Wing signal transfer adapter device

By using the magnetic adsorption and toothed meshing structure of the signal relay module, connecting plate, mounting block and fixing components, the problem of unstable installation of UAV remote control signal relay device is solved, realizing stable installation and convenient disassembly, extending service life and reducing cost.

CN223665082UActive Publication Date: 2025-12-12XIAN HONGFENG AEROSPACE ELECTRONIC TECHNOLOGY CO LTD
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Patent Information

Application Number
CN202422917521.5
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-11-28
Publication Date
2025-12-12
Estimated Expiration
2034-11-28

AI Technical Summary

Technical Problem

Existing drone remote control signal relay devices have poor installation stability, are prone to falling off and being damaged, affecting their service life and cost.

Method used

The design employs a signal relay module, connecting plate, mounting block, and fixing components, utilizing magnetic adsorption and toothed meshing structure to achieve stable installation and convenient disassembly.

Benefits of technology

This improves the installation stability of the signal relay module, reduces the risk of detachment, extends its service life, and lowers the cost of use.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model discloses a wing signal transfer adapting device, which relates to the technical field of signal transfer and comprises a signal relay module, a connecting plate is fixedly mounted at one end of the signal relay module, a mounting block is fixedly mounted at one end of the connecting plate, and a fixing component is movably mounted in the mounting block. The fixing assembly is composed of a toothed bar, two mounting shafts, a rotating plate, two toothed plates, an inserting block, a second magnet and a connecting plate, the two mounting shafts are fixedly mounted at the upper end and the lower end of the toothed bar respectively, the rotating plate is fixedly mounted at the lower end of the mounting shaft on the lower side, and the two toothed plates are symmetrically mounted on the two sides of the toothed bar; according to the signal relay module, the connecting plate, the mounting block, the fixing assembly and the auxiliary assembly are arranged and matched with one another, so that the signal relay module is convenient to disassemble and assemble, the mounting stability of the signal relay module is good, the signal relay module is not prone to falling off and being broken in the using process, and finally the service life of the signal relay module can be guaranteed; and the use cost of a user is reduced.
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Description

Technical Field

[0001] This utility model relates to the field of signal conversion technology, and in particular to a wing signal conversion adapter. Background Technology

[0002] A wing-mounted signal adapter is a device specifically designed for signal transfer on aircraft wings. It enables flexible signal transfer and adaptation to meet the communication needs of different devices. When the wing-mounted signal adapter receives signals from different devices, it uses a signal transfer module on its circuit board to transfer and adapt the signals. Specifically, the signal transfer module converts the signal type and format into a format recognizable by the target device and outputs it to the target device through the corresponding interface. This allows for smooth communication and data transmission between different devices. Wing-mounted signal adapters have broad application prospects in the aviation field. For example, on unmanned aerial vehicles (UAVs), it can enable communication and data transmission between the UAV and ground control stations, as well as collaborative work between the UAV and other devices. The existing patent application with application number CN202020212905.6 proposes a drone remote control signal relay device. It speeds up the assembly and disassembly of the drone remote control signal relay device by using a locking block to engage with the locking part of the drone. However, the locking block and the locking part are inserted together and fixed only by friction, which results in poor installation stability of the signal relay device. The signal relay device is easy to fall off and be damaged. Therefore, it needs to be improved. Utility Model Content

[0003] The main purpose of this invention is to provide a wing signal transfer adapter that can effectively solve the problems in the background art.

[0004] To achieve the above objectives, the technical solution adopted by this utility model is as follows:

[0005] A wing signal relay adapter includes a signal relay module. A connecting plate is fixedly mounted at one end of the signal relay module, and a mounting block is fixedly mounted at one end of the connecting plate. A fixing assembly is movably mounted within the mounting block. The fixing assembly consists of a rack, a mounting shaft, a rotating plate, a toothed plate, insert blocks, a second magnet, and the connecting plate. There are two mounting shafts, each fixedly mounted at the upper and lower ends of the rack. The rotating plate is fixedly mounted at the lower end of the lower mounting shaft. There are two toothed plates, symmetrically mounted on both sides of the rack, and the toothed plates simultaneously mesh with the rack. There are two insert blocks, each fixedly mounted at the outer end of one of the two toothed plates. There are two second magnets, each fixedly mounted at the outer end of one of the two insert blocks. The signal relay module is mounted on an auxiliary assembly via the connecting plate, mounting block, and fixing assembly. The auxiliary assembly consists of a C-shaped frame and two first magnets, symmetrically fixedly mounted within the C-shaped frame.

[0006] Preferably, the C-shaped frame on the auxiliary component is fixedly installed at one end of the drone, and two slots are symmetrically opened on the inner walls of the left and right sides of the C-shaped frame. The two first magnets are two in number and fixedly installed on the inner walls of the two slots respectively.

[0007] Preferably, the signal relay module is located at one end of the C-shaped frame, and the connecting plate and mounting block are inserted into the C-shaped frame.

[0008] Preferably, the mounting block has a receiving groove, two shaft holes are symmetrically opened at the upper and lower ends of the mounting block, and two through grooves are symmetrically opened at the left and right ends of the mounting block, and the shaft holes and through grooves are all connected to the receiving groove.

[0009] Preferably, the toothed rod on the fixing component is rotatably installed in the receiving groove, the mounting shaft is rotatably installed in the shaft hole, the rotating plate is located below the mounting block, the toothed plate is slidably installed in the receiving groove, and the insert block is movably inserted into the through groove.

[0010] Preferably, the insert on the fixing component is simultaneously inserted into the slot, and the second magnet is attracted to the first magnet.

[0011] Compared with the prior art, the present invention has the following beneficial effects:

[0012] By setting up connecting plates, mounting blocks, fixing components, and auxiliary components, and having them work together, the signal repeater module can be easily disassembled and assembled, while also ensuring good installation stability. This makes the signal repeater module less likely to fall off and be damaged during use, ultimately guaranteeing its service life and reducing user costs. Attached Figure Description

[0013] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0014] Figure 2 For the present utility model Figure 1 A magnified view of point A;

[0015] Figure 3 This is a cross-sectional view of the C-shaped frame of this utility model;

[0016] Figure 4 This is a structural schematic diagram of the signal relay module, mounting block, fixing component, and connecting plate of this utility model.

[0017] Figure 5 This is a cross-sectional structural diagram of the mounting block of this utility model;

[0018] Figure 6This is an exploded view of the fixing component of this utility model.

[0019] In the diagram: 1. Signal relay module; 2. Mounting block; 3. Fixing component; 4. Auxiliary component; 5. UAV; 6. Receiving slot; 7. Through slot; 8. Shaft hole; 9. C-shaped frame; 10. Slot; 11. First magnet; 12. Gear bar; 13. Mounting shaft; 14. Rotating plate; 15. Gear plate; 16. Insert block; 17. Second magnet; 18. Connecting plate. Detailed Implementation

[0020] To make the technical means, creative features, objectives and effects of this utility model easier to understand, the present utility model will be further described below in conjunction with specific embodiments.

[0021] Please see Figure 1 , Figure 2 , Figure 3 , Figure 4 , Figure 5 , Figure 6As shown, a wing signal relay adapter includes a signal relay module 1. A connecting plate 18 is fixedly mounted at one end of the signal relay module 1, and a mounting block 2 is fixedly mounted at the other end of the connecting plate 18. A fixing assembly 3 is movably mounted within the mounting block 2. The fixing assembly 3 consists of a rack 12, a mounting shaft 13, a rotating plate 14, a toothed plate 15, an insert block 16, a second magnet 17, and the connecting plate 18. There are two mounting shafts 13, fixedly mounted at the upper and lower ends of the rack 12 respectively. The rotating plate 14 is fixedly mounted at the lower end of the lower mounting shaft 13. There are two toothed plates 15, symmetrically mounted on both sides of the rack 12, and the toothed plates 15 simultaneously mesh with the rack 12. There are two insert blocks 16, fixedly mounted at the outer ends of the two toothed plates 15 respectively. There are two second magnets 17, fixedly mounted at the outer ends of the two insert blocks 16 respectively. The signal relay module 1 is mounted on an auxiliary assembly 4 via the connecting plate 18, the mounting block 2, and the fixing assembly 3. The auxiliary assembly 4 consists of a C-shaped frame 9 and a first magnet 11. The signal relay module 1 is installed in two symmetrically fixed positions within the C-shaped frame 9. When installing the signal relay module 1, the connecting plate 18 and the mounting block 2 can be inserted into the C-shaped frame 9 on the auxiliary component 4. After the connecting plate 18 and the mounting block 2 are fully inserted into the C-shaped frame 9, the insertion block 16 and the second magnet 17 will be inserted into the slot 10 under the magnetic force of the first magnet 11 and the second magnet 17. Finally, when the second magnet 17 and the first magnet 11 are attracted together, the installation of the signal relay module 1 is completed. When it is necessary to disassemble the signal relay module 1, the toothed rod 12 on the fixing component 3 can be rotated to drive the insertion block 16 and the second magnet 17 to retract into the mounting block 2 through the toothed plate 15. After the insertion block 16 and the second magnet 17 are fully retracted into the mounting block 2, the signal relay module 1, the connecting plate 18, and the mounting block 2 can be moved downwards, so that the connecting plate 18 and the mounting block 2 are finally removed from the C-shaped frame 9, and the disassembly of the signal relay module 1 is completed.

[0022] Ultimately, by setting up the connecting plate 18, mounting block 2, fixing component 3, and auxiliary component 4, and making them work together, the signal relay module 1 can be easily disassembled and assembled, while also ensuring good installation stability. This makes the signal relay module 1 less likely to fall off and be damaged during use, thus guaranteeing the service life of the signal relay module 1 and reducing the user's operating costs.

[0023] Furthermore, the C-shaped frame 9 on the auxiliary component 4 is fixedly installed at one end of the drone 5. Two slots 10 are symmetrically opened on the inner walls of the left and right sides of the C-shaped frame 9. Two first magnets 11 are respectively fixedly installed on the inner walls of the two slots 10. The signal relay module 1 is located at one end of the C-shaped frame 9. The connecting plate 18 and the mounting block 2 are inserted into the C-shaped frame 9. The mounting block 2 has a receiving groove 6. Two shaft holes 8 are symmetrically opened at the upper and lower ends of the mounting block 2. Two through grooves 7 are symmetrically opened at the left and right ends of the mounting block 2. The shaft holes 8 and the through grooves 7 are all connected to the receiving groove 6. The toothed rod 12 on the fixing component 3 is rotatably installed in the receiving groove 6. The mounting shaft 13 is rotatably installed in the shaft hole 8. The rotating plate 14 is located below the mounting block 2. The toothed plate 15 is slidably installed in the receiving groove 6. The insert block 16 is movably inserted into the through groove 7. The insert block 16 on the fixing component 3 is also inserted into the slot 10. The second magnet 17 and the first When the magnets 11 are attracted together, and the connecting plate 18 and the mounting block 2 are fully inserted into the C-shaped frame 9, the through slot 7 will align with the slot 10. At this time, under the magnetic force of the first magnet 11 and the second magnet 17, the second magnet 17, the insert block 16, and the toothed plate 15 will move outward. Finally, the insert block 16 and the second magnet 17 will be inserted into the slot 10, and the first magnet 11 and the second magnet 17 will attract together. When the second magnet 17, the insert block 16, and the toothed plate 15 move outward, the toothed bar 12 that meshes with the toothed plate 15 will rotate. At the same time, the mounting shaft 13 and the rotating plate 14 will also rotate. When it is necessary to completely retract the insert block 16 and the second magnet 17 into the mounting block 2, the mounting shaft 13 and the toothed bar 12 can be rotated through the rotating plate 14. The toothed bar 12 will drive the toothed plate 15 to move inward. Finally, under the drive of the toothed plate 15, the insert block 16 and the second magnet 17 will completely retract into the mounting block 2.

[0024] The above description is merely a preferred embodiment of this utility model and is not intended to limit the scope of this utility model. Although the utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of this utility model should be included within the protection scope of this utility model. The scope of protection of this utility model is defined by the appended claims and their equivalents.

Claims

1. A wing signal relay adapter, comprising a signal relay module (1), characterized in that: One end of the signal relay module (1) is fixedly mounted with a connecting plate (18), and one end of the connecting plate (18) is fixedly mounted with a mounting block (2). A fixing component (3) is movably mounted inside the mounting block (2). The fixing component (3) consists of a rack (12), a mounting shaft (13), a rotating plate (14), a toothed plate (15), a plug (16), a second magnet (17), and the connecting plate (18). There are two mounting shafts (13), which are fixedly mounted at the upper and lower ends of the rack (12), respectively. The rotating plate (14) is fixedly mounted at the lower end of the mounting shaft (13) on the lower side. The toothed plate (15) Two are symmetrically installed on both sides of the toothed bar (12), the toothed plate (15) meshes with the toothed bar (12) at the same time, there are two inserts (16) and they are respectively fixedly installed on the outer ends of the two toothed plates (15), there are two second magnets (17) and they are respectively fixedly installed on the outer ends of the two inserts (16), the signal relay module (1) is installed on the auxiliary component (4) through the connecting plate (18), the mounting block (2) and the fixing component (3), the auxiliary component (4) is composed of a C-shaped frame (9) and a first magnet (11), there are two first magnets (11) and they are symmetrically fixedly installed in the C-shaped frame (9).

2. The wing signal switching adapter according to claim 1, characterized in that: The C-shaped frame (9) on the auxiliary component (4) is fixedly installed at one end of the drone (5). Two slots (10) are symmetrically opened on the inner walls of the left and right sides of the C-shaped frame (9). The two first magnets (11) are two in number and are fixedly installed on the inner walls of the two slots (10) respectively.

3. The wing signal switching adapter according to claim 2, characterized in that: The signal relay module (1) is located at one end of the C-shaped frame (9), and the connecting plate (18) and the mounting block (2) are inserted into the C-shaped frame (9).

4. The wing signal switching adapter according to claim 3, characterized in that: The mounting block (2) has a receiving groove (6) inside. The mounting block (2) has two shaft holes (8) symmetrically opened at the upper and lower ends. The mounting block (2) has two through grooves (7) symmetrically opened at the left and right ends. The shaft holes (8) and through grooves (7) are connected to the receiving groove (6).

5. The wing signal switching adapter according to claim 4, characterized in that: The toothed rod (12) on the fixed component (3) is rotatably installed in the receiving groove (6), the mounting shaft (13) is rotatably installed in the shaft hole (8), the rotating plate (14) is located below the mounting block (2), the toothed plate (15) is slidably installed in the receiving groove (6), and the insert (16) is movably inserted into the through groove (7).

6. The wing signal switching adapter according to claim 5, characterized in that: The insert (16) on the fixing component (3) is simultaneously inserted into the slot (10), and the second magnet (17) is attracted together with the first magnet (11).

Citation Information

Patent Citations

  • Unmanned aerial vehicle remote control signal relay device

    CN210629495U