Compact unmanned aerial vehicle nest suitable for iron tower installation
By designing a compact drone nest suitable for tower installation, and utilizing a clamping mechanism, shock absorption components, and angle adjustment function, the problems of inconvenient installation and poor stability of traditional drone nests are solved, enabling drones to be stably and accurately charged and land safely, thus improving operational efficiency.
Patent Information
- Application Number
- CN202511134554.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-08-13
- Publication Date
- 2025-11-14
AI Technical Summary
Traditional drone nests are inconvenient to install, have poor stability, lack shock absorption and angle adjustment functions, and cannot provide charging services, which increases manual maintenance costs and reduces operational efficiency.
A compact drone nest suitable for tower installation was designed, comprising a clamping mechanism, a nest base mechanism, a nest fence mechanism, and drone auxiliary components. It utilizes components such as hydraulic cylinders, piston rods, connecting rods, and locking teeth to achieve a stable clamping, and combines shock-absorbing components and angle tilting components to provide charging and positioning functions.
It improves the stability and adaptability of drone installation on iron towers, enhances the stability and flexibility of take-off and landing, enables precise charging and safe landing of drones, and improves the practicality of drone nests.
Smart Images

Figure CN120942618A_ABST
Abstract
Description
Technical Field
[0001] This invention relates to the field of unmanned aerial vehicles (UAVs), specifically to a compact UAV nest suitable for tower mounting. Background Technology
[0002] In fields such as power line inspection and communication base station monitoring, towers, as high-altitude infrastructure, are characterized by their wide distribution and moderate height. If drone nests can be deployed on towers, drones can use the towers as bases to carry out routine inspections without having to take off and land frequently from the ground, which will greatly improve operational efficiency and coverage, while reducing dependence on ground sites. Therefore, there is an urgent need for such compact drone nests.
[0003] However, traditional drone nests are usually installed by bolting or welding, which is not only time-consuming and labor-intensive, but also difficult to adapt to tower structures of different diameters, resulting in poor stability. Secondly, traditional nests lack effective shock absorption and angle adjustment functions, making drones susceptible to vibration during take-off and landing, leading to equipment damage or positioning deviations. In addition, traditional nests with limited functions cannot provide services such as charging for drones, increasing manual maintenance costs and reducing operational efficiency. Therefore, we propose a compact drone nest suitable for tower installation. Summary of the Invention
[0004] To address the shortcomings of existing technologies, this invention provides a compact drone nest suitable for tower installation, thus solving the aforementioned problems.
[0005] To achieve the above-mentioned objectives, the present invention provides the following technical solution: a compact UAV nest suitable for tower installation, comprising a support base, the support base being the main support, and a connecting plate fixedly installed on one side wall of the support base;
[0006] A first connecting shaft is symmetrically fixedly installed on the connecting plate on the support base, and a second connecting shaft is also symmetrically fixedly installed on the connecting plate, with the first connecting shaft and the second connecting shaft being inclined.
[0007] A clamping mechanism is provided on the connecting plate of the support base. The clamping mechanism includes a transmission component and a clamp. The connecting plate and connecting shaft of the support base are provided with a transmission component. A clamp is installed on the transmission component. A stabilizing component is provided on the inner arc surface of the clamp.
[0008] The upper surface of the support base is fixedly provided with a nest base mechanism, which includes a shock-absorbing component and an angle tilting component. A base plate is fixedly installed on the upper surface of the support base, and a shock-absorbing component is provided on the base plate. An angle tilting component is provided on the shock-absorbing component.
[0009] An organic nesting fence mechanism and a drone-assisted component are disposed above the tilting component.
[0010] Preferably, the transmission assembly includes a push plate, a connecting rod 1, a hydraulic cylinder 2, and a piston rod 2. The hydraulic cylinder 2 is also fixedly installed on the side wall of the support base where the connecting plate is installed. The piston rod 2 is drivenly connected to the hydraulic cylinder 2. The push plate is fixedly installed on the other end of the piston rod 2. The plane of the push plate has symmetrically opened inclined waist-shaped holes near the two side walls. One end of the connecting rod 1 is hinged to the connecting shaft 1 on the support base. The connecting shaft 1 is also fixedly installed at this end of the connecting rod 1. The connecting shaft on the connecting rod 1 is tangent to and slidably connected to the waist-shaped hole on the push plate. The connecting shaft 2 on the support base is hinged to the connecting rod 1 near the other end.
[0011] A hinge seat is fixedly installed on the other end of the connecting rod.
[0012] Preferably, a hinge block is fixedly installed at the middle of the outer arc surface of the clamp, and the hinge seat on the connecting rod and the hinge block on the clamp are hinged together.
[0013] Preferably, the stabilizing component includes locking teeth and spring 2. Locking teeth are fixedly installed at equal intervals on the inner arc surfaces of the two clamps on both sides. A connecting hole is opened between two corresponding locking teeth on the inner arc surface, and spring 2 is fixedly installed in the connecting hole.
[0014] Preferably, the shock absorption assembly includes a sliding ring, a spring, and a connecting rod. Support blocks are fixedly installed on the upper surface of the base plate near the four corners. A connecting rod is fixedly installed between two opposing support blocks. Sliding rings are symmetrically slidably connected to the connecting rod. A spring is fixedly installed between two sliding rings on the same side. The spring and the connecting rod on the base plate are coaxially sleeved. A hinge seat is fixedly installed on the upper surface of the sliding ring. The connecting rod is hinged inside the hinge seat.
[0015] The bottom surface of the support base is rectangular and fixedly equipped with four hinge blocks. The other ends of the four connecting rods are respectively hinged to the four hinge blocks on the bottom surface of the support base.
[0016] Preferably, the tilting assembly includes a support base, a hydraulic cylinder, a piston rod, and a limiting shaft. Support plates are symmetrically fixedly installed on the upper surface of the support base near both sides. Limiting shafts are symmetrically fixedly installed on the opposite surfaces of the two support plates. A hinge base is fixedly installed on the upper surface of the support base between the two support plates. A hydraulic cylinder is hinged in the hinge base. A piston rod is drivenly connected to the hydraulic cylinder. A hinge block is fixedly installed on the other end of the piston rod.
[0017] The tilting assembly also includes a nest support base, on which rotating support plates are symmetrically and fixedly installed. Each rotating support plate has an arc groove, and a hinge seat is fixedly installed between two rotating support plates on the bottom surface of the nest support base.
[0018] The hinge block on the piston rod is hinged to the hinge seat at the bottom of the machine nest support.
[0019] The limiting shaft and the arc groove are slidably connected.
[0020] Preferably, a support plate is fixedly installed on the upper surface of the nest support base corresponding to one side, and brackets are symmetrically fixedly installed on the upper surface of the nest support base corresponding to both sides of the support plate.
[0021] Support plates are symmetrically fixedly installed on the outer wall of the bracket near the support plate.
[0022] Preferably, the nest enclosure mechanism includes a sliding block, a lead screw, and a motor. The lead screw is rotatably connected between two support plates on the bracket. The motor is fixedly installed on the bottom surface of the lower support plate of the bracket. The output shaft of the motor and the lead screw are coaxially fixedly connected. The sliding block is threaded onto the lead screw.
[0023] A rotating shaft is fixedly installed on the outer wall of the bracket, corresponding to the support plate near the top.
[0024] A rotating shaft is also fixedly installed on one side wall of the sliding block.
[0025] Preferably, the nest enclosure mechanism further includes a sliding enclosure plate, a second connecting rod, and a third connecting rod. Multiple sliding enclosure plates are slidably connected to the bracket. A rotating shaft is fixedly installed on the plane of the sliding enclosure plate near the top. An oblong hole is opened on the plane of the sliding enclosure plate below the rotating shaft. A third connecting rod is hinged to the rotating shaft on the bracket. A second connecting rod is hinged to the rotating shaft on the sliding block. The second connecting rod and the third connecting rod are cross-hinged.
[0026] The other end of the second connecting rod is hinged to the rotating shaft on the sliding plate, and the other end of the third connecting rod is tangent to and slidably connected to the waist-shaped hole on the sliding plate;
[0027] Another set of connecting rods three and two is hinged to the other end of connecting rod three and connecting rod two, and this set of connecting rods three and connecting rod two is connected to another sliding panel in the same way.
[0028] Preferably, the drone auxiliary components include a water outlet, a charging contact, and a magnetic metal sheet. The drone nest support base has water outlets equidistantly opened on the side wall facing the support plate. A charging contact is fixedly installed in the middle of the landing plane of the drone nest support base. Magnetic metal sheets are also fixedly installed near the four corners of the landing plane of the drone nest support base.
[0029] Compared with the prior art, the present invention provides a compact drone nest suitable for tower installation, which has the following features:
[0030] Beneficial effects:
[0031] 1. This compact drone housing suitable for tower installation uses a clamping mechanism. The hydraulic cylinder and piston rod in the transmission assembly drive the push plate to move. Combined with the hinge structure of the connecting rod and the connecting shaft, the clamp can tightly grip the tower. The locking teeth and spring in the stabilizing component of the inner arc surface of the clamp can adapt to towers of different diameters, enhancing the stability and adaptability of the installation.
[0032] 2. This compact drone nest suitable for tower installation has a nest base mechanism that includes a shock-absorbing component and an angle tilting component. The sliding ring, spring 1, and connecting rod 4 in the shock-absorbing component can effectively absorb the vibration during drone take-off and landing. The angle tilting component drives the nest support to tilt through hydraulic cylinder 1 and piston rod 1. With the sliding connection of limit shaft and arc groove, the nest angle can be adjusted according to needs. Compared with traditional nests, which have poor shock absorption and inconvenient angle adjustment, this greatly improves the stability of drone take-off and landing and the flexibility of nest use.
[0033] 3. This compact drone nest, suitable for tower installation, features a nest enclosure mechanism where a motor drives a lead screw to rotate, causing a sliding block to move. This movement is then connected to two connecting rods, which in turn move the sliding enclosure plate, allowing the enclosure to open and close. The charging contacts and magnetic metal sheets in the drone auxiliary components enable precise charging and positioning of the drone. Rainwater can be drained from the outlet through the tilting component, solving the problem of the traditional single-function drone nest and improving its practicality. Attached Figure Description
[0034] Figure 1 This is a schematic diagram of the structure of the present invention;
[0035] Figure 2 This is a cross-sectional view of the present invention;
[0036] Figure 3 This is a schematic diagram of the clamping mechanism of the present invention;
[0037] Figure 4 This is an exploded view of the nest base mechanism of the present invention;
[0038] Figure 5 This is a schematic diagram of the nest enclosure mechanism of the present invention;
[0039] Figure 6 for Figure 3 A magnified view of part A in the diagram.
[0040] In the diagram: 1. Support base; 2. Push plate; 3. Link 1; 4. Clamp; 5. Base plate; 6. Sliding ring; 7. Spring 1; 8. Support base; 9. Mechanism support base; 10. Water outlet; 11. Charging contact; 12. Magnetic metal sheet; 13. Sliding enclosure; 14. Link 2; 15. Link 3; 16. Sliding block; 17. Lead screw; 18. Support plate; 19. Motor; 20. Link 4; 21. Hydraulic cylinder 1; 22. Piston rod 1; 23. Limiting shaft; 24. Arc groove; 25. Clamping tooth; 26. Spring 2; 27. Hydraulic cylinder 2; 28. Piston rod 2; 29. Bracket. Detailed Implementation
[0041] The technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the scope of protection of the present invention.
[0042] Please see Figure 1-6 A compact drone nest suitable for tower installation includes a support base 1, which serves as the main support, and a connecting plate is fixedly installed on one side wall of the support base 1.
[0043] A connecting shaft 1 is symmetrically fixedly installed on the connecting plate on the support base 1, and a connecting shaft 2 is also symmetrically fixedly installed on the connecting plate, with the connecting shaft 1 and the connecting shaft 2 being inclined.
[0044] A clamping mechanism is provided on the connecting plate on the support base 1. The clamping mechanism includes a transmission component and a clamp 4. The connecting plate and the connecting shaft on the support base 1 are provided with a transmission component. The clamp 4 is installed on the transmission component. A stabilizing component is provided on the inner arc surface of the clamp 4.
[0045] A nest base mechanism is fixedly installed on the upper surface of the support base 1. The nest base mechanism includes a shock-absorbing component and an angle tilting component. A base plate 5 is fixedly installed on the upper surface of the support base 1. A shock-absorbing component is installed on the base plate 5. An angle tilting component is installed on the shock-absorbing component.
[0046] An organic nesting fence mechanism and a drone-assisted component are installed above the tilting component.
[0047] Furthermore, the transmission assembly includes a push plate 2, a connecting rod 3, a hydraulic cylinder 27, and a piston rod 28. The hydraulic cylinder 27 is also fixedly installed on the side wall of the support base 1 where the connecting plate is installed. The piston rod 28 is connected to the hydraulic cylinder 27. The push plate 2 is fixedly installed on the other end of the piston rod 28. The plane of the push plate 2 has symmetrically opened inclined waist-shaped holes near the two side walls. One end of the connecting rod 3 is hinged to the connecting shaft 1 on the support base 1. The connecting shaft 1 is also fixedly installed at this end of the connecting rod 3. The connecting shaft on the connecting rod 3 is tangent to and slidably connected to the waist-shaped hole on the push plate 2. The connecting shaft 2 on the support base 1 is hinged to the connecting rod 3 near the other end. The inclined waist-shaped hole design on the push plate 2, in conjunction with the connecting shaft on the connecting rod 3, can convert the linear motion of the piston rod 28 into the swing motion of the connecting rod 3.
[0048] A hinge seat is fixedly installed on the other end of the connecting rod 3.
[0049] Furthermore, a hinge block is fixedly installed at the middle of the outer arc surface of the clamp 4, and the hinge seat on the connecting rod 3 and the hinge block on the clamp 4 are hinged together.
[0050] Furthermore, the stabilizing components include locking teeth 25 and springs 26. Locking teeth 25 are equidistantly fixed on the inner arc surfaces of the clamps 4 on both sides. Connecting holes are opened between corresponding locking teeth 25 on the inner arc surfaces, and springs 26 are fixedly installed in the connecting holes. In addition to adapting to towers of different diameters, springs 26 can also absorb impact force through elastic deformation when the housing is subjected to external vibration or wind interference, maintain continuous contact between locking teeth 25 and the surface of the tower, prevent the clamps 4 from loosening, and ensure that the housing is stably installed on the tower for a long time.
[0051] Furthermore, the shock absorption assembly includes a sliding ring 6, a spring 7, and a connecting rod 20. Support blocks are fixedly installed on the upper surface of the base plate 5 near the four corners. A connecting rod is fixedly installed between two opposing support blocks. Sliding rings 6 are symmetrically slidably connected to the connecting rod. A spring 7 is fixedly installed between two sliding rings 6 on the same side. The spring 7 and the connecting rod on the base plate 5 are coaxially sleeved. A hinge seat is fixedly installed on the upper surface of the sliding ring 6. The connecting rod 20 is hinged inside the hinge seat.
[0052] The bottom surface of the support base 8 is rectangular and fixedly equipped with four hinge blocks. The other ends of the four connecting rods 20 are respectively hinged to the four hinge blocks on the bottom surface of the support base 8.
[0053] Furthermore, the tilting assembly includes a support base 8, a hydraulic cylinder 21, a piston rod 22, and a limiting shaft 23. Support plates are symmetrically fixedly installed on the upper surface of the support base 8 near both sides. Limiting shafts 23 are symmetrically fixedly installed on the opposite surfaces of the two support plates. A hinge seat is fixedly installed on the upper surface of the support base 8 between the two support plates. The hydraulic cylinder 21 is hinged in the hinge seat. The piston rod 22 is drivenly connected to the hydraulic cylinder 21. A hinge block is fixedly installed on the other end of the piston rod 22.
[0054] The tilting assembly also includes a nest support base 9, on which rotating support plates are symmetrically fixedly installed on the bottom surface of the nest support base 9. Each rotating support plate is provided with an arc groove 24, and a hinge seat is fixedly installed between two rotating support plates on the bottom surface of the nest support base 9.
[0055] The hinge block on piston rod 22 is hinged to the hinge seat at the bottom of the machine nest support 9;
[0056] The limiting shaft 23 and the arc groove 24 are slidably connected. The cooperation between the limiting shaft 23 and the arc groove 24 can control the tilt angle of the nest support 9, preventing excessive tilting from damaging the equipment inside the nest or causing the drone to slip off.
[0057] Furthermore, a support plate 18 is fixedly installed on one side of the upper surface of the nest support base 9, and brackets 29 are symmetrically fixedly installed on both sides of the upper surface of the nest support base 9 corresponding to the support plate 18.
[0058] Support plates are symmetrically fixed to the outer wall of bracket 29 near the support plate 18.
[0059] Furthermore, the nest enclosure mechanism includes a sliding block 16, a lead screw 17, and a motor 19. The lead screw 17 is rotatably connected between two support plates on the bracket 29. The motor 19 is fixedly installed on the bottom surface of the lower support plate of the bracket 29. The output shaft of the motor 19 and the lead screw 17 are coaxially fixedly connected. The sliding block 16 is threadedly connected to the lead screw 17.
[0060] A rotating shaft is fixedly installed on the outer wall of the bracket 29, corresponding to the support plate near the top;
[0061] A rotating shaft is also fixedly installed on one side wall of the sliding block 16.
[0062] Furthermore, the nest enclosure mechanism also includes a sliding enclosure plate 13, a second connecting rod 14, and a third connecting rod 15. Multiple sliding enclosure plates 13 are slidably connected to the bracket 29. A rotating shaft is fixedly installed on the plane of the sliding enclosure plate 13 near the top. An oblong hole is opened on the plane of the sliding enclosure plate 13 corresponding to the bottom of the rotating shaft. The third connecting rod 15 is hinged to the rotating shaft on the bracket 29. The second connecting rod 14 is hinged to the rotating shaft on the sliding block 16, and the second connecting rod 14 and the third connecting rod 15 are cross-hinged.
[0063] The other end of connecting rod 14 is hinged to the rotating shaft on sliding plate 13, and the other end of connecting rod 15 is tangent to and slidably connected to the waist-shaped hole on sliding plate 13.
[0064] Another set of connecting rods 15 and 14 is hinged to the other end of connecting rod 3 and 14. This set of connecting rods 15 and 14 is connected to another sliding panel 13 in the same way. The four-bar linkage design with connecting rods 2 and 3 is not only able to realize the synchronous opening and closing of the sliding panel 13, but also to change the direction and magnitude of the force during the opening and closing process, so as to realize a larger opening and closing action of the sliding panel 13 with a smaller driving force.
[0065] Furthermore, the drone auxiliary components include water outlets 10, charging contacts 11, and magnetic metal sheets 12. Water outlets 10 are equidistantly provided on the side wall of the nest support base 9 facing the support plate 18. Charging contacts 11 are fixedly installed in the middle of the landing plane of the nest support base 9. Magnetic metal sheets 12 are also fixedly installed near the four corners of the landing plane of the nest support base 9. The magnetic metal sheets 12 have strong magnetism and can generate a certain attraction force on the drone during the drone landing process, assisting the drone in accurate positioning, while reducing the impact force of the drone landing and improving the safety and accuracy of the landing.
[0066] Structural Description:
[0067] Support 1: Support 1 is the main support of the UAV nest. A connecting plate is fixed on one side wall for installing the clamping mechanism. It provides basic support for the entire nest and ensures the stability of the nest after it is installed on the tower. It is an important basic part of the nest structure.
[0068] Push plate 2: Push plate 2 is installed on the side wall of the support base 1 with the connecting plate. It is driven by the piston rod 28 of the hydraulic cylinder 27. Inclined waist-shaped holes are opened on both sides of its plane. It is slidably connected to the connecting shaft on the connecting rod 3. It realizes the transmission of the clamp 4 by moving. It is the key transmission component of the clamping mechanism.
[0069] Link 1 3: One end of link 1 3 is hinged to the connecting shaft 1 of support base 1, and the other end is hinged to the connecting shaft 2 of support base 1. The connecting shaft at this end is slidably connected to the waist-shaped hole of push plate 2. By moving push plate 2, link 1 3 is driven to rotate, thereby realizing the clamping or loosening action of clamp 4.
[0070] Clamp 4: Clamp 4 is installed on the transmission assembly. The outer arc surface has a hinge block that is hinged to the connecting rod 3. The inner arc surface is equipped with a stabilizing component. It contacts the iron tower through the locking teeth 25 and the spring 26, which can tightly hug iron towers of different diameters and enhance the stability of the machine nest installation.
[0071] Base plate 5: Base plate 5 is fixed on the upper plane of support base 1 and is the foundation of the nest base mechanism. It has support blocks at its four corners and connecting rods between the support blocks. It is used to install the sliding ring 6 and spring 7 of the shock absorption component, providing a shock absorption foundation structure for the nest.
[0072] Sliding ring 6: Sliding ring 6 is symmetrically slidably connected to the connecting rod of the base plate 5. There is a spring 7 between the two sliding rings 6 on the same side. The upper part of the spring 7 is hinged to the connecting rod 20. By sliding on the connecting rod and acting on the spring 7, the shock absorption function of the machine nest is realized.
[0073] Spring 7: Spring 7 is coaxially sleeved on the connecting rod of the base plate 5 and located between the two sliding rings 6 on the same side. When the drone is vibrated, spring 7 is compressed or extended to absorb the vibration energy. Together with the sliding ring 6 and the connecting rod 20, it effectively reduces the vibration of the drone during take-off and landing.
[0074] Support base 8: The bottom surface of support base 8 has four hinge blocks, which are hinged to the other end of connecting rod 4 20. The support plate of the tilting component, hydraulic cylinder 1 21 and other components are installed on it. It is the intermediate support structure connecting the shock absorption component and the tilting component.
[0075] Nest support 9: Nest support 9 is located above the tilting component. Its bottom surface has a rotating support plate and an arc groove 24, which is slidably connected to the limiting shaft 23. It can be tilted by hydraulic cylinder 21. Its upper surface is equipped with support plate 18, bracket 29, etc., for supporting the UAV and related mechanisms.
[0076] Water outlet 10: Water outlet 10 is equidistantly opened on the side wall of the machine nest support base 9 facing the support plate 18. When the machine nest is tilted by the angle tilting component, rainwater and other water can be discharged from the water outlet 10 to prevent water accumulation in the machine nest and protect the internal equipment.
[0077] Charging contact 11: The charging contact 11 is fixed in the middle of the landing plane of the nest support 9. When the drone lands on the nest, it connects with the drone charging interface to provide charging function for the drone and solve the drone's battery life problem.
[0078] Magnetic conductive metal sheet 12: The magnetic conductive metal sheet 12 is installed at the four corners of the landing plane of the nest support 9. It uses magnetic force to attract the drone, helping the drone to accurately locate the landing position, and at the same time enhances the stability of the nest when the drone lands.
[0079] Sliding enclosure 13: The sliding enclosure 13 slides on the bracket 29. It has a rotating shaft at the top and an oblong hole at the bottom. It is opened and closed through the transmission of connecting rod 3 15 and connecting rod 2 14. It is used to form a drone nest fence to protect the drones and equipment inside the nest.
[0080] Link 2 14: One end of link 2 14 is hinged to the rotating shaft of sliding block 16, and the other end is hinged to the rotating shaft of sliding enclosure 13. It is cross-hinged with link 3 15. When sliding block 16 moves, it drives sliding enclosure 13 to move through link 2 14. It is one of the transmission links of the nest enclosure mechanism.
[0081] Link 3 15: One end of link 3 15 is hinged to the rotating shaft of bracket 29, and the other end is slidably connected to the waist-shaped hole of sliding plate 13. It is cross-hinged with link 2 14 in the middle. By moving the sliding block 16, link 3 15 is driven to rotate, thereby realizing the lifting and lowering of sliding plate 13.
[0082] Sliding block 16: Sliding block 16 is threadedly connected to lead screw 17. A rotating shaft is fixed on one side wall of the sliding block 16 and is hinged to connecting rod 2 14. When motor 19 drives lead screw 17 to rotate, sliding block 16 moves on lead screw 17, thereby driving connecting rod 2 14 and connecting rod 3 15 to move, realizing the opening and closing control of sliding panel 13.
[0083] Lead screw 17: Lead screw 17 is rotatably connected between the two support plates of bracket 29. The output shaft of motor 19 is fixed coaxially with it. The motor 19 drives lead screw 17 to rotate, causing sliding block 16 to move on lead screw 17, thereby realizing the power transmission of the fence mechanism.
[0084] Support plate 18: The support plate 18 is fixed to one side of the upper surface of the nest support base 9 and is used to install components such as bracket 29, providing support for the nest fence mechanism and UAV auxiliary components, and enhancing the stability of the nest structure.
[0085] Motor 19: Motor 19 is installed on the bottom surface of the support plate below bracket 29. The output shaft is coaxially fixed with lead screw 17. It serves as the power source for the nest enclosure mechanism. By driving lead screw 17 to rotate, it moves sliding block 16 and controls the opening and closing of sliding enclosure 13.
[0086] Link 4 20: One end of link 4 20 is hinged to the hinge seat on the upper surface of the sliding ring 6, and the other end is hinged to the hinge block on the bottom surface of the support seat 8. Through the sliding of the sliding ring 6 and its own rotation, in conjunction with the spring 1 7, the shock absorption function of the machine nest is realized.
[0087] Hydraulic cylinder 21: Hydraulic cylinder 21 is hinged in the hinge seat on the upper plane of support seat 8, and the other end of its piston rod 22 is hinged to the bottom of the machine nest support seat 9. By extending and retracting hydraulic cylinder 21, the piston rod 22 is moved, causing the machine nest support seat 9 to tilt around the hinge point.
[0088] Piston rod 22: Piston rod 22 is connected to hydraulic cylinder 21 for transmission, and its other end is hinged to the bottom hinge seat of the machine nest support 9. Under the action of hydraulic cylinder 21, it extends and retracts, causing the machine nest support 9 to tilt, thereby realizing the angle adjustment function.
[0089] Limiting shaft 23: The limiting shaft 23 is symmetrically fixed on the opposite surface of the support plate of the support base 8 and is slidably connected to the arc groove 24 on the rotating support plate of the nest support base 9. When the nest support base 9 is tilted, the limiting shaft 23 slides in the arc groove 24 to limit the tilt range and guide it.
[0090] Arc groove 24: Arc groove 24 is formed on the rotating support plate of the machine nest support 9 and is slidably connected to the limiting shaft 23. When the hydraulic cylinder 21 drives the machine nest support 9 to tilt, the arc groove 24 slides along the limiting shaft 23 to ensure smooth tilting action and limit the angle.
[0091] Clamping teeth 25: Clamping teeth 25 are fixed at equal intervals on the inner arc surfaces of the two clamps 4. When in contact with the surface of the iron tower, clamping teeth 25 are embedded in the iron tower, which enhances the friction between the clamps 4 and the iron tower and the connection stability, and is suitable for iron towers of different diameters.
[0092] Spring 26: Spring 26 is installed in the connecting hole between the two teeth 25 on the inner arc surface of the clamp 4. When the clamp 4 clamps the iron tower, spring 26 is compressed, so that the teeth 25 fit the iron tower surface better, enhancing adaptability and stability.
[0093] Hydraulic cylinder 27: Hydraulic cylinder 27 is fixed on the side wall of the support base 1 with the connecting plate, and is connected to piston rod 28. By extending and retracting hydraulic cylinder 27, piston rod 28 is moved, thereby pushing push plate 2 to achieve the clamping or loosening of clamp 4.
[0094] Piston rod 28: Piston rod 28 is connected to hydraulic cylinder 27, and the other end is fixed to push plate 2. It extends and retracts under the action of hydraulic cylinder 27, driving push plate 2 to move. It is the key transmission component for pushing push plate 2 in the clamping mechanism.
[0095] Support bracket 29: Support bracket 29 is symmetrically fixed on both sides of the support plate 18 on the upper surface of the nest support base 9. Its outer wall has upper and lower symmetrical support plates for installing components such as screw rod 17 and motor 19. It is the support structure of the nest enclosure mechanism.
[0096] Working principle: When the machine nest needs to be installed on the iron tower, hydraulic cylinder 27 is activated, and its piston rod 28 extends to drive the push plate 2 to move. The inclined waist-shaped hole on the push plate 2 slides and engages with the connecting shaft on the connecting rod 3, causing the connecting rod 3 to rotate around the connecting shaft 1 and connecting shaft 2 on the support base 1. This, in turn, drives the clamp 4 to tighten around the iron tower. The locking teeth 25 on the inner arc surface of the clamp 4 contact the surface of the iron tower. The spring 26 between the locking teeth 25 is deformed by pressure, adapting to different diameters of the iron tower, enhancing the stability and adaptability of the clamping, and realizing the firm installation of the machine nest on the iron tower.
[0097] When the drone is preparing to land in the nest, motor 19 drives lead screw 17 to rotate, causing sliding block 16 to move along lead screw 17. Sliding block 16 pushes connecting rod 2 14 and cross-hinged connecting rod 3 15 to move through rotating shaft. Connecting rod 2 14 pulls the rotating shaft at the top of sliding enclosure 13, while connecting rod 3 15 slides along the waist-shaped hole of sliding enclosure 13, so that multiple sliding enclosures 13 unfold synchronously to form a protective fence. During the drone landing, the shock absorption component of the nest base mechanism plays a role. The impact force of the drone landing is transmitted to the nest support seat 9, and then to the sliding ring 6 through connecting rod 4 20. The sliding ring 6 slides on the connecting rod of the base plate 5, compressing spring 1 7. The elastic force of spring 1 7 absorbs the vibration energy, reduces the impact of vibration on the nest and drone, and ensures that the drone lands smoothly.
[0098] When the drone lands on the landing surface of the nest support 9, the magnetic metal plates 12 near the four corners of the landing surface use magnetic force to attract the drone, enabling the drone to be accurately positioned. At the same time, the charging contact 11 in the middle of the landing surface connects with the drone's charging interface to charge the drone. When it is necessary to drain the rainwater from the nest, the hydraulic cylinder 21 is activated, and its piston rod 22 extends or retracts, causing the nest support 9 to rotate around the hinge seat at the bottom. The arc groove 24 on the rotating support plate on the bottom surface of the nest support 9 slides on the limiting shaft 23 on the support 8, limiting the tilt angle of the nest and causing the nest to tilt. The rainwater is drained from the water outlet 10 on the side wall of the support plate 18 facing the nest support 9.
[0099] Although embodiments of the 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 invention, the scope of which is defined by the appended claims and their equivalents.
Claims
1. A compact drone nest suitable for tower mounting, characterized in that, include: Support base (1), the support base (1) is the main support, and a connecting plate is fixedly installed on one side wall of the support base (1); A connecting shaft one is symmetrically fixedly installed on the connecting plate on the support base (1), and a connecting shaft two is also symmetrically fixedly installed on the connecting plate, and the connecting shaft one and the connecting shaft two are inclined. A clamping mechanism is provided on the connecting plate of the support base (1). The clamping mechanism includes a transmission component and a clamp (4). A transmission component is provided on the connecting plate and the connecting shaft of the support base (1). A clamp (4) is installed on the transmission component. A stabilizing component is provided on the inner arc surface of the clamp (4). The upper surface of the support base (1) is fixedly provided with a nest base mechanism, which includes a shock-absorbing component and an angle tilting component. A base plate (5) is fixedly installed on the upper surface of the support base (1), and a shock-absorbing component is provided on the base plate (5). An angle tilting component is provided on the shock-absorbing component. An organic nesting fence mechanism and a drone-assisted component are disposed above the tilting component.
2. A compact UAV nest suitable for tower installation according to claim 1, characterized in that, The transmission assembly includes a push plate (2), a connecting rod (3), a hydraulic cylinder (27), and a piston rod (28). The support base (1) is also fixedly mounted on the side wall of the connecting plate. The hydraulic cylinder (27) is connected to the piston rod (28) via transmission. The other end of the piston rod (28) is fixedly mounted on the push plate (2). The plane of the push plate (2) is symmetrically provided with inclined waist-shaped holes near the two side walls. One end of the connecting rod (3) is hinged to the connecting shaft on the support base (1). The connecting shaft on the connecting rod (3) is also fixedly mounted on this end. The connecting shaft on the connecting rod (3) is tangent to and slidably connected to the waist-shaped hole on the push plate (2). The connecting shaft on the support base (1) is hinged to the connecting rod (3) near the other end. A hinge seat is fixedly installed on the other end of the connecting rod (3).
3. A compact UAV nest suitable for tower installation according to claim 2, characterized in that, A hinge block is fixedly installed at the middle of the outer arc surface of the clamp (4), and the hinge seat on the connecting rod (3) and the hinge block on the clamp (4) are hinged together.
4. A compact UAV nest suitable for tower installation according to claim 3, characterized in that, The stabilizing component includes a locking tooth (25) and a second spring (26). The locking teeth (25) are fixedly installed at equal intervals on the inner arc surfaces of the clamps (4) on both sides. A connecting hole is opened between two locking teeth (25) on the inner arc surface, and a second spring (26) is fixedly installed in the connecting hole.
5. A compact UAV nest suitable for tower installation according to claim 1, characterized in that, The shock absorption assembly includes a sliding ring (6), a spring (7), and a connecting rod (20). Support blocks are fixedly installed on the upper surface of the base plate (5) near the four corners. A connecting rod is fixedly installed between two opposing support blocks. Sliding rings (6) are symmetrically slidably connected to the connecting rod. Springs (7) are fixedly installed between the two sliding rings (6) on the same side. Springs (7) and the connecting rod on the base plate (5) are coaxially sleeved. A hinge seat is fixedly installed on the upper surface of the sliding ring (6). Connecting rod (20) is hinged in the hinge seat. The bottom surface of the support base (8) is rectangular and fixedly equipped with four hinge blocks. The other ends of the four connecting rods (20) are respectively hinged to the four hinge blocks on the bottom surface of the support base (8).
6. A compact UAV nest suitable for tower installation according to claim 5, characterized in that, The tilting assembly includes a support base (8), a hydraulic cylinder (21), a piston rod (22), and a limiting shaft (23). Support plates are symmetrically fixedly installed on the upper surface of the support base (8) near both sides. Limiting shafts (23) are symmetrically fixedly installed on the opposite surfaces of the two support plates. A hinge seat is fixedly installed on the upper surface of the support base (8) between the two support plates. A hydraulic cylinder (21) is hinged in the hinge seat. A piston rod (22) is driven and connected to the hydraulic cylinder (21). A hinge block is fixedly installed on the other end of the piston rod (22). The tilting assembly also includes a nest support base (9), on which rotating support plates are symmetrically fixedly installed. Each rotating support plate is provided with an arc groove (24). A hinge seat is fixedly installed between the two rotating support plates on the bottom surface of the nest support base (9). The hinge block on the piston rod (22) is hinged to the hinge seat at the bottom of the machine nest support (9); The limiting shaft (23) and the arc groove (24) are slidably connected.
7. A compact UAV nest suitable for tower installation according to claim 6, characterized in that, A support plate (18) is fixedly installed on the upper surface of the nest support base (9) at one side, and brackets (29) are symmetrically fixedly installed on the upper surface of the nest support base (9) on both sides of the support plate (18). Support plates are symmetrically fixedly installed on the outer wall of the bracket (29) near the support plate (18).
8. A compact UAV nest suitable for tower installation according to claim 7, characterized in that, The nest enclosure mechanism includes a sliding block (16), a lead screw (17), and a motor (19). The lead screw (17) is rotatably connected between two support plates on the bracket (29). The motor (19) is fixedly installed on the bottom surface of the lower support plate of the bracket (29). The output shaft of the motor (19) and the lead screw (17) are coaxially fixedly connected. The sliding block (16) is threaded onto the lead screw (17). A rotating shaft is fixedly installed on the outer wall of the bracket (29) corresponding to the support plate near the top; A rotating shaft is also fixedly installed on one side wall of the sliding block (16).
9. A compact UAV nest suitable for tower installation according to claim 8, characterized in that, The nest enclosure mechanism also includes a sliding enclosure plate (13), a second connecting rod (14), and a third connecting rod (15). Multiple sliding enclosure plates (13) are slidably connected to the bracket (29). A rotating shaft is fixedly installed on the plane of the sliding enclosure plate (13) near the top. A waist-shaped hole is opened on the plane of the sliding enclosure plate (13) corresponding to the bottom of the rotating shaft. The third connecting rod (15) is hinged to the rotating shaft on the bracket (29). The second connecting rod (14) is hinged to the rotating shaft on the sliding block (16). The second connecting rod (14) and the third connecting rod (15) are cross-hinged. The other end of the second connecting rod (14) is hinged to the rotating shaft on the sliding enclosure (13), and the other end of the third connecting rod (15) is tangent to and slidably connected to the waist-shaped hole on the sliding enclosure (13); Another set of the third (15) and the second (14) is hinged to the other end of the third (15) and the second (14), and this set of the third (15) and the second (14) is connected to another sliding panel (13) in the same way.
10. A compact UAV nest suitable for tower installation according to claim 7, characterized in that, The drone auxiliary components include a water outlet (10), a charging contact (11), and a magnetic metal sheet (12). The drone nest support base (9) has water outlets (10) equidistantly spaced on the side wall facing the support plate (18). The charging contact (11) is fixedly installed in the middle of the landing plane of the drone nest support base (9). The magnetic metal sheet (12) is also fixedly installed near the four corners of the landing plane of the drone nest support base (9).