Quick-release multifunctional unmanned aerial vehicle load mounting device

Abstract

The utility model discloses a quick detachable multifunctional unmanned plane load mounting device, including the flat plate, set up the clamping mechanism on the flat plate, set up the adjusting mechanism below the flat plate and set up the thing mechanism below the adjusting mechanism. The application provides a quick detachable multifunctional unmanned plane load mounting device, can cooperate with unmanned plane through the mode of clamping, greatly improves the product's dismounting / assembling efficiency, and simultaneously the product can also cooperate with different loads through the storage rack, can better improve the application range of product, still can reduce the vibration of storage rack through the setting of spring, further improves the use effect of product.

Description

Technical Field

[0001] This application relates to the field of drone accessories, specifically to a quick-release multi-functional drone payload mounting device. Background Technology

[0002] In recent years, drone technology has been widely used in many fields such as surveying and mapping, agricultural plant protection, power line inspection, security monitoring, and emergency rescue due to its advantages of high mobility, low cost, and flexible deployment. As application scenarios continue to expand and deepen, drones need to carry different types of payload equipment, such as high-definition cameras, multispectral sensors, pesticide spraying devices, and material delivery boxes, so that they can complete diverse tasks.

[0003] Traditional drone payload mounts typically employ a single, fixed method, resulting in a simple structure, limited functionality, and cumbersome disassembly and installation processes. In practical use, changing to different types of payloads often requires complex disassembly and reinstallation operations using tools, consuming significant time and labor costs, severely impacting operational efficiency and cost. For example, during power line inspections, drones need to carry high-definition cameras, while in agricultural plant protection operations, these cameras need to be replaced with pesticide spraying devices. Traditional mounts struggle to quickly switch between these payloads, leading to low efficiency when transitioning between different tasks.

[0004] Furthermore, different loads vary significantly in size, weight, and interface requirements, and traditional mounting devices lack versatility and adaptability, failing to meet the installation needs of diverse loads. Simultaneously, during UAV flight, the shock absorption and protection performance of traditional mounting devices is relatively poor, making it difficult to effectively reduce the impact of vibration, collisions, and environmental factors on the load equipment. This can easily lead to damage to the load equipment, thereby affecting mission performance and equipment lifespan. Utility Model Content

[0005] To address the shortcomings of existing technologies, this application provides a quick-release multi-functional drone load mount device that can quickly engage with drones via clamping, greatly improving the efficiency of product assembly / disassembly. Furthermore, the device can be used with different loads via a shelf, broadening its applicability. The spring mechanism also reduces shelf vibration, further enhancing the product's performance.

[0006] A quick-release multi-functional drone payload mounting device includes a flat plate, a clamping mechanism disposed on the flat plate, an adjustment mechanism disposed below the flat plate, and a storage mechanism disposed below the adjustment mechanism.

[0007] Furthermore, the clamping mechanism consists of two sets of clamping structures mirror-arranged on the left and right sides of the plate, and a limiting mechanism arranged on the clamping structures.

[0008] Preferably, the clamping structure consists of clamping plates disposed opposite to each other on the front and rear sides of the flat plate, an anti-slip component disposed between the two clamping plates and located on the lower side of the top of the clamping plates, two rocker plates disposed obliquely and symmetrically at the lower ends of the two clamping plates, and a connecting plate disposed between the two rocker plates; the bottom end of the clamping plate is rotatably fixed to the end of the front or rear side of the flat plate.

[0009] Furthermore, the anti-slip component consists of a clamping plate with both ends fixed to the opposite surfaces of the two clamping plates, and an anti-slip pad disposed on the lower side of the clamping plate.

[0010] Furthermore, the limiting mechanism consists of two horizontally arranged fixed rods, positioning blocks at both ends of the fixed rods, an annular groove formed at the middle of the outer side of the positioning block with the fixed rods as the center, and tension springs respectively set in the annular grooves of the two corresponding positioning blocks at both ends.

[0011] Furthermore, the adjustment mechanism consists of an electric telescopic rod vertically positioned at the center of the lower side of the flat plate, and a mounting plate horizontally positioned at the lower end of the electric telescopic rod; the lower end of the electric telescopic rod is fixed at the center of the mounting plate.

[0012] Preferably, the side of the mounting plate is also provided with several hooks.

[0013] In addition, the storage mechanism consists of a storage rack horizontally positioned below the mounting plate, sliding support columns vertically positioned at the four corners of the upper side of the storage rack and extending upward through the mounting plate, a stop block positioned at the top of the sliding support column, and a spring fitted onto the sliding support column, with its upper end abutting against the stop block and its lower end abutting against the mounting plate.

[0014] Preferably, a hanging mechanism is provided at the center of the lower side of the shelf; the hanging mechanism consists of a connecting shaft fixed to the lower side of the shelf, a support column vertically arranged on the lower side of the connecting shaft and capable of rotating around the shaft axis, and at least one hook provided at the lower end of the support column.

[0015] Compared with the prior art, the embodiments of this application have the following beneficial effects:

[0016] This invention can be quickly integrated with drones via a clamping mechanism, greatly improving the efficiency of product assembly / disassembly. Furthermore, the product can be used with different loads via a shelf, expanding its applicability. The spring mechanism also reduces shelf vibration, further enhancing the product's usability.

[0017] Some of the additional features of this application will be described in the following description. These additional features will become apparent to those skilled in the art upon examination of the following description and the accompanying drawings, or upon understanding the production or operation of the embodiments. The features disclosed in this application can be implemented and achieved through the practice or use of various methods, means, and combinations thereof with respect to the specific embodiments described below. Attached Figure Description

[0018] The accompanying drawings, which are provided to further illustrate this application and constitute a part of this application, illustrate exemplary embodiments of this application and are used to explain this application, but do not constitute a limitation thereof. In the drawings, the same reference numerals denote the same components.

[0019] Figure 1 This is a three-dimensional representation of the present invention. Figure 1 ;

[0020] Figure 2 This utility model is a three-dimensional Figure 2 ;

[0021] Figure 3 yes Figure 1 A magnified view of a section at point A in the middle;

[0022] Figure 4 yes Figure 1 A magnified view of a section at point B in the middle;

[0023] Figure 5 yes Figure 2 A magnified view of a section at point C;

[0024] Figure 6 yes Figure 2 A magnified view of a section at point D.

[0025] Explanation of reference numerals in the attached figures:

[0026] 1. Flat panel;

[0027] 2. Clamping mechanism; 21. Clamping plate; 22. Pry bar; 23. Connecting plate;

[0028] 3. Anti-slip components; 31. Clamping plate; 32. Anti-slip mat;

[0029] 4. Limiting mechanism; 41. Fixing rod; 42. Positioning block; 43. Tension spring;

[0030] 5. Adjustment mechanism; 51. Electric telescopic rod; 52. Mounting plate; 53. Hook;

[0031] 6. Storage mechanism; 61. Sliding support; 62. Stop; 63. Spring; 64. Shelf;

[0032] 7. Mounting mechanism; 71. Connecting shaft; 72. Support column; 73. Hook. Detailed Implementation

[0033] To enable those skilled in the art to better understand the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present application, and not all embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative effort should fall within the scope of protection of the present application.

[0034] It should be noted that if the terms "first," "second," etc., are used in the specification, claims, and accompanying drawings of this application, they are used to distinguish similar objects and are not necessarily used to describe a specific order or sequence. It should be understood that such data can be interchanged where appropriate for the embodiments of this application described herein. Furthermore, the terms "comprising" and "having," and any variations thereof, are intended to cover non-exclusive inclusion; for example, a process, method, system, product, or apparatus that comprises a series of steps or units is not necessarily limited to those steps or units explicitly listed, but may include other steps or units not explicitly listed or inherent to such processes, methods, products, or apparatus.

[0035] In this application, when terms such as "upper," "lower," "left," "right," "front," "rear," "top," "bottom," "inner," "outer," "middle," "vertical," "horizontal," "lateral," and "longitudinal" are used, they indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. These terms are mainly for better describing this application and its embodiments, and are not intended to limit the indicated device, element, or component to having a specific orientation, or to be constructed and operated in a specific orientation.

[0036] Furthermore, in addition to indicating location or positional relationship, some of the aforementioned terms may also have other meanings. For example, the term "above" may also be used in some cases to indicate a certain dependency or connection relationship. Those skilled in the art can understand the specific meaning of these terms in this application based on the specific circumstances.

[0037] Furthermore, in this application, the terms "installation," "setup," "equipped with," "connection," "linking," and "socketing," etc., should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral structure; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium, or an internal connection between two devices, components, or parts. Those skilled in the art can understand the specific meaning of the above terms in this application according to the specific circumstances.

[0038] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. This application will now be described in detail with reference to the accompanying drawings and embodiments.

[0039] Example 1

[0040] like Figure 1 , 2 As shown, a quick-release multi-functional drone payload mounting device includes a flat plate 1, a clamping mechanism 2 disposed on the flat plate 1, an adjustment mechanism 5 disposed below the flat plate 1, and a placement mechanism 6 disposed below the adjustment mechanism 5.

[0041] The clamping mechanism 2 consists of two sets of clamping structures mirror-arranged on the left and right sides of the plate 1, and a limiting mechanism 4 arranged on the clamping structures.

[0042] The clamping structure consists of clamping plates 21 disposed opposite to each other on the front and rear sides of the plate 1, an anti-slip component 3 disposed between the two clamping plates 21 and located on the lower side of the top of the clamping plates 21, two rocker plates 22 respectively disposed obliquely and symmetrically at the lower ends of the two clamping plates 21, and a connecting plate 23 disposed between the two rocker plates 22; the bottom end of the clamping plate 21 is rotatably fixed to the end of the front or rear side of the plate 1.

[0043] The clamping mechanism can hold the drone on both sides like a clamp. Its structure is simple and easy to use, and it does not require fastening with threads, which greatly improves the loading and unloading efficiency of the product.

[0044] like Figure 5 As shown, the anti-slip component 3 consists of a clamping plate 31 with both ends fixed to the opposite surfaces of the two clamping plates 21, and an anti-slip pad 32 disposed on the lower side of the clamping plate 31.

[0045] The anti-slip component effectively abuts against the upper side of the drone when clamped by the clamping mechanism. The anti-slip pad effectively increases static friction, thus ensuring that the product is not prone to slipping during use and further improving the product's stability.

[0046] like Figure 4As shown, the limiting mechanism 4 consists of two horizontally arranged fixed rods 41, positioning blocks 42 arranged at both ends of the fixed rods 41, an annular groove formed at the middle position of the outer side of the positioning block 42 with the fixed rods 41 as the center, and tension springs 43 arranged at both ends in the annular grooves of the two corresponding positioning blocks 42.

[0047] The limiting mechanism can pull the clamping structures on both sides together with a tension spring. Without damaging the drone shell or other parts, the greater the spring force, the better the clamping effect of the clamping structure.

[0048] The adjustment mechanism 5 consists of an electric telescopic rod 51 vertically positioned at the center of the lower side of the flat plate 1, and a mounting plate 52 horizontally positioned at the lower end of the electric telescopic rod 51; the lower end of the electric telescopic rod 51 is fixed at the center of the mounting plate 52.

[0049] The electric telescopic pole is existing technology. It can be electrically connected to the drone and its length can be adjusted remotely. Therefore, it can ensure sufficient working space during use according to the actual load equipment requirements. The setting and use of this structure are existing technologies. Those skilled in the art can set it up and use it without creative labor, so it will not be described in detail here.

[0050] like Figure 3 As shown, the storage mechanism 6 consists of a storage rack 64 horizontally positioned below the mounting plate 52, sliding support columns 61 vertically positioned at the four corners of the upper side of the storage rack 64 and extending upward through the mounting plate 52, a stop block 62 positioned at the top of the sliding support column 61, and a spring 63 sleeved on the sliding support column 61, with its upper end abutting against the stop block 62 and its lower end abutting against the mounting plate 52.

[0051] After the storage mechanism bears a load, it can effectively reduce the impact of vibration on the load through springs, and has a good shock absorption effect.

[0052] Example 2

[0053] The difference between this embodiment and embodiment 1 is that the side of the mounting plate 52 is also provided with several hooks 53.

[0054] Hooks can be used to hang small items that need to be carried or transported, further enhancing the product's functionality.

[0055] Example 3

[0056] like Figure 6As shown, a hanging mechanism 7 is also provided at the center of the lower side of the shelf 64; the hanging mechanism 7 consists of a connecting shaft 71 fixed to the lower side of the shelf 64, a support column 72 vertically arranged on the lower side of the connecting shaft 71 and capable of rotating around the axis of the connecting shaft 71, and at least one hook 73 provided at the lower end of the support column 72.

[0057] The mounting mechanism can be used to mount heavy items, making it easier to carry and transport them. Because the force is applied at the center of the product, it can better ensure that the drone's center does not deviate, reducing the impact on the drone during use and improving the product's performance.

[0058] It should be noted that all features disclosed in this specification, or all steps in all methods or processes disclosed, may be combined in any way, except for mutually exclusive features and / or steps.

[0059] Furthermore, the specific embodiments described above are exemplary. Those skilled in the art can devise various solutions inspired by the disclosure of this utility model, and these solutions all fall within the scope of this utility model and its protection. Those skilled in the art should understand that this utility model specification and its drawings are illustrative and not intended to limit the scope of the claims. The scope of protection of this utility model is defined by the claims and their equivalents.

Claims

1. A quick-release multifunctional unmanned aerial vehicle load mounting device, characterized in that, It includes a flat plate (1), a clamping mechanism (2) disposed on the flat plate (1), an adjustment mechanism (5) disposed below the flat plate (1), and a storage mechanism (6) disposed below the adjustment mechanism (5).

2. The quick-release multi-functional unmanned aerial vehicle load carrying device of claim 1, wherein, The clamping mechanism (2) consists of two sets of clamping structures mirror-arranged on the left and right sides of the plate (1), and a limiting mechanism (4) arranged on the clamping structure.

3. The quick-release multi-functional unmanned aerial vehicle load carrying device of claim 2, wherein, The clamping structure consists of clamping plates (21) arranged opposite to each other on the front and rear sides of the plate (1), an anti-slip component (3) arranged between the two clamping plates (21) and located on the lower side of the top of the clamping plates (21), two rocker plates (22) respectively inclined and symmetrically arranged at the lower ends of the two clamping plates (21), and a connecting plate (23) arranged between the two rocker plates (22); the bottom end of the clamping plate (21) is rotatably fixed to the end of the front or rear side of the plate (1).

4. The quick-release multi-functional unmanned aerial vehicle load carrying device of claim 3, wherein, The anti-slip component (3) consists of a clamping plate (31) with its two ends fixed to the opposite surfaces of the two clamping plates (21), and an anti-slip pad (32) disposed on the lower side of the clamping plate (31).

5. The quick-release multi-functional unmanned aerial vehicle load carrying device of claim 4, wherein, The limiting mechanism (4) consists of two horizontally arranged fixed rods (41), positioning blocks (42) at both ends of the fixed rods (41), an annular groove with the fixed rods (41) as the center and located in the middle of the outer side of the positioning block (42), and tension springs (43) respectively set in the annular grooves of the two corresponding positioning blocks (42).

6. The quick-release multi-functional unmanned aerial vehicle load carrying device of claim 5, wherein, The adjustment mechanism (5) consists of an electric telescopic rod (51) vertically set at the center of the lower side of the flat plate (1) and a mounting plate (52) horizontally set at the lower end of the electric telescopic rod (51); the lower end of the electric telescopic rod (51) is fixed at the center of the mounting plate (52).

7. The quick-release multi-functional unmanned aerial vehicle load carrying device of claim 6, wherein, The mounting plate (52) is also provided with several hooks (53) on its side.

8. The quick-release multi-functional unmanned aerial vehicle load carrying device of claim 7, wherein, The storage mechanism (6) consists of a storage rack (64) horizontally positioned below the mounting plate (52), a sliding support column (61) vertically positioned at the four corners of the upper side of the storage rack (64) and extending upward through the mounting plate (52), a stop block (62) positioned at the top of the sliding support column (61), and a spring (63) fitted onto the sliding support column (61), with its upper end abutting against the stop block (62) and its lower end abutting against the mounting plate (52).

9. The quick-release multi-functional unmanned aerial vehicle load carrying device of claim 8, wherein, A hanging mechanism (7) is also provided at the center of the lower side of the shelf (64); the hanging mechanism (7) consists of a connecting shaft (71) fixed to the lower side of the shelf (64), a support column (72) vertically arranged on the lower side of the connecting shaft (71) and capable of rotating around the axis of the shaft (71), and at least one hook (73) provided at the lower end of the support column (72).

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