Flight shooting unmanned aerial vehicle for cadastral surveying and mapping

Abstract

The utility model relates to the technical field of shooting unmanned aerial vehicles, and discloses a flight shooting unmanned aerial vehicle for cadastral surveying and mapping, which comprises an unmanned aerial vehicle main body, connecting rods are fixedly mounted at four corners of the side surface of the unmanned aerial vehicle main body, propellers are arranged on the upper sides of the connecting rods, and a first movable cavity is formed in the unmanned aerial vehicle main body; the first movable cavity is a fan-shaped cavity, a swing block is movably mounted in the first movable cavity, a first mounting cavity is formed in the side face of the swing block, a fixed shooting camera is arranged in the first mounting cavity, and two second movable cavities are symmetrically formed in the inner side of the first movable cavity. According to the utility model, before a working environment is reached, the extrusion block extrudes the first clamping structure to fix the swing block, so that the shooting camera is located in the first movable cavity to protect the lens of the camera, and unnecessary wear caused by impact with insects in the flying process is reduced.

Description

Technical Field

[0001] This utility model relates to the field of drone technology, and in particular to a drone for cadastral mapping. Background Technology

[0002] With the advancement of social technology, drones are now mostly used for surveying and mapping in the process of cadastral surveying and mapping.

[0003] Existing drones use cameras to take pictures during flight. In current technology, the camera is mounted on the bottom of the drone. When the camera is in high-speed flight, it will wear down when it collides with small insects. To address this, we propose a drone for aerial photography of cadastral mapping. Utility Model Content

[0004] The present invention aims to solve the technical problems existing in the prior art and provide a drone for cadastral surveying and mapping.

[0005] To achieve the above objectives, this utility model adopts the following technical solution: a drone for cadastral mapping and photography, comprising a drone body, connecting rods fixedly installed at the four corners of the drone body, a propeller on the upper side of the connecting rods, a first movable cavity inside the drone body (fan-shaped cavity), a swing block movably installed inside the first movable cavity, a first mounting cavity on the side of the swing block (fixed camera inside the first mounting cavity), two second movable cavities symmetrically opened on the inner side of the first movable cavity (arc-shaped cavity), a first snap-fit ​​structure fixedly installed on the side of the swing block corresponding to the position of the second movable cavity, two adapter cavities symmetrically opened on the side of the swing block (arc-shaped groove), two fixed support frames on the bottom side of the drone body (arc-shaped blocks adapted to the adapter cavities), a second snap-fit ​​structure adapted to the first snap-fit ​​structure at one end of the support frame, and a compression block for pressing the first snap-fit ​​structure inside the second movable cavity.

[0006] Preferably, the first snap-fit ​​structure includes a mounting block fixedly installed on the side of the swing block, and a limiting block is fixedly installed on the side of the mounting block. The limiting block is a trapezoidal block.

[0007] Preferably, a limiting cavity is formed at the center of the side of the limiting block, the limiting cavity is an arc-shaped cavity, and the extrusion block is a hollow arc-shaped block.

[0008] Preferably, the second snap-fit ​​structure includes a connecting block fixedly installed at one end of the support frame. The connecting block is a trapezoidal block, and a claw is fixedly installed at one end of the connecting block. The claw is an arc-shaped block that matches the side of the limiting block.

[0009] Preferably, a first support rod is fixedly installed on the upper side of the support frame, and the end of the first support rod away from the support frame is fixedly installed on the side of the drone body. Two second support blocks are symmetrically fixedly installed on the upper side of the support frame, and the end of the second support block away from the support frame is fixedly installed on the side of the drone body. Two protrusions are fixedly installed on the bottom side of the support frame. The protrusions are arc-shaped blocks.

[0010] Preferably, a second mounting cavity is provided on the side of the main body of the drone, and a fixed rotary motor is provided inside the second mounting cavity. The output end of the rotary motor is fixedly mounted on the side of the swing block.

[0011] Beneficial effects

[0012] This utility model provides a drone for aerial photography in cadastral surveying and mapping. It has the following beneficial effects:

[0013] (1) Before the drone for cadastral mapping is in the working environment, the first snap-fit ​​structure is squeezed by the squeezing block to fix the swing block, so that the camera is inside the first active cavity to protect the camera lens and reduce unnecessary wear caused by collision with insects during flight.

[0014] (2) When the drone for cadastral mapping is in flight, the swing block starts to swing, so that the first locking structure and the second locking structure fit together to form a hard limit on the movement of the swing block. The first locking structure and the second locking structure also constrain and squeeze the swing block to improve the stability in the working state. Attached Figure Description

[0015] To more clearly illustrate the embodiments of this utility model or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings in the following description are merely exemplary, and those skilled in the art can derive other embodiments based on the provided drawings without creative effort.

[0016] The structures, proportions, sizes, etc. illustrated in this specification are only for the purpose of assisting those skilled in the art in understanding and reading the content disclosed herein, and are not intended to limit the implementation conditions of this utility model. Therefore, they have no substantial technical significance. Any modifications to the structure, changes in the proportional relationships, or adjustments to the size, without affecting the effects and purposes that this utility model can produce, should still fall within the scope of the technical content disclosed in this utility model.

[0017] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0018] Figure 2 This is a partial structural schematic diagram of the first support rod of this utility model;

[0019] Figure 3 This utility model Figure 2 Enlarged structural diagram at point A in the middle;

[0020] Figure 4 This is a side sectional view of the present invention;

[0021] Figure 5 This utility model Figure 4 Enlarged structural diagram at point B.

[0022] Legend:

[0023] 1. Drone body; 2. Connecting rod; 3. First movable cavity; 4. Swing block; 5. First mounting cavity; 6. Camera; 7. Second movable cavity; 8. Adaptor cavity; 9. Support frame; 10. Mounting block; 11. Limiting block; 12. Claw; 13. Limiting cavity; 14. Pressing block; 15. First support rod; 16. Second support block; 17. Protrusion; 18. Second mounting cavity; 19. Rotary motor; 20. Connecting block. Detailed Implementation

[0024] 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.

[0025] like Figures 1-5As shown, a cadastral mapping drone includes a drone body 1. Connecting rods 2 are fixedly installed at the four corners of the drone body 1. A propeller is mounted on the upper side of each connecting rod 2. A first movable cavity 3, which is fan-shaped, is formed inside the drone body 1. A swing block 4 is movably installed inside the first movable cavity 3. A first mounting cavity 5 is formed on the side of the swing block 4. A fixed camera 6 is installed inside the first mounting cavity 5. Two second movable cavities 7, which are arc-shaped, are symmetrically formed inside the first movable cavity 3. A first snap-fit ​​structure is fixedly installed on the side of the swing block 4 corresponding to the position of the second movable cavity 7. Two adapter cavities 8, which are arc-shaped grooves, are symmetrically formed on the side of the swing block 4. Two fixed support frames 9, which are arc-shaped blocks that adapt to the adapter cavities 8, are provided on the bottom side of the drone body 1. One end of each support frame 9 is provided with... A second locking structure is adapted to the first locking structure. A pressing block 14 is provided on the inner side of the second movable cavity 7 to press the first locking structure. When not in operation, the pressing block 14 presses the first locking structure to fix the swing block 4, so that the camera 6 is located inside the first movable cavity 3 to protect the camera lens and reduce unnecessary wear caused by collision with insects during flight. When flying, the swing block 4 starts to swing, so that the first locking structure and the second locking structure fit together to form a hard limit on the movement of the swing block 4. The first locking structure and the second locking structure also constrain and press the swing block 4 to improve stability. A second mounting cavity 18 is opened on the side of the drone body 1. A fixed rotary motor 19 is provided inside the second mounting cavity 18. The output end of the rotary motor 19 is fixedly installed on the side of the swing block 4.

[0026] The first snap-fit ​​structure includes a mounting block 10 fixedly installed on the side of the swing block 4. A limiting block 11 is fixedly installed on the side of the mounting block 10. The limiting block 11 is a trapezoidal block. The inclined surface of the limiting block 11 guides the snap-fit ​​position of the second snap-fit ​​structure. A limiting cavity 13 is opened at the center of the side of the limiting block 11. The limiting cavity 13 is an arc-shaped cavity. The squeezing block 14 is a hollow arc-shaped block. The squeezing block 14 squeezes into the interior of the limiting cavity 13 to constrain the movement of the limiting block 11 and the mounting block 10, thereby constraining the movement of the swing block 4. The second snap-fit ​​structure includes a connecting block 20 fixedly installed at one end of the support frame 9. The connecting block 20 is a trapezoidal block. A claw 12 is fixedly installed at one end of the connecting block 20. The claw 12 is an arc-shaped block adapted to the side of the limiting block 11. The connecting block 20 and the limiting block 11 perform a snap-fit ​​operation. The movement of the limiting block 11 is constrained by the deformation of the connecting block 20.

[0027] A first support rod 15 is fixedly installed on the upper side of the support frame 9. The end of the first support rod 15 away from the support frame 9 is fixedly installed on the side of the drone body 1. Two second support blocks 16 are symmetrically fixedly installed on the upper side of the support frame 9. The end of the second support block 16 away from the support frame 9 is fixedly installed on the side of the drone body 1. Two protrusions 17 are arc-shaped blocks fixedly installed on the bottom side of the support frame 9. The first support rod 15, the second support blocks 16, the support frame 9 and the protrusions 17 form a support frame 9 to support the drone body 1.

[0028] The working principle of this utility model:

[0029] In use, when not in operation, the squeezing block 14 presses against the first locking structure to fix the swing block 4, keeping the camera 6 inside the first movable cavity 3 to protect the camera lens and reduce unnecessary wear caused by collisions with insects during flight. When in flight, the swing block 4 begins to swing, causing the first and second locking structures to fit together to create a hard limit on the movement of the swing block 4. The first and second locking structures also constrain and compress the swing block 4. To improve stability, the inclined surface of the limiting block 11 guides the snap-fit ​​position of the second snap-fit ​​structure. The pressing block 14 presses into the interior of the limiting cavity 13 to constrain the movement of the limiting block 11 and the mounting block 10, thereby constraining the movement of the swing block 4. The connecting block 20 snaps into the limiting block 11, and the deformation of the connecting block 20 constrains the movement of the limiting block 11. The first support rod 15, the second support block 16, the support frame 9 and the protrusion 17 form a support frame 9 to support the main body of the drone 1.

[0030] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claims. The scope of protection of this utility model is defined by the appended claims and their equivalents.

Claims

1. A drone for cadastral mapping and aerial photography, comprising a drone body (1), wherein connecting rods (2) are fixedly installed at the four corners of the side of the drone body (1), and a propeller is provided on the upper side of the connecting rods (2), characterized in that: The inside of the unmanned aerial vehicle body (1) is provided with a first movable cavity (3), the first movable cavity (3) is a fan-shaped cavity, a swing block (4) is movably arranged in the first movable cavity (3), a first mounting cavity (5) is formed in the side of the swing block (4), a fixed shooting camera (6) is arranged in the first mounting cavity (5), two second movable cavities (7) are symmetrically formed in the inside of the first movable cavity (3), the second movable cavities (7) are arc-shaped cavities, a first clamping structure is fixedly arranged on the side of the swing block (4) corresponding to the position of the second movable cavities (7), two adaptive cavities (8) are symmetrically formed in the side of the swing block (4), the adaptive cavities (8) are arc-shaped grooves, two fixed support frames (9) are arranged on the bottom side of the unmanned aerial vehicle body (1), the support frames (9) are arc-shaped blocks matched with the adaptive cavities (8), a second clamping structure matched with the first clamping structure is arranged at one end of the support frame (9), and an extrusion block (14) for extruding the first clamping structure is arranged on the inside of the second movable cavity (7).

2. The aerial surveying unmanned aerial vehicle for cadastral mapping of claim 1, wherein: The first clamping structure comprises a mounting block (10) fixedly arranged on the side of the swing block (4), a limiting block (11) fixedly arranged on the side of the mounting block (10), and the limiting block (11) is a trapezoidal block. 3.The aerial photography unmanned aerial vehicle for cadastral mapping of claim 2, wherein: A limiting cavity (13) is formed in the center of the side of the limiting block (11), the limiting cavity (13) is an arc-shaped cavity, and the extrusion block (14) is a hollow arc-shaped block.

4. The aerial surveying unmanned aerial vehicle for cadastral mapping of claim 3, wherein: The second clamping structure comprises a connecting block (20) fixedly arranged at one end of the support frame (9), the connecting block (20) is a trapezoidal block, a clamping jaw (12) is fixedly arranged at one end of the connecting block (20), and the clamping jaw (12) is an arc-shaped block matched with the side of the limiting block (11).

5. The aerial surveying unmanned aerial vehicle for cadastral mapping of claim 1, wherein: A first supporting rod (15) is fixedly arranged on the upper side of the support frame (9), one end of the first supporting rod (15) away from the support frame (9) is fixedly arranged on the side of the unmanned aerial vehicle body (1), two second supporting blocks (16) are symmetrically fixedly arranged on the upper side of the support frame (9), one end of the second supporting blocks (16) away from the support frame (9) is fixedly arranged on the side of the unmanned aerial vehicle body (1), two convex blocks (17) are fixedly arranged on the bottom side of the support frame (9), and the convex blocks (17) are arc-shaped blocks.

6. The aerial surveying unmanned aerial vehicle for cadastral mapping of claim 1, wherein: A second mounting cavity (18) is formed in the side of the unmanned aerial vehicle body (1), a fixed rotary motor (19) is arranged in the second mounting cavity (18), and the output end of the rotary motor (19) is fixedly arranged on the side of the swing block (4).

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