Lifting holder for monitoring unmanned aerial vehicle probe
By designing a lifting gimbal for drones and using quick disassembly and reinforcement components, the problem of difficulty in disassembly and assembly of drones is solved, and rapid disassembly and assembly and fixation is achieved, improving user experience and usage effect.
Patent Information
- Application Number
- CN202421827513.5
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-07-31
- Publication Date
- 2025-06-24
- Estimated Expiration
- 2034-07-31
AI Technical Summary
It is very difficult to disassemble and assemble the drone gimbal, which makes it possible to become a whole and the drone need to be sent to repair the drone, which leads to long repair time and difficulty in repairing, and it is inconvenient for users to replace the gimbal.
A lifting gimbal for monitoring UAV probes was designed, using quick disassembly and reinforcement components. Through the sliding of the push and pull rod and the displacement of the snap, the rapid disassembly and assembly and fixation of the gimbal was achieved.
The rapid disassembly and assembly of the gimbal is realized, reducing the maintenance time of the maintenance personnel. Users can manually replace the gimbal by themselves, improving the user experience and usage effect.
Smart Images

Figure CN223014919U_ABST
Abstract
Description
Technical Field
[0001] The utility model belongs to the technical field of UAV gimbals, and particularly relates to a lifting gimbal for monitoring the probe of a UAV. Background Art
[0002] A UAV gimbal is a support device used for installing and fixing monitoring devices or loading other devices on a UAV, and at the same time has the function of stabilizing images when the UAV moves, and has corresponding control functions for some devices.
[0003] Since the development of UAVs to date, they have been applied in various fields. Due to different application fields and functions, UAV gimbals are designed with different structures. However, no matter how their structures change, the disassembly and assembly of UAV gimbals are very difficult, making the gimbal and the UAV an integral whole. This requires sending the UAV for repair together, resulting in a long repair time and difficult repair of the UAV gimbal. At the same time, it is also inconvenient for users to replace the gimbal. Content of the Utility Model
[0004] The purpose of the utility model is to solve the problems that since the development of UAVs to date, they have been applied in various fields. Due to different application fields and functions, UAV gimbals are designed with different structures. However, no matter how their structures change, the disassembly and assembly of UAV gimbals are very difficult, making the gimbal and the UAV an integral whole. This requires sending the UAV for repair together, resulting in a long repair time and difficult repair of the UAV gimbal. At the same time, it is also inconvenient for users to replace the gimbal, and a lifting gimbal for monitoring the probe of a UAV is proposed.
[0005] To achieve the above purpose, the utility model adopts the following technical scheme: a lifting gimbal for monitoring the probe of a UAV, including an external fixing frame, a steering arm is rotatably installed on the inner wall of the external fixing frame, a telescopic rod is arranged on the steering arm, a quick-release component is arranged at the top of the telescopic rod, and a reinforcement component is arranged at the top of the quick-release component.
[0006] As a further description of the above technical scheme:
[0007] The steering arm includes a vertical steering arm, the vertical steering arm is fixedly installed on the outer wall of the external fixing frame, the top of the vertical steering arm is fixedly installed with a horizontal steering shaft, and the telescopic rod is rotatably installed on the top of the horizontal steering shaft.
[0008] As a further description of the above technical scheme:
[0009] The quick-release component includes a fixed disk, the fixed disk is fixedly installed at the top of the telescopic rod, an outer ring is fixedly installed on the top of the fixed disk, a telescopic hole is arranged on the side wall of the outer ring, and a push-pull rod is clamped and installed on the inner wall of the telescopic hole.
[0010] As a further description of the above technical solution:
[0011] One end of the push rod is fixedly installed with a first buckle and a second buckle, and a first spring telescopic rod is fixedly installed on the outer walls of the first buckle and the second buckle.
[0012] As a further description of the above technical solution:
[0013] The reinforcement component includes a spiral housing, and a second spring telescopic rod is fixedly installed on the inner wall of the spiral housing.
[0014] As a further description of the above technical solution:
[0015] The bottom end of the second spring telescopic rod is fixedly installed with a fixing plate, and the inner wall of the spiral housing is provided with a thread and an installation groove.
[0016] In summary, due to the adoption of the above technical solution, the beneficial effects of the present utility model are as follows:
[0017] 1. In the present utility model, by providing a quick-release component, before installation, the push rod is pulled to fit the inner wall of the outer ring. At this time, the fixing plate is placed at the bottom of the first buckle and the second buckle, and then the push rod is released, so that the first buckle and the second buckle clamp the fixing plate at the bottom. During installation, the push rod moves inward, driving the first buckle to move inward to the installation groove, and the second buckle on the other side also moves inward. At this time, the first buckle and the second buckle clamp the fixing plate tightly and fit the second spring telescopic rod. The first spring telescopic rod is compressed to the limit, and the push rod reaches the top dead center. At this time, the installation of the pan-tilt is completed. The disassembly is the same. Through this design, the disassembly and assembly are effectively realized simply and quickly, reducing the maintenance time of maintenance personnel, and also enabling users to manually replace the pan-tilt by themselves to improve the user experience, and the use effect is good.
[0018] 2. In the present utility model, by providing a reinforcement component, when installing, the push rod is clamped into the installation groove, and the push rod slides in the installation groove, thereby driving the quick-release component to move upward. The inside of the spiral housing is a trapezoidal spiral hole, so while moving upward, the push rod will move inward. The push rod drives the first buckle to move inward, and as the first buckle moves, the first spring telescopic rod is compressed. When the first spring telescopic rod is compressed to the limit, the push rod reaches the top dead center, and the fixation of the pan-tilt is completed. Through this design, on the basis of quick release, the fixing effect is effectively ensured to be good, and there will be no shaking to affect the normal operation of the functions of the peripheral components, and the use effect is good. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] Figure 1 It is a three-dimensional structural schematic diagram of a lifting pan-tilt for monitoring a drone probe.
[0020] Figure 2It is an exploded three-dimensional structure diagram of a lifting pan-tilt for monitoring the probe of a drone.
[0021] Figure 3 It is an exploded three-dimensional structure diagram of the reinforcement group of a lifting pan-tilt for monitoring the probe of a drone.
[0022] Figure 4 It is a schematic diagram of the spiral housing structure of a lifting pan-tilt for monitoring the probe of a drone.
[0023] Legend Explanation:
[0024] 1. Peripheral fixed frame; 2. Steering arm; 21. Vertical steering arm; 22. Horizontal steering shaft; 3. Quick-release component; 31. Push-pull rod; 32. First buckle; 33. First spring telescopic rod; 34. Telescopic hole; 35. Fixed disk; 36. Outer ring; 37. Second buckle; 4. Reinforcement component; 41. Spiral housing; 42. Second spring telescopic rod; 43. Fixed plate; 44. Thread; 45. Installation groove; 5. Telescopic rod. Specific Embodiment
[0025] Next, the technical solutions in the embodiments of the present invention will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without making creative efforts fall within the protection scope of the present invention.
[0026] Please refer to Figures 1-4 , the present invention provides a technical solution: a lifting pan-tilt for monitoring the probe of a drone, including a peripheral fixed frame 1, a steering arm 2 is rotatably installed on the inner wall of the peripheral fixed frame 1, a telescopic rod 5 is arranged on the steering arm 2, a quick-release component 3 is arranged at the top of the telescopic rod 5, and a reinforcement component 4 is arranged at the top of the quick-release component 3;
[0027] The quick-release component 3 includes a fixed disk 35, the fixed disk 35 is fixedly installed on the top of the telescopic rod 5, an outer ring 36 is fixedly installed on the top of the fixed disk 35, a telescopic hole 34 is arranged on the side wall of the outer ring 36, a push-pull rod 31 is clamped and installed on the inner wall of the telescopic hole 34, a first buckle 32 and a second buckle 37 are fixedly installed at one end of the push-pull rod 31, and a first spring telescopic rod 33 is fixedly installed on the outer walls of the first buckle 32 and the second buckle 37;
[0028] The specific implementation method is as follows: During installation, the push rod 31 is snapped into the installation groove 45, and the push rod 31 slides within the installation groove 45, thereby driving the quick-release assembly 3 to move upward. The interior of the spiral housing 41 is a trapezoidal spiral hole. Therefore, while moving upward, the push rod 31 will move inward. The push rod 31 drives the first buckle 32 to move inward. As the first buckle 32 moves, the first spring telescopic rod 33 is compressed. When the first spring telescopic rod 33 is compressed to the limit, the push rod 31 reaches the top dead center, and at this time, the installation of this pan-tilt is completed.
[0029] The reinforcement assembly 4 includes a spiral housing 41. A second spring telescopic rod 42 is fixedly installed on the inner wall of the spiral housing 41. The bottom end of the second spring telescopic rod 42 is fixedly installed with a fixing plate 43. A thread 44 and an installation groove 45 are provided on the inner wall of the spiral housing 41;
[0030] The specific implementation method is as follows: Before installation, the push rod 31 is pulled to fit the inner wall of the outer ring 36. At this time, the fixing plate 43 is placed at the bottom of the first buckle 32 and the second buckle 37. Then the push rod 31 is released, so that the first buckle 32 and the second buckle 37 clamp the fixing plate 43 at the bottom. During installation, the push rod 31 moves inward, driving the first buckle 32 to move inward, and the second buckle 37 on the other side also moves inward. At this time, the first buckle 32 and the second buckle 37 clamp the fixing plate 43 tightly and fit the second spring telescopic rod 42, completing the fixation of this pan-tilt.
[0031] Working principle: During installation, the push rod 31 is snapped into the installation groove 45, and the push rod 31 slides within the installation groove 45, thereby causing the push rod 31 to move upward. The push rod 31 drives the outer ring 36 to move upward through the telescopic hole 34, driving the first buckle 32 to move upward. The first buckle 32 drives the first spring telescopic rod 33 to move upward. The interior of the spiral housing 41 is a trapezoidal spiral hole. Therefore, while moving upward, the push rod 31 will move inward. The push rod 31 drives the first buckle 32 to move inward. As the first buckle 32 moves, the first spring telescopic rod 33 is compressed. When the first spring telescopic rod 33 is compressed to the limit, the push rod 31 reaches the top dead center, and at this time, the installation of this pan-tilt is completed. Before installation, the push rod 31 is pulled to fit the inner wall of the outer ring 36. At this time, the fixing plate 43 is placed at the bottom of the first buckle 32 and the second buckle 37. Then the push rod 31 is released, so that the first buckle 32 and the second buckle 37 clamp the fixing plate 43 at the bottom. During installation, the push rod 31 moves inward, driving the first buckle 32 to move inward, and the second buckle 37 on the other side also moves inward. At this time, the first buckle 32 and the second buckle 37 clamp the fixing plate 43 tightly and fit the second spring telescopic rod 42, completing the fixation of this pan-tilt.
[0032] The above are only the preferred specific embodiments of the present utility model, but the protection scope of the present utility model is not limited thereto. Any person skilled in the art within the technical scope disclosed by the present utility model, according to the technical solution and the inventive concept of the present utility model, making equivalent substitutions or changes, shall be covered by the protection scope of the present utility model.
Claims
1. A lifting platform for monitoring a drone probe, comprising an external fixing frame (1), characterized in that: A steering arm (2) is rotatably mounted on the inner wall of the external fixing frame (1); a telescopic rod (5) is arranged on the steering arm (2); a quick-release assembly (3) is arranged at the top of the telescopic rod (5); and a reinforcement assembly (4) is arranged at the top of the quick-release assembly (3).
2. The lifting platform for monitoring drone probe according to claim 1 is characterized in that: The steering arm (2) comprises a vertical steering arm (21), the vertical steering arm (21) is fixedly mounted on the outer wall of the external fixing frame (1), a horizontal steering shaft (22) is fixedly mounted on the top of the vertical steering arm (21), and a telescopic rod (5) is rotatably mounted on the top of the horizontal steering shaft (22).
3. The lifting platform for monitoring drone probe according to claim 2 is characterized in that: The quick-release assembly (3) comprises a fixed plate (35), wherein the fixed plate (35) is fixedly mounted on the top of the telescopic rod (5), an outer ring (36) is fixedly mounted on the top of the fixed plate (35), a telescopic hole (34) is provided on the side wall of the outer ring (36), and a push-pull rod (31) is clamped and mounted on the inner wall of the telescopic hole (34).
4. The lifting platform for monitoring drone probe according to claim 3 is characterized in that: A first buckle (32) and a second buckle (37) are fixedly mounted on one end of the push-pull rod (31), and a first spring telescopic rod (33) is fixedly mounted on the outer walls of the first buckle (32) and the second buckle (37).
5. The lifting platform for monitoring drone probe according to claim 4 is characterized in that: The reinforcement assembly (4) comprises a spiral shell (41), and a second spring telescopic rod (42) is fixedly mounted on the inner wall of the spiral shell (41).
6. The lifting platform for monitoring drone probe according to claim 5, characterized in that: A fixing plate (43) is fixedly mounted on the bottom end of the second spring telescopic rod (42), and a thread (44) and a mounting groove (45) are provided on the inner wall of the spiral housing (41).