Carbon fiber unmanned aerial vehicle body

Abstract

The utility model discloses a carbon fiber unmanned aerial vehicle body, and belongs to the technical field of unmanned aerial vehicles. The machine body comprises a machine body made of a carbon fiber material, a mounting plate is mounted on the outer wall of the machine body, the section of the mounting plate is in a right-angle shape, a plurality of mounting holes are formed in the mounting plate, and a plurality of lock catches are arranged on the mounting plate and located at the mounting holes. The lock catch comprises a fixed part and a rotating part installed on the fixed part, and the rotating part can rotate so that the fixed part can be arranged on an object to be transported in a penetrating mode. By arranging the mounting plate and the lock catch, the rotating part is pressed down, then the fixing part penetrates through the to-be-transported object and the mounting plate, and then the rotating part is loosened, the to-be-transported object can be driven to move by movement of the fuselage body, the to-be-transported object cannot be separated from the lock catch, and the to-be-transported object can be transported in the flying process of the fuselage body.

Description

Technical Field

[0001] The present application relates to the field of UAV technology, and in particular to a carbon fiber UAV fuselage. Background Art

[0002] Carbon fiber, a high-strength, high-modulus fiber with a carbon content of over 90%, is an excellent material for manufacturing high-tech equipment such as aerospace. Its low density and light weight significantly reduce the overall weight of drones compared to traditional metal materials, thereby improving their endurance and flight performance.

[0003] The patent with announcement number CN212654531U discloses a civilian express delivery load-bearing drone. In this device, a cargo box is installed on the outer shell of the drone, and the cargo to be transported can be placed in the cargo box. However, the drone usually has limited power, and the cargo box itself has a certain weight. This application can only transport the cargo in the cargo box, but not all cargo needs to be transported in the cargo box. If the cargo box is not installed, there is nowhere to put the cargo, which is more inconvenient. Utility Model Content

[0004] The purpose of this application is to address the above-mentioned problems existing in the prior art and propose a carbon fiber drone fuselage.

[0005] The present application can be implemented through the following technical solution: a carbon fiber drone fuselage, comprising a fuselage body made of carbon fiber material, a mounting plate installed on the outer wall of the fuselage body, the cross-section of the mounting plate is right-angled, a plurality of mounting holes are opened on the mounting plate, and a plurality of locks are provided on the mounting plate and located at the mounting holes, the locks include a fixed part and a rotating part installed on the fixed part, the rotating part can be rotated so that the fixed part can be passed through the object to be transported.

[0006] In the above technical solution, by setting the mounting plate and the lock, pressing the rotating part, and then passing the fixing part through the object to be transported and the mounting plate, and then releasing the rotating part, the movement of the fuselage body can drive the movement of the object to be transported and the object to be transported will not be separated from the lock. The object to be transported can be transported during the flight of the fuselage body.

[0007] Furthermore, a plurality of clips are provided on the fuselage body, and the clips clamp a wrapping layer, and the wrapping layer is used to cover the object to be transported, and a buffer pad is provided on the wrapping layer.

[0008] In the above technical solution, by providing a wrapping layer and a buffer pad on the wrapping layer, when the drone malfunctions and falls, the buffer pad can cushion the object to be transported, thereby reducing the possibility of the object to be transported being damaged by impact.

[0009] Further, the buffer pad is made of sponge.

[0010] In the above technical solution, the sponge is light in weight and is more suitable as a buffer pad.

[0011] Further, male magic tapes are provided on the wrapping layer, and female magic tapes are provided on the buffer pad, and the male magic tapes can be adhered to the female magic tapes.

[0012] In the above technical solution, by providing male magic tapes and female magic tapes, it is convenient to replace the buffer pad when the buffer pad is contaminated or damaged.

[0013] Further, the mounting plate is made of carbon fiber material.

[0014] In the above technical solution, the carbon fiber material has the characteristics of light weight and high strength, and it is more suitable to use a mounting plate made of carbon fiber material.

[0015] Further, the mounting plate is mounted on the fuselage body through a first screw.

[0016] In the above technical solution, the mounting plate is mounted on the fuselage through a first screw, which is convenient for disassembly and assembly.

[0017] Further, several mounting plates are provided, a cargo box is placed between two mounting plates, and threaded holes are provided on the mounting plates.

[0018] In the above technical solution, by providing multiple mounting plates and providing threaded holes on the mounting plates, it is convenient for the installation of the cargo box.

[0019] Further, several buffer pads are provided.

[0020] In the above technical solution, several buffer pads are provided, and the buffering effect on the object to be transported is better.

[0021] In summary, the present application has the following technical effects: by providing a mounting plate and a lock, press the rotating part, then pass the fixing part through the object to be transported and the mounting plate, and then release the rotating part. The fuselage body can drive the object to be transported to move and the object to be transported will not break away from the lock. During the flight of the fuselage body, the object to be transported can be transported. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] Figure 1 is the overall structural schematic diagram of the present application;

[0023] Figure 2 is the position schematic diagram of the mounting plate in the present application;

[0024] Figure 3 is the position schematic diagram of the buffer pad in the present application.

[0025] Description of reference numerals:

[0026] 1. Body; 2. Mounting plate; 21. Mounting hole; 22. Threaded hole; 3. Lock; 31. Fixing part; 32. Rotating part; 4. Clip; 5. Wrapping layer; 6. Cushioning pad; 7. Male Velcro; 8. Female Velcro; 9. Screw 1; 10. Screw 2. DETAILED DESCRIPTION

[0027] Please refer to the attached drawings in the manual Figure 1 and Figure 2 One embodiment of the present application provides a carbon fiber drone fuselage, comprising a fuselage body 1, wherein the fuselage body 1 is used to accommodate electronic devices used in the drone, and a carbon fiber mounting plate 2 is installed at the bottom of the fuselage body 1. The mounting plate 2 is long and has a right-angled cross-section. The horizontal portion of the mounting plate 2 is mounted on the fuselage body 1 by screws 9, and three mounting holes 21 are formed through the vertical portion of the mounting plate 2. Three locks 3 are installed on the mounting plate 2. The locks 3 in this embodiment are key chains, and the locks 3 have a fixed portion 31 and a rotating portion 32 that can rotate relative to the fixed portion 31. By pressing the rotating portion 32, the fixed portion 31 can pass through the mounting hole 21, and the lock 3 can be installed on the mounting plate 2. When the force is removed from the rotating portion 32, the rotating portion 32 can reset itself. At this time, the lock 3 will not be separated from the mounting hole 21. In the same way, the fixed portion 31 can be inserted into the object to be transported. In this embodiment, the object to be transported is a courier. The fixed portion 31 can be inserted into the courier packaging bag of the courier, and the fuselage body 1 can transport the object to be transported during flight.

[0028] Please refer to the attached drawings in the manual Figure 2 and Figure 3 , four clips 4 are provided on the fuselage body 1, and the clips 4 are fixed to the fuselage body 1 by screws 10. The four clips 4 clamp the same wrapping layer 5, which can be a plastic cloth. The wrapping layer 5 can be covered on the object to be transported. A plurality of male Velcro 7 are sewn on the inner wall of the wrapping layer 5, and several buffer pads 6 are provided on the wrapping layer 5. The buffer pad 6 can be a sponge, and a female Velcro 8 is adhered to the buffer pad 6. The male Velcro 7 can be bonded with the female Velcro 8 to fix the position of the buffer pad 6 relative to the wrapping layer 5. By setting the male Velcro 7 and the female Velcro 8, the buffer pad 6 is easy to replace when it is contaminated or damaged.

[0029] Please refer to the attached drawings in the manual Figure 2 There are two mounting plates 2 in total. The length directions of the two mounting plates 2 are consistent. The two mounting plates 2 are spaced apart. A cargo box is placed between the two mounting plates 2. Two threaded holes 22 are provided on the vertical parts of the two mounting plates 2. The cargo box can be installed on the threaded holes 22 by screws 3 to fix the position of the cargo box relative to the fuselage body 1.

[0030] Working principle of this embodiment: The object to be transported is fixed to the mounting plate 2 through the buckle 3, and the object to be transported can be transported during the flight of the fuselage body 1.

[0031] The above are all preferred embodiments of this application. The protection scope of this application is not limited hereby. Therefore, all equivalent changes made according to the structure, shape, and principle of this application shall be covered within the protection scope of this application.

Claims

1. A carbon fiber drone fuselage, characterized in that, It includes a fuselage body (1) made of carbon fiber material. An installation plate (2) is installed on the outer wall of the fuselage body (1). The cross-section of the installation plate (2) is right-angled. Several installation holes (21) are formed in the installation plate (2). Several locks (3) are provided at the positions of the installation holes (21) on the installation plate (2). The lock (3) includes a fixing part (31) and a rotating part (32) installed on the fixing part (31). The rotating part (32) can rotate so that the fixing part (31) can penetrate through the object to be transported.

2. The carbon fiber drone fuselage according to claim 1, wherein Several clips (4) are provided on the fuselage body (1). The clips (4) hold a wrapping layer (5). The wrapping layer (5) is used to cover the object to be transported. A buffer pad (6) is provided at the wrapping layer (5).

3. A carbon fiber drone fuselage according to claim 2, wherein, The buffer pad (6) is made of sponge.

4. A carbon fiber drone fuselage according to claim 2, characterized in that, A male magic tape (7) is provided on the wrapping layer (5), and a female magic tape (8) is provided on the buffer pad (6). The male magic tape (7) can be adhered to the female magic tape (8).

5. A carbon fiber drone fuselage according to claim 1, wherein, The installation plate (2) is made of carbon fiber material.

6. A carbon fiber drone fuselage according to claim 1, characterized in that, The installation plate (2) is installed on the fuselage body (1) through a screw one (9).

7. A carbon fiber drone fuselage according to claim 1, characterized in that, Several installation plates (2) are provided. A shipping container is placed between two installation plates (2). Threaded holes (22) are formed in the installation plate (2).

8. A carbon fiber drone fuselage according to claim 2, characterized in that, Several buffer pads (6) are provided.

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