Unmanned aerial vehicle mounting mechanism capable of being quickly disassembled

Abstract

The utility model discloses an unmanned aerial vehicle mounting mechanism capable of being quickly disassembled, which comprises an upper quick-disassembly mounting component and a lower quick-disassembly mounting component, the upper quick-disassembly mounting component and the lower quick-disassembly mounting component are mutually rotated and buckled and are assembled and fixed by a loose screw, and after the upper quick-disassembly mounting component and the lower quick-disassembly mounting component are initially mounted in place, the quick-disassembly mounting component and the lower quick-disassembly mounting component are fixed by the loose screw. The quick-release mounting upper assembly and the quick-release mounting lower assembly rotate by an angle R in a certain direction, it is ensured that the quick-release mounting upper assembly and the quick-release mounting lower assembly are rotationally installed in place, and the quick-release mounting upper assembly and the quick-release mounting lower assembly are screwed and fixed together through a fixing nut on the quick-release mounting upper assembly and a captive screw on the quick-release mounting lower assembly.

Description

Technical Field

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

[0002] Unmanned aerial vehicles (UAVs) are unmanned aircraft controlled by radio remote control equipment and their own program control devices, or operated autonomously, either completely or intermittently, by an onboard computer. When used in dangerous or special locations, UAVs can transport goods via mounting mechanisms. Existing UAV mounting mechanisms on the market are relatively simple or single-function, often using straps or fixed brackets for mounting and positioning. These mechanisms cannot be quickly assembled or disassembled, significantly reducing the adaptability and efficiency of UAV use and limiting their carrying capabilities. Furthermore, the inability to quickly assemble and disassemble these mechanisms results in larger packaging volumes for UAVs, making them inconvenient to pack and transport, and increasing transportation costs. Summary of the Invention

[0003] In view of this, the purpose of this utility model is to provide a quick-release mounting mechanism for use on unmanned aerial vehicles (UAVs).

[0004] To achieve the above objectives, this utility model provides the following technical solution: a quick-release drone mounting mechanism, comprising a quick-release upper mounting component and a quick-release lower mounting component. The quick-release upper mounting component and the quick-release lower mounting component are rotatably engaged and assembled. After the quick-release upper mounting component and the quick-release lower mounting component are initially installed in place, the quick-release upper mounting component and the quick-release lower mounting component are rotated by an angle R in a certain direction to ensure that the quick-release upper mounting component and the quick-release lower mounting component are rotated and installed in place. They are then tightened together by a fixing nut on the quick-release upper mounting component and a non-detachable screw on the quick-release lower mounting component.

[0005] Preferably, the quick-release mounting upper component includes an upper component fixing plate, a boss hook, a fixing nut, and screws. The upper component fixing plate includes a first fixing plate hole straight surface, a fixing plate groove surface, a second fixing plate hole straight surface, a fixing plate upper surface, and a fixing plate lower surface. The first fixing plate hole straight surface and the second fixing plate hole straight surface are irregularly shaped surfaces to facilitate the anti-rotation of the fixing component and ensure its secure fixation.

[0006] Preferably, the boss hook includes an inner screw hole, a lower side surface, an inner side surface of a first boss hook, an inner side surface of a second boss hook, and a straight surface of the irregularly shaped boss hook. The straight surface of the irregularly shaped boss hook is irregularly shaped to facilitate anti-rotation and secure fixing of the fastener. The straight surface of the irregularly shaped boss hook and the lower side surface of the boss hook respectively contact the straight surfaces of the first fixing plate holes and the groove surfaces of the fixing plate distributed on the upper component fixing plate. The boss hook and the upper component fixing plate are fixed together by screws.

[0007] Preferably, the fixing nut includes an inner side surface, a straight surface of the fixing nut boss, and an internal threaded hole. The straight surface of the fixing nut boss is an irregularly shaped surface, which facilitates the anti-rotation and secure fixing of the fastener. The inner side surface and the straight surface of the fixing nut boss respectively correspond to and contact the upper surface of the fixing plate and the straight surface of the hole in the second fixing plate. The fixing nut and the upper component fixing plate are fixed together by screws.

[0008] Preferably, the quick-release mounting lower component includes a lower component fixing compartment and an anti-loosening screw. The lower component fixing compartment includes an upper surface of the fixing compartment, a lower surface of the fixing compartment, an inner side of a first annular hole, and an inner side of a second annular hole. The lower surface of the compartment and the anti-loosening screw are riveted or bonded together.

[0009] Preferably, the corresponding number of protruding hooks distributed on the upper quick-release mounting component are installed in directional alignment with the corresponding number of first annular holes distributed on the lower component fixing compartment of the lower quick-release mounting component. The lower surface of the upper component fixing plate on the upper quick-release mounting component contacts the upper surface of the fixing compartment on the lower quick-release mounting component. The inner surfaces of the first and second protruding hooks respectively contact the lower surface and upper surface of the lower component fixing compartment.

[0010] Compared with the prior art, the advantages of this utility model are: the quick-release mounting mechanism of this utility model is simple, easy and quick to operate, and has high safety; it has the advantages of small packaging volume, convenient handling and carrying, and correspondingly low transportation cost. Attached Figure Description

[0011] Figure 1 This is an exploded view of a quick-release mounting mechanism for an unmanned aerial vehicle (UAV) according to this utility model.

[0012] Figure 2 This is an initial assembly drawing of a quick-release mounting mechanism for an unmanned aerial vehicle (UAV) according to this utility model.

[0013] Figure 3 This utility model provides an assembly diagram of a quick-release mounting mechanism for use on a drone after rotation.

[0014] Figure 4This is an assembly drawing of the components of the quick-release mounting mechanism of this utility model;

[0015] Figure 5 This is an exploded view of the components of the quick-release mounting mechanism of this utility model;

[0016] Figure 6 This is a diagram of the component fixing plate of the quick-release mounting mechanism of this utility model;

[0017] Figure 7 This is a diagram of the hook on the upper component of the quick-release mounting mechanism of this utility model;

[0018] Figure 8 This is a diagram showing the fixing nut for the components of the quick-release mounting mechanism of this utility model;

[0019] Figure 9 This is an assembly drawing of the lower component of the quick-release mounting mechanism of this utility model;

[0020] Figure 10 This is an exploded view of the lower component of the quick-release mounting mechanism of this utility model;

[0021] Figure 11 This utility model relates to a quick-release mounting mechanism for drones, illustrated in the following diagram.

[0022] Explanation of main component symbols: Detailed Implementation

[0023] 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.

[0024] Please see Figure 1-10 As shown, this utility model provides a technical solution: a quick-release drone mounting mechanism, characterized in that it includes a quick-release upper mounting component I and a quick-release lower mounting component II, which are rotatably engaged and assembled with each other. After the quick-release upper mounting component I and quick-release lower mounting component II are initially installed in place, they are rotated by an angle R in a certain direction to ensure that they are rotated into place. They are then tightened together by a fixing nut on the quick-release upper mounting component I and a non-detachable screw on the quick-release lower mounting component II.

[0025] Preferably, the quick-release mounting upper component I includes an upper component fixing plate 001, a boss hook 002, a fixing nut 003, and a screw 004. The upper component fixing plate 001 includes a first fixing plate hole straight surface 101, a fixing plate groove surface 102, a second fixing plate hole straight surface 103, a fixing plate upper upper surface 104, and a fixing plate lower surface 105. The first fixing plate hole straight surface 101 and the second fixing plate hole straight surface 103 are irregularly shaped surfaces, which facilitates the anti-rotation of the fixing component and ensures a firm fixation.

[0026] Preferably, the boss hook 002 includes a boss hook inner screw hole 201, a boss hook lower side 202, a first boss hook inner side 203, a second boss hook inner side 204, and a boss hook irregular boss straight surface 205. The boss hook irregular boss straight surface 205 is an irregular surface, which facilitates the anti-rotation of the fastener and secure fixation. The boss hook irregular boss straight surface 205 and the boss hook lower side 202 respectively contact the first fixing plate hole straight surface 101 and the fixing plate groove surface 102 distributed on the upper component fixing plate 001. The boss hook 002 and the upper component fixing plate 001 are fixed together by screws 004.

[0027] Preferably, the fixing nut 003 includes an inner surface 301, a boss surface 302, and an internal threaded hole 303. The boss surface 302 is an irregularly shaped surface, which facilitates the anti-rotation and secure fixing of the fixing component. The inner surface 301 and the boss surface 302 are respectively in contact with the upper surface 104 of the fixing plate and the hole surface 103 of the second fixing plate. The fixing nut 003 and the upper component fixing plate 001 are fixed together by screws 004.

[0028] Preferably, the quick-release mounting lower component II includes a lower component fixing compartment 005 and an anti-loosening screw 006. The lower component fixing compartment 005 includes an upper surface 501, a lower surface 502, an inner surface 503 of a first annular hole, and an inner surface 504 of a second annular hole. The lower surface 502 and the anti-loosening screw 006 are riveted or bonded together.

[0029] Preferably, a corresponding number of protruding hooks 002 distributed on the quick-release upper component I are installed in directional alignment with a corresponding number of the inner surfaces 503 of the first annular holes distributed on the lower component fixing compartment 005 of the quick-release lower component II. The lower surface 105 of the upper component fixing plate on the quick-release upper component I is in contact with the upper surface of the fixing compartment 005 on the quick-release lower component II. The inner surfaces 203 of the first protruding hooks and the inner surfaces 204 of the second protruding hooks are in contact with the lower surface 502 and the upper surface 501 of the fixing compartment, respectively.

[0030] This utility model relates to a quick-release upper component I and a quick-release lower component II that are rotatably fastened together. After the quick-release upper component I and quick-release lower component II are initially installed in place, they are rotated by an angle R in a certain direction to ensure that they are rotated into place. The fixing nut on the quick-release upper component I and the non-removable screw on the quick-release lower component II are tightened together, effectively preventing the quick-release upper component I and quick-release lower component II from loosening or falling off.

[0031] Please see Figure 11 This utility model provides a schematic diagram of the mounting of the unmanned aerial vehicle (UAV) part 010 and the quick-release mounting mechanism 020.

[0032] This invention enables the rapid and convenient transport and handling of items through the installation of a mounting mechanism. Existing drone mounting mechanisms on the market are relatively simple or single-function, mostly using straps or fixed brackets for item mounting and positioning. However, they cannot be quickly assembled or disassembled during use, significantly reducing their adaptability and efficiency for drone applications, thus limiting their mounting capabilities. Furthermore, the inability to quickly assemble and disassemble drone mounting mechanisms also results in larger packaging volume for the drone, making packaging and transportation inconvenient and increasing transportation costs.

[0033] Compared with other existing technologies, the mounting mechanism of this utility model is simple, convenient and quick to operate, and suitable for heavy-load transportation, especially in the drone industry. This new innovative structure has higher safety; at the same time, the quick-release mounting mechanism is convenient for packaging, has a small volume, is easy to handle and carry, and has the corresponding lower transportation costs.

[0034] 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 quick-release drone mounting mechanism, characterized in that: It includes a quick-release upper component (I) and a quick-release lower component (II). The quick-release upper component (I) and quick-release lower component (II) are assembled by rotating and engaging with each other. After the quick-release upper component (I) and quick-release lower component (II) are initially installed in place, the quick-release upper component (I) and quick-release lower component (II) are rotated by an angle R in a certain direction to ensure that the quick-release upper component (I) and quick-release lower component (II) are rotated and installed in place. They are then tightened together by the fixing nut on the quick-release upper component (I) and the non-detachable screw on the quick-release lower component (II).

2. The quick-release drone mounting mechanism according to claim 1, characterized in that: The quick-release mounting upper component (I) includes an upper component fixing plate (001), a boss hook (002), a fixing nut (003), and a screw (004). The upper component fixing plate (001) includes a first fixing plate hole straight surface (101), a fixing plate groove surface (102), a second fixing plate hole straight surface (103), a fixing plate upper upper surface (104), and a fixing plate lower surface (105). The first fixing plate hole straight surface (101) and the second fixing plate hole straight surface (103) are irregularly shaped surfaces, which facilitates the anti-rotation of the fixing parts and ensures a firm fixation.

3. The quick-release drone mounting mechanism according to claim 2, characterized in that: The boss hook (002) includes a screw hole (201) inside the boss hook, a lower side surface (202) of the boss hook, an inner side surface (203) of the first boss hook, an inner side surface (204) of the second boss hook, and a straight body surface (205) of the boss hook with an irregular shape. The straight body surface (205) of the boss hook with an irregular shape is an irregular surface, which facilitates the anti-rotation of the fastener and makes it secure. The straight body surface (205) of the boss hook with an irregular shape and the lower side surface (202) of the boss hook are respectively in contact with the straight body surface (101) of the first fixing plate hole and the groove surface (102) of the fixing plate distributed on the upper component fixing plate (001). The boss hook (002) and the upper component fixing plate (001) are fixed together by screws (004).

4. The quick-release drone mounting mechanism according to claim 3, characterized in that: The fixing nut (003) includes an inner side surface (301), a straight surface of the fixing nut boss (302), and an internal threaded hole (303). The straight surface of the fixing nut boss (302) is an irregular surface, which facilitates the anti-rotation and secure fixing of the fastener. The inner side surface (301) and the straight surface of the fixing nut boss (302) are respectively in contact with the upper surface of the fixing plate (104) and the straight surface of the second fixing plate hole (103). The fixing nut (003) and the upper component fixing plate (001) are fixed together by screws (004).

5. The quick-release drone mounting mechanism according to claim 4, characterized in that: The quick-release mounting lower component (II) includes a lower component fixing compartment (005) and an anti-loosening screw (006). The lower component fixing compartment (005) includes an upper surface (501), a lower surface (502), an inner side of a first annular hole (503), and an inner side of a second annular hole (504). The lower surface (502) and the anti-loosening screw (06) are riveted or bonded together.

6. The quick-release drone mounting mechanism according to claim 5, characterized in that: The corresponding number of boss hooks (002) distributed on the quick-release upper component (I) are installed in the corresponding number of inner surfaces (503) of the first annular holes distributed on the lower component fixing compartment (005) of the quick-release lower component (II) in the same direction. The lower surface (105) of the upper component fixing plate on the quick-release upper component (I) is in contact with the upper surface of the fixing compartment (005) on the quick-release lower component (II). The inner surfaces (203) of the first boss hook and the inner surfaces (204) of the second boss hook are in contact with the lower surface (502) and the upper surface (501) of the fixing compartment, respectively.

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