Quick-release mounting assembly of unmanned aerial vehicle

Abstract

The utility model discloses a mounting assembly of quick release type unmanned aerial vehicle relates to unmanned aerial vehicle technical field, including shell and connecting subassembly, the top of shell is equipped with the top plate, connecting subassembly is provided in the interior of shell, connecting subassembly includes spacing hole, spacing block, fixed plate, location hole, rubber mat, screw, swivel nut, connecting rod, slider and location post, the top of shell is equipped with the spacing hole, spacing block, fixed plate, location hole, rubber mat, screw, swivel nut, connecting rod, slider and location post, and the top of shell is equipped with the spacing hole, spacing block, fixed plate, location hole, rubber mat, screw, swivel nut, connecting rod, slider and location post. A limiting hole is formed in the bottom of the shell, a limiting block is slidably connected into the limiting hole, and a fixing plate is fixed to the bottom of the limiting block. According to the mounting assembly of the quick-release unmanned aerial vehicle, through the arrangement of the connecting assembly, before the mounting assembly is used, a fixing plate is fixed to a mounting object through a bolt, then during assembling, only a limiting block needs to be inserted into a limiting hole and a screw rod needs to be rotated, a threaded sleeve can move, and therefore a positioning column on a sliding block is driven by a connecting rod to be inserted into a positioning hole in the limiting block; therefore, the mounting and the unmanned aerial vehicle body can be quickly assembled and connected.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically to a quick-release UAV mounting component. Background Technology

[0002] Unmanned aerial vehicles, or "drones" for short, are unmanned aircraft controlled by radio remote control equipment and their own program control devices, or operated autonomously by an onboard computer, either completely or intermittently. Currently, drones need to be equipped with different payloads depending on their intended use.

[0003] Existing drones typically require multiple screws to secure them to their mounts. After use, the mounts need to be removed and stored separately from the drone, resulting in frequent disassembly and assembly. Furthermore, additional tools are needed to loosen multiple screws during disassembly and assembly, making each disassembly and assembly time-consuming and laborious.

[0004] Therefore, in view of this, we have studied and improved the existing structure and its shortcomings, and provided a quick-release drone mounting component. Utility Model Content

[0005] The purpose of this invention is to provide a quick-release mounting component for unmanned aerial vehicles (UAVs) to solve the problems mentioned in the background section.

[0006] To achieve the above objectives, this utility model provides the following technical solution: a quick-release drone mounting component, comprising a shell and a connecting component. A top plate is mounted on the top of the shell, and the connecting component is disposed inside the shell. The connecting component includes a limiting hole, a limiting block, a fixing plate, a positioning hole, a rubber pad, a screw, a screw sleeve, a connecting rod, a slider, and a positioning post. A limiting hole is formed at the bottom of the shell, and a limiting block is slidably connected inside the limiting hole. A fixing plate is fixed to the bottom of the limiting block, and a positioning hole is formed on one side of the limiting block. A rubber pad is fixed to the center of the top of the fixing plate. A screw is rotatably connected to the center of the interior of the shell, and a screw sleeve is threadedly connected to the outer side of the middle part of the screw. A connecting rod is rotatably connected to both sides of the screw sleeve, and a slider is rotatably connected to the end of the connecting rod. A positioning post is fixed to one side of the slider.

[0007] Furthermore, the slider is slidably connected to the housing, and there are two sliders.

[0008] Furthermore, the diameter of the positioning post is equal to the inner diameter of the positioning hole, and the positioning posts are symmetrically distributed about the center line of the slider.

[0009] Furthermore, an adjustment assembly is provided on the top of the top plate. The adjustment assembly includes a connecting hole and an adjustment plate. The top of the top plate has a connecting hole, and adjustment plates are symmetrically arranged at both ends of the top of the top plate.

[0010] Furthermore, the adjustment assembly also includes an adjustment groove, which is provided on the outer side of the adjustment plate, and the cross-section of the adjustment groove is T-shaped.

[0011] Furthermore, the length of the adjusting plate is the same as the width of the chassis, and the adjusting plate is fixedly connected to the top plate by bolts.

[0012] Furthermore, the adjustment assembly also includes a chassis and an adjustment hole, with the top of the adjustment plate connected to the chassis and the bottom of the chassis having an adjustment hole.

[0013] Furthermore, the adjustment holes are equidistant from the bottom of the chassis, and the chassis is fixedly connected to the adjustment plate by bolts.

[0014] This utility model provides a quick-release drone mounting component, which has the following advantages:

[0015] 1. This utility model, through the setting of the connecting components, first uses bolts to fix the fixing plate to the hanger before use. Then, during assembly, simply insert the limiting block into the limiting hole and rotate the screw to move the screw sleeve. This allows the positioning pin on the slider to be inserted into the positioning hole on the limiting block via the connecting rod, enabling quick assembly and connection between the hanger and the drone body. At the same time, rubber pads are used to tighten the shell and the fixing plate to prevent up-and-down swaying due to gaps. Similarly, during disassembly, simply rotate the screw in the opposite direction to quickly release the limitation of the limiting block, allowing the hanger to be disassembled. Thus, when there is a need for frequent disassembly and assembly, the hanger can be disassembled and assembled without the aid of other tools, which improves the convenience of use.

[0016] 2. By adjusting the components, this utility model allows for the selection of the number and position of the connecting components during installation through multiple adjustment holes when fixing the connecting components. At the same time, the T-shaped adjustment groove can limit the head of the bolt and facilitate changing the position of the bolt inside, thereby allowing the horizontal position of the top plate to be adjusted according to the requirements, further improving the adaptability of the mounting components. Attached Figure Description

[0017] Figure 1 This is a bottom view of the shell structure of a quick-release drone mounting component according to the present invention.

[0018] Figure 2 This is a schematic diagram of the adjustment component of the mounting assembly of a quick-release drone according to the present invention.

[0019] Figure 3 This is a schematic diagram of the connecting component of a quick-release drone mounting assembly according to the present invention.

[0020] In the diagram: 1. Housing; 2. Top plate; 3. Adjustment assembly; 301. Connecting hole; 302. Adjustment plate; 303. Adjustment groove; 304. Chassis; 305. Adjustment hole; 4. Connecting assembly; 401. Limiting hole; 402. Limiting block; 403. Fixing plate; 404. Positioning hole; 405. Rubber pad; 406. Screw; 407. Screw sleeve; 408. Connecting rod; 409. Slider; 410. Positioning post. Detailed Implementation

[0021] The embodiments of this utility model will be described in further detail below with reference to the accompanying drawings and examples. The following examples are for illustrative purposes only and should not be construed as limiting the scope of this utility model.

[0022] like Figure 1 and Figure 2 As shown, a quick-release drone mounting assembly includes a housing 1 and a connecting assembly 4. A top plate 2 is mounted on the top of the housing 1, and an adjustment assembly 3 is mounted on the top of the top plate 2. The adjustment assembly 3 includes a connecting hole 301 and an adjustment plate 302. The connecting hole 301 is provided on the top of the top plate 2, and the adjustment plates 302 are symmetrically arranged at both ends of the top of the top plate 2. The adjustment assembly 3 also includes an adjustment groove 303. The adjustment groove 303 is provided on the outer side of the adjustment plate 302, and the cross-section of the adjustment groove 303 is T-shaped. The length of the adjustment plate 302 is the same as the width of the chassis 304, and the adjustment plate 302 is connected to the chassis 304 by bolts. The top plate 2 is fixedly connected. By changing the position of the bolts inside the adjustment groove 303, the horizontal position of the top plate 2 can be adjusted according to the needs, further improving the adaptability range of the mounting components. The adjustment component 3 also includes a chassis 304 and adjustment holes 305. The top of the adjustment plate 302 is connected to the chassis 304, and the bottom of the chassis 304 is provided with adjustment holes 305. The adjustment holes 305 are evenly distributed about the bottom of the chassis 304, and the chassis 304 is fixedly connected to the adjustment plate 302 by bolts. The number and position of the connection components 4 can be selected according to the needs through multiple adjustment holes 305.

[0023] like Figure 2 and Figure 3As shown, the connecting component 4 is disposed inside the housing 1. The connecting component 4 includes a limiting hole 401, a limiting block 402, a fixing plate 403, a positioning hole 404, a rubber pad 405, a screw 406, a screw sleeve 407, a connecting rod 408, a slider 409, and a positioning post 410. The limiting hole 401 is provided at the bottom of the housing 1, and the limiting block 402 is slidably connected inside the limiting hole 401. The limiting hole 401 limits the horizontal position of the limiting block 402. The fixing plate 403 is fixed at the bottom of the limiting block 402, and the fixing plate 403 can be fixed to the hanging object by bolts. The positioning hole 404 is provided on one side of the limiting block 402. A rubber pad 405 is fixed at the top center of the fixing plate 403. The rubber pad 405 is used to tighten the housing 1 and the fixing plate 403 to prevent up-and-down shaking due to gaps. The screw 406 is rotatably connected to the center of the inside of the housing 1, and the screw 406... A threaded sleeve 407 is connected to the outer side of the middle section. A connecting rod 408 is rotatably connected to both sides of the threaded sleeve 407, and a slider 409 is rotatably connected to the end of the connecting rod 408. A positioning post 410 is fixed on one side of the slider 409. The slider 409 is slidably connected to the housing 1, and there are two sliders 409. The housing 1 can guide the movement of the slider 409. The diameter of the positioning post 410 is equal to the inner diameter of the positioning hole 404, and the positioning posts 410 are symmetrically distributed about the center line of the slider 409. By rotating the screw 406, the threaded sleeve 407 can be moved, thereby driving the positioning post 410 on the slider 409 to be inserted into the positioning hole 404 on the limiting block 402 through the connecting rod 408. This allows for quick assembly and connection between the mount and the drone body. Similarly, during disassembly, simply rotating the screw 406 in the opposite direction can quickly release the restriction of the limiting block 402, allowing for disassembly of the mount.

[0024] In summary, when using the mounting components of this quick-release drone, firstly according to... Figure 1 , Figure 2 and Figure 3The structure shown first uses bolts, nuts, and adjusting holes 305 to install the adjusting plate 302 at the bottom of the chassis 304. Then, using bolts, nuts, and connecting holes 301, the top plate 2 is installed at the bottom of the adjusting plate 302. At this point, the number and position of the connecting components 4 can be selected according to requirements through multiple adjusting holes 305. Simultaneously, by changing the position of the bolts inside the adjusting grooves 303, the horizontal position of the top plate 2 can be adjusted as needed. Next, the fixing plate 403 is fixed to the hanger using bolts. During assembly, simply insert the limiting block 402 into the limiting hole 401 and rotate the screw 406 to move the screw sleeve 407. This will cause the positioning pin 410 on the slider 409 to be inserted into the positioning hole 404 on the limiting block 402 via the connecting rod 408, allowing for quick assembly and connection between the mount and the drone body. Finally, when the drone has finished its operation and the mount needs to be disassembled for storage, simply rotate the screw 406 in the opposite direction to quickly release the restriction of the limiting block 402, allowing for the disassembly of the mount.

[0025] The embodiments of this utility model are given for illustrative and descriptive purposes only, and are not intended to be exhaustive or to limit the utility model to the forms disclosed. Many modifications and variations will be apparent to those skilled in the art. The embodiments were chosen and described in order to better illustrate the principles and practical applications of this utility model, and to enable those skilled in the art to understand this utility model and design various embodiments with various modifications suitable for a particular purpose.

Claims

1. A quick-release unmanned aerial vehicle mounting assembly comprising a housing (1) and a connecting assembly (4), characterized in that, The top of the shell (1) is provided with a top plate (2), the connecting assembly (4) is arranged in the shell (1), the connecting assembly (4) comprises a limiting hole (401), a limiting block (402), a fixed plate (403), a positioning hole (404), a rubber pad (405), a screw rod (406), a screw sleeve (407), a connecting rod (408), a sliding block (409) and a positioning column (410), the bottom of the shell (1) is provided with a limiting hole (401), and the limiting hole (401) is in sliding connection with a limiting block (402) in the inside, the bottom of the limiting block (402) is fixedly connected with a fixed plate (403), one side of the limiting block (402) is provided with a positioning hole (404), the top of the fixed plate (403) is fixedly connected with a rubber pad (405), the inside of the shell (1) is rotatably connected with a screw rod (406), and the outer side of the middle part of the screw rod (406) is threadedly connected with a screw sleeve (407), the two sides of the screw sleeve (407) are rotatably connected with a connecting rod (408), the end of the connecting rod (408) is rotatably connected with a sliding block (409), and one side of the sliding block (409) is fixedly connected with a positioning column (410).

2. The mounting assembly of claim 1, wherein, The sliding block (409) is in sliding connection with the shell (1), and the number of the sliding blocks (409) is two.

3. The quick-release unmanned aerial vehicle mounting assembly of claim 1, wherein, The diameter of the positioning column (410) is equal to the inner diameter of the positioning hole (404), and the positioning column (410) is symmetrically distributed about the center line of the sliding block (409).

4. The quick-release unmanned aerial vehicle mounting assembly of claim 1, wherein, The top of the top plate (2) is provided with an adjusting assembly (3), the adjusting assembly (3) comprises a connecting hole (301) and an adjusting plate (302), the top of the top plate (2) is provided with a connecting hole (301), and the top of the top plate (2) is provided with an adjusting plate (302) at two ends.

5. The quick-release unmanned aerial vehicle mounting assembly of claim 4, wherein, The adjusting assembly (3) further comprises an adjusting groove (303), the outer side of the adjusting plate (302) is provided with an adjusting groove (303), and the cross section of the adjusting groove (303) is T-shaped.

6. The quick-release unmanned aerial vehicle mounting assembly of claim 4, wherein, The length of the adjusting plate (302) is consistent with the width of the bottom disc (304), and the adjusting plate (302) is fixedly connected with the top plate (2) through bolts.

7. The quick-release unmanned aerial vehicle mounting assembly of claim 5, wherein, The adjusting assembly (3) further comprises a bottom disc (304) and an adjusting hole (305), the top of the adjusting plate (302) is connected with a bottom disc (304), and the bottom of the bottom disc (304) is provided with an adjusting hole (305).

8. The quick-release unmanned aerial vehicle mounting assembly of claim 7, wherein, The adjusting holes (305) are equidistantly distributed about the bottom of the bottom disc (304), and the bottom disc (304) is fixedly connected with the adjusting plate (302) through bolts.

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