A multi-rotor unmanned aerial vehicle assembling and training platform

By designing clamping and upward rotating components, the problems of component shaking and displacement in the multi-rotor UAV assembly and adjustment training platform were solved, thereby improving the stability of UAV assembly and operational efficiency.

CN224674839UActive Publication Date: 2026-08-25HANGZHOU QICAI TECH CO LTD
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Patent Information

Application Number
CN202521542997.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-07-23
Publication Date
2026-08-25
Estimated Expiration
2035-07-23

AI Technical Summary

Technical Problem

Existing multi-rotor UAV assembly and adjustment training platforms suffer from component shaking or displacement during assembly, which makes operation inconvenient, increases the risk of damage, and affects assembly efficiency and safety.

Method used

A multi-rotor UAV assembly and adjustment training platform was designed, which includes a clamping component and an upward rotation component. The control panel drives the motor and electric push rod to achieve stable clamping and rotation of the UAV, preventing the components from shaking.

Benefits of technology

To ensure that the drone remains stable during assembly, reduce the risk of component damage, improve operational comfort and efficiency, and reduce operator fatigue.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model belongs to the technical field of unmanned plane, concretely relates to a kind of multi-rotor unmanned plane installation and adjustment practical training platform, including practical training platform ontology, the top of practical training platform ontology is fixedly installed with control panel, one side of the top of practical training platform ontology is fixedly installed sliding seat, clamping assembly and upper shift rotating assembly are provided on the sliding seat, the clamping assembly includes the slide rail of installation in the top of practical training platform one side, the one side of slide rail is opened with strip slot, two-way screw rod is rotatably connected in the both ends of strip slot inner wall, motor is fixedly installed in the one side of slide rail, and the output of motor is fixedly connected on two-way screw rod, the surface both ends of two-way screw rod are slidably connected with clamping plate.The utility model can effectively clamp unmanned plane, ensure that unmanned plane is stable and unmoved in assembly process, avoid the shaking or displacement problem of spare part, and it is convenient for operator to be in the most comfortable assembly posture, reduce operation fatigue.
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Description

Technical Field

[0001] This utility model belongs to the field of unmanned aerial vehicle (UAV) technology, specifically relating to a multi-rotor UAV assembly and adjustment training platform. Background Technology

[0002] The multi-rotor UAV assembly and adjustment training platform is a comprehensive teaching and training device that integrates core components, assembly and adjustment tools, and auxiliary equipment of multi-rotor UAVs. It is mainly used for teaching and skills training in UAV-related majors, helping students master practical skills such as mechanical structure assembly and electronic system debugging of multi-rotor UAVs. It can also be combined with simulation software for virtual debugging training before flight, thereby improving students' understanding of the overall structure and working principle of multi-rotor UAVs.

[0003] Currently, commercially available multi-rotor drone assembly and adjustment training platforms require the precise assembly of various components such as the frame, motors, and arms during drone assembly operations. This involves numerous meticulous operations, including tightening screws, connecting wires, and calibration. Because these components are delicate and fragile, they are prone to shaking or displacement if handled carelessly. Currently, assembly is usually done by hand, which is not only inconvenient but also increases the risk of component damage. Especially when tightening screws and connecting wires, improper force control or unstable operation can easily cause components to slip off. Once slipped, it may not only damage the components but also cause accidental bumps or injuries to the operator, directly affecting the drone assembly efficiency, prolonging the assembly time, and impacting the safety and smooth progress of the entire assembly process. Utility Model Content

[0004] The purpose of this invention is to provide a multi-rotor UAV assembly and adjustment training platform that can effectively hold the UAV, ensuring that the UAV remains stable during assembly, avoiding the shaking or displacement of parts, allowing operators to be in the most comfortable assembly posture, and reducing operator fatigue.

[0005] The specific technical solution adopted by this utility model is as follows:

[0006] A multi-rotor UAV assembly and adjustment training platform includes a training platform body, a control panel fixedly installed on the top of the training platform body, and a sliding seat fixedly installed on one side of the top of the training platform body. The sliding seat is provided with a clamping component and an upward rotation component.

[0007] Preferably, the clamping assembly includes a slide rail installed on one side of the top of the training platform body. A strip groove is provided on one side of the slide rail. Two bidirectional lead screws are rotatably connected to the two ends of the inner wall of the strip groove. A motor is fixedly installed on one side of the slide rail, and the output end of the motor is fixedly connected to the bidirectional lead screw. Clamping plates are slidably connected to both ends of the surface of the bidirectional lead screw.

[0008] Preferably, a sponge strip is fixedly installed on one side of the two clamping plates opposite to each other, and the surface of the sponge strip is provided with anti-slip texture.

[0009] Preferably, the upward rotating assembly includes a groove formed on one side of the sliding seat, a slider slidably connected in the groove, an electric push rod fixedly installed on one side of the bottom of the training platform body, and the piston rod of the electric push rod fixedly connected to the bottom of the slider, a connecting block fixedly installed on one side of the slider, a V-shaped plate rotatably connected to the end of the connecting block near the slide rail, a round rod fixedly installed on the side of the V-shaped plate near the slide rail, one end of the round rod fixedly connected to the slide rail, two fixed rods fixedly connected to the side of the V-shaped plate near the round rod, a sliding seat fixedly connected to the top of the training platform body and the bottom near the fixed rod, a limit rod slidably connected to the top of the sliding seat, a triangular limit block fixedly installed at the bottom of the inner cavity of the limit rod, and a tension limit assembly provided at the end of the connecting block away from the V-shaped plate.

[0010] Preferably, the tension limiting assembly includes a strip rod rotatably connected to one side of the connecting block, one end of the strip rod being fixedly connected to a V-shaped plate, a support rod being fixedly connected to the side of the connecting block near the bottom of the strip rod, a spring being mounted on the surface of the end of the strip rod away from the connecting block and the other end of the spring being mounted on the support rod, and two round blocks being fixedly mounted on the side of the connecting block near the strip rod.

[0011] Preferably, a pull-out groove is fixedly connected to one side of the bottom of the training platform body, and a drawer box is slidably connected in the pull-out groove.

[0012] The technical effects achieved by this utility model are as follows:

[0013] This utility model discloses a multi-rotor drone assembly and adjustment training platform. By setting up a clamping assembly and an upward rotation assembly, a control panel drives a motor to rotate a bidirectional lead screw, thereby displacing the relative position between two clamping plates to securely hold the multi-rotor drone and facilitate assembly. The control panel drives an electric push rod, pushing a slider upwards within a groove on a sliding seat. This, in turn, moves the connecting block, V-shaped plate, and round rod upwards together. When the V-shaped plate reaches the top of the limiting rod, it is blocked and rotates, causing the slide rail on one side of the round rod to flip, facilitating the flipping of the multi-rotor drone clamped on that side. Next, the control panel drives the electric push rod in the opposite direction, moving the connecting block, V-shaped plate, and round rod downwards together. At this point, the V-shaped plate is fixed by a triangular limiting block at the bottom of the limiting rod's inner cavity, facilitating the flipping assembly or disassembly of the drone. This device effectively clamps the drone, ensuring its stability during assembly and preventing component shaking or displacement. It also allows operators to maintain a comfortable assembly posture, reducing operator fatigue. Attached Figure Description

[0014] Figure 1 This is a schematic diagram of the main structure of this utility model;

[0015] Figure 2 This is a three-dimensional structural view of the clamping assembly of this utility model;

[0016] Figure 3 This is a utility model Figure 2 Enlarged view of the structure at point A in the middle;

[0017] Figure 4 This is a cross-sectional view of the upward rotating component of this utility model.

[0018] The attached diagram lists the components represented by each number as follows:

[0019] 1. Training platform body; 2. Sliding seat; 3. Slide rail; 4. Strip groove; 5. Two-way lead screw; 6. Motor; 7. Clamping plate; 8. Sponge strip; 9. Slide groove; 10. Slider; 11. Electric push rod; 12. Connecting block; 13. V-shaped plate; 14. Round rod; 15. Fixed rod; 16. Sliding seat; 17. Limiting rod; 18. Strip rod; 19. Support rod; 20. Spring; 21. Round block; 22. Pull-out groove. Detailed Implementation

[0020] To make the objectives and advantages of this utility model clearer, the following detailed description is provided in conjunction with embodiments. It should be understood that the following text is merely used to describe one or more specific embodiments of this utility model and does not strictly limit the scope of protection specifically claimed by this utility model.

[0021] like Figure 1 - Figure 4 As shown, a multi-rotor UAV assembly and adjustment training platform includes a training platform body 1, a control panel is fixedly installed on the top of the training platform body 1, and a sliding seat 2 is fixedly installed on one side of the top of the training platform body 1. The sliding seat 2 is provided with a clamping component and an upward rotation component.

[0022] The control panel controls the operation of the entire device. The training platform body 1 supports the multi-rotor drone, facilitating the assembly and disassembly of the drone by staff. The sliding seat 2 clamps the multi-rotor drone for easy assembly and adjustment. The clamping components are adjustable according to the shape and size of different parts of the multi-rotor drone, ensuring stable clamping and convenient operation. The upward rotation component moves the clamped multi-rotor drone parts upward and flips them over, making it easier for staff to assemble or disassemble the bottom, thus improving the assembly and adjustment efficiency and accuracy of the multi-rotor drone.

[0023] like Figure 2 and Figure 3 As shown, the clamping assembly includes a slide rail 3 installed on one side of the top of the training platform body 1. A strip groove 4 is provided on one side of the slide rail 3. Two bidirectional lead screws 5 are rotatably connected to the two ends of the inner wall of the strip groove 4. A motor 6 is fixedly installed on one side of the slide rail 3, and the output end of the motor 6 is fixedly connected to the bidirectional lead screw 5. Clamping plates 7 are slidably connected to both ends of the surface of the bidirectional lead screw 5.

[0024] Specifically, the control panel drives the motor 6, causing the bidirectional lead screw 5 to rotate, which in turn causes relative displacement between the two clamping plates 7, so as to securely clamp the multi-rotor drone, provide structural support for the multi-rotor drone, and facilitate the assembly of the multi-rotor drone by the staff.

[0025] like Figure 3 As shown, a sponge strip 8 is fixedly installed on one side of the two clamping plates 7 facing each other, and the surface of the sponge strip 8 is provided with anti-slip texture.

[0026] The design of the sponge strip 8 is intended to prevent the clamping plate 7 from directly contacting the multi-rotor drone, reducing possible scratches or damage during clamping. The anti-slip texture increases the friction between the sponge strip 8 and the multi-rotor drone, ensuring a more stable clamping and preventing slippage, thereby further improving the safety and efficiency of assembly and disassembly operations.

[0027] like Figure 3 and Figure 4 As shown, the upward rotating assembly includes a groove 9 opened on one side of the sliding seat 2, a slider 10 slidably connected in the groove 9, an electric push rod 11 fixedly installed on one side of the bottom of the training platform body 1, and the piston rod of the electric push rod 11 fixedly connected to the bottom of the slider 10, a connecting block 12 fixedly installed on one side of the slider 10, a V-shaped plate 13 rotatably connected to one end of the connecting block 12 near the slide rail 3, a round rod 14 fixedly installed on one side of the V-shaped plate 13 near the slide rail 3, and one end of the round rod 14 fixedly connected to the slide rail 3, two fixed rods 15 fixedly connected to one side of the V-shaped plate 13 near the round rod 14, a sliding seat 16 fixedly connected to the top of the training platform body 1 and the bottom near the fixed rod 15, a limit rod 17 slidably connected to the top of the sliding seat 16, a triangular limit block fixedly installed at the bottom of the inner cavity of the limit rod 17, and a tension limit assembly provided at the end of the connecting block 12 away from the V-shaped plate 13.

[0028] Specifically, the electric push rod 11 is driven by the control panel to push the slider 10 to slide upward in the groove 9 on the sliding seat 2, thereby pushing the connecting block 12 to move the V-shaped plate 13 and the round rod 14 upward. When the V-shaped plate 13 moves to the top of the limiting rod 17, the V-shaped plate 13 is blocked by the top of the limiting rod 17. At this time, the V-shaped plate 13 rotates, thereby causing the slide rail 3 on one side of the round rod 14 to flip, so as to flip the multi-rotor drone clamped on one side of the slide rail 3. Then, the electric push rod 11 is driven by the control panel to move in the opposite direction, thereby driving the connecting block 12, the V-shaped plate 13 and the round rod 14 to move downward. At this time, the V-shaped plate 13 is fixed by the triangular limiting block at the bottom of the inner cavity of the limiting rod 17, which facilitates the clamping, assembly or disassembly of the drone.

[0029] like Figure 1 and Figure 2 As shown, the tension limiting assembly includes a strip rod 18 rotatably connected to one side of the connecting block 12. One end of the strip rod 18 is fixedly connected to the V-shaped plate 13. A support rod 19 is fixedly connected to the side of the connecting block 12 near the bottom of the strip rod 18. A spring 20 is installed on the surface of the end of the strip rod 18 away from the connecting block 12, and the other end of the spring 20 is installed on the support rod 19. Two round blocks 21 are fixedly installed on the side of the connecting block 12 near the strip rod 18.

[0030] The strip rod 18 is fixedly connected to one end of the V-shaped plate 13, thereby enabling the V-shaped plate 13 to rotate synchronously and drive the strip rod 18 to rotate. The spring 20 can generate a certain tension between the strip rod 18 and the support rod 19. The elastic material used has a certain buffering effect, ensuring stability when the V-shaped plate 13 drives the slide rail 3 to flip. The round block 21 is used to limit and support the rotation angle of the strip rod 18, and also to limit and support the rotation angle of the slide rail 3.

[0031] like Figure 1 As shown, a pull-out groove 22 is fixedly connected to one side of the bottom of the training platform body 1, and a drawer box is slidably connected inside the pull-out groove 22.

[0032] Specifically, the pull-out slot 22 and the drawer box are designed to store parts disassembled from the multi-rotor drone, preventing parts from being lost, and also making it easier for staff to quickly retrieve the required parts, thus improving work efficiency.

[0033] The working principle of this utility model is as follows: First, the control panel drives the motor 6 to rotate the bidirectional lead screw 5, realizing the relative displacement between the two clamping plates 7, thus completing the stable clamping of the multi-rotor drone. Then, the electric push rod 11 is driven to push the slider 10 to slide in the slide groove 9, which drives the connecting block 12, the round rod 14 and the slide rail 3 to move upward until the V-shaped plate 13 reaches the top of the limiting rod 17. The top of the limiting rod 17 blocks the rotation, thus turning the drone over. Finally, the electric push rod 11 is driven in the opposite direction to move the connecting block 12, the V-shaped plate 13 and the round rod 14 downward. The V-shaped plate 13 is fixed by the triangular limiting block at the bottom of the inner cavity of the limiting rod 17 and by the tension of the spring 20, preventing the V-shaped plate 13 from rotating, thereby completing the clamping and turning of the drone.

[0034] The above description is merely a preferred embodiment of this utility model. It should be noted that those skilled in the art can make various improvements and modifications without departing from the principle of this utility model, and these improvements and modifications should also be considered within the scope of protection of this utility model. Structures, devices, and operating methods not specifically described or explained in this utility model, unless otherwise specified or limited, shall be implemented using conventional methods in the field.

Claims

1. A multi-rotor unmanned aerial vehicle (UAV) assembly and adjustment training platform, characterized in that: The training platform includes a training platform body (1), a control panel is fixedly installed on the top of the training platform body (1), and a sliding seat (2) is fixedly installed on one side of the top of the training platform body (1). The sliding seat (2) is provided with a clamping component and an upward rotation component. The clamping assembly includes a slide rail (3) installed on one side of the top of the training platform body (1). A strip groove (4) is provided on one side of the slide rail (3). Two bidirectional lead screws (5) are rotatably connected to the two ends of the inner wall of the strip groove (4). A motor (6) is fixedly installed on one side of the slide rail (3) and the output end of the motor (6) is fixedly connected to the bidirectional lead screw (5). Clamping plates (7) are slidably connected to both ends of the surface of the bidirectional lead screw (5). The upward rotating assembly includes a groove (9) on one side of the sliding seat (2), a slider (10) is slidably connected in the groove (9), an electric push rod (11) is fixedly installed on one side of the bottom of the training platform body (1), and the piston rod of the electric push rod (11) is fixedly connected to the bottom of the slider (10). A connecting block (12) is fixedly installed on one side of the slider (10), and a V-shaped plate (13) is rotatably connected to one end of the connecting block (12) near the slide rail (3). The V-shaped plate (13) is fixedly installed on one side of the slide rail (3). A round rod (14) is mounted on the slide rail (3), and one end of the round rod (14) is fixedly connected to the slide rail (3). Two fixed rods (15) are fixedly connected to the side of the V-shaped plate (13) near the round rod (14). A slide seat (16) is fixedly connected to the top of the training platform body (1) and the bottom near the fixed rod (15). A limit rod (17) is slidably connected to the top of the slide seat (16). A triangular limit block is fixedly installed at the bottom of the inner cavity of the limit rod (17). A tension limit component is provided at the end of the connecting block (12) away from the V-shaped plate (13).

2. The multi-rotor UAV assembly and adjustment training platform according to claim 1, characterized in that: A sponge strip (8) is fixedly installed on one side of the two clamping plates (7), and the surface of the sponge strip (8) is provided with anti-slip texture.

3. The multi-rotor UAV assembly and adjustment training platform according to claim 1, characterized in that: The tension limiting assembly includes a strip rod (18) rotatably connected to one side of the connecting block (12). One end of the strip rod (18) is fixedly connected to the V-shaped plate (13). A support rod (19) is fixedly connected to the side of the connecting block (12) near the bottom of the strip rod (18). A spring (20) is installed on the surface of the end of the strip rod (18) away from the connecting block (12), and the other end of the spring (20) is installed on the support rod (19). Two round blocks (21) are fixedly installed on the side of the connecting block (12) near the strip rod (18).

4. The multi-rotor UAV assembly and adjustment training platform according to claim 1, characterized in that: A pull-out groove (22) is fixedly connected to one side of the bottom of the training platform body (1), and a drawer box is slidably connected inside the pull-out groove (22).