飞入的狭窄空间,导致相机无法捕捉裂缝细节,存在一定的不足之处,为此,我们提出了一种无人机检测桥梁裂缝扫描装置
[0010]通过采用上述技术方案,本实用新型所取得的有益效果为:本实用设置的驱动电机可运转通过第一齿轮和第二齿轮带动丝杆,使得前移动座和后移动座不断地远离,从而调节相机和加重块的位置,调节后相机可移动至狭窄空间,且设置的旋转电机可带动相机旋转,以便捕捉裂缝细节,使用范围大,同时通过加重块可增加直线移动组件后部的重量,以便保持平衡,然后设置的弹簧具有一定的弹性势能,使得紧固杆可移动脱离安装板的限位孔,脱离后可旋转转板不再阻挡安装板,从而可直接拆卸直线移动组件,以便使用。
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Figure CN224899131U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of bridge crack detection technology, specifically a drone scanning device for detecting bridge cracks. Background Technology
[0002] The UAV scanning device for detecting bridge cracks is an intelligent detection system that combines UAV technology with high-precision sensing equipment. It is used to quickly and safely identify defects such as cracks, spalling, and corrosion on bridge surfaces. While the UAV scanning device captures crack details using a camera, it has limitations in narrow spaces such as inside box girders, behind piers, and under expansion joints, where the camera cannot directly access these areas. Therefore, we propose a UAV scanning device for detecting bridge cracks. Utility Model Content
[0003] The present invention aims to solve the problems existing in the prior art or related technologies.
[0004] Therefore, the technical solution adopted by this utility model is as follows: a scanning device for detecting bridge cracks using an unmanned aerial vehicle (UAV), comprising a body, a linear motion component, and a front moving seat. The top of the body is provided with a slot. The linear motion component includes a mounting plate inserted into the slot, a limiting hole opened on the mounting plate, a frame fixedly mounted on the top of the mounting plate, a lead screw connected to the frame bearing, a first gear fixedly mounted on the lead screw, a second gear meshing with the first gear, and a drive motor fixedly connected to the second gear. The front moving seat is threadedly connected to the lead screw, and a rotary motor is provided on the front moving seat. A camera is fixed to the output end of the rotary motor.
[0005] Preferably, the exterior of the machine body is fixed with several arms, and each of the arms is fixed with a propeller.
[0006] Preferably, the lead screw has external threads in different directions at its front and rear ends.
[0007] Preferably, it also includes a rear movable seat, which is threadedly connected to the lead screw, and a weight is fixed to the top of the rear movable seat.
[0008] Preferably, it also includes a fastening assembly, which includes a T-shaped column fixedly disposed at the top of the machine body, a rotating plate rotatably connected to the T-shaped column, a fastening rod inserted through the rotating plate, and a spring disposed on the fastening rod and the rotating plate.
[0009] Preferably, two adjacent fastening components form a group, and two groups are arranged symmetrically.
[0010] By adopting the above technical solution, the beneficial effects achieved by this utility model are as follows: The drive motor of this utility model can drive the lead screw through the first gear and the second gear, so that the front moving seat and the rear moving seat move away from each other, thereby adjusting the position of the camera and the weight block. After adjustment, the camera can be moved to a narrow space, and the set rotary motor can drive the camera to rotate in order to capture crack details, thus having a wide range of applications. At the same time, the weight block can increase the weight of the rear of the linear movement component to maintain balance. Then, the set spring has a certain elastic potential energy, which allows the fastening rod to move away from the limiting hole of the mounting plate. After it moves away, the rotating plate can be rotated and no longer obstructs the mounting plate, so the linear movement component can be directly disassembled for use. Attached Figure Description
[0011] Figure 1 This is a schematic diagram of the structure of this utility model;
[0012] Figure 2 This utility model Figure 1 A schematic diagram of the structure of the middle body;
[0013] Figure 3 This utility model Figure 1 A schematic diagram of the linear motion component;
[0014] Figure 4 This utility model Figure 3 A schematic diagram of the structure of the front moving base and the camera;
[0015] Figure 5 This utility model Figure 1 A schematic diagram of the structure of the central fastening assembly.
[0016] Figure label:
[0017] 100. Airframe; 101. Arm; 102. Propeller; 103. Slot;
[0018] 200. Linear movement assembly; 201. Frame; 202. Lead screw; 203. First gear; 204. Second gear; 205. Drive motor; 206. Mounting plate; 2061. Limiting hole;
[0019] 300. Front moving base; 301. Camera; 302. Rotary motor;
[0020] 400. Rear movable seat; 401. Weight block;
[0021] 500, Fastening assembly; 501, T-post; 502, Rotating plate; 503, Fastening rod; 504, Spring. Detailed Implementation
[0022] To make the objectives, technical solutions, and advantages of this utility model clearer, the present utility model will be further described in detail below with reference to specific embodiments and accompanying drawings. It should be noted that, unless otherwise specified, the embodiments and features of the present utility model can be combined with each other.
[0023] The following describes some embodiments of the present invention with reference to the accompanying drawings, providing a drone-based bridge crack detection scanning device.
[0024] Example 1:
[0025] Reference Figure 1-5 This is the first embodiment of the present invention. This embodiment provides a scanning device for detecting bridge cracks using an unmanned aerial vehicle (UAV), including a body 100, a linear motion component 200, and a front moving base 300.
[0026] Specifically, the top of the fuselage 100 is provided with a slot 103, and several arms 101 are fixed to the outside of the fuselage 100. Each of the arms 101 is fixed with a propeller 102. In use, the linear motion component 200 can be fixed through the slot 103. The arms 101 are used to support and fix the propeller 102, and the propeller 102 can rotate at high speed so that the fuselage 100 can take off.
[0027] Specifically, the linear motion assembly 200 includes a mounting plate 206 inserted into the slot 103, a limiting hole 2061 opened on the mounting plate 206, a frame 201 fixedly mounted on the top of the mounting plate 206, a lead screw 202 connected to the frame 201 by a bearing, a first gear 203 fixedly mounted on the lead screw 202, a second gear 204 meshing with the first gear 203, and a drive motor 205 fixedly connected to the second gear 204. The front and rear parts of the lead screw 202 are provided with external threads in different directions. In use, the mounting plate 206 can increase the contact area between the linear motion assembly 200 and the machine body 100 for fixing, while the limiting hole 2061 has a limiting effect to fix the assembly 500. The drive motor 205 can drive the first gear 203, the second gear 204 and the lead screw 202 to rotate, so that the lead screw 202 can push the front moving seat 300 to move, thereby adjusting the position of the camera 301 so that the camera 301 can be moved into narrow spaces.
[0028] Specifically, the front moving base 300 is threaded onto the lead screw 202. A rotary motor 302 is installed on the front moving base 300. A camera 301 is fixed to the output end of the rotary motor 302. In use, the front moving base 300 can drive the camera 301 to move so that the camera 301 can move into a narrow space to capture crack details. The rotary motor 302 can drive the camera 301 to rotate so that the angle of the camera 301 can be adjusted.
[0029] Example 2:
[0030] Reference Figure 1 and Figure 3 This is the second embodiment of the present invention, which differs from the first embodiment in that it also includes a rear movable seat 400, which is threadedly connected to the lead screw 202. A weight block 401 is fixed to the top of the rear movable seat 400. In use, the rear movable seat 400 and the weight block 401 can be moved by the lead screw 202. The weight block 401 can be symmetrical with the camera 301. The weight block 401 can increase the weight of the rear of the linear motion component 200 in order to maintain balance.
[0031] Example 3:
[0032] Reference Figure 1 and Figure 5 This is the third embodiment of the present invention, which differs from the previous two embodiments in that it also includes a fastening assembly 500. The fastening assembly 500 includes a T-shaped column 501 fixedly installed at the top of the body 100, a rotating plate 502 rotatably connected to the T-shaped column 501, a fastening rod 503 inserted on the rotating plate 502, and a spring 504 installed on the fastening rod 503 and the rotating plate 502. Two adjacent fastening assemblies 500 form a group, and two groups are symmetrically arranged. In use, the spring 504 makes the fastening rod 503 movable so that the fastening rod 503 can disengage from the limiting hole 2061. After disengagement, the rotating plate 502 can be rotated to no longer block the mounting plate 206, so as to quickly disassemble the linear movement assembly 200.
[0033] The working principle and usage process of this utility model are as follows: In use, the mounting plate 206 can be inserted into the slot 103, then the fastening rod 503 can be pulled to a suitable height, and the rotating plate 502 can be rotated until the bottom of the fastening rod 503 is aligned with the limiting hole 2061 of the mounting plate 206. Then the fastening rod 503 can be released. After release, the fastening rod 503 can be inserted into the limiting hole 2061, thus fixing the linear movement component 200 on the machine body 100. Then the drive motor 205 is controlled to run. The running drive motor 205 will drive the lead screw 202 to rotate through the first gear 203 and the second gear 204. The rotating lead screw 202 will push the front moving seat 300 and the rear moving seat 400 to move away from each other. After moving to a suitable position, the rotary motor 302 can be controlled to run. The running rotary motor 302 can drive the camera 301 to rotate, thus capturing the details of the crack.
[0034] Although embodiments of the present invention have been shown and described, those skilled in the art will understand that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the claims and their equivalents.
Claims
1. A UAV scanning device for detecting bridge cracks, characterized in that, include: The top of the body (100) is provided with a slot (103); The linear motion assembly (200) includes a mounting plate (206) inserted into the slot (103), a limiting hole (2061) opened on the mounting plate (206), a frame (201) fixedly mounted on the top of the mounting plate (206), a lead screw (202) bearing connected to the frame (201), a first gear (203) fixedly mounted on the lead screw (202), a second gear (204) meshing with the first gear (203), and a drive motor (205) fixedly connected to the second gear (204). A front movable seat (300) is threadedly connected to the lead screw (202). A rotary motor (302) is provided on the front movable seat (300), and a camera (301) is fixed to the output end of the rotary motor (302).
2. The UAV bridge crack detection scanning device according to claim 1, characterized in that, The body (100) has several arms (101) fixed to its exterior, and each of the arms (101) has a propeller (102) fixed to it.
3. The UAV scanning device for detecting bridge cracks according to claim 1, characterized in that, The lead screw (202) has external threads with different directions at its front and rear.
4. The UAV scanning device for detecting bridge cracks according to claim 1, characterized in that, It also includes a rear movable seat (400), which is threadedly connected to the lead screw (202), and a weight block (401) is fixed to the top of the rear movable seat (400).
5. The UAV scanning device for detecting bridge cracks according to claim 1, characterized in that, It also includes a fastening assembly (500), which includes a T-shaped post (501) fixedly disposed at the top of the body (100), a rotating plate (502) rotatably connected to the T-shaped post (501), a fastening rod (503) inserted through the rotating plate (502), and a spring (504) disposed on the fastening rod (503) and the rotating plate (502).
6. The UAV scanning device for detecting bridge cracks according to claim 5, characterized in that, Two adjacent fastening components (500) form a group, and two groups are symmetrically arranged.