Surveying and mapping laser device carried on basis of unmanned aerial vehicle

Abstract

The utility model discloses a surveying and mapping laser device carried based on an unmanned aerial vehicle, and relates to the technical field of surveying and mapping, the surveying and mapping laser device comprises an unmanned aerial vehicle body and a laser surveying and mapping device body, a mounting seat is fixedly mounted on the lower side of the center of the unmanned aerial vehicle body, and a telescopic column is fixedly mounted in the center of the lower side of the mounting seat; the laser surveying and mapping device body is located on the lower side of the mounting base, and a plurality of triangular supports are arranged between the laser surveying and mapping device body and the mounting base. According to the utility model, a stable support structure for mounting the laser surveying and mapping device is designed, and an inverted pyramid form of the triangular support and the side mounting seat is adopted to ensure the longitudinal and transverse stability of the device in flight, so that a stable working condition is provided for data surveying and mapping; the laser surveying and mapping device can be quickly assembled and disassembled, the laser surveying and mapping device comprises a limiting sliding piece and a telescopic column, the real-time position adjustment and fixation of the unmanned aerial vehicle body can be carried out, and the assembly efficiency and the operation flexibility are greatly improved.

Description

Technical Field

[0001] The utility model relates to the technical field of surveying and mapping, in particular to a surveying and mapping laser device carried by an unmanned aerial vehicle (UAV). Background Art

[0002] Surveying and mapping refers to the science and technology of measuring, recording, and mapping the positions, shapes, sizes, mutual relationships, and attributes of surface, underground, and spatial objects. It covers fields such as map making, spatial data acquisition and processing, and the application of geographic information systems (GIS). The development of surveying and mapping technologies enables humans to more accurately understand and utilize the Earth's surface and other spatial information.

[0003] Traditional surveying and mapping devices need to move on the ground. Therefore, there are significant limitations for complex terrains (such as mountainous areas, forests, rivers, etc., which are difficult to traverse) or harsh environments (such as desert or polar regions), making it difficult to achieve complete coverage and accurate surveying and mapping. UAVs can conduct surveying and mapping in rugged terrains or other inaccessible areas, such as high mountains, forests, swamps, etc. They can quickly fly over large areas and conduct continuous surveying and mapping, covering a wider area than traditional hand-held or ground-mounted laser scanners.

[0004] However, existing UAVs generate various types of vibrations during flight, including mechanical vibrations from rotors or propellers, aerodynamic vibrations, and attitude vibrations caused by flight attitude adjustments. These vibrations are directly transmitted to the laser surveying and mapping equipment mounted on the UAV, affecting the measurement accuracy and stability. The mechanical installation structure of the laser surveying and mapping device may not be suitable for direct connection to the UAV body, making it impossible to achieve a quick connection between the laser surveying and mapping device and the UAV body, and ensuring stable surveying and mapping conditions when the surveying and mapping device follows in flight. The present utility model specifically proposes a surveying and mapping laser device carried by an unmanned aerial vehicle to solve the problems mentioned in the above background art. Summary of the Utility Model

[0005] The purpose of the present utility model is to address the drawbacks existing in the prior art, and to propose a surveying and mapping laser device carried by an unmanned aerial vehicle.

[0006] To achieve the above purpose, the present utility model adopts the following technical solutions:

[0007] A surveying and mapping laser device based on an unmanned aerial vehicle comprises an unmanned aerial vehicle body and a laser surveying and mapping device body, wherein a mounting seat is fixedly installed on the lower center side of the unmanned aerial vehicle body, a telescopic column is fixedly installed on the lower center side of the mounting seat, the laser surveying and mapping device body is located on the lower side of the mounting seat, and a plurality of triangular brackets are arranged between the laser surveying and mapping device body and the mounting seat, a sliding piece is rotatably connected to the upper end of the triangular bracket, the sliding piece slides translationally on the lower side of the mounting seat of the mounting seat, and a rotating rod connected to the mounting seat is arranged on one side of each of the plurality of sliding pieces.

[0008] Preferably, the lower side of the mounting seat is rotatably connected to an end face gear ring located outside the mounting seat, a torsion spring is provided at the transition point of the rotating rod, and a face gear meshing with the end face gear ring is fixed to the inner end of the rotating rod;

[0009] The outer end of the rotating rod is fixed with a second limiting block, and one side of the sliding sheet is provided with a plurality of limiting grooves corresponding to the second limiting block.

[0010] Preferably, the telescopic column includes a sleeve and a sliding column, the sliding column slides inside and outside the sleeve, and a strong spring corresponding to the sliding column is arranged inside the sleeve.

[0011] Preferably, a mounting sleeve is fixed to the lower end of the sliding column of the telescopic column, and a mounting insert corresponding to the mounting sleeve is fixed to the upper side of the laser surveying and mapping device body.

[0012] Preferably, a plurality of card seats are fixed on the peripheral side of the installation sleeve, and the lower ends of a plurality of the triangular brackets are rotatably connected to the corresponding card seats.

[0013] Preferably, a plurality of sockets corresponding to the card seat are fixed on the periphery of the installation insert, limiting grooves corresponding to the sockets are opened on the periphery of the installation sleeve, a plurality of clamping heads are fixed on one side of the card seat, and through grooves corresponding to the clamping heads are opened in the sockets.

[0014] Preferably, a limiting block 1 is fixed at the inner center of the installation sleeve, and a rectangular groove corresponding to the limiting block 1 is opened at the center of the upper side of the installation insert.

[0015] Compared with the prior art, the beneficial effects of the utility model are:

[0016] 1. The laser vehicle surveying and mapping device mounted on the drone of the utility model is designed with a stable bracket structure for installing the laser surveying and mapping device. The triangular bracket is matched with the upper mounting seat to form an inverted pyramid-shaped stable support structure, which can not only achieve longitudinal but also take into account the lateral stability requirements, and provide stable working conditions for data surveying and mapping collection of the laser surveying and mapping device;

[0017] 2. The installation sleeve and installation insertion cylinder sleeved connection structure provided by the utility model can realize the rapid assembly and disassembly of the laser mapping device on the unmanned aircraft body. The provided limiting structure for the limiting sliding piece and the telescopic column facilitate the immediate adjustment and fixation of the up and down positions of the installed unmanned aircraft body, greatly improving the assembly efficiency of the laser mapping device. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 The following is a schematic structural diagram of a mapping laser device based on a drone Figure One ;

[0019] Figure 2 The following is a schematic structural diagram of a mapping laser device based on a drone Figure Two ;

[0020] Figure 3 The following is a schematic structural diagram of a mapping laser device based on a drone Figure Three ;

[0021] Figure 4 The following is a bottom view structural schematic diagram of a mapping laser device based on a drone proposed by the present utility model.

[0022] In the figure: 1, unmanned aircraft body; 2, laser mapping device body; 3, mounting seat; 4, triangular bracket; 5, telescopic column; 6, first limiting block; 7, sliding piece; 8, end face tooth ring; 9, face gear; 10, rotating rod; 11, second limiting block; 12, installation sleeve; 13, card seat; 14, installation insertion cylinder; 15, limiting groove; 16, rectangular groove. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0023] Next, the technical solutions in the embodiments of the present utility model will be clearly and completely described in conjunction with the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are only a part of the embodiments of the present utility model, rather than all of the embodiments.

[0024] Referring to Figures 1-4 , a mapping laser device based on a drone includes an unmanned aircraft body 1 and a laser mapping device body 2. A mounting seat 3 is fixedly installed on the lower center of the unmanned aircraft body 1. A telescopic column 5 is fixedly installed at the center of the lower side of the mounting seat 3. The telescopic column 5 includes a sleeve and a sliding column. The sliding column slides inside and outside the sleeve, and a strong spring corresponding to the sliding column is arranged inside the sleeve. The laser mapping device body 2 is located below the mounting seat 3. The sliding column of the telescopic column 5 is fixedly provided with an installation sleeve 12 at the lower end, and an installation insertion cylinder 14 corresponding to the installation sleeve 12 is fixedly installed on the upper side of the laser mapping device body 2. The laser mapping device body 2 is inserted into the installation sleeve 12 through the upper installation insertion cylinder 14, so that the laser mapping device body 2 is installed on the unmanned aircraft body 1;

[0025] Furthermore, a plurality of triangular brackets 4 are arranged between the laser surveying and mapping device body 2 and the mounting seat 3, a plurality of card seats 13 are fixed on the peripheral side of the mounting sleeve 12, the lower ends of the plurality of triangular brackets 4 are rotatably connected with the corresponding card seats 13, a plurality of sockets corresponding to the card seats 13 are fixed on the peripheral side of the mounting insert 14, limiting grooves 15 corresponding to the sockets are provided on the peripheral side of the mounting sleeve 12, a plurality of card heads are fixed on one side of the card seat 13, and through grooves corresponding to the card heads are provided in the sockets, a limiting block 6 is fixed to the inner center of the mounting sleeve 12, and a rectangular groove 16 corresponding to the limiting block 6 is provided at the upper center of the mounting insert 14. When the installation insert tube 14 device enters the installation sleeve 12, the inner square groove 16 of the installation insert tube 14 corresponds to the fixed limit block 6. At this time, the card seat 13 on the side of the installation insert tube 14 can also enter the installation sleeve 12 through the limit groove 15 until the installation insert tube 14 completely enters the sleeve. The installation insert tube 14 in the sleeve can be rotated to one side, and the square groove 16 is misaligned with the limit block 6, so that the installation insert tube 14 is locked in the sleeve. After the installation insert tube 14 is rotated at an angle, several card heads on the card seat 13 enter the through grooves inside the socket, further improving the connection between the installation insert tube 14 and the installation sleeve 12;

[0026] Furthermore, the upper end of the triangular bracket 4 is rotatably connected with a sliding piece 7, and the sliding piece 7 is translated and slid on the lower side of the mounting seat 3 of the mounting seat 3. A rotating rod 10 connected to the mounting seat 3 is arranged on one side of the plurality of sliding pieces 7. The lower side of the mounting seat 3 is rotatably connected with an end face gear ring 8 located outside the mounting seat 3. A torsion spring is arranged at the connecting part of the rotating rod 10. A face gear 9 meshing with the end face gear ring 8 is fixed at the inner end of the rotating rod 10. A limited block 11 is fixed at the outer end of the rotating rod 10, and a plurality of limit grooves corresponding to the limit block 11 are opened on one side of the sliding piece 7. When the drone body 1 needs to be mounted below When the height of the laser surveying and mapping device body 2 is adjusted, the drone body 1 can be directly pushed up, the strong spring inside the telescopic column 5 is compressed, and the plurality of triangular brackets 4 are rotated at an angle, and the sliding sheet 7 connected thereto is pressed and moved outward, and the upper limit block 2 11 of the rotating rod 10 cooperates with the limit groove to fix the adjusted position immediately. When the upper and lower positions need to be adjusted back, the end face gear ring 8 on the mounting seat 3 is rotated, and through the linkage of the plurality of face gears 9, the rotating rod 10 drives the connected limit block 2 11 to disengage from the limit groove, and then the laser surveying and mapping device body 2 at the lower end of the telescopic column 5 can be adjusted back.

[0027] The above description is only a preferred specific implementation manner of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can make equivalent replacements or changes within the technical scope disclosed by the present invention according to the technical scheme and the utility model concept of the present invention, which should be covered by the protection scope of the present invention.

Claims

1. A surveying laser device mounted on an unmanned aerial vehicle, comprising an unmanned aerial vehicle body (1) and a laser surveying device body (2), characterized in that: A mounting seat (3) is fixedly mounted on the lower center of the drone body (1), a telescopic column (5) is fixedly mounted on the lower center of the mounting seat (3), the laser surveying and mapping device body (2) is located on the lower side of the mounting seat (3), and a plurality of triangular brackets (4) are arranged between the laser surveying and mapping device body (2) and the mounting seat (3), a sliding sheet (7) is rotatably connected to the upper end of the triangular bracket (4), the sliding sheet (7) slides translationally on the lower side of the mounting seat (3) of the mounting seat (3), and a rotating rod (10) connected to the mounting seat (3) is arranged on one side of the plurality of sliding sheets (7).

2. The surveying laser device based on an unmanned aerial vehicle according to claim 1, characterized in that: The lower side of the mounting seat (3) is rotatably connected to an end face toothed ring (8) located outside the mounting seat (3); a torsion spring is provided at the transition point of the rotating rod (10); and a face gear (9) meshing with the end face toothed ring (8) is fixed to the inner end of the rotating rod (10); A second limiting block (11) is fixed to the outer end of the rotating rod (10), and a plurality of limiting grooves corresponding to the second limiting block (11) are provided on one side of the sliding sheet (7).

3. The surveying laser device based on an unmanned aerial vehicle according to claim 1, characterized in that: The telescopic column (5) comprises a sleeve and a sliding column, the sliding column slides inside and outside the sleeve, and a strong spring corresponding to the sliding column is arranged inside the sleeve.

4. The surveying laser device based on an unmanned aerial vehicle according to claim 1, characterized in that: A mounting sleeve (12) is fixed to the lower end of the sliding column of the telescopic column (5), and a mounting insert (14) corresponding to the mounting sleeve (12) is fixed to the upper side of the laser mapping device body (2).

5. The surveying laser device based on an unmanned aerial vehicle according to claim 4, characterized in that: A plurality of card seats (13) are fixed on the peripheral side of the installation sleeve (12), and the lower ends of a plurality of the triangular brackets (4) are rotatably connected to the corresponding card seats (13).

6. The surveying laser device based on an unmanned aerial vehicle according to claim 4, characterized in that: A plurality of sockets corresponding to the card seat (13) are fixed on the peripheral side of the installation plug cylinder (14), a limiting groove (15) corresponding to the sockets is opened on the peripheral side of the installation sleeve (12), a plurality of clamping heads are fixed on one side of the card seat (13), and a through groove corresponding to the clamping head is opened in the socket.

7. The surveying laser device based on an unmanned aerial vehicle according to claim 4, characterized in that: A limiting block (6) is fixed at the inner center of the installation sleeve (12), and a rectangular groove (16) corresponding to the limiting block (6) is opened at the center of the upper side of the installation insert (14).

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