Multifunctional surveying and mapping unmanned aerial vehicle for geographic information
By designing folding and rotating components on a multi-functional geographic information surveying and mapping drone, the problem of difficult folding of traditional drone components is solved, achieving more compact storage and higher space utilization.
Patent Information
- Application Number
- CN202422097734.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-08-28
- Publication Date
- 2025-06-10
- Estimated Expiration
- 2034-08-28
AI Technical Summary
Traditional multi-functional geographic information surveying and mapping drone components are difficult to fold, which makes it take up more space during transportation and is inconvenient to carry.
By designing the drone outer shell including supporting rods, torsion springs, threaded blocks, sliding sleeves and telescopic springs, folding of the support rods and rotation of the support columns is achieved. Combined with the design of sliders and arc-shaped slide chutes, the support columns can slide and retract in the preset track.
It realizes the ease of folding and storage of drones, reduces the volume, allows them to place more equipment in a limited storage environment, and improves space utilization.
Smart Images

Figure CN222960069U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of surveying and mapping unmanned aerial vehicles, in particular to a surveying and mapping unmanned aerial vehicle for multi-functional geographic information. Background Art
[0002] Geographic information refers to the data and information describing the location, shape, and characteristics of natural and human phenomena on the Earth's surface. Geographic information is widely used in fields such as urban planning, environmental protection, disaster management, and resource management. The application of surveying and mapping unmanned aerial vehicles in geographic information acquisition has become increasingly popular because they can quickly and efficiently obtain large-area and high-precision geographic data. Unmanned aerial vehicles have an aerial perspective, can cover complex terrains and inaccessible areas, reduce labor and time costs, and improve the accuracy and real-time nature of data. In addition, the flexibility of unmanned aerial vehicles makes them suitable for various tasks such as land surveying, 3D modeling, environmental monitoring, and agricultural management, providing more comprehensive and accurate support for geographic information.
[0003] Traditional surveying and mapping unmanned aerial vehicles for multi-functional geographic information carry high-precision camera equipment, lidar, GPS and other sensors, fly over the designated area, and collect geographic data in real time. The operator first sets the flight path and task parameters at the ground station, and the unmanned aerial vehicle flies according to the predetermined path, automatically taking high-definition images or laser scanning the terrain. After completing the data collection, the unmanned aerial vehicle returns to the ground station, and the operator downloads the data and performs processing and analysis. Through professional software, high-precision digital terrain models (DTMs), orthophoto maps and other results can be generated, providing reliable geographic information support for urban planning, environmental monitoring, agricultural management, etc.
[0004] For traditional surveying and mapping unmanned aerial vehicles for multi-functional geographic information, in order to ensure flight stability and the safety of equipment, surveying and mapping unmanned aerial vehicles usually have a sturdy frame and a large wingspan, resulting in difficult folding of components, thus occupying more space during transportation and being inconvenient to carry. Summary of the Utility Model
[0005] To make up for the above deficiencies, the utility model provides a surveying and mapping unmanned aerial vehicle for multi-functional geographic information, aiming to improve the problem that components of traditional surveying and mapping unmanned aerial vehicles for multi-functional geographic information are difficult to fold, thus occupying more space during transportation and being inconvenient to carry.
[0006] To achieve the above object, the utility model provides the following technical solution: a surveying and mapping drone for multi-functional geographic information, including a drone outer shell, wherein a support base is fixedly connected to the outer wall of the drone outer shell, a first sliding rod is rotatably connected to the inside of the drone outer shell, a fixed sleeve is slidably connected to the outer wall of the first sliding rod, a support column is arranged on the inner wall of the fixed sleeve, a buckle is fixedly connected to the outer wall of the support column, a fixed seat is fixedly connected to one end of the support column, a rotating shaft is fixedly connected to the lower surface of the fixed seat, a fixed shaft is fixedly connected to the inside of the rotating shaft, a support rod is rotatably connected to the outer wall of the fixed shaft, a torsion spring is sleeved on the outer wall of the fixed shaft, one end of the torsion spring is fixedly connected to the outer wall of the support rod, and the other end of the torsion spring is fixedly connected to the inside of the rotating shaft. A first fixing plate is rotatably connected to the top of the support base, a threaded rod is fixedly connected to the upper surface of the first fixing plate, a threaded block is threadedly connected to the outer wall of the threaded rod, the upper surface of the threaded block is rotatably connected to the inside of the fixed sleeve, a sliding block is fixedly connected to the upper surface of the fixed sleeve, a fixed column is fixedly connected to the inside of the drone outer shell, the outer wall of the sliding block is slidably connected to the inside of the fixed column, and a fixing component is arranged inside the fixed column for fixing the sliding block.
[0007] Further, the fixing component includes a sliding sleeve, the outer wall of the sliding sleeve is slidably connected to the inside of the fixed column, a first clamping block is fixedly connected to the middle of the sliding sleeve, the outer wall of the first clamping block is slidably connected to the inside of the fixed column and the sliding block, a second sliding rod is fixedly connected to the upper surface of the first clamping block, the outer wall of the second sliding rod is slidably connected to the inside of the fixed column, a telescopic spring is sleeved on the outer wall of the second sliding rod, one end of the telescopic spring is fixedly connected to the inside of the fixed column, and the other end of the telescopic spring is fixedly connected to the upper surface of the first clamping block.
[0008] Further, a fan blade is arranged on the upper surface of the fixed seat, a second fixing plate is fixedly connected to the inner wall of the drone outer shell, and a surveying and mapping component is slidably connected to the inside of the second fixing plate.
[0009] Further, the outer wall of the surveying and mapping component is slidably connected to the inside of the drone outer shell, and a rotating rod is rotatably connected to the inside of the second fixing plate.
[0010] Further, a worm is fixedly connected to the outer wall of the rotating rod, and a rotating plate is rotatably connected to the inside of the second fixing plate.
[0011] Further, a worm gear ring is fixedly connected to the outer wall of the rotating plate, and the worm gear ring is engaged with the worm.
[0012] Furthermore, a sliding shaft is slidably connected inside the rotating plate, an arc-shaped sliding groove is formed inside the rotating plate, and the outer wall of the sliding shaft is slidably connected inside the arc-shaped sliding groove.
[0013] Furthermore, a second clamping block is fixedly connected to the outer wall of the sliding shaft, and the outer wall of the second clamping block is slidably connected inside the second fixing plate and the surveying component.
[0014] The utility model has the following beneficial effects:
[0015] 1. In the utility model, first, pull the support rod and cooperate with the support column, buckle, fixed seat, torsion spring and fixed shaft to realize the folding of the support rod. Then, drive the threaded block and cooperate with the threaded rod, first fixing plate and fixed sleeve to rotate the support column. Finally, pull the sliding sleeve and cooperate with the second sliding rod, telescopic spring, first clamping block and slider to realize folding, which solves the problem that the components of the surveying UAV are difficult to fold, thus occupying more space during transportation and being inconvenient to carry, and achieves the purpose of being convenient for folding, storage and carrying, significantly reducing the volume of the UAV, enabling more devices to be placed in a limited storage environment and improving space utilization.
[0016] 2. In the utility model, first, position through the second fixing plate. Then, drive the rotating rod and cooperate with the worm, worm gear ring, rotating plate, sliding shaft and arc-shaped sliding groove to drive the second clamping block to slide inside the second fixing plate and the surveying component, achieving the ability to quickly replace the surveying component according to different surveying requirements, adapting to diverse task requirements, realizing multi-functional and rapid replacement, and improving the overall work efficiency. Description of the Drawings
[0017] Figure 1 is a three-dimensional structural schematic diagram of the surveying UAV for multi-functional geographic information proposed by the utility model;
[0018] Figure 2 is a schematic diagram of the structure on one side of the support column of the surveying UAV for multi-functional geographic information proposed by the utility model;
[0019] Figure 3 is a schematic diagram of the structure of the lower part of the fixed column of the surveying UAV for multi-functional geographic information proposed by the utility model;
[0020] Figure 4 is a schematic diagram of the internal structure of the fixed column of the surveying UAV for multi-functional geographic information proposed by the utility model;
[0021] Figure 5 is a schematic diagram of the internal structure of the fixing plate of the surveying UAV for multi-functional geographic information proposed by the utility model;
[0022] Figure 6 is a schematic diagram of the structure of the rotating plate of the surveying UAV for multi-functional geographic information proposed by the utility model.
[0023] Legend Explanation:
[0024] 1. Drone outer shell; 2. Support base; 3. First sliding rod; 4. Fixed sleeve; 5. Support pillar; 6. Buckle; 7. Fixed seat; 8. Rotating shaft; 9. Support rod; 10. Torsion spring; 11. Fixed shaft; 12. First fixing plate; 13. Threaded rod; 14. Threaded block; 15. Slider; 16. Fixed column; 17. First clamping block; 18. Sliding sleeve; 19. Second sliding rod; 20. Telescopic spring; 21. Second fixing plate; 22. Surveying and mapping part; 23. Rotating rod; 24. Worm; 25. Worm gear ring; 26. Rotating plate; 27. Sliding shaft; 28. Arc-shaped sliding groove; 29. Second clamping block; 30. Fan blade. 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. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without making creative efforts belong to the protection scope of the present invention.
[0026] Refer to Figures 1-4, an embodiment provided by the present utility model: a multi-functional mapping unmanned aerial vehicle for geographic information, comprising an unmanned aerial vehicle outer casing 1, a support base 2 fixedly connected to the outer wall of the unmanned aerial vehicle outer casing 1, a first sliding rod 3 rotatably connected to the inside of the unmanned aerial vehicle outer casing 1, a fixed sleeve 4 slidably connected to the outer wall of the first sliding rod 3, a support column 5 arranged on the inner wall of the fixed sleeve 4, a buckle 6 fixedly connected to the outer wall of the support column 5, a fixed base 7 fixedly connected to one end of the support column 5, a rotating shaft 8 fixedly connected to the lower surface of the fixed base 7, a fixed shaft 11 fixedly connected to the inside of the rotating shaft 8, a support rod 9 rotatably connected to the outer wall of the fixed shaft 11, a torsion spring 10 sleeved on the outer wall of the fixed shaft 11, one end of the torsion spring 10 fixedly connected to the outer wall of the support rod 9, and the other end of the torsion spring 10 fixedly connected to the inside of the rotating shaft 8. A first fixing plate 12 is rotatably connected to the top of the support base 2, a threaded rod 13 is fixedly connected to the upper surface of the first fixing plate 12, a threaded block 14 is threadedly connected to the outer wall of the threaded rod 13, the upper surface of the threaded block 14 is rotatably connected to the inside of the fixed sleeve 4, a slider 15 is fixedly connected to the upper surface of the fixed sleeve 4, a fixed column 16 is fixedly connected to the inside of the unmanned aerial vehicle outer casing 1, the outer wall of the slider 15 is slidably connected to the inside of the fixed column 16, and a fixing component is arranged inside the fixed column 16. The fixing component is used for fixing the slider 15. The fixing component includes a sliding sleeve 18, the outer wall of the sliding sleeve 18 is slidably connected to the inside of the fixed column 16, a first clamping block 17 is fixedly connected to the middle of the sliding sleeve 18, the outer wall of the first clamping block 17 is slidably connected to the inside of the fixed column 16 and the slider 15, a second sliding rod 19 is fixedly connected to the upper surface of the first clamping block 17, the outer wall of the second sliding rod 19 is slidably connected to the inside of the fixed column 16, a telescopic spring 20 is sleeved on the outer wall of the second sliding rod 19, one end of the telescopic spring 20 is fixedly connected to the inside of the fixed column 16, and the other end of the telescopic spring 20 is fixedly connected to the upper surface of the first clamping block 17;
[0027] Specifically, first pull the support rod 9 to rotate it around the fixed shaft 11, so that the outer wall of the support rod 9 is clamped inside the buckle 6 for fixation, and at the same time twist the torsion spring 10. Then drive the threaded block 14 to rotate on the outer wall of the threaded rod 13. Due to the threaded relationship between the threaded rod 13 and the threaded block 14, the threaded block 14 drives the lower fixed sleeve 4 to move downward, so that the protrusion inside the fixed sleeve 4 disengages from the inside of the support column 5. Then drive the support column 5 to rotate 90°. Then rotate the threaded block 14 in the reverse direction to drive the fixed sleeve 4 to fix the support column 5 again. Then pull the sliding sleeve 18 to drive the first clamping block 17 to slide inside the slider 15 and the fixed column 16, and at the same time contract the telescopic spring 20. When the first clamping block 17 completely moves inside the fixed column 16, the support column 5 can be pulled to rotate. During this process, since the top of the slider 15 is semicircular and the inner chute of the fixed column 16 is arc-shaped, the support column 5 can slide in a preset trajectory, so that the support column 5 is retracted to one side of the outer wall of the drone housing 1. Then release the sliding sleeve 18, and at this time the telescopic spring 20 rebounds to drive the first clamping block 17 to return to the inside of the slider 15 for fixation, achieving the folding effect. When unfolding, first pull the sliding sleeve 18, then pull back the support column 5, then drive the threaded block 14, and rotate the support column 5 so that the fan blade 30 faces upward. Finally, pull the support rod 9 out of the buckle 6. At this time, the torsion spring 10 is no longer stressed and rotates back, driving the support rod 9 back to its original position, realizing the folding and unfolding of the drone.
[0028] Refer to Figure 1 , Figure 5 and Figure 6 , a fan blade 30 is arranged on the upper surface of the fixed seat 7. The inner wall of the drone housing 1 is fixedly connected with a second fixing plate 21. A surveying member 22 is slidably connected inside the second fixing plate 21. The outer wall of the surveying member 22 is slidably connected inside the drone housing 1. A rotating rod 23 is rotatably connected inside the second fixing plate 21. A worm 24 is fixedly connected to the outer wall of the rotating rod 23. A rotating plate 26 is rotatably connected inside the second fixing plate 21. A worm gear ring 25 is fixedly connected to the outer wall of the rotating plate 26. The worm gear ring 25 is meshed with the worm 24. A sliding shaft 27 is slidably connected inside the rotating plate 26. An arc-shaped chute 28 is formed inside the rotating plate 26. The outer wall of the sliding shaft 27 is slidably connected inside the arc-shaped chute 28. A second clamping block 29 is fixedly connected to the outer wall of the sliding shaft 27. The outer wall of the second clamping block 29 is slidably connected inside the second fixing plate 21 and the surveying member 22;
[0029] Specifically, the driving rotating rod 23 drives the worm 24 to rotate inside the second fixing plate 21. Due to the meshing relationship between the worm 24 and the worm gear ring 25, the worm gear ring 25 drives the rotating plate 26 to rotate with the rotation of the worm 24, so that the rotating plate 26 rotates inside the second fixing plate 21. Furthermore, the sliding shaft 27 slides inside the arc-shaped chute 28, thereby driving the second clamping block 29 to slide inside the second fixing plate 21 and the surveying and mapping component 22, realizing the disassembly and assembly of the surveying and mapping component 22, so that the surveying and mapping component 22 can be quickly repaired or replaced. At the same time, it can also be quickly switched between a high-resolution camera, a multi-spectral camera, a thermal imaging camera, a lidar, etc. to achieve the effect of multi-functionality.
[0030] Working principle: When the multi-functional geographic information surveying and mapping UAV is needed, first pull the support rod 9 to make it rotate around the fixed shaft 11, and snap the outer wall of the support rod 9 into the buckle 6 to fix the support rod 9. Then drive the threaded block 14 to rotate on the outer wall of the threaded rod 13. The threaded block 14 drives the fixed sleeve 4 to move downward, so that the protrusion inside the fixed sleeve 4 disengages from the support column 5. Then rotate the support column 5, reverse drive the threaded block 14, and the fixed sleeve 4 fixes the support column 5 again. Pull the sliding sleeve 18 to drive the first clamping block 17 to slide inside the slider 15 and the fixed column 16, and the telescopic spring 20 contracts. When the first clamping block 17 completely moves into the fixed column 16, pull the support column 5 to rotate. The support column 5 slides along the preset track under the cooperation of the semi-circular shape at the top of the slider 15 and the arc-shaped chute 28 inside the fixed column 16, and retracts to one side of the outer shell 1 of the UAV. Release the sliding sleeve 18, and the telescopic spring 20 rebounds. The first clamping block 17 returns to the inside of the slider 15 to be fixed. When deploying the UAV, pull the sliding sleeve 18, pull back the support column 5, drive the threaded block 14, rotate the support column 5 to make the fan blade 30 face upward, pull the support rod 9 out of the buckle 6, and the torsion spring 10 rotates back. The support rod 9 returns to its original position. Drive the rotating rod 23 to drive the worm 24 to rotate inside the second fixing plate 21. The worm 24 meshes with the worm gear ring 25, and the worm gear ring 25 drives the rotating plate 26 to rotate. The sliding shaft 27 slides inside the arc-shaped chute 28, driving the second clamping block 29 to slide inside the second fixing plate 21 and the surveying and mapping component 22, realizing the disassembly and assembly of the surveying and mapping component 22, quickly repairing or replacing the surveying and mapping component 22, or quickly switching between a high-resolution camera, a multi-spectral camera, a thermal imaging camera, a lidar, etc. to achieve the multi-functional surveying and mapping effect.
[0031] Finally, it should be noted that the above are only the preferred embodiments of the present invention and are not used to limit the present invention. Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.
Claims
1. A multifunctional geographic information surveying and mapping drone, comprising a drone outer shell (1), characterized in that: The outer wall of the drone outer shell (1) is fixedly connected to a support seat (2), the interior of the drone outer shell (1) is rotatably connected to a slide bar (3), the outer wall of the slide bar (3) is slidably connected to a fixing sleeve (4), the inner wall of the fixing sleeve (4) is provided with a pillar (5), the outer wall of the pillar (5) is fixedly connected to a buckle (6), one end of the pillar (5) is fixedly connected to a fixing seat (7), the lower surface of the fixing seat (7) is fixedly connected to a rotating shaft (8), the interior of the rotating shaft (8) is fixedly connected to a fixing shaft (11), the outer wall of the fixing shaft (11) is rotatably connected to a supporting rod (9), the outer wall of the fixing shaft (11) is sleeved with a torsion spring (10), one end of the torsion spring (10) is fixedly connected to the support rod (9). The outer wall of the unmanned aerial vehicle (UAV) is fixedly connected to the inner part of the rotating shaft (8); the top of the support seat (2) is rotatably connected to a fixing plate (12); the upper surface of the fixing plate (12) is fixedly connected to a threaded rod (13); the outer wall of the threaded rod (13) is threadedly connected to a threaded block (14); the upper surface of the threaded block (14) is rotatably connected to the inner part of the fixing sleeve (4); the upper surface of the fixing sleeve (4) is fixedly connected to a slider (15); the inner part of the UAV outer shell (1) is fixedly connected to a fixing column (16); the outer wall of the slider (15) is slidably connected to the inner part of the fixing column (16); a fixing component is arranged inside the fixing column (16); the fixing component is used to fix the slider (15).
2. The multifunctional geographic information surveying and mapping drone according to claim 1, characterized in that: The fixing assembly comprises a sliding sleeve (18), the outer wall of the sliding sleeve (18) is slidably connected to the interior of the fixing column (16), a clamping block (17) is fixedly connected to the middle part of the sliding sleeve (18), the outer wall of the clamping block (17) is slidably connected to the interior of the fixing column (16) and the sliding block (15), a sliding rod (19) is fixedly connected to the upper surface of the clamping block (17), the outer wall of the sliding rod (19) is slidably connected to the interior of the fixing column (16), and the outer wall of the sliding rod (19) is sleeved with a telescopic spring (20), one end of the telescopic spring (20) is fixedly connected to the interior of the fixing column (16), and the other end of the telescopic spring (20) is fixedly connected to the upper surface of the clamping block (17).
3. The multifunctional geographic information surveying and mapping drone according to claim 1, characterized in that: The upper surface of the fixing seat (7) is provided with a fan blade (30), the inner wall of the outer shell (1) of the drone is fixedly connected with a fixing plate 2 (21), and the interior of the fixing plate 2 (21) is slidably connected with a mapping component (22).
4. The multifunctional geographic information surveying and mapping drone according to claim 3 is characterized in that: The outer wall of the surveying and mapping member (22) is slidably connected to the interior of the outer shell (1) of the drone, and a rotating rod (23) is rotatably connected to the interior of the second fixing plate (21).
5. The multifunctional geographic information surveying and mapping drone according to claim 4, characterized in that: The outer wall of the rotating rod (23) is fixedly connected to a worm (24), and the interior of the second fixed plate (21) is rotatably connected to a rotating plate (26).
6. The multifunctional geographic information surveying and mapping drone according to claim 5, characterized in that: A worm gear ring (25) is fixedly connected to the outer wall of the rotating plate (26), and the worm gear ring (25) is meshed with the worm (24).
7. The multifunctional geographic information surveying and mapping drone according to claim 6, characterized in that: The interior of the rotating plate (26) is slidably connected with a sliding shaft (27), an arc-shaped sliding groove (28) is provided inside the rotating plate (26), and the outer wall of the sliding shaft (27) is slidably connected inside the arc-shaped sliding groove (28).
8. The multifunctional geographic information surveying and mapping drone according to claim 7, characterized in that: The outer wall of the sliding shaft (27) is fixedly connected with a second clamping block (29), and the outer wall of the second clamping block (29) is slidably connected to the inside of the second fixing plate (21) and the surveying and mapping component (22).