Vertical take-off and landing unmanned aerial vehicle mounting structure

Abstract

The utility model discloses a vertical take-off and landing unmanned aerial vehicle mounting structure which comprises a mounting mechanism, the upper portion of the mounting mechanism is connected with a vehicle body through bolts, the mounting mechanism comprises a mounting block, two mounting holes are formed in the side face of the mounting block, the bottom of the mounting block is welded to a connecting block, and the side edges of the two ends of the connecting block are arranged to be of a triangular structure. Two connecting plates are welded to the bottom of the connecting block, and vibration receptors are symmetrically installed on the tops of the two sides of each connecting plate. By arranging the mounting box and the mounting block corresponding to the mounting box, the structures of the mounting box and the mounting block are simple, the mounting is relatively convenient, and the use cost and the time cost are greatly reduced; the vibration sensor is placed on the connecting plate, vibration of the mounting mechanism can be sensed through the vibration sensor so as to generate data, the loosening condition of the mounting mechanism can be known in advance by analyzing the data, and the safety of ground personnel and facilities is effectively improved.

Description

Technical Field

[0001] This utility model relates to the technical field of airframe mounting mechanisms, and in particular to a mounting structure for a vertical take-off and landing unmanned aerial vehicle (UAV). Background Technology

[0002] The technological background of aircraft mounting mechanisms is closely related to the development of aircraft technology and application needs, and these mechanisms continue to evolve with the increasing number of application scenarios. For example, in logistics and distribution, mounting mechanisms need to be able to stably carry goods and achieve precise delivery; in the surveying and mapping field, high-precision surveying equipment needs to be mounted, requiring mounting mechanisms to have good stability and shock absorption performance to ensure the accuracy of surveying data; in the firefighting field, fire extinguishing equipment needs to be mounted to achieve rapid response and fire suppression.

[0003] Currently, related mounting devices and drones, such as the Chinese patent "A Mounting Device and Drone" with authorization announcement number CN 211893680U, include a quick-release assembly for connecting to the drone; a connector connected to the quick-release assembly, with both ends of the connector extending to the sides to form two fixing parts; a camera assembly disposed on one of the fixing parts; and a speaker assembly disposed on the other fixing part; the drone is equipped with the aforementioned mounting device.

[0004] The design of the mounting mechanism in existing related technologies is relatively complex, the installation process is cumbersome, and it requires professional personnel to operate, which increases the cost of use and time. Utility Model Content

[0005] The purpose of this utility model is to provide a mounting structure for vertical take-off and landing unmanned aerial vehicles (UAVs), which includes a mounting box and a corresponding mounting block. The simple structure of the mounting box and mounting block reduces usage and time costs. By placing a vibration sensor on the connecting plate, the vibration of the mounting mechanism can be sensed, thereby generating data. By analyzing the data, the loosening of the mounting mechanism can be detected in advance, effectively increasing the safety of ground personnel and facilities.

[0006] To achieve the above objectives, a vertical take-off and landing (VTOL) UAV mounting structure is provided, including a mounting mechanism. The mounting mechanism is bolted to the upper part of the UAV. The mounting mechanism includes a mounting block with two mounting holes on its side, which are symmetrical about the side center. The bottom of the mounting block is welded to a connecting block, and the two short sides of the connecting block are configured as a triangular structure. Two connecting plates are welded to the bottom of the connecting block, and these connecting plates are mirror-symmetrical about the center line of the long surface of the connecting block. Vibration sensors are symmetrically mounted on the top of both sides of the connecting plates, which can effectively increase the safety of the UAV.

[0007] According to the aforementioned vertical take-off and landing UAV mounting structure, the characteristic is that two mounting frames are welded to the bottom of both sides of the connecting plate, the two mounting frames are symmetrical about the center line of the connecting block, and the two short sides of the mounting frames are set as triangular structures.

[0008] According to the aforementioned vertical take-off and landing (VTOL) UAV mounting structure, the body includes a shell, the shell being a cube structure, four wings fixedly connected to the four corners of the shell, the wings being made of stainless steel, a first connecting post fixedly connected to the upper side of the wing, a second connecting post coaxially connected to the top surface of the first connecting post, a third connecting post coaxially connected to the top surface of the second connecting post, and propellers evenly distributed on the side of the third connecting post.

[0009] According to the aforementioned vertical take-off and landing UAV mounting structure, the bottom front end of the fuselage is bolted to a connecting seat, and a night vision camera is bolted to the bottom of the connecting seat; a flight control board is fixedly connected to the bottom of the fuselage, and the flight control board is fixedly connected to the side away from the connecting seat.

[0010] According to the aforementioned vertical take-off and landing UAV mounting structure, the bottom corner of the fuselage is bolted to a connecting base, the bottom of the connecting base is bolted to a motor, the bottom of the fuselage is bolted to a battery box, a battery is placed inside the battery box, and the battery is electrically connected to the motor.

[0011] According to the aforementioned vertical take-off and landing UAV mounting structure, the two mounting boxes are fixedly connected to both sides of the bottom of the casing. The two mounting boxes are symmetrical about the center of the bottom surface. The long side of the mounting box is provided with two through holes, which correspond to the mounting holes.

[0012] The above-mentioned solution has the following beneficial effects:

[0013] 1. By setting up an installation box and its corresponding installation block, the structure of the installation box and installation block is simple and easy to install, which greatly reduces the cost of use and time.

[0014] 2. By placing vibration sensors on the connecting plate, the vibration of the mounting mechanism can be sensed and data can be generated. By analyzing the data, the loosening of the mounting mechanism can be known in advance, which effectively increases the safety of personnel and facilities on the ground.

[0015] Additional aspects and advantages of this invention will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. Attached Figure Description

[0016] The present invention will be further described below with reference to the accompanying drawings and embodiments;

[0017] Figure 1 This is a three-dimensional view of the overall structure of a vertical take-off and landing unmanned aerial vehicle (UAV) mounting structure according to this utility model;

[0018] Figure 2 This is a perspective view of the mounting mechanism of a vertical take-off and landing unmanned aerial vehicle (UAV) according to this utility model.

[0019] Figure 3 This is a frontal offset view of the overall structure of the vertical take-off and landing unmanned aerial vehicle (UAV) mounting structure of this utility model;

[0020] Figure 4 This is a top view of the overall structure of a vertical take-off and landing unmanned aerial vehicle (UAV) mounting structure according to this utility model;

[0021] Figure 5 This is a front view of a UAV with a vertical take-off and landing (VTOL) UAV mounting structure according to the present invention.

[0022] Figure 6 This is a top view of the mounting mechanism of a vertical take-off and landing unmanned aerial vehicle (UAV) according to this utility model.

[0023] Legend:

[0024] 1. Wing; 2. Fuselage; 3. Motor; 4. Propeller; 5. First connecting post; 6. Third connecting post; 7. Casing; 8. Second connecting post; 9. Night vision camera; 10. Connecting bracket; 11. Battery box; 12. Connecting base; 13. Flight control board; 14. Connecting plate; 15. Connecting block; 16. Mounting block; 17. Vibration sensor; 18. Mounting rack; 19. Mounting hole; 20. Mounting mechanism; 21. Mounting box; 22. Through hole. Detailed Implementation

[0025] This section will describe in detail the specific embodiments of the present utility model. The preferred embodiments of the present utility model are shown in the accompanying drawings. The purpose of the drawings is to supplement the textual description with graphics, so that people can intuitively and vividly understand each technical feature and the overall technical solution of the present utility model, but they should not be construed as limiting the scope of protection of the present utility model.

[0026] Reference Figure 1-6 This utility model embodiment provides a vertical take-off and landing unmanned aerial vehicle (UAV) mounting structure, which includes:

[0027] Specifically: a mounting mechanism 20 is bolted to the upper part of the mounting mechanism 20, the mounting mechanism 20 includes a mounting block 16, the mounting block 16 has two mounting holes 19 on its side, the two mounting holes 19 are symmetrical about the side center, the bottom of the mounting block 16 is welded to the connecting block 15, the two short sides of the connecting block 15 are set as a triangular structure; the bottom of the connecting block 15 is welded to two connecting plates 14, the two connecting plates 14 are mirror symmetrical about the center line of the long surface of the connecting block 15, and vibration sensors 17 are symmetrically installed on the top of both sides of the connecting plates 14, which can effectively increase the safety of the body 2.

[0028] It should be noted that by placing a vibration sensor 17 on top of the connecting plate 14, the vibration of the mounting mechanism 20 can be sensed by the vibration sensor 17, thereby generating data. By analyzing the data, the loosening of the mounting mechanism 20 can be known in advance, which effectively increases the safety of ground personnel and facilities.

[0029] Specifically, two mounting brackets 18 are welded to the bottom of both sides of the connecting plate 14. The two mounting brackets 18 are symmetrical about the center line of the connecting block 15, and the two short sides of the mounting brackets 18 are set as triangular structures.

[0030] It should be noted that by setting the short face to a triangular structure, wind resistance can be effectively reduced, resulting in less drag and smoother flight for the drone.

[0031] Specifically: the body 2 includes a shell 7, which is a cube structure. Four wings 1 are fixedly connected to the four corners of the shell 7. The wings 1 are made of stainless steel. A first connecting post 5 is fixedly connected to the upper side of the wings 1. A second connecting post 8 is coaxially connected to the top surface of the first connecting post 5. A third connecting post 6 is coaxially connected to the top surface of the second connecting post 8. Propellers 4 are evenly distributed on the side of the third connecting post 6.

[0032] It should be noted that by setting wings 1 at the four corners of the fuselage 7, the overall force on the fuselage 2 can be evenly distributed, making it less prone to shaking and maintaining excellent stability.

[0033] Specifically: a connector 10 is bolted to the bottom front end of the housing 7, and a night vision camera 9 is bolted to the bottom of the connector 10; a flight control board 13 is fixedly connected to the bottom of the housing 7, and the flight control board 13 is fixedly connected to the side away from the connector 10.

[0034] It should be noted that by installing a night vision camera 9 on the body 2, the body 2 can work at night, making it unrestricted by time and greatly improving its efficiency.

[0035] Specifically: a connecting base 12 is bolted to one corner of the bottom of the housing 7, a motor 3 is bolted to the bottom of the connecting base 12, a battery box 11 is bolted to the bottom of the housing 7, a battery is placed inside the battery box 11, and the battery is electrically connected to the motor 3.

[0036] It should be noted that by setting the motor 3 and battery box 11 at the bottom of the casing 7, the body 2 can be provided with continuous power.

[0037] Specifically, two mounting boxes 21 are fixedly connected to both sides of the bottom of the housing 7. The two mounting boxes 21 are symmetrical about the center of the bottom surface. Two through holes 22 are opened on the long side of the mounting box 21, and the two through holes 22 correspond to the mounting holes 19.

[0038] It should be noted that by setting up the installation box 21 and its corresponding installation block 16, the structure of the installation box 21 and the installation block 16 is simple and easy to install, which greatly reduces the cost of use and time.

[0039] Working principle: When the drone is working, the battery in the battery box provides power to the motor. The motor rotates, and the drone begins to take off. At this time, the night vision camera is turned on, and the electronic device can observe the ground below through the camera. The night vision camera is used, and the mounting box 21 and its corresponding mounting block 16 are set up. The structure of the mounting box 21 and the mounting block 16 is simple and easy to install. By placing a vibration sensor 17 on the connecting plate 14, the vibration sensor 17 can sense the vibration of the mounting mechanism 20 and generate data. By analyzing the data, the looseness of the mounting mechanism 20 can be known in advance, which effectively increases the safety of ground personnel and facilities. By setting a flight control board on the top of the drone, which is the brain of the drone, it is responsible for processing sensor data, controlling flight attitude and navigation. The operator can easily operate the drone, so that the drone can move better in the air.

[0040] The embodiments of the present utility model have been described in detail above with reference to the accompanying drawings. However, the present utility model is not limited to the above embodiments. Within the scope of knowledge possessed by those skilled in the art, various changes can be made without departing from the spirit of the present utility model.

Claims

1. A mounting structure for a vertical takeoff and landing unmanned aerial vehicle (UAV), comprising: The mounting mechanism (20) is bolted to the upper part of the mounting mechanism (20), characterized in that the mounting mechanism (20) includes a mounting block (16), the mounting block (16) has two mounting holes (19) on its side, the two mounting holes (19) are symmetrical about the side center, the bottom of the mounting block (16) is welded to a connecting block (15), the two ends of the connecting block (15) are set as triangular structures; the bottom of the connecting block (15) is welded with two connecting plates (14), the two connecting plates (14) are mirror symmetrical about the long surface center line of the connecting block (15), and vibration sensors (17) are symmetrically installed on the top of both sides of the connecting plates (14).

2. The mounting structure for a vertical takeoff and landing unmanned aerial vehicle (UAV) according to claim 1, characterized in that, Two mounting brackets (18) are welded to the bottom of both sides of the connecting plate (14). The two mounting brackets (18) are symmetrical about the center line of the connecting block (15), and the two short sides of the mounting brackets (18) are set as triangular structures.

3. The mounting structure for a vertical takeoff and landing unmanned aerial vehicle (UAV) according to claim 1, characterized in that, The body (2) includes a shell (7), which is a cube structure. Four wings (1) are fixedly connected to the four corners of the shell (7). The wings (1) are made of stainless steel. A first connecting post (5) is fixedly connected to the upper side of the wing (1). A second connecting post (8) is coaxially connected to the top surface of the first connecting post (5). A third connecting post (6) is coaxially connected to the top surface of the second connecting post (8). Propellers (4) are evenly distributed on the side of the third connecting post (6).

4. The mounting structure for a vertical takeoff and landing unmanned aerial vehicle (UAV) according to claim 3, characterized in that, The bottom front end of the housing (7) is bolted to a connecting seat (10), and a night vision camera (9) is bolted to the bottom of the connecting seat (10); a flight control board (13) is fixedly connected to the bottom of the housing (7), and the flight control board (13) is fixedly connected to the side away from the connecting seat (10).

5. The mounting structure for a vertical takeoff and landing unmanned aerial vehicle (UAV) according to claim 3, characterized in that, A connecting base (12) is bolted to one corner of the bottom of the housing (7), and a motor (3) is bolted to the bottom of the connecting base (12). A battery box (11) is bolted to the bottom of the housing (7), and a battery is placed inside the battery box (11). The battery is electrically connected to the motor (3).

6. The mounting structure for a vertical takeoff and landing unmanned aerial vehicle (UAV) according to claim 3, characterized in that, Two mounting boxes (21) are fixedly connected to the two sides of the bottom of the housing (7). The two mounting boxes (21) are symmetrical about the center of the bottom surface. Two through holes (22) are opened on the long side of the mounting box (21), and the two through holes (22) correspond to the mounting holes (19).

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