Modularized disassembly and assembly unmanned aerial vehicle mounting type X-ray flaw detection device

Abstract

The utility model discloses a modularly disassembled and assembled unmanned aerial vehicle mounted X-ray flaw detection device which comprises an unmanned aerial vehicle body and a mounted X-ray flaw detection mechanism, and the mounted X-ray flaw detection mechanism is fixedly mounted at the bottom of the unmanned aerial vehicle body through bolts; the mounting X-ray flaw detection mechanism comprises a connecting plate, a plurality of frame rods, a frame plate, an X-ray flaw detection assembly and a locking assembly; and the plurality of frame rods are symmetrically mounted at the bottom of the connecting plate. The unmanned aerial vehicle mounting type X-ray flaw detection device capable of being modularly disassembled and assembled is reasonable in structural design and convenient to use, X-ray flaw detection equipment is installed in a clamping mode, corresponding tool operation is not needed when the X-ray flaw detection equipment is disassembled and assembled, the operation convenience is improved, the operation time is shortened, a multi-direction clamping mechanism is adopted, and the unmanned aerial vehicle mounting type X-ray flaw detection device is convenient to disassemble and assemble. The installation stability of the X-ray flaw detection device can be guaranteed to the maximum extent, it is guaranteed that the unmanned aerial vehicle cannot slide in the flying process, and the good using effect is achieved.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) payload technology, specifically a modularly detachable UAV-mounted X-ray flaw detection device. Background Technology

[0002] The main function of unmanned payload devices is to endow drones with more functions, playing an important role in security, agriculture, forestry, power, rescue, and other fields. Currently, X-ray flaw detectors are usually mounted on drone payload devices using bolts. However, bolt mounting requires corresponding tools for disassembly and assembly, which consumes time and effort. This method cannot quickly install the X-ray flaw detector on the drone payload device, thus reducing the effectiveness of the drone-mounted X-ray flaw detector and directly affecting the rapid deployment of the X-ray flaw detector. Therefore, we propose a modular, disassembly-and-assemble drone-mounted X-ray flaw detector device to solve the problems mentioned in the background. Utility Model Content

[0003] The purpose of this invention is to provide a modular, detachable, UAV-mounted X-ray flaw detection device to solve the problems mentioned in the background art.

[0004] To achieve the above objectives, this utility model provides the following technical solution: a modularly detachable UAV-mounted X-ray flaw detection device, comprising a UAV body and a mounted X-ray flaw detection mechanism, wherein the mounted X-ray flaw detection mechanism is fixedly installed on the bottom of the UAV body by bolts;

[0005] The mounting X-ray flaw detection mechanism includes a connecting plate, a support rod, a frame plate, an X-ray flaw detection component, and a locking component. There are multiple support rods, which are symmetrically installed at the bottom of the connecting plate. The frame plate is fixedly connected to one end of several support rods. The top of the frame plate has an installation groove, and the X-ray flaw detection component is installed in the installation groove. There are two locking components, which are symmetrically installed at the bottom of the frame plate.

[0006] Furthermore, the X-ray flaw detection assembly includes an X-ray flaw detection machine, a rectangular insert plate is fixedly connected to the bottom of the X-ray flaw detection machine, and a connecting block is fixedly installed at the bottom of the rectangular insert plate.

[0007] Furthermore, the frame plate has a slot and a storage slot respectively on the left and right sides of the inner wall of the mounting groove, and a through hole communicating with the mounting groove is opened at the bottom of the frame plate. The left end of the rectangular insert plate extends into the slot, and the bottom of the connecting block extends through to the outside of the through hole.

[0008] Furthermore, the locking assembly includes a bottom shell, which is fixedly installed at the bottom of the frame plate. A transverse plate is slidably connected inside the bottom shell via two guide sliders. A locking rod is fixedly installed on the side of the transverse plate near the connecting block. One end of the locking rod passes through a circular insertion hole on the outside of the connecting block. Several thrust springs are also fixedly connected between the transverse plate and the inner wall of the bottom shell. A protrusion is fixedly connected to the bottom of the transverse plate. A corresponding through-hole is provided on the bottom shell at the position of the protrusion. One side of the protrusion extends outside the through-hole. A hanging ring is rotatably connected to the protrusion located outside the bottom shell. A hanging rod that cooperates with the hanging ring is also fixedly connected to the bottom of the bottom shell.

[0009] Furthermore, a clamping frame is slidably connected laterally within the mounting slot and to the right side of the corresponding rectangular insert plate. A circular rotating plate is rotatably connected inside the clamping frame. A screw is fixedly connected at the center of the right side of the circular rotating plate. The right end of the screw passes through the clamping frame and the storage slot in sequence and extends to the outside of the frame plate, where a rotating handle is fixedly connected. The screw is threadedly connected to the frame plate. A guide slide is symmetrically installed on the right side of the clamping frame. One end of the guide slide is slidably connected to a groove on the side wall of the storage slot. A clamping block is installed inside the clamping frame, extending into the rectangular insertion hole on the right side of the rectangular insert plate.

[0010] Furthermore, the transverse cross-sectional length of the through hole is greater than the transverse cross-sectional length of the connecting block.

[0011] Compared with the prior art, the beneficial effects of this utility model are as follows:

[0012] When the X-ray flaw detector needs to be removed, the hanging ring at the bottom of the base is pulled first. This causes the protrusion to move the transverse plate under the limit of the guide slider, compressing the thrust spring until it approaches the hanging rod. Then, the hanging ring is rotated to hang the plate on it, preventing the thrust spring from pushing the transverse plate back to its original position. At this time, the locking rod has disengaged from the connecting block. Then, the screw on the right side is rotated. Through the threaded connection with the frame plate, the circular rotating plate can be rotated to the right. Under the limit of the guide slide, the rotating circular plate can drive the clamping frame to move to the right and rotate it into the storage slot. At this time, the clamping block also disengages from the rectangular insert plate. After grasping the X-ray flaw detector, pull it to the right to disengage the rectangular insert from the slot, allowing it to be removed from the mounting slot. Similarly, during installation, simply reverse the above steps. This modular, disassembled UAV-mounted X-ray flaw detector features a reasonable structural design and is easy to use. It employs a snap-fit ​​method for installation, eliminating the need for tools during assembly and disassembly, thus improving ease of operation and shortening operation time. Furthermore, the multi-directional snap-fit ​​mechanism maximizes the stability of the X-ray flaw detector installation, preventing slippage during UAV flight and ensuring optimal performance. Attached Figure Description

[0013] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0014] Figure 2 This is a three-dimensional structural diagram of the X-ray flaw detection mechanism mounted on this utility model;

[0015] Figure 3 This is a three-dimensional structural diagram of the X-ray flaw detection component of this utility model;

[0016] Figure 4 This is a top view of the frame structure of this utility model;

[0017] Figure 5 This is a three-dimensional structural diagram of the frame plate of this utility model;

[0018] Figure 6 This is a top view of the locking assembly of this utility model.

[0019] In the diagram: 1. Unmanned aerial vehicle body; 2. Mounted X-ray flaw detection mechanism; 21. Connecting plate; 22. Frame pole; 23. Frame plate; 24. X-ray flaw detection assembly; 241. X-ray flaw detection machine; 242. Rectangular insert plate; 243. Connecting block; 25. Locking assembly; 251. Bottom shell; 252. Guide slider; 253. Horizontal sliding plate; 254. Locking rod; 255. Thrust spring; 256. Protrusion; 257. Hanging ring; 258. Hanging rod; 26. Mounting slot; 27. Slot; 28. Storage slot; 29. ​​Through hole; 210. Pressure frame; 211. Circular rotating plate; 212. Screw; 213. Guide slide; 214. Clamping block. Detailed Implementation

[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0021] Please see Figure 1-6A modular, detachable UAV-mounted X-ray flaw detection device includes a UAV body 1 and a mounting X-ray flaw detection mechanism 2. The mounting X-ray flaw detection mechanism 2 is fixedly installed on the bottom of the UAV body 1 by bolts. The UAV body 1 is a mature existing technology, mainly composed of a fuselage, propeller blades, and landing gear. The mounting X-ray flaw detection mechanism 2 is installed under the fuselage. The mounting X-ray flaw detection mechanism 2 includes a connecting plate 21, a support rod 22, a frame plate 23, an X-ray flaw detection component 24, and a locking component 25. There are multiple support rods 22, which are symmetrically installed on the bottom of the connecting plate 21. The frame plate 23 is fixedly connected to one end of several support rods 22. The top of the frame plate 23 has a mounting groove 26, and the X-ray flaw detection component 24 is placed in the mounting groove 26. There are two locking components 25, which are symmetrically installed on the bottom of the frame plate 23.

[0022] X-ray flaw detection assembly 24 includes an X-ray flaw detection machine 241, a rectangular insert plate 242 is fixedly connected to the bottom of the X-ray flaw detection machine 241, and a connecting block 243 is fixedly installed on the bottom of the rectangular insert plate 242.

[0023] The mounting plate 23 has a slot 27 and a storage slot 28 connected to each other on the left and right sides of the inner wall of the mounting groove 26, respectively. The bottom of the mounting plate 23 has a through hole 29 that communicates with the mounting groove 26. The left end of the rectangular insert 242 extends into the slot 27, and the bottom of the connecting block 243 extends through to the outside of the through hole 29. The transverse cross-sectional length of the through hole 29 is greater than the transverse cross-sectional length of the connecting block 243, which allows the rectangular insert 242 to be pushed to the left after being placed into the mounting groove 26, so that the left end of the rectangular insert 242 is inserted into the slot 27, forming a preliminary fixation.

[0024] The locking assembly 25 includes a base shell 251, which is fixedly installed on the bottom of the frame plate 23. A transverse plate 253 is slidably connected inside the base shell 251 via two guide sliders 252. A locking rod 254 is fixedly installed on the side of the transverse plate 253 near the connecting block 243. One end of the locking rod 254 passes through a circular insertion hole on the outside of the connecting block 243. Several thrust springs 255 are also fixedly connected between the transverse plate 253 and the inner wall of the base shell 251. A protrusion 256 is fixedly connected to the bottom of the transverse plate 253, and the base shell 251 is positioned corresponding to the protrusion 256. A passageway adapted to it is provided, and one side of the protrusion 256 extends to the outside of the passageway. A hanging ring 257 is rotatably connected to the protrusion 256 located outside the bottom shell 251. A hanging rod 258 that works with the hanging ring 257 is also fixedly connected to the bottom of the bottom shell 251. When the hanging ring 257 is hung on the hanging rod 258, the thrust spring 255 will be in a contracted state, which can prevent the thrust spring 255 from pushing the transverse plate 253 and the locking rod 254 to move inward during the installation of the X-ray flaw detection component 24, thus blocking the installation of the connecting block 243.

[0025] A clamping frame 210 is slidably connected laterally to the right side of the mounting slot 26 and corresponding to the rectangular insert 242. A circular rotating plate 211 is rotatably connected inside the clamping frame 210. A screw 212 is fixedly connected to the center of the right side of the circular rotating plate 211. The right end of the screw 212 passes through the clamping frame 210 and the storage slot 28, extending to the outside of the frame plate 23 and is fixedly connected to a handle. The screw 212 is threadedly connected to the frame plate 23. A guide slide 213 is symmetrically installed on the right side of the clamping frame 210. One end of the guide slide 213 is slidably connected to a groove on the side wall of the storage slot 28. A clamping block 214 is installed on the inner side of the frame 210. The clamping block 214 extends into the rectangular insertion hole on the right side of the rectangular insert plate 242. After the left end of the rectangular insert plate 242 is inserted into the slot 27, the screw 212 can be rotated. Through the threaded connection with the frame plate 23, the circular rotating plate 211 can be rotated and moved to the left. Under the limit of the guide slide 213, the rotating circular rotating plate 211 can drive the clamping frame 210 to move to the left, so that the clamping block 214 is inserted into the right end of the rectangular insert plate 242, forming a lateral abutment and insertion fixation, further improving the installation stability.

[0026] This modular, detachable UAV-mounted X-ray flaw detection device features a reasonable structural design and is easy to use. It employs a snap-fit ​​method for installation, eliminating the need for tools during assembly and disassembly, thus improving ease of operation and reducing operation time. Furthermore, the multi-directional snap-fit ​​mechanism maximizes the stability of the X-ray flaw detection device installation, preventing slippage during UAV flight and ensuring optimal performance.

[0027] Working principle: When the X-ray flaw detector 241 needs to be removed, first pull the hanging ring 257 below the bottom shell 251, so that the protrusion 256 drives the transverse plate 253 to press the thrust spring 255 under the limit of the guide slider 252 until it approaches the hanging rod 258. Then rotate the hanging ring 257 to hang it on it, preventing the thrust spring 255 from pushing the transverse plate 253 back to its original position. At this time, the locking rod 254 has disengaged from the connecting block 243. Then rotate the screw 212 on the right side, through the connection with the frame plate 23. The threaded connection between the two can drive the circular rotating plate 211 to rotate and move to the right. Under the limit of the guide slide 213, the rotating circular rotating plate 211 can drive the clamping frame 210 to move to the right and rotate it into the storage slot 28. At this time, the clamping block 214 also disengages from the rectangular insert plate 242. After holding the X-ray flaw detector 241, pull it to the right to disengage the rectangular insert plate 242 from the slot 27, and it can be taken out from the mounting slot 26. Similarly, during installation, simply reverse the above steps.

[0028] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art 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 appended claims and their equivalents.

Claims

1. A modularized unmanned aerial vehicle (UAV) mounted X-ray flaw detection device, comprising a UAV body (1) and a mounted X-ray flaw detection mechanism (2), characterized in that: The X-ray flaw detection mechanism (2) is fixedly installed on the bottom of the UAV body (1) by bolts; The mounted X-ray flaw detection mechanism (2) includes a connecting plate (21), a support rod (22), a frame plate (23), an X-ray flaw detection component (24), and a locking component (25). There are multiple support rods (22) symmetrically installed at the bottom of the connecting plate (21). The frame plate (23) is fixedly connected to one end of several support rods (22). The top of the frame plate (23) is provided with a mounting groove (26). The X-ray flaw detection component (24) is set in the mounting groove (26). There are two locking components (25) symmetrically installed at the bottom of the frame plate (23).

2. The modular and dismountable unmanned aerial vehicle mounted X-ray inspection device according to claim 1, characterized in that: The X-ray flaw detection assembly (24) includes an X-ray flaw detection machine (241), and a rectangular insert plate (242) is fixedly connected to the bottom of the X-ray flaw detection machine (241). A connecting block (243) is fixedly installed on the bottom of the rectangular insert plate (242).

3. The modular, detachable, UAV-mounted X-ray flaw detection device according to claim 2, characterized in that: The frame plate (23) has a slot (27) and a storage slot (28) connected to each other on the left and right sides of the inner wall of the mounting groove (26). The bottom of the frame plate (23) has a through hole (29) that communicates with the mounting groove (26). The left end of the rectangular insert plate (242) extends into the slot (27), and the bottom of the connecting block (243) extends through to the outside of the through hole (29).

4. The modular and dismountable X-ray inspection device for UAVs according to claim 3, characterized in that: The locking assembly (25) includes a bottom shell (251), which is fixedly installed on the bottom of the frame plate (23). A transverse plate (253) is slidably connected inside the bottom shell (251) via two guide sliders (252). A locking rod (254) is fixedly installed on the side of the transverse plate (253) near the connecting block (243). One end of the locking rod (254) passes through a circular insertion hole on the outside of the connecting block (243). The transverse plate (253) is connected to the inner wall of the bottom shell (251). Several thrust springs (255) are fixedly connected between them. A protrusion (256) is fixedly connected to the bottom of the transverse plate (253). The bottom shell (251) has a passage opening that matches the position of the protrusion (256). One side of the protrusion (256) extends to the outside of the passage opening. A hanging ring (257) is rotatably connected to the protrusion (256) located outside the bottom shell (251). A hanging rod (258) that works with the hanging ring (257) is also fixedly connected to the bottom of the bottom shell (251).

5. The modular and dismountable X-ray inspection device for UAVs according to claim 4, characterized in that: A clamping frame (210) is slidably connected laterally to the right side of the mounting slot (26) and corresponding to the rectangular insert plate (242). A circular rotating plate (211) is rotatably connected inside the clamping frame (210). A screw (212) is fixedly connected at the center of the right side of the circular rotating plate (211). The right end of the screw (212) passes through the clamping frame (210) and the storage slot (28) in sequence and extends to the outside of the frame plate (23) and is fixedly connected to a rotating handle. The screw (212) is threadedly connected to the frame plate (23). A guide slide (213) is symmetrically installed on the right side of the clamping frame (210). One end of the guide slide (213) is slidably connected to the slide groove on the side wall of the storage slot (28). A clamping block (214) is installed on the inner side of the clamping frame (210). The clamping block (214) extends into the rectangular insertion hole on the right side of the rectangular insert plate (242).

6. The modular and demodular unmanned aerial vehicle mounted X-ray inspection device according to claim 5, characterized in that: The transverse cross-sectional length of the through hole (29) is greater than that of the transverse cross-sectional length of the connecting block (243).

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