Fixed-wing unmanned aerial vehicle with multifunctional mounting system

Abstract

The fixed-wing unmanned aerial vehicle with the multifunctional mounting system comprises an unmanned aerial vehicle body and a mounting assembly, connecting rods are installed on the two sides of the lower portion of the unmanned aerial vehicle body, a mounting column is rotationally installed between the two connecting rods, friction assemblies used for pressing the mounting column are arranged on the surfaces of the connecting rods, and the mounting assembly is connected with the mounting assembly. A plurality of insertion holes are formed in the surface of the mounting column, the mounting assembly comprises studs, an equipment mounting plate and nuts, the studs penetrate through the insertion holes, the equipment mounting plate is fixedly mounted at one ends of the studs, the nuts are mounted on the outer sides of the studs in a threaded mode, and a cambered surface matched with the outer side of the mounting column in shape is arranged on one side of the equipment mounting plate. The stud penetrates through the insertion hole in the proper position of the surface of the mounting column, one side of the cambered surface of the equipment mounting plate is pushed to be attached to the outer side of the mounting column, and then the nut is mounted on the outer side of the stud, so that the equipment mounting plate and the mounting column are fixed, and the mounting work of equipment to be mounted is completed.

Description

Technical Field

[0001] The utility model relates to the technical field of fixed-wing unmanned aerial vehicles, and particularly relates to a fixed-wing unmanned aerial vehicle with a multi-functional mounting system. Background Technique

[0002] Under the background of the rapid development of modern technology, fixed-wing unmanned aerial vehicles play an increasingly important role in multiple fields, such as military reconnaissance, geological exploration, environmental monitoring, etc. These fields often require unmanned aerial vehicles to carry various different devices and components to achieve specific task requirements.

[0003] The mounting methods of traditional unmanned aerial vehicles are usually relatively single, and it is difficult to mount multiple different components at the same time. For example, when performing complex tasks, it may be necessary to carry multiple devices such as radars and cameras at the same time for information collection, but most traditional unmanned aerial vehicles cannot meet such requirements. Therefore, it is often necessary to fly multiple times or use multiple unmanned aerial vehicles, which not only increases the cost and operation difficulty, but also reduces the work efficiency. Moreover, the flexibility of the traditional mounting system is poor and cannot be flexibly adjusted according to the characteristics of different devices and task requirements. When it is necessary to replace the mounted device, it may be necessary to perform complex modifications on the unmanned aerial vehicle, wasting a lot of time and resources. For this reason, we propose a fixed-wing unmanned aerial vehicle with a multi-functional mounting system. Content of the Utility Model

[0004] The purpose of the utility model is to provide a fixed-wing unmanned aerial vehicle with a multi-functional mounting system to solve the problems raised in the above background technique.

[0005] To achieve the above purpose, the utility model provides the following technical solution: A fixed-wing unmanned aerial vehicle with a multi-functional mounting system, including an unmanned aerial vehicle main body and a mounting component. Connecting rods are installed on both sides of the lower part of the unmanned aerial vehicle main body. A mounting column is rotatably installed between the two connecting rods. A friction component for pressing the mounting column is arranged on the surface of the connecting rod.

[0006] A plurality of jacks are opened on the surface of the mounting column. The mounting component includes a stud, an equipment mounting plate and a nut. The stud passes through the jack. One end of the stud is fixedly installed with an equipment mounting plate. A nut is threadedly installed on the outer side of the stud. An arc surface adapted to the outer shape of the mounting column is arranged on one side of the equipment mounting plate.

[0007] Preferably, a plurality of landing gears for supporting the unmanned aerial vehicle main body are installed on the bottom surface of the unmanned aerial vehicle main body.

[0008] Preferably, the friction component includes a sliding rod. The sliding rod slidably penetrates through the connecting rod. An arc-shaped clamping plate is installed at the lower end of the sliding rod. An anti-slip pad is arranged on the bottom surface of the arc-shaped clamping plate. An adjusting part for driving the arc-shaped clamping plate to move is arranged on the top surface of the arc-shaped clamping plate.

[0009] Preferably, the anti-slip pad is bonded to the bottom surface of the arc-shaped clamping plate, and the anti-slip pad is made of rubber material.

[0010] Preferably, the adjusting member includes a threaded rod, the threaded rod threadedly penetrates through the connecting rod, and a knob is installed at the upper end of the threaded rod.

[0011] Preferably, a device to be mounted is mounted on one side of the device mounting plate.

[0012] Compared with the prior art, the beneficial effects of the present utility model are as follows:

[0013] 1. For the fixed-wing UAV with a multi-functional mounting system, the device to be mounted and the device mounting plate are fixed by means of bolts or the like. The stud is passed through the jack at a suitable position on the surface of the mounting column, and the arc-shaped side of the device mounting plate is pushed against the outside of the mounting column. Then, by installing the nut on the outside of the stud, the device mounting plate and the mounting column are fixed, completing the installation of the device to be mounted. Multiple devices that can work at the same angle or multiple identical devices can be mounted on the outside of the mounting column at the same time, improving the practicability of the UAV.

[0014] 2. For the fixed-wing UAV with a multi-functional mounting system, first rotate the mounting column to change the angles of the device mounting plate and the device. After adjusting the device angle to a suitable position, rotate the knob to drive the threaded rod to rotate, thereby driving the arc-shaped clamping plate and the anti-slip pad to move downward until the anti-slip pad is in close contact with the outside of the mounting column, so as to fix the angular position of the mounting column through friction. The adjustment is relatively convenient and easy to use. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 It is a schematic diagram of the overall structure of the present utility model;

[0016] Figure 2 It is a schematic diagram of the bottom structure of the present utility model;

[0017] Figure 3 It is a schematic diagram of the cross-sectional structure of the mounting column of the present utility model;

[0018] Figure 4 It is a schematic diagram of the enlarged structure A of the present utility model.

[0019] In the figure: 1, UAV main body; 2, landing gear; 3, connecting rod; 4, mounting column; 5, sliding rod; 6, arc-shaped clamping plate; 7, anti-slip pad; 8, threaded rod; 9, knob; 10, jack; 11, stud; 12, device mounting plate; 13, nut. DETAILED DESCRIPTION OF THE EMBODIMENTS

[0020] 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 the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative efforts shall fall within the protection scope of the present utility model.

[0021] Embodiment 1

[0022] Please refer to Figures 1-4 As shown, the present utility model provides a fixed-wing unmanned aerial vehicle with a multi-functional mounting system, including an unmanned aerial vehicle main body 1 and a mounting assembly. Connecting rods 3 are installed on both sides of the lower part of the unmanned aerial vehicle main body 1. A mounting column 4 is rotatably installed between the two connecting rods 3. A friction assembly for pressing the mounting column 4 is arranged on the surface of the connecting rod 3.

[0023] A plurality of jacks 10 are formed on the surface of the mounting column 4. The mounting assembly includes a stud 11, an equipment mounting plate 12, and a nut 13. The stud 11 passes through the jack 10. An equipment mounting plate 12 is fixedly installed at one end of the stud 11. A nut 13 is threadedly installed on the outer side of the stud 11. An arc surface adapted to the outer shape of the mounting column 4 is arranged on one side of the equipment mounting plate 12. Equipment to be mounted is installed on one side of the equipment mounting plate 12.

[0024] Specifically, the stud 11 is passed through the jack 10 at a suitable position on the surface of the mounting column 4. The arc surface side of the equipment mounting plate 12 is pushed against the outside of the mounting column 4. Then, by installing the nut 13 on the outer side of the stud 11, the equipment mounting plate 12 is fixed to the mounting column 4, completing the installation work of the equipment to be mounted.

[0025] Among them: A plurality of landing gears 2 for supporting the unmanned aerial vehicle main body 1 are installed on the bottom surface of the unmanned aerial vehicle main body 1.

[0026] Among them: The friction assembly includes a sliding rod 5. The sliding rod 5 slidably penetrates the connecting rod 3. An arc-shaped clamping plate 6 is installed at the lower end of the sliding rod 5. An anti-slip pad 7 is arranged on the bottom surface of the arc-shaped clamping plate 6. An adjusting member for driving the movement of the arc-shaped clamping plate 6 is arranged on the top surface of the arc-shaped clamping plate 6. The anti-slip pad 7 is bonded to the bottom surface of the arc-shaped clamping plate 6. The anti-slip pad 7 is made of rubber material. The adjusting member includes a threaded rod 8. The threaded rod 8 threadedly penetrates the connecting rod 3. A knob 9 is installed at the upper end of the threaded rod 8. Rotating the knob 9 drives the threaded rod 8 to rotate, thereby driving the arc-shaped clamping plate 6 and the anti-slip pad 7 to move downward until the anti-slip pad 7 is in close contact with the outside of the mounting column 4, thereby fixing the angular position of the mounting column 4 through friction.

[0027] Working principle: The utility model is a fixed-wing unmanned aerial vehicle with a multi-functional mounting system. The equipment to be mounted is fixed to the equipment mounting plate 12 by means of bolts or the like. The stud 11 is passed through the jack 10 at a suitable position on the surface of the mounting column 4, and the arc side of the equipment mounting plate 12 is pushed against the outside of the mounting column 4. Then, by installing the nut 13 on the outside of the stud 11, the equipment mounting plate 12 is fixed to the mounting column 4, completing the installation of the equipment to be mounted. Multiple devices that can work at the same angle or multiple identical devices can be mounted on the outside of the mounting column 4 at the same time, improving the practicality of the unmanned aerial vehicle;

[0028] Then, by first rotating the mounting column 4 to change the angles of the equipment mounting plate 12 and the equipment, after adjusting the equipment angle to a suitable position, rotate the knob 9 to drive the threaded rod 8 to rotate, thereby driving the arc-shaped clamping plate 6 and the anti-slip pad 7 to move downward until the anti-slip pad 7 is in close contact with the outside of the mounting column 4, so as to fix the angular position of the mounting column 4 through friction. The adjustment is relatively convenient and easy to use.

[0029] The content not described in detail in this specification belongs to the prior art well-known to those skilled in the art.

[0030] Although the present utility model 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 perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present utility model shall be included within the protection scope of the present utility model.

Claims

1. A fixed-wing UAV with a multifunctional mounting system, comprising a UAV body (1) and a mounting assembly, characterized in that: Connecting rods (3) are installed on both sides of the lower part of the drone body (1), a mounting column (4) is rotatably installed between the two connecting rods (3), and a friction component for pressing the mounting column (4) is provided on the surface of the connecting rod (3); The surface of the mounting column (4) is provided with a plurality of insertion holes (10), and the installation assembly comprises a stud (11), a device installation plate (12) and a nut (13); the stud (11) passes through the insertion hole (10), one end of the stud (11) is fixedly mounted with the device installation plate (12), the outer side of the stud (11) is threadedly mounted with a nut (13), and one side of the device installation plate (12) is provided with an arc surface adapted to the outer shape of the mounting column (4).

2. The fixed-wing UAV with a multifunctional mounting system according to claim 1, characterized in that: A plurality of landing gears (2) for supporting the drone body (1) are installed on the bottom surface of the drone body (1).

3. The fixed-wing UAV with a multifunctional mounting system according to claim 1, characterized in that: The friction assembly comprises a sliding rod (5), the sliding rod (5) slidingly passes through the connecting rod (3), an arc-shaped clamping plate (6) is installed at the lower end of the sliding rod (5), an anti-slip pad (7) is arranged on the bottom surface of the arc-shaped clamping plate (6), and an adjusting member for driving the arc-shaped clamping plate (6) to move is arranged on the top surface of the arc-shaped clamping plate (6).

4. The fixed-wing UAV with a multifunctional mounting system according to claim 3, characterized in that: The anti-skid pad (7) is bonded to the bottom surface of the arc-shaped clamping plate (6), and the anti-skid pad (7) is made of rubber material.

5. The fixed-wing UAV with a multifunctional mounting system according to claim 3, characterized in that: The adjusting member comprises a threaded rod (8), one end of which is rotatably mounted on one side of the arc-shaped clamping plate (6), the threaded rod (8) is threadedly passed through the connecting rod (3), and a knob (9) is mounted on the upper end of the threaded rod (8).

6. The fixed-wing UAV with a multifunctional mounting system according to claim 1, characterized in that: The equipment to be mounted is installed on one side of the equipment mounting plate (12).

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