A drone payload mount

Abstract

This utility model discloses a drone payload mount, including a payload frame, a clamping sleeve at the top of the payload frame, a control sleeve on the outside of the clamping sleeve, a clamping rod on the inside of the clamping sleeve, a clamping groove on the outside of the clamping rod, a control groove in the control sleeve, a control plate in the control groove, the outer wall of the control plate fitting against the inner wall of the control groove, a clamping frame connected to one side of the control plate, one end of the clamping frame being inserted into the clamping groove, a locking frame on one side of the control sleeve, a locking rod slidingly disposed in the locking frame, a locking groove on the outside of the clamping sleeve, a connecting plate on the outside of the clamping sleeve, multiple movable sleeves rotatably disposed on the connecting plate, a small gear fixedly connected to one end of each movable sleeve, a use sleeve movably disposed on the outside of the clamping sleeve, a drive wheel connected to one side of the use sleeve, a locking sleeve movably disposed on the outside of the clamping sleeve, and multiple movable rods connected to one side of the locking sleeve. This utility model ensures stable installation of the payload frame while enabling convenient disassembly and assembly.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) payload rack technology, and more specifically, to a UAV payload rack. Background Technology

[0002] In existing technologies, drone payload racks generally suffer from inconvenient installation and removal, which severely restricts the flexible application of drones in multi-mission scenarios. Specifically, existing technologies cannot easily install the payload rack on the bottom of the drone, nor can they easily remove it from the bottom. This problem is particularly prominent in practical applications. When operators need to change the drone payload rack according to different mission requirements, they usually need to use a variety of professional tools such as wrenches, screwdrivers, and Allen wrenches for assistance. This not only increases the carrying burden but also significantly prolongs the payload replacement time. In complex field environments or emergency mission scenarios, this cumbersome disassembly and assembly process greatly reduces work efficiency and may even lead to mission interruption due to lack of tools.

[0003] Secondly, while some improved designs have indeed emerged in the industry to address the aforementioned issues, and some devices have achieved convenient replacement of the payload rack without the need for tools to a certain extent, these designs generally suffer from obvious defects such as simple structure and insufficient reliability. These simple quick-release structures often lack multiple safety mechanisms, and during high-speed flight or complex missions of drones, external factors such as vibration and impact can easily cause the fixed structure to loosen or even completely fall off. Especially under severe weather conditions or during long-term missions, such simple quick-release devices may fail unexpectedly, leading to unstable installation of the payload rack or even accidental detachment during flight. Once a payload detachment accident occurs, it will not only cause damage to expensive equipment, but may also pose a serious threat to the safety of personnel and property on the ground. It will also lead to mission failure and data loss, causing huge economic losses and safety hazards to users. Utility Model Content

[0004] (a) Technical problems to be solved

[0005] In view of the problems existing in the prior art, this utility model provides a drone payload mount to solve the technical problems mentioned in the background art.

[0006] (II) Technical Solution

[0007] To achieve the above objectives, this utility model provides the following technical solution: a drone payload mount, comprising a payload frame, a detachable clamping sleeve at the top of the payload frame, a control sleeve rotatably fitted around the outer side of the clamping sleeve, a detachable clamping rod on the inner side of the clamping sleeve, a clamping groove on the outer side of the clamping rod, a control groove in the control sleeve, a control plate movably mounted within the control groove, the outer wall of the control plate fitting against the inner wall of the control groove, a clamping bracket connected to one side of the control plate, one end of the clamping bracket being engaged in the clamping groove, and a locking bracket fixedly mounted on one side of the control sleeve. The locking frame has a sliding locking rod, and the outer side of the locking sleeve has a locking groove. One end of the locking rod is inserted into the locking groove. A connecting plate is fixedly installed on the outer side of the locking sleeve. Multiple movable sleeves are rotatably installed on the connecting plate. A small gear is fixedly connected to one end of each movable sleeve. A use sleeve is movably fitted on the outer side of the locking sleeve. A drive wheel is connected to one side of the use sleeve. The multiple small gears mesh with the drive wheel respectively. A locking sleeve is movably fitted on the outer side of the locking sleeve. Multiple moving rods are connected to one side of the locking sleeve. The moving rods are movably connected to the movable sleeves via threads.

[0008] The present invention is further configured such that a frame is provided at the top of the load frame, a base plate is fixedly provided at the bottom of the frame, and the clamping rod passes through the base plate and the reserved mounting hole on the load frame to be detachably connected with the clamping sleeve. This through-type connection structure makes the load frame and the frame form a stable whole, and the detachable connection between the clamping rod and the clamping sleeve provides sufficient mechanical strength.

[0009] The present invention is further configured such that a control spring is movably sleeved on the outer side of the clamping frame, and the two ends of the control spring are respectively connected to the control plate and the clamping sleeve.

[0010] The present invention is further configured such that a sliding groove is provided on the outer side of the locking sleeve, the depth of the sliding groove is shallower than that of the locking groove, and both ends of the sliding groove are respectively connected to the locking groove. This ingenious groove design forms a precise guide rail for the movement of the locking rod. The difference in the shallow and deep structure and the connection design ensure that the locking rod can move smoothly along the predetermined trajectory during the unlocking and locking process.

[0011] The present invention is further configured such that the connection between the locking groove and the sliding groove is rounded, and one end of the locking rod is designed with a rounded corner structure. This rounded corner transition design reduces the frictional resistance between the locking rod and the groove wall during the sliding process, reduces the degree of mechanical wear, improves the service life of the parts, and makes the locking and unlocking operations smoother.

[0012] The present invention is further configured such that a locking plate is connected to one end of the locking rod, and a connecting spring is movably sleeved on the outside of the locking rod. The two ends of the connecting spring are respectively connected to the lock frame and the locking plate. This elastic reset structure ensures that the locking rod can automatically return to the locking position by the elastic force of the connecting spring, so that the locking rod can be stably inserted into the lock groove.

[0013] The present invention is further configured such that both the control groove and the control plate are variable diameter structures. This variable diameter structure is the core mechanism. Through the gradual change of radial dimension, combined with the change of the state of the control spring, the movement of the control plate and the clamping frame is precisely controlled, so that the clamping frame can be smoothly inserted into or withdrawn from the clamping groove.

[0014] The present invention is further configured such that the clamping groove is formed in an annular structure on the outside of the clamping rod. The annular structure simplifies the alignment requirements during installation, and the operator does not need to consider the angle correspondence between the clamping frame and the clamping groove, which greatly improves the convenience of installation and the efficiency of operation.

[0015] (III) Beneficial Effects

[0016] Compared with the prior art, the present invention provides a drone payload mount, which has the following advantages:

[0017] 1. This utility model designs a rapid installation and disassembly system consisting of a load frame, a clamping sleeve, a control sleeve, a clamping rod, and a clamping groove. It enables convenient installation and disassembly of the load frame without any tools. Through the cooperation of the control groove and control board in the control sleeve, and the precise interaction between the locking frame, locking rod, and locking groove, a fully manual, convenient assembly and disassembly mechanism is constructed. The operator simply rotates the control sleeve, and the variable-diameter structure of the control groove and control board, along with the cooperation of the control spring, automatically pulls the clamping frame out of the clamping groove, easily disconnecting the load frame from the frame. The entire assembly and disassembly process requires no tools, greatly reducing the carrying burden in field operations and significantly improving the efficiency of load replacement. Especially in complex environments or emergency mission scenarios, this rapid assembly and disassembly mechanism can complete load replacement in a very short time, avoiding mission interruptions due to tool shortages. It fully meets the urgent need for rapid load replacement in multi-mission scenarios for UAVs, greatly improving the application flexibility and work efficiency of UAVs.

[0018] 2. By cleverly combining components such as sleeves, drive wheels, pinions, movable sleeves, movable rods, and locking sleeves, a highly reliable fixing system that is vibration-proof and prevents loosening is constructed. This utility model employs a first-level locking mechanism, where the threaded connection between the movable sleeve and the movable rod drives the locking sleeve to position itself. The locking sleeve's limiting design on the locking plate forms a second-level mechanical locking mechanism. Furthermore, the locking rod and locking groove work together to achieve a third-level locking of the locking frame and control sleeve. This multi-layered security design ensures that even in extreme working environments such as high-speed flight of the UAV or encountering strong vibrations, the payload frame can maintain a stable and reliable fixing effect, avoiding the risk of the payload frame loosening or falling off. Locking and unlocking can be completed with a simple rotation action, while also possessing sufficient safety mechanisms. This fundamentally solves the stability problem of the UAV payload frame in harsh environments, ensuring that the UAV always maintains a stable and reliable working state, providing a solid guarantee for flight safety and mission success, and effectively avoiding economic losses and safety hazards caused by equipment damage, personnel injury, and mission failure. Attached Figure Description

[0019] Figure 1 This is a schematic diagram of the overall structure of a drone payload mount according to the present invention;

[0020] Figure 2 This is a schematic diagram of the load-bearing frame in this utility model;

[0021] Figure 3 This is a schematic diagram showing the dispersed structure of the clamping rod, clamping sleeve, control sleeve, locking sleeve, and use sleeve in this utility model;

[0022] Figure 4 This is a cross-sectional structural diagram of the clamping rod, clamping sleeve, control sleeve, locking sleeve, and use sleeve in this utility model;

[0023] Figure 5 This is a cross-sectional structural diagram of the clamping sleeve, control sleeve, locking sleeve, and use sleeve in this utility model.

[0024] In the diagram: 1. Load frame; 2. Clamping sleeve; 3. Control sleeve; 4. Clamping rod; 5. Clamping groove; 6. Control groove; 7. Control plate; 8. Clamping frame; 9. Lock frame; 10. Locking rod; 11. Lock groove; 12. Connecting plate; 13. Moving sleeve; 14. Pinion; 15. Usage sleeve; 16. Drive wheel; 17. Locking sleeve; 18. Moving rod; 19. Frame; 20. Base plate; 21. Control spring; 22. Sliding groove; 23. Locking plate; 24. Connecting spring. Detailed Implementation

[0025] It should be noted that, unless otherwise specified, the embodiments and features described in this application can be combined with each other. The present invention will now be described in detail with reference to the accompanying drawings and embodiments.

[0026] It should be noted that, unless otherwise specified, all technical and scientific terms used in this application have the same meaning as commonly understood by one of ordinary skill in the art to which this application pertains.

[0027] In this utility model, unless otherwise stated, the orientations used, such as "up" and "down", usually refer to the direction shown in the accompanying drawings, or to the vertical, perpendicular, or gravitational direction; similarly, for ease of understanding and description, "left" and "right" usually refer to the left and right shown in the accompanying drawings; "inner" and "outer" refer to the inner and outer contours of each component itself, but the above directional terms are not used to limit this utility model.

[0028] Please see Figures 1-5 A drone payload mount includes a payload frame 1. A clamping sleeve 2 is detachably mounted on the top of the payload frame 1. A control sleeve 3 is rotatably mounted on the outer side of the clamping sleeve 2. A clamping rod 4 is detachably mounted on the inner side of the clamping sleeve 2. A clamping groove 5 is formed on the outer side of the clamping rod 4. A control groove 6 is formed in the control sleeve 3. A control plate 7 is movably mounted in the control groove 6. The outer wall of the control plate 7 is fitted against the inner wall of the control groove 6. A clamping frame 8 is connected to one side of the control plate 7. One end of the clamping frame 8 is inserted into the clamping groove 5. A locking frame 9 is fixedly mounted on one side of the control sleeve 3. A locking rod 10 is slidably mounted in the locking frame 9. A locking groove 11 is provided, and one end of the locking rod 10 is inserted into the locking groove 11. A connecting plate 12 is fixedly provided on the outside of the clamping sleeve 2. Multiple movable sleeves 13 are rotatably installed on the connecting plate 12. A small gear 14 is fixedly connected to one end of the movable sleeve 13. A use sleeve 15 is movably sleeved on the outside of the clamping sleeve 2. A drive wheel 16 is connected to one side of the use sleeve 15. The multiple small gears 14 mesh with the drive wheel 16 respectively. A locking sleeve 17 is movably sleeved on the outside of the clamping sleeve 2. Multiple movable rods 18 are connected to one side of the locking sleeve 17. The movable rods 18 are movably connected to the movable sleeves 13 by threads.

[0029] The top of the load frame 1 is provided with a frame 19, and the bottom of the frame 19 is fixedly provided with a base plate 20. The clamping rod 4 passes through the base plate 20 and the reserved mounting hole on the load frame 1 and is detachably connected to the clamping sleeve 2.

[0030] In this embodiment, when the load frame 1 needs to be removed from the bottom of the frame 19, the sleeve 15 is first rotated forward. The sleeve 15 drives the drive wheel 16 on one side to rotate forward. Then, the drive wheel 16 drives the multiple small gears 14 meshing with it to rotate in the opposite direction, thereby driving the movable sleeve 13 to rotate in the opposite direction on the connecting plate 12. Since the movable sleeve 13 is threadedly fitted onto the outside of the movable rod 18, the movable rod 18 then drives the locking sleeve 17 on one side to slide, so that the locking sleeve... 17. The outer wall of the locking plate 23 is no longer limited. Then, the control sleeve 3 is rotated forward. The control sleeve 3 drives one side of the locking frame 9 to rotate forward, and the locking frame 9 will drive the locking rod 10, the locking plate 23 and the connecting spring 24 to rotate forward. Then, the inner wall of the locking groove 11 presses against one end of the locking rod 10. Due to the rounded corner design of one end of the locking rod 10 and the rounded corner treatment at the connection between the locking groove 11 and the sliding groove 22, one end of the locking rod 10 slides out of the locking groove 11 and slides into the sliding groove 22 for sliding. The other end will drive the locking plate 23 to move outward, causing the locking plate 23 to drive the connecting spring 24 to stretch outward. At the same time, the control sleeve 3 will drive the control groove 6 opened in the inner diameter-changing structure to rotate in the forward direction. During this process, the control spring 21 gradually resets and pushes the control plate 7 outward, so that the outer wall of the control plate 7 is always in close contact with the inner wall of the control groove 6, and the control plate 7 drives one side of the clamping frame 8 to gradually pull out of the clamping groove 5. When the locking frame 9 drives the locking rod 10 and other components to rotate to the locking groove 11 connected to the other end of the sliding groove 22, the connecting spring 24 resets and pulls the locking plate 23, causing the locking plate 23 to drive the locking rod 10 to slide inward, so that one end of the locking rod 10 is inserted into the locking groove 11 here. At this time, the clamping frame 8 is completely pulled out of the clamping groove 5. Then the clamping sleeve 2 is pulled down to remove the clamping sleeve 2 here. Then, the other clamping sleeves 2 are removed by referring to the above steps. Then the load frame 1 can be removed from the bottom frame of the machine frame 19.

[0031] Please see Figures 3-5 As a further implementation of the overall equipment: a control spring 21 is movably sleeved on the outside of the clamping frame 8, and the two ends of the control spring 21 are connected to the control plate 7 and the clamping sleeve 2 respectively.

[0032] The outer side of the locking sleeve 2 is provided with a sliding groove 22, the depth of which is shallower than that of the locking groove 11, and both ends of the sliding groove 22 are connected to the locking groove 11 respectively.

[0033] The connection between the locking groove 11 and the sliding groove is rounded, and one end of the locking rod 10 is designed with a rounded corner.

[0034] A locking plate 23 is connected to one end of the locking rod 10, and a connecting spring 24 is movably sleeved on the outside of the locking rod 10. The two ends of the connecting spring 24 are connected to the locking frame 9 and the locking plate 23 respectively.

[0035] Both the control slot 6 and the control plate 7 are variable diameter structures.

[0036] The locking groove 5 is a ring-shaped structure located on the outside of the locking rod 4.

[0037] More specifically, when the load frame 1 needs to be reinstalled on the underside of the base plate 20, first, align the top of the load frame 1 with the lower end face of the base plate 20, ensuring that the mounting holes on the base plate 20 are concentrically aligned with the mounting holes on the load frame 1. Then, pass the clamping rod 4 through the mounting holes of the base plate 20 and the load frame 1 from the top. Next, directly fit the clamping sleeve 2 onto the outside of the clamping rod 4 from the bottom. Then, rotate the control sleeve 3 in the reverse direction. The control sleeve 3, through its locking frame 9 on one side, drives the locking rod 10, the locking plate 23, and the connecting spring 24 to rotate in the reverse direction. The rotation causes the inner wall of the locking groove 11 to press against one end of the locking rod 10. Then, one end of the locking rod 10 slides out of the locking groove 11 and into the sliding groove 22. Meanwhile, the other end of the locking rod 10 is stretched outward by the connecting spring 24 driven by the locking plate 23. At the same time, the control sleeve 3 will drive the inner diameter-type control groove 6 to rotate in the opposite direction, causing the inner wall of the control groove 6 to gradually press against the outer wall of the control plate 7. This causes the control plate 7 to gradually press against the connecting spring 24 on one side, and the control plate 7 drives the clamping bracket 8 on one side to gradually move inward. The side-sliding reset allows one end of the locking bracket 8 to gradually enter the locking groove 5. When the locking bracket 9 moves the locking rod 10 and other components to the position corresponding to the original locking groove 11, the connecting spring 24 pulls the locking rod 10 inward through the locking plate 23 to slide and reset, so that one end of the locking rod 10 is reinserted into the original locking groove 11. At this time, one end of the locking bracket 8 is fully inserted into the locking groove 5. Then, the sleeve 15 is rotated in the opposite direction, and the sleeve 15 drives one of its driving wheels 16 to rotate in the opposite direction, so that the driving wheel 16 rotates in the opposite direction through multiple... The engagement of the small gear 14 drives the movable sleeve 13 to rotate forward on the connecting plate 12. Then, the movable rod 18 drives the locking sleeve 17 to slide and reset, so that the inner wall of the locking sleeve 17 re-limits the outer wall of the locking plate 23, preventing the locking plate 23 and the locking rod 10 from sliding outward. Then, the engagement of the locking rod 10 and the locking groove 11 achieves positioning and locking of the locking frame 9, preventing accidental rotation of the locking frame 9 and the control sleeve 3, thereby preventing accidental unlocking, ensuring the stable installation of the load frame 1, and enabling the equipment to be used stably.

[0038] In summary, during the use or operation of the overall equipment: when it is necessary to remove the load frame 1 from the bottom of the frame 19, first rotate the sleeve 15 in the forward direction. The sleeve 15 drives the one-sided drive wheel 16 to rotate in the forward direction. Then, the drive wheel 16 drives the multiple small gears 14 meshing with it to rotate in the reverse direction, thereby driving the movable sleeve 13 to rotate in the reverse direction on the connecting plate 12. Since the movable sleeve 13 is threadedly fitted onto the outside of the movable rod 18, the movable rod 18 then drives the one-sided locking sleeve 17 to rotate... The sliding motion causes the lock sleeve 17 to no longer limit the outer wall of the lock plate 23. Then, the control sleeve 3 rotates forward, causing one side of the lock frame 9 to rotate forward. The lock frame 9 also causes the lock rod 10, lock plate 23, and connecting spring 24 to rotate forward. Then, the inner wall of the lock groove 11 presses against one end of the lock rod 10. Due to the rounded corner design of one end of the lock rod 10 and the rounded corner treatment at the connection between the lock groove 11 and the sliding groove 22, one end of the lock rod 10 slides out of the lock groove 11 and into the sliding groove 22 for sliding. Furthermore, the other end of the locking rod 10 will drive the locking plate 23 to move outward, causing the locking plate 23 to stretch the connecting spring 24 outward. At the same time, the control sleeve 3 will drive the control groove 6 opened in the inner diameter-changing structure to rotate in the forward direction. During this process, the control spring 21 gradually resets and pushes the control plate 7 outward, so that the outer wall of the control plate 7 is always in close contact with the inner wall of the control groove 6, and the control plate 7 drives the clamping bracket 8 on one side to gradually be pulled out of the clamping groove 5. When the locking bracket 9 drives the locking rod 10 and other components to rotate... When the sliding groove 22 moves to the locking groove 11 connected to the other end, the connecting spring 24 resets and pulls the locking plate 23, causing the locking plate 23 to drive the locking rod 10 to slide inward, so that one end of the locking rod 10 is inserted into the locking groove 11. At this time, the clamping frame 8 is completely pulled out from the clamping groove 5. Then the clamping sleeve 2 is pulled down to remove the clamping sleeve 2. Then, the other clamping sleeves 2 are removed by referring to the above steps. Then the load frame 1 can be removed from the bottom frame of the machine frame 19.

[0039] When it is necessary to reinstall the load frame 1 to the underside of the base plate 20, first, align the top of the load frame 1 with the lower end face of the base plate 20, ensuring that the mounting holes on the base plate 20 are concentrically aligned with the mounting holes on the load frame 1. Then, pass the clamping rod 4 through the mounting holes of the base plate 20 and the load frame 1 from the top. Next, directly fit the clamping sleeve 2 onto the outside of the clamping rod 4 from the bottom. Then, rotate the control sleeve 3 in the reverse direction. The control sleeve 3, through its side locking frame 9, drives the locking rod 10, the locking plate 23, and the connecting spring 24 to rotate in the reverse direction. This causes the inner wall of the locking groove 11 to press against one end of the locking rod 10. Then, one end of the locking rod 10 slides out of the locking groove 11 and into the sliding groove 22. Meanwhile, the other end of the locking rod 10 is stretched outward by the connecting spring 24 driven by the locking plate 23. At the same time, the control sleeve 3 will drive the inner diameter-type control groove 6 to rotate in the opposite direction, causing the inner wall of the control groove 6 to gradually press against the outer wall of the control plate 7. This causes the control plate 7 to gradually press against the connecting spring 24 on one side, and the control plate 7 drives the clamping bracket 8 on one side to gradually slide inward. The locking mechanism 8 is gradually inserted into the locking groove 5. When the locking frame 9 moves the locking rod 10 and other components to the position corresponding to the original locking groove 11, the connecting spring 24 pulls the locking rod 10 inward through the locking plate 23 to reset, so that one end of the locking rod 10 is reinserted into the original locking groove 11. At this time, one end of the locking frame 8 is fully inserted into the locking groove 5. Then, the sleeve 15 is rotated in the opposite direction, which drives the drive wheel 16 on one side to rotate in the opposite direction, so that the drive wheel 16 rotates in the opposite direction through multiple... The engagement of the pinion 14 drives the movable sleeve 13 to rotate forward on the connecting plate 12. Then, the movable rod 18 drives the locking sleeve 17 to slide and reset, so that the inner wall of the locking sleeve 17 re-limits the outer wall of the locking plate 23, preventing the locking plate 23 and the locking rod 10 from sliding outward. Then, the engagement of the locking rod 10 and the locking groove 11 achieves positioning and locking of the locking frame 9, preventing accidental rotation of the locking frame 9 and the control sleeve 3, thereby preventing accidental unlocking, ensuring the stable installation of the load frame 1, and enabling the equipment to be used stably.

[0040] Of all the solutions mentioned above, those involving the connection between two components can be selected according to the actual situation, such as welding, bolt and nut connection, bolt or screw connection, or other known connection methods, which will not be elaborated here. For all the fixed connections mentioned above, welding is preferred. Although embodiments of this utility model have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations can be made to these embodiments without departing from the principles and spirit of this utility model. The scope of this utility model is defined by the appended claims and their equivalents.

Claims

1. An unmanned aerial vehicle payload rack comprising a payload rack (1) characterised by: The load frame (1) is provided with a clamping sleeve (2) at the top. A control sleeve (3) is provided on the outside of the clamping sleeve (2). A clamping rod (4) is provided on the inside of the clamping sleeve (2). A clamping groove (5) is provided on the outside of the clamping rod (4). A control groove (6) is provided in the control sleeve (3). A control plate (7) is provided in the control groove (6). The outer wall of the control plate (7) is in contact with the inner wall of the control groove (6). A clamping frame (8) is connected to one side of the control plate (7). One end of the clamping frame (8) is inserted into the clamping groove (5). A locking frame (9) is provided on one side of the control sleeve (3). A locking rod (10) is slidably provided in the locking frame (9). A locking groove (11) is provided on the outside of the clamping sleeve (2). One end of the locking rod (10) is... Inserted into the locking groove (11), the clamping sleeve (2) is provided with a connecting plate (12) on the outside, and multiple movable sleeves (13) are rotatably provided on the connecting plate (12). One end of the movable sleeve (13) is fixedly connected to a small gear (14). The clamping sleeve (2) is movably fitted with a use sleeve (15). One side of the use sleeve (15) is connected to a drive wheel (16). The multiple small gears (14) mesh with the drive wheel (16) respectively. The clamping sleeve (2) is movably fitted with a locking sleeve (17). One side of the locking sleeve (17) is connected to multiple moving rods (18). The moving rods (18) are movably connected to the movable sleeves (13) through threads.

2. The UAV payload mount according to claim 1, characterized in that: The load frame (1) has a frame (19) at the top and a base plate (20) at the bottom. The clamping rod (4) passes through the base plate (20) and the pre-reserved mounting hole on the load frame (1) and is detachably connected to the clamping sleeve (2).

3. A UAV payload mount according to any one of claims 1 or 2, characterized in that: The clamping frame (8) is movably sleeved with a control spring (21), and the two ends of the control spring (21) are connected to the control plate (7) and the clamping sleeve (2) respectively.

4. The UAV payload mount according to claim 1, characterized in that: The locking sleeve (2) has a sliding groove (22) on its outer side. The depth of the sliding groove (22) is shallower than that of the locking groove (11), and both ends of the sliding groove (22) are connected to the locking groove (11).

5. A UAV payload mount according to claim 4, characterized in that: The connection between the locking groove (11) and the sliding groove (22) is rounded, and one end of the locking rod (10) is designed with a rounded corner structure.

6. A UAV payload mount according to claim 5, characterized in that: One end of the locking rod (10) is connected to a locking plate (23), and a connecting spring (24) is movably sleeved on the outside of the locking rod (10). The two ends of the connecting spring (24) are connected to the locking frame (9) and the locking plate (23) respectively.

7. A UAV payload mount according to claim 3, characterized in that: Both the control slot (6) and the control plate (7) are variable diameter structures.

8. A UAV payload mount according to claim 7, characterized in that: The locking groove (5) is a ring structure located on the outside of the locking rod (4).

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