High-precision topographic surveying and mapping unmanned aerial vehicle load device
Patent Information
- Application Number
- CN202522237683.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-10-23
- Publication Date
- 2026-09-29
- Estimated Expiration
- 2035-10-23
AI Technical Summary
[0003]现有技术中,在通过载荷装置使测绘模块与无人机机体连接时,一般通过螺纹孔与螺栓的配合实现刚性连接,但由于螺纹孔位置固定,使得仅支持单一尺寸的测绘模块的安装,无法兼容多变规格的测绘模块
[0014]1、该高精度地形测绘无人机载荷装置,通过调整机构实现安装宽度的调节,通过长槽可以使测绘模块能够前后移动,以便将其调整至无人机主体底端的中部位置,从而使得该载荷装置能够适应不同规格的测绘模块的安装;
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Figure CN224810943U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the field of unmanned aerial vehicles (UAVs), specifically a high-precision terrain mapping UAV payload device. Background Technology
[0002] The high-precision topographic mapping UAV payload device is a modular device designed specifically for UAVs. It is used to carry the mapping module (i.e., the payload, which is a sensor or device that directly performs data acquisition, such as an optical camera, lidar, or RTK / PPK positioning system) and realize the acquisition and processing of topographic data. Its core function is to replace traditional manual mapping, improve efficiency and accuracy, and is widely used in land surveys, engineering construction and other fields. The mapping module needs to be connected to the UAV body through the payload device and relies on its power supply, communication and protection functions.
[0003] In existing technologies, when connecting a mapping module to the UAV body via a load device, a rigid connection is generally achieved through the engagement of threaded holes and bolts. However, since the position of the threaded holes is fixed, it only supports the installation of mapping modules of a single size and cannot be compatible with mapping modules of various specifications. Utility Model Content
[0004] The purpose of this invention is to provide a high-precision terrain mapping UAV payload device to solve the technical problems mentioned in the background art.
[0005] To achieve the above objectives, this utility model provides the following technical solution: a high-precision terrain mapping UAV payload device, comprising a UAV body and a mapping module, wherein the UAV body is positioned above the mapping module, and threaded columns are symmetrically arranged at the top of the mapping module, and nuts are threadedly connected to the surface of the threaded columns;
[0006] The bottom of the UAV body is symmetrically provided with upright plates, and two upright plates are movably connected to symmetrically arranged load frames. The load frames have symmetrically opened long slots for threaded columns to pass through, and the long slots cooperate with the threaded columns and nuts to realize the installation between the mapping module and the load frame. An adjustment mechanism is provided between the two upright plates to pass through the load frame, and the adjustment mechanism is used to adjust the installation width. The adjustment mechanism includes a bidirectional lead screw connected to the upright plate through a bearing and a handle movably connected to one side of the bidirectional lead screw. A positioning mechanism is provided between the handle and the bidirectional lead screw to improve the stability after the installation width is adjusted.
[0007] Preferably, elastic pads are provided at both the upper and lower ends of the load frame to protect the surveying module and the nuts.
[0008] Preferably, the bidirectional lead screw is threadedly connected to the load frame, and the bidirectional lead screw is used to make the two load frames move synchronously in opposite directions.
[0009] Preferably, guide rods are symmetrically welded between the two upright plates, and the guide rods are slidably connected to the load frame so that the load frame can only move in a linear motion.
[0010] Preferably, the positioning mechanism includes a movable column fixed to the side of the handle and a movable groove formed on one side of the bidirectional lead screw. A return spring is connected between the movable column and the movable groove so that the movable column can automatically return to its original position.
[0011] Preferably, the side of the handle is symmetrically provided with positioning posts, and the side of one of the upright plates is provided with positioning grooves at equal angles to form a locking structure with the positioning posts, and the positioning posts and positioning grooves cooperate to prevent the handle from rotating on its own.
[0012] Preferably, the inner surface of the movable groove is symmetrically provided with limiting grooves, and both the upper and lower ends of the movable column are provided with limiting blocks that form a sliding structure with the limiting grooves. The limiting grooves and limiting blocks cooperate to make the bidirectional lead screw rotate synchronously with the movable column.
[0013] Compared with the prior art, the beneficial effects of this utility model are:
[0014] 1. The high-precision terrain mapping UAV payload device adjusts the installation width through an adjustment mechanism. The long slot allows the mapping module to move back and forth to be adjusted to the middle position of the bottom of the UAV body, thus enabling the payload device to adapt to the installation of mapping modules of different specifications.
[0015] 2. The high-precision terrain mapping UAV payload device locks the rotary handle through a positioning mechanism to prevent the rotary handle from rotating on its own, thereby improving the stability after the installation width is adjusted. Attached Figure Description
[0016] Figure 1 This is a three-dimensional structural diagram of the present invention;
[0017] Figure 2 This is a three-dimensional structural diagram of the surveying module and adjustment mechanism of this utility model;
[0018] Figure 3 This is a three-dimensional exploded view of the adjustment mechanism and load frame of this utility model;
[0019] Figure 4 This is a three-dimensional exploded view of the positioning mechanism and the bidirectional lead screw of this utility model;
[0020] Figure 5 This is a schematic diagram of the main structure of this utility model.
[0021] In the diagram: 1. UAV body; 2. Mapping module; 3. Payload frame; 301. Long slot; 4. Vertical plate; 5. Adjustment mechanism; 501. Two-way lead screw; 502. Rotary handle; 503. Guide rod; 6. Positioning mechanism; 601. Movable column; 602. Return spring; 603. Movable slot; 604. Positioning column; 605. Positioning slot; 606. Limit block; 607. Limit slot; 7. Elastic pad; 8. Threaded column; 9. Nut. Detailed Implementation
[0022] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.
[0023] Please see Figures 1-3 and Figure 5 This utility model provides a technical solution: a high-precision terrain mapping UAV payload device, including a UAV body 1 and a mapping module 2. The UAV body 1 is set above the mapping module 2. Threaded posts 8 are symmetrically arranged at the top of the mapping module 2, and nuts 9 are threadedly connected to the surface of the threaded posts 8.
[0024] The bottom of the UAV body 1 is symmetrically provided with upright plates 4. The two upright plates 4 are movably connected to the symmetrically arranged load frame 3. The load frame 3 has symmetrically opened long slots 301 for threaded columns 8 to pass through. The long slots 301 cooperate with the threaded columns 8 and nuts 9 to realize the installation between the mapping module 2 and the load frame 3.
[0025] Specifically, since the threaded post 8 is slidably connected to the long slot 301, after the threaded post 8 at the top of the mapping module 2 passes through the long slot 301, the mapping module 2 can be moved back and forth to adjust it to the middle position at the bottom of the UAV body 1. At this time, the nut 9 is put on the outside of the threaded post 8 and tightened, thereby completing the installation of the mapping module 2. By adopting this operation, the installation of mapping modules 2 of different specifications can be adapted.
[0026] The UAV body 1 drives the surveying module 2 to move, so that the surveying module 2 can realize high-precision surveying of terrain data and improve efficiency. The surveying module 2 relies on the power supply, communication and protection functions of the UAV body 1.
[0027] exist Figure 2 and Figure 3 In the middle: elastic pads 7 are provided at both the upper and lower ends of the load frame 3. The elastic pads 7 are made of silicone.
[0028] Specifically, the elastic pad 7 can prevent hard contact between the surveying module 2, the nut 9 and the load frame 3, thus providing protection. At the same time, it can increase friction and improve installation stability.
[0029] exist Figures 1-5 In the middle: An adjustment mechanism 5 is provided between the two upright plates 4, which passes through the load frame 3. The adjustment mechanism 5 is used to adjust the installation width. The adjustment mechanism 5 includes a double-acting screw 501 connected to the upright plate 4 through a bearing and a guide rod 503 symmetrically welded between the two upright plates 4. The double-acting screw 501 is threadedly connected to the load frame 3. A handle 502 is movably connected to one side of the double-acting screw 501. The double-acting screw 501 is used to make the two load frames 3 move synchronously in opposite directions.
[0030] Specifically, since the load frame 3 is threadedly connected to the bidirectional lead screw 501 and slidably connected to the guide rod 503, the symmetrically arranged load frame 3 can be moved in the opposite direction in the horizontal direction by rotating the handle 502 and the bidirectional lead screw 501, thereby realizing the adjustment of the installation width to adapt to the installation of different specifications of surveying modules 2.
[0031] exist Figures 1-3 and Figure 5 In the middle: the guide rod 503 is slidably connected to the load frame 3, and the guide rod 503 is used to make the load frame 3 only perform linear motion.
[0032] Specifically, the guide rod 503 can be used to support and limit the load frame 3, so that the load frame 3 can only move in a straight line.
[0033] exist Figure 3 and Figure 4 In the middle: A positioning mechanism 6 is provided between the handle 502 and the double-acting lead screw 501. The positioning mechanism 6 is used to improve the stability after the installation width is adjusted. The positioning mechanism 6 includes a movable column 601 fixed on the side of the handle 502 and a movable groove 603 opened on one side of the double-acting lead screw 501. A return spring 602 is connected between the movable column 601 and the movable groove 603. The return spring 602 is used to make the movable column 601 automatically return to its original position. Positioning columns 604 are symmetrically arranged on the side of the handle 502. A positioning groove 605 is opened at equal angles on the side of a vertical plate 4 to form a locking structure with the positioning column 604. The positioning column 604 and the positioning groove 605 cooperate to lock the handle 502 and prevent the handle 502 from rotating.
[0034] Specifically, since the movable column 601 and the movable groove 603 are elastically connected by the return spring 602 and slidably connected by the limiting block 606 and the limiting groove 607, the return spring 602 can be stretched by pulling the handle 502 outward, which in turn separates the positioning column 604 from the positioning groove 605. At this time, the locking of the handle 502 can be released, allowing the handle 502 to rotate. After the load frame 3 is adjusted to the designated position, the handle 502 is released, and the handle 502 and the movable column 601 will automatically reset under the action of the return spring 602. At the same time, the positioning column 604 will engage with the positioning groove 605, thereby locking the handle 502 to prevent the handle 502 from rotating on its own.
[0035] exist Figure 4 In the middle: the inner surface of the movable groove 603 is symmetrically provided with limiting grooves 607, and the upper and lower ends of the movable column 601 are provided with limiting blocks 606 that form a sliding structure with the limiting grooves 607. The limiting grooves 607 and the limiting blocks 606 cooperate to make the bidirectional lead screw 501 rotate synchronously with the movable column 601.
[0036] Specifically, through the cooperation of the limiting groove 607 and the limiting block 606, the bidirectional lead screw 501 can rotate synchronously with the movable column 601.
[0037] In use, the return spring 602 can be stretched by pulling the handle 502 outward, which will simultaneously separate the positioning post 604 from the positioning groove 605. At this time, the lock on the handle 502 can be released. Then, the handle 502 and the two-way screw 501 can be rotated as needed, so that the symmetrically arranged load frame 3 can move in the opposite direction in the horizontal direction, thereby completing the adjustment of the installation width. After the handle 502 is released, it and the movable post 601 will automatically reset under the action of the return spring 602, and at the same time, the positioning post 604 will engage with the positioning groove 605, thereby locking the handle 502. At this time, the threaded post 8 at the top of the mapping module 2 is inserted through the long groove 301, and the mapping module 2 is adjusted to the middle position of the bottom of the UAV body 1 by moving the mapping module 2 back and forth. Then, the nut 9 is put on the outside of the threaded post 8 and tightened, thereby completing the installation of the mapping module 2.
[0038] Electrical equipment (including but not limited to motors, electric actuators, etc.) is safely powered by an external power source and controlled by a control box. The contents not described in detail in this specification are existing technologies known to those skilled in the art.
[0039] Although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some of the technical features. Any modifications, equivalent substitutions, improvements, etc., made within the spirit and principles of the present invention should be included within the protection scope of the present invention.
Claims
1. A high-precision terrain mapping UAV payload device, comprising a UAV body (1) and a mapping module (2), wherein the UAV body (1) is disposed above the mapping module (2), and threaded posts (8) are symmetrically arranged at the top of the mapping module (2), and nuts (9) are threadedly connected to the surface of the threaded posts (8); characterized in that: The bottom of the UAV body (1) is symmetrically provided with upright plates (4), and the two upright plates (4) are movably connected with symmetrically provided load frames (3). The load frames (3) are symmetrically provided with long slots (301) for threaded columns (8) to pass through. The long slots (301) cooperate with the threaded columns (8) and nuts (9) to realize the installation between the mapping module (2) and the load frames (3). An adjustment mechanism (5) is provided between the two upright plates (4) to pass through the load frames (3). The adjustment mechanism (5) is used to realize the adjustment of the installation width. The adjustment mechanism (5) includes a two-way lead screw (501) connected to the upright plate (4) through a bearing and a handle (502) movably connected to one side of the two-way lead screw (501). A positioning mechanism (6) is provided between the handle (502) and the two-way lead screw (501) to improve the stability after the installation width is adjusted.
2. The high-precision terrain mapping UAV payload device according to claim 1, characterized in that: The load frame (3) is provided with elastic pads (7) at both the upper and lower ends to protect the surveying module (2) and the nut (9).
3. The high-precision terrain mapping UAV payload device according to claim 1, characterized in that: The bidirectional lead screw (501) is threadedly connected to the load frame (3), and the bidirectional lead screw (501) is used to make the two load frames (3) move synchronously in opposite directions.
4. The high-precision terrain mapping UAV payload device according to claim 1, characterized in that: Guide rods (503) are symmetrically welded between the two upright plates (4). The guide rods (503) are slidably connected to the load frame (3) so that the load frame (3) can only move in a straight line.
5. The high-precision terrain mapping UAV payload device according to claim 1, characterized in that: The positioning mechanism (6) includes a movable column (601) fixed on the side of the handle (502) and a movable groove (603) opened on the side of the double-acting screw (501). A return spring (602) is connected between the movable column (601) and the movable groove (603) so that the movable column (601) can be automatically reset.
6. The high-precision terrain mapping UAV payload device according to claim 5, characterized in that: The handle (502) is symmetrically provided with positioning posts (604) on its side. A positioning groove (605) is provided at equal angles on the side of a vertical plate (4) to form a locking structure with the positioning post (604). The positioning post (604) and the positioning groove (605) cooperate to prevent the handle (502) from rotating.
7. A high-precision terrain mapping UAV payload device according to claim 5, characterized in that: The inner surface of the movable groove (603) is symmetrically provided with limiting grooves (607). Both the upper and lower ends of the movable column (601) are provided with limiting blocks (606) that form a sliding structure with the limiting grooves (607). The limiting grooves (607) and the limiting blocks (606) cooperate to make the bidirectional lead screw (501) rotate synchronously with the movable column (601).