Novel unmanned aerial vehicle arm

Abstract

The novel unmanned aerial vehicle arm comprises a supporting assembly and a limiting assembly, the limiting assembly is installed in the supporting assembly and used for further limiting the supporting assembly, the supporting assembly comprises a vehicle body, the vehicle body extends outwards to be provided with a first vehicle arm, and the first vehicle arm is provided with a second vehicle arm. The first vehicle arm is arranged at one end of the vehicle body, a second vehicle arm corresponding to the first vehicle arm is arranged at one end of the vehicle body, and the second vehicle arm is arranged at one end of the vehicle body. The novel unmanned aerial vehicle arm can show higher flexibility and adaptability in a complex and changeable task environment. The unmanned aerial vehicle can be rapidly adjusted according to different task requirements through the adjustable structures of the first vehicle arm and the second vehicle arm and the ingenious layout of the arc-shaped plate, the connecting support and other components, and therefore the operation efficiency and accuracy are effectively improved.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) technology, specifically a novel UAV arm. Background Technology

[0002] With the rapid development of drone technology, drones have demonstrated broad application potential in numerous fields. From initial military reconnaissance to today's civilian aerial photography, logistics delivery, and agricultural plant protection, the functions and application scenarios of drones are constantly expanding. In this process, the drone arm, as an important component of the drone, directly affects the drone's operational flexibility, load capacity, and operational efficiency. Traditional drone arms typically adopt a fixed design. While this design is simple in structure, it lacks flexibility and adaptability when facing complex and ever-changing mission environments. To address this issue, the inventors have proposed a novel drone arm. Utility Model Content

[0003] To address the shortcomings of the aforementioned technologies, this utility model provides a novel unmanned aerial vehicle (UAV) arm.

[0004] To achieve the above objectives, the present invention adopts the following technical solution: a novel unmanned aerial vehicle (UAV) arm, comprising a support component and a limiting component, wherein the limiting component is installed inside the support component for further limiting the support component; the support component comprises a fuselage body, wherein a first arm extends outward from the fuselage body and is disposed at one end of the fuselage body; and a second arm corresponding to the first arm is disposed at one end of the fuselage body.

[0005] As further explained, the first arm extends outward and is provided with an arc-shaped plate, which is respectively disposed between the first arm and the second arm.

[0006] As further explained, the arc-shaped plate extends outward and is provided with a connecting bracket, which is located at one end of the arc-shaped plate. The connecting bracket extends outward and is provided with an inner side plate, which is located at one end of the connecting bracket.

[0007] As further explained, the limiting component includes arm limiting holes, which are respectively opened on the inner sidewalls of the first arm and the second arm, and there are multiple arm limiting holes arranged at intervals.

[0008] As a further explanation, it also includes a latch, which is located in the middle of the main body and is used to engage with other components.

[0009] As a further explanation, it also includes a mounting groove, which is formed on one side wall of the connecting bracket. The mounting groove extends outward and has mounting holes formed on the inner side wall of the mounting groove. There are multiple mounting holes that are spaced apart.

[0010] As a further explanation, it also includes a groove, which is formed inside the body of the device. The groove extends outward and is provided with a connecting hole. The connecting hole is located inside the groove, and there are multiple connecting holes arranged at intervals.

[0011] As a further explanation, it also includes a limiting plate, which is disposed on the inner side wall of the connecting bracket and is used to limit the movement of mating parts.

[0012] In summary, this utility model has the following beneficial effects: This utility model provides a novel drone arm that, through the design of support and limiting components, exhibits greater flexibility and adaptability in complex and ever-changing task environments. The adjustable structure of the first and second arms, along with the ingenious layout of components such as the arc-shaped plate and connecting brackets, allows the drone to quickly adjust according to different task requirements, thereby effectively improving operational efficiency and accuracy. Attached Figure Description

[0013] Figure 1 This is a three-dimensional structural diagram of a novel unmanned aerial vehicle (UAV) arm according to the present invention;

[0014] Figure 2 This is a three-dimensional structural diagram of a novel unmanned aerial vehicle (UAV) arm according to the present invention;

[0015] Figure 3 This is a schematic diagram of the structure of a novel unmanned aerial vehicle (UAV) arm according to this utility model. Detailed Implementation

[0016] 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.

[0017] like Figure 1-3As shown, this utility model discloses a novel UAV arm, including a support component and a limiting component. The limiting component is installed inside the support component to further limit the support component. The support component includes a fuselage body 11, and a first arm 101 extends outward from the fuselage body 11. The first arm 101 is located at one end of the fuselage body 11, and a second arm 102 corresponding to the first arm 101 is located at one end of the fuselage body 11.

[0018] Specifically, the fuselage 11, as the core part of the drone, carries all the key components. The first arm 101 and the second arm 102 extend outward from one end of the fuselage 11, forming the drone's dual-arm structure.

[0019] The first arm 101 extends outward and is provided with an arc-shaped plate 111. The arc-shaped plate 111 is respectively located between the first arm 101 and the second arm 102. The arc-shaped plate 111 extends outward and is provided with a connecting bracket 110. The connecting bracket 110 is located at one end of the arc-shaped plate 111. The connecting bracket 110 extends outward and is provided with an inner side plate 120. The inner side plate 120 is located at one end of the connecting bracket 110.

[0020] Specifically, the arc-shaped plate 111 connects the first arm 101 and the second arm 102, which not only enhances the overall strength of the arms but also provides an installation base for the connecting bracket 110. The connecting bracket 110 extends further outward, and the inner side plate 120 is provided with an interface for installing other components.

[0021] The limiting assembly includes arm limiting holes 21, which are respectively opened on the inner sidewalls of the first arm 101 and the second arm 102. Multiple arm limiting holes 21 are provided and spaced apart. It also includes a buckle 201, which is located in the middle of the body 11 and is used to cooperate with other parts. It also includes a mounting groove 210, which is opened on one sidewall of the connecting bracket 110. The mounting groove 210 extends outward to provide mounting holes 211, which are opened on the inner sidewall of the mounting groove 210. Multiple mounting holes 211 are provided and spaced apart. It also includes a groove 220, which is opened inside the body 11. The groove 220 extends outward to provide connecting holes 221, which are located inside the groove 220. Multiple connecting holes 221 are provided and spaced apart.

[0022] Specifically, the arm limiting hole 21 is formed on the inner sidewall of the first arm 101 and the second arm 102 to precisely limit the extension position of the arm and ensure the stability of the arm during extension and retraction. The buckle 201 is located in the middle of the body 11 and, through cooperation with other components, achieves a stable connection between the arm and the body. The mounting groove 210 and mounting hole 211 are used to install and fix other key components, such as motors and cameras. The design of the groove 220 and the connection hole 221 facilitates the connection between the connecting bracket 110 and the body 11, while providing additional limiting functions to ensure the stability of the connecting bracket 110 during operation.

[0023] It also includes a limiting plate 222, which is located on the inner side wall of the connecting bracket 110 and is used to limit the movement of mating parts.

[0024] Specifically, when the drone needs to adjust its flight attitude or perform a specific task, the first arm 101 and the second arm 102 in the support assembly will adjust according to the control command. At this time, the arm limiting hole 21 in the limiting assembly will precisely limit the range of motion of the arm, ensuring the stability and accuracy of the arm during extension or retraction.

[0025] Meanwhile, components such as the clip 201, mounting slot 210, and mounting hole 211 work together to ensure a tight fit and secure connection between the components. This precise fit not only improves the overall structural stability of the drone but also reduces the risk of components loosening or being damaged due to vibration or external impact.

[0026] During operation, the inner plate 120 on the connecting bracket 110 supports other critical components, such as motors and cameras, ensuring that these components can work stably and perform at their best. The limiting plate 222 limits the mating parts to prevent safety accidents caused by parts falling off or becoming loose.

[0027] It will be apparent to those skilled in the art that this invention is not limited to the details of the exemplary embodiments described above, and that it can be implemented in other specific forms without departing from the spirit or essential characteristics of this invention. Therefore, the embodiments should be considered illustrative and non-limiting in all respects, and the scope of this invention is defined by the appended claims rather than the foregoing description. Thus, it is intended that all variations falling within the meaning and scope of equivalents of the claims be included within this invention. No reference numerals in the claims should be construed as limiting the scope of the claims.

[0028] Furthermore, it should be understood that although this specification describes embodiments, not every embodiment contains only one independent technical solution. This narrative style is merely for clarity. Those skilled in the art should consider the specification as a whole, and the technical solutions in each embodiment can also be appropriately combined to form other embodiments that can be understood by those skilled in the art.

Claims

1. A novel drone arm characterized by: Including support assembly; Limiting assembly, the limiting assembly is installed in the inside of the support assembly, for further limiting of the support assembly; The support assembly includes a fuselage body, the first machine arm is provided outside the fuselage body, the first machine arm is arranged at one end of the fuselage body, and the second machine arm corresponding to the first machine arm is arranged at one end of the fuselage body.

2. The novel unmanned aerial vehicle arm according to claim 1, wherein: The first machine arm is provided outside the arc-shaped plate, and the arc-shaped plate is arranged between the first machine arm and the second machine arm.

3. The novel unmanned aerial vehicle arm of claim 2, wherein: The connecting bracket is provided outside the arc-shaped plate, the connecting bracket is arranged at one end of the arc-shaped plate, the inner side plate is provided outside the connecting bracket, and the inner side plate is arranged at one end of the connecting bracket.

4. The novel unmanned aerial vehicle arm of claim 3, wherein: The limiting assembly includes a machine arm limiting hole, the machine arm limiting hole is respectively arranged in the inner side wall of the first machine arm and the second machine arm, and the machine arm limiting hole is provided with a plurality of and is arranged at intervals.

5. The novel drone arm of claim 4, wherein: It also includes a buckle, the buckle is arranged in the middle of the fuselage body, for the cooperation of the remaining parts.

6. The novel unmanned aerial vehicle arm of claim 5, wherein: It also includes a mounting groove, the mounting groove is arranged on the side wall of the connecting bracket, the mounting groove is provided outside the mounting hole, the mounting hole is arranged in the inner side wall of the mounting groove, the mounting hole is provided with a plurality of and is arranged at intervals.

7. The novel drone arm of claim 6, wherein: It also includes a groove, the groove is arranged in the inside of the fuselage body, the connecting hole is provided outside the groove, the connecting hole is arranged in the inside of the groove, the connecting hole is provided with a plurality of and is arranged at intervals.

8. The novel drone arm of claim 7, wherein: It also includes a limiting plate, the limiting plate is arranged in the inner side wall of the connecting bracket, for limiting the cooperating parts.

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