Unmanned aerial vehicle carrying device
Through the design of the sliding arm and self-locking mechanism, the automatic adjustment and fixation of the drone on the mounting platform is solved, and the problem of unstable drop and landing in harsh environments is improved, and the landing accuracy and safety are improved.
Patent Information
- Application Number
- CN202422795779.2
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-18
- Publication Date
- 2025-08-19
- Estimated Expiration
- 2034-11-18
AI Technical Summary
When existing drone-mounted devices descend in harsh environments, the landing accuracy is insufficient, which can easily lead to the drone rollover and affect transportation safety.
The design of sliding arms, sliding blocks, motors, connecting blocks, shrink rods, extension rods and self-locking mechanisms is adopted. Through sliding and self-locking mechanisms, the automatic adjustment and fixing of the drone is achieved to ensure landing accuracy and stability.
The drone can be automatically adjusted to the designated position and firmly fixed, improving the accuracy and safety of landing and avoiding the risk of drone rolling over in harsh environments.
Smart Images

Figure CN223237999U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of unmanned aerial vehicles (UAVs), and in particular to a UAV carrying device. Background Art
[0002] Drones are widely used in reality, and play a significant role in daily life, military operations, agriculture and other scenarios. Drones generally have a certain range of use and route distance when in use. At this time, it is necessary to use equipment that can carry drones to send the drones to the designated location.
[0003] After searching, Chinese patent announcement number: CN220974595U discloses a drone technology for a drone carrying device, including a drone, the drone is provided with a tripod; a carrying platform for carrying the drone; a mobile carrier for installing the carrying platform and driving the carrying platform to move; a carrying seat is provided on the carrying platform, a telescopic lock is provided on the carrying seat, one end of the telescopic lock extends to form a locking part, and a lock that cooperates with the lock is provided on the tripod. The utility model provides a telescopic lock that cooperates with the tripod on the carrying seat, so that the drone can be firmly limited on the carrying platform, effectively preventing the drone from accidentally loosening. When the drone descends to the carrying platform, the locking part extends and abuts against the top of the locking rod, ensuring the stable limitation of the drone during transportation, and improving the transportation safety and reliability of the drone carrying device.
[0004] When the above device is in use, the guide slope at the top of the platform provides guidance for the drone during landing, thereby reducing the accuracy of the drone's landing. However, using this method, if the drone encounters a more severe environment during landing, the deviation of the drone during landing will be greater, and the bottom bracket part of the drone will directly contact the top of the guide slope during landing, and the drone will roll over. Therefore, a drone carrying device is proposed to solve the above problem. Utility Model Content
[0005] In order to make up for the above shortcomings, the utility model provides a UAV carrying device, which aims to improve the problem of unstable landing of UAVs due to other factors during landing in the prior art.
[0006] In order to achieve the above-mentioned purpose, the present invention adopts the following technical solutions: a UAV carrying device, comprising a carrying platform, a UAV is arranged on the upper part of the carrying platform, the UAV includes a landing bracket, the inner wall of the carrying platform is provided with a slide groove, the inner wall of the slide groove is slidably connected with a sliding block, the outer wall of the sliding block is fixedly connected with a sliding arm, the outer wall of the sliding arm is slidably connected with a connecting block, the connecting blocks are provided with two groups, the lower end of one group of connecting blocks is fixedly connected with a retracting rod, and the lower end of the other group of connecting blocks is fixedly connected with an extending rod, the inner wall of the retracting rod is slidably connected to the outer wall of the extending rod, and the outer walls of the retracting rod and the extending rod are both provided with a self-locking mechanism.
[0007] As a further description of the above technical solution:
[0008] The upper end of the landing bracket is fixedly connected to the drone body, and the lower end of the landing bracket is in contact with the upper end of the carrying platform.
[0009] As a further description of the above technical solution:
[0010] The outer wall of the connecting block is fixedly connected to a motor, the inner wall of the connecting block is rotatably connected to a pulley, and the outer wall of the pulley is slidably connected to the outer wall of the sliding arm.
[0011] As a further description of the above technical solution:
[0012] The outer wall of the sliding block is fixedly connected to a rack, the outer wall of the rack is meshed with a gear, the outer wall of the gear is rotatably connected to the outer wall of the carrying platform, and the motor is provided with two groups, the output end of one group of motors is fixedly connected to the outer wall of the pulley, and the output end of the other group of motors is fixedly connected to the gear.
[0013] As a further description of the above technical solution:
[0014] The self-locking mechanism includes a protrusion, and the protrusions are provided in two groups. The outer wall of the protrusions in one group is fixedly connected to the outer wall of the retracted rod, and the outer wall of the protrusions in the other group is fixedly connected to the outer wall of the extension rod. The inner wall of the protrusion is rotatably connected to a locking plate, and the locking plate is elastically connected to the protrusion through a spring.
[0015] As a further description of the above technical solution:
[0016] One end of the spring is fixedly connected to the outer wall of the lock plate, and the other end of the spring is fixedly connected to the inner wall of the protrusion.
[0017] As a further description of the above technical solution:
[0018] The inner wall of the protrusion is slidably connected to a self-locking block, the inner wall of the protrusion is fixedly connected to a steering shaft, the outer wall of the steering shaft is slidably connected to a pull rope, the locking plate is connected to the self-locking block through the pull rope, and the outer wall of the landing bracket is in contact with the left outer wall of the self-locking block.
[0019] As a further description of the above technical solution:
[0020] One end of the pull rope is fixedly connected to the outer wall of the locking plate, and the other end of the pull rope is fixedly connected to the right outer wall of the self-locking block.
[0021] The utility model has the following beneficial effects:
[0022] 1. In the present invention, through the design of the sliding arm, sliding block, motor, connecting block retractable rod, pulley, roller, slide groove and extension rod, the position of the drone can be actively adjusted and fixed after landing, and the required accuracy of the landing position of the drone is more relaxed. The drone only needs to land on the carrying platform slot to adjust and fix the drone.
[0023] 2. In the present invention, the self-locking mechanism is designed so that after the position of the drone is fixed, the self-locking block pulls the pull rope to rotate the lock plate to fix the drone landing bracket, making the device more effective in fixing the drone. BRIEF DESCRIPTION OF THE DRAWINGS
[0024] Figure 1 This is a schematic diagram of the main structure of a UAV carrying device proposed in the utility model;
[0025] Figure 2 A schematic diagram of a drone carrying device proposed in the present invention;
[0026] Figure 3 This is a schematic diagram of a sliding block of a UAV carrying device proposed in the present invention;
[0027] Figure 4 This is a schematic diagram of the connection blocks of a UAV carrying device proposed in the present invention;
[0028] Figure 5 This is a schematic diagram of an extension rod of a UAV carrying device proposed in the present invention;
[0029] Figure 6 This is a schematic diagram of the self-locking mechanism of the drone carrying device proposed in the utility model.
[0030] Legend:
[0031] 1. Carrying platform; 2. UAV body; 3. Landing bracket; 4. Sliding arm; 5. Sliding block; 6. Motor; 7. Connecting block; 8. Retracting rod; 9. Pulley; 10. Rack; 11. Slide; 12. Extension rod; 13. Bump; 14. Locking plate; 15. Self-locking block; 16. Pull rope; 17. Steering shaft; 18. Spring; 19. Gear. DETAILED DESCRIPTION
[0032] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.
[0033] Reference Figure 1 - Figure 3 The utility model provides an embodiment: a UAV carrying device, including a carrying platform 1, which is a prior art. The carrying platform 1 can be used to carry a UAV and can bring the UAV to a designated area. A UAV is provided on the upper part of the carrying platform 1. The UAV includes a landing bracket 3. The upper end of the landing bracket 3 is fixedly connected to a UAV body 2. The UAV is a prior art. The UAV body 2 includes a spiral blade, a drive motor, a control device, etc. The lower end of the landing bracket 3 contacts the upper end of the carrying platform 1, so that the landing bracket 3 is raised when the UAV lands. To provide a supporting effect, a slide groove 11 is provided on the inner wall of the carrying platform 1, and a sliding block 5 is slidably connected to the inner wall of the slide groove 11. The slide groove 11 is engaged with the rear end protrusion of the sliding block 5 and can slide on the inner wall of the slide groove 11 to provide a guiding effect. The outer wall of the sliding block 5 is fixedly connected to the sliding arm 4. The sliding block 5 moves inward to tighten the sliding arms 4 on both sides. The tightening of the sliding arms 4 will adjust the drone to a horizontal state after landing on the carrying platform 1. The outer wall of the sliding arm 4 is slidably connected to the connecting block 7. The retracting rod 8 and the extending rod 12 are relatively fixed to the sliding arm 4 through the connecting block 7 to provide a fixing effect.
[0034] Reference Figure 2 、 Figure 5 , there are two groups of connecting blocks 7. The lower end of one group of connecting blocks 7 is fixedly connected to the retracting rod 8, and the lower end of the other group of connecting blocks 7 is fixedly connected to the extending rod 12. The inner wall of the retracting rod 8 is slidably connected to the outer wall of the extending rod 12. When the sliding arms 4 on both sides move inward, the extending rod 12 will be driven to retract and retract on the inner wall of the retracting rod 8. The connecting block 7 drives the extending rod 12 and the retracting rod 8 to move inward, so that the drone moves to the designated position after landing. The outer walls of the retracting rod 8 and the extending rod 12 are both provided with a self-locking mechanism. The self-locking mechanism will self-lock when the connecting block 7 moves to make the self-locking block 15 contact the landing bracket 3, thereby providing a fixing effect for the drone.
[0035] Reference Figure 2 、 Figure 4 The outer wall of the connecting block 7 is fixedly connected to the motor 6. The motor 6 and the motor 6 are the existing technology and can drive the output end connection part to rotate. The inner wall of the connecting block 7 is rotatably connected to the pulley 9. The outer wall of the pulley 9 is made of rubber material with large friction, so that the pulley 9 will not slip and idle when sliding on the sliding arm 4. The output end of the motor 6 is fixedly connected to the outer wall of the pulley 9, so that the motor 6 drives the pulley 9 to rotate. The outer wall of the pulley 9 is slidably connected to the outer wall of the sliding arm 4, so that the rotation of the pulley 9 will drive the connecting block 7 to move on the sliding arm 4.
[0036] refer to Figure 3 The outer wall of the sliding block 5 is fixedly connected to a rack 10. The rack 10 has two groups, an upper group and an lower group, and the two groups of racks 10 are in opposite directions. The outer wall of the rack 10 is engaged with a gear 19. The rotation of the gear 19 will cause the upper and lower racks 10 to move in opposite directions, causing the sliding block 5 to shrink. The outer wall of the gear 19 is rotatably connected to the outer wall of the carrying platform 1. The output end of another group of motors 6 is fixedly connected to the gear 19, and the motor 6 will drive the gear to rotate.
[0037] refer to Figure 2 、 Figure 6The self-locking mechanism includes a protrusion 13, which is provided with two groups. The outer wall of one group of protrusions 13 is fixedly connected to the outer wall of the retracted rod 8, and the outer wall of the other group of protrusions 13 is fixedly connected to the outer wall of the extension rod 12, so that the extension rod 12 and the retracted rod 8 provide a fixing effect for the protrusion 13, and the inner wall of the protrusion 13 is rotatably connected with a locking plate 14. When the lock plate 14 is rotated to a vertical position, it will be stuck with the protrusion 13 to provide a fixing effect for the landing bracket 3, and the lock plate 14 is elastically connected to the protrusion 13 by a spring 18. One end of the spring 18 is fixedly connected to the outer wall of the lock plate 14, and the other end of the spring 18 is fixedly connected to the inner wall of the protrusion 13 when no external force is applied. The spring 18 will cause the lock plate 14 to rotate to a horizontal position. When the lock plate 14 is pulled by the pull rope 16, the lock plate 14 will be vertical, and the inner wall of the protrusion 13 is slidably connected with a self-locking block 15, which is on the inner wall of the protrusion 13 The sliding movement laterally causes the protrusion 13 to provide a guiding effect on the self-locking block 15. The inner wall of the protrusion 13 is fixedly connected to a steering shaft 17. The steering shaft 17 is provided with multiple groups. The steering shaft 17 can change the force direction of the pull rope 16, so that the pulling effect on the lock plate 14 is more stable when the pull rope 16 is pulled. The steering shaft 17 prevents the pull rope 16 from directly contacting and wearing the inner wall of the protrusion 13. The outer wall of the pull rope 16 is slidably connected to the outer wall of the steering shaft 17. The lock plate 14 is connected to the self-locking block 15 through the pull rope 16. One end of the pull rope 16 is fixedly connected to the outer wall of the lock plate 14, and the other end of the pull rope 16 is fixedly connected to the right outer wall of the self-locking block 15. After the self-locking block 15 contacts the landing bracket 3, it will cause the self-locking block 15 to slide toward the inside of the protrusion 13, and the outer wall of the landing bracket 3 contacts the left outer wall of the self-locking block 15. The inward movement of the self-locking block 15 will pull the pull rope 16, and the pull rope 16 will pull the lock plate 14 to rotate.
[0038] Working principle: After the drone lands, if the drone is fixed on the carrying platform 1, after the drone lands on the carrying platform 1, the motor 6 drives the gear 19 to rotate, causing the upper and lower racks 10 to contract and drive the sliding block 5 to move, while driving the sliding arm 4 to contract inward, and at the same time causing the extension rod 12 to contract toward the inner wall of the retracted rod 8. The sliding arm 4 will correct the drone to make it parallel, and then the motor 6 will drive the pulley 9 to rotate, causing the connecting block 7 to move inward, which will drive the extension rod 12 and the retracted rod 8 to move. When it contacts the landing bracket 3, it will drive the drone to the center and fix the drone.
[0039] After the drone reaches the designated position, it needs to be fixed. When the landing bracket 3 at the bottom of the drone contacts the self-locking block 15, it will push the self-locking block 15 to slide inward of the protrusion 13. The self-locking block 15 will pull the pull rope 16, and the guidance of the steering shaft 17 can more stably drive the locking plate 14 to rotate. When the locking plate 14 rotates to a vertical position, it will be stuck with the protrusion 13 to fix the landing bracket 3.
[0040] When the drone is to be used, the motor 6 is rotated in the reverse direction, at which time the self-locking block 15 will release its contact with the landing bracket 3 , and the locking plate 14 will return to a horizontal position driven by the spring 18 to release the fixing effect.
[0041] Finally, it should be noted that the above is only a preferred embodiment of the present invention and is not intended to limit the present invention. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art can still modify the technical solutions described in the aforementioned embodiments or make equivalent replacements for some of the technical features therein. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention should be included in the scope of protection of the present invention.
Claims
1. A UAV carrying device, comprising a carrying platform (1), characterized in that: A drone is provided on the upper portion of the carrying platform (1), and the drone includes a landing bracket (3). A slide groove (11) is provided on the inner wall of the carrying platform (1), and a sliding block (5) is slidably connected to the inner wall of the slide groove (11), and the outer wall of the sliding block (5) is fixedly connected to the sliding arm (4), and the outer wall of the sliding arm (4) is slidably connected to the connecting block (7). The connecting blocks (7) are provided in two groups, and the lower end of one group of the connecting blocks (7) is fixedly connected to the retracting rod (8), and the lower end of the other group of the connecting blocks (7) is fixedly connected to the extending rod (12). The inner wall of the retracting rod (8) is slidably connected to the outer wall of the extending rod (12), and the outer walls of the retracting rod (8) and the extending rod (12) are both provided with self-locking mechanisms.
2. The UAV carrying device according to claim 1, characterized in that: The upper end of the landing bracket (3) is fixedly connected to the drone body (2), and the lower end of the landing bracket (3) is in contact with the upper end of the carrying platform (1).
3. The UAV carrying device according to claim 1, characterized in that: The outer wall of the connecting block (7) is fixedly connected to the motor (6), the inner wall of the connecting block (7) is rotatably connected to the pulley (9), and the outer wall of the pulley (9) is slidably connected to the outer wall of the sliding arm (4).
4. The UAV carrying device according to claim 3, characterized in that: The outer wall of the sliding block (5) is fixedly connected to a rack (10), the outer wall of the rack (10) is meshed with a gear (19), the outer wall of the gear (19) is rotatably connected to the outer wall of the carrying platform (1), and the motor (6) is divided into two groups, the output end of one group of the motor (6) is fixedly connected to the outer wall of the pulley (9), and the output end of the other group of the motor (6) is fixedly connected to the gear (19).
5. The UAV carrying device according to claim 1, characterized in that: The self-locking mechanism includes a protrusion (13), and the protrusion (13) is provided in two groups. The outer wall of the protrusion (13) of one group is fixedly connected to the outer wall of the retracting rod (8), and the outer wall of the protrusion (13) of the other group is fixedly connected to the outer wall of the extending rod (12). The inner wall of the protrusion (13) is rotatably connected to a locking plate (14), and the locking plate (14) is elastically connected to the protrusion (13) through a spring (18).
6. The UAV carrying device according to claim 5, characterized in that: One end of the spring (18) is fixedly connected to the outer wall of the lock plate (14), and the other end of the spring (18) is fixedly connected to the inner wall of the protrusion (13).
7. The UAV carrying device according to claim 5, characterized in that: The inner wall of the protrusion (13) is slidably connected to a self-locking block (15), the inner wall of the protrusion (13) is fixedly connected to a steering shaft (17), the outer wall of the steering shaft (17) is slidably connected to a pull rope (16), the locking plate (14) is connected to the self-locking block (15) via the pull rope (16), and the outer wall of the landing bracket (3) is in contact with the left outer wall of the self-locking block (15).
8. The drone carrying device according to claim 7, characterized in that: One end of the pull rope (16) is fixedly connected to the outer wall of the locking plate (14), and the other end of the pull rope (16) is fixedly connected to the right outer wall of the self-locking block (15).
Citation Information
Patent Citations
Drone carrying device
CN220974595U