Anti-interference unmanned aerial vehicle core component copper plating film covering cap

Abstract

The application discloses an anti-interference unmanned aerial vehicle core component copper-plated film covering cap and relates to the technical field of unmanned aerial vehicles.The application comprises a bottom plate, the top of the bottom plate is provided with spare parts, and the top of the bottom plate is provided with a top cover; a dismounting assembly is arranged in the inner cavity of the bottom plate, and the dismounting assembly comprises a rotating rod movably connected to the inner cavity of the bottom plate.The linkage structure of the rotating rod and the cam drives the sliding block to slide transversely, the inserting rod is quickly inserted into or withdrawn from the insertion slot at the bottom of the top cover, the elastic reset function of the first spring is matched, one-handed operation type dismounting of the cover body is realized, the application is especially suitable for narrow space operation, in addition, the inclined surfaces of the inclined block and the inclined strip automatically push the reinforcing plate to press the spare parts when the top cover is closed, the buffer effect of the second spring is combined, the structural stability after installation is ensured, the tool operation required by traditional bolt fixing is avoided, and therefore, the task response efficiency and practicality of the unmanned aerial vehicle are improved.

Description

Technical Field

[0001] This invention belongs to the field of unmanned aerial vehicle (UAV) technology, and in particular relates to a copper-plated film covering for anti-interference UAV core components. Background Technology

[0002] The enclosure for the core components of a drone refers to the outer shell or cover used to protect the core components inside the drone. Its main function is to provide physical protection for the drone's key electronic components, sensors, flight control system, battery, power system, etc., and to prevent damage to the internal components from external environmental factors such as rain, dust, moisture, and collisions. The enclosure not only plays a protective role, but also needs to take into account aerodynamic performance to ensure the drone's flight stability and efficiency.

[0003] Existing drone core component covers still present some problems during use. For example, the installation space for many drone core components is relatively small, and existing covers are usually fixed to the surface of the core components with bolts. Although this fixing method is simple and effective, it is difficult to install and disassemble in a confined space, making the operation cumbersome and affecting the performance. Due to space constraints, operators need to spend more time and effort on installation and maintenance, thereby reducing the drone's work efficiency and convenience. In addition, drones may be subject to electromagnetic interference from internal systems or the external environment during flight, and most covers lack effective anti-interference design, which can easily affect the drone's flight stability and mission execution.

[0004] To address these issues, we provide an anti-interference copper-plated film covering for core components of drones. Summary of the Invention

[0005] The purpose of this invention is to provide an anti-interference copper-plated film covering for the core components of drones. By combining disassembly and assembly components and composite components, it solves the problems of inconvenient disassembly and assembly and poor anti-interference capability of the existing drone core component coverings.

[0006] To solve the above-mentioned technical problems, the present invention is achieved through the following technical solution.

[0007] This invention relates to a copper-plated film covering for anti-interference core components of a drone, comprising a base plate, components mounted on the top of the base plate, and a top cover mounted on the top of the base plate; a disassembly assembly is provided in the inner cavity of the base plate, the disassembly assembly comprising a rotating rod movably connected to the inner cavity of the base plate, cams fixedly connected to both sides of the rotating rod surface, sliders slidably connected to both sides of the inner cavity of the base plate, and a plug rod fixedly connected to one side of the slider, the disassembly assembly being used for quick disassembly and assembly of the covering; a composite component is provided on the surface of the top cover, the composite component comprising an energy-absorbing layer, a shielding layer fixedly connected to the surface of the energy-absorbing layer, and an anti-collision layer fixedly connected to the surface of the shielding layer, the composite component being composed of the energy-absorbing layer, the shielding layer, and the anti-collision layer.

[0008] The invention is further configured such that a positioning groove is provided on the top of the base plate, and support bars are fixedly connected to both sides of the top of the positioning groove. An inclined block is slidably connected to one side of the inner cavity of the support bar, and a reinforcing plate is fixedly connected to one side of the inclined block.

[0009] The present invention is further configured such that positioning plates are fixedly connected to both sides of the inner cavity of the base plate, and a first spring is sleeved on the surface of the insertion rod. One end of the first spring is fixedly connected to one side of the positioning plate, and the other end of the first spring is fixedly connected to one side of the slider.

[0010] The invention is further configured such that a second spring is sleeved on the surface of the inclined block, and inclined strips are fixedly connected to both sides of the inner cavity of the top cover, with one side of the inclined block slidably connected to one side of the inclined strip.

[0011] The present invention is further configured such that a heat-conducting plate is fixedly connected to the top of the inner part of the top cover, and the bottom of the heat-conducting plate is in contact with the top of the component.

[0012] The present invention is further configured such that the energy-absorbing layer is made of foamed silicone, the shielding layer is made of copper-plated film, and the anti-collision layer is made of ultra-high molecular weight polyethylene.

[0013] The present invention is further configured such that slots are provided on both sides of the top of the base plate, and one side of the bottom of the top cover is slidably connected to the inner cavity of the slot.

[0014] The present invention has the following beneficial effects.

[0015] 1. This invention uses a linkage structure between a rotating rod and a cam to drive a slider to slide laterally, allowing the insertion rod to quickly insert into or retract from the slot at the bottom of the top cover. Combined with the elastic reset function of the first spring, it enables one-handed disassembly and assembly of the cover, making it particularly suitable for operations in confined spaces. Furthermore, the inclined surfaces of the inclined block and the inclined strip automatically push the reinforcing plate to press the components when the top cover is closed. Combined with the buffering effect of the second spring, this ensures the structural stability after installation and avoids the tool operation required for traditional bolt fixing, thereby improving the mission response efficiency and practicality of the UAV.

[0016] 2. This invention achieves electromagnetic shielding, physical protection, and heat dissipation optimization simultaneously within a single enclosure through the integration of multi-layer materials in composite components. The shielding layer composed of copper-plated film can effectively reflect or absorb electromagnetic waves, reducing the impact of internal and external electromagnetic interference on the flight control system. The ultra-high molecular weight polyethylene anti-collision layer provides high impact resistance, resisting the risk of collisions or falls during flight. The foamed silicone energy-absorbing layer buffers vibration energy through elastic deformation, protecting precision electronic components. Furthermore, the heat-conducting plate is in direct contact with the components, efficiently conducting heat to the surface of the enclosure for diffusion, solving the heat dissipation problem in a confined environment.

[0017] Of course, any product implementing this invention does not necessarily need to achieve all of the advantages described above at the same time. Attached Figure Description

[0018] To more clearly illustrate the technical solutions of the embodiments of the present invention, the accompanying drawings used in the description of the embodiments will be briefly introduced below.

[0019] Figure 1 A three-dimensional view of a copper-plated film covering for a core component of an anti-interference drone.

[0020] Figure 2 An exploded view of the bottom plate and top cover of a copper-plated film-coated cover for a core component of an anti-interference drone.

[0021] Figure 3 This is a schematic diagram of the top structure of the bottom plate of a copper-plated film-coated cover for a core component of an anti-interference drone.

[0022] Figure 4 This is a cross-sectional view of the bottom plate of a copper-plated film-coated cover for an anti-interference drone core component.

[0023] Figure 5 An exploded view of the internal structure of the base plate of a copper-plated film-coated cover for a core component of an anti-interference drone.

[0024] Figure 6 This is a schematic diagram of the material composition of a copper-plated film-coated composite component for an anti-interference drone core component.

[0025] In the attached diagram: 1. Base plate; 2. Components; 3. Top cover; 4. Rotating rod; 5. Cam; 6. Slider; 7. Insert rod; 8. Energy-absorbing layer; 9. Shielding layer; 10. Anti-collision layer; 11. Positioning groove; 12. Support bar; 13. Inclined block; 14. Reinforcing plate; 15. Positioning plate; 16. First spring; 17. Second spring; 18. Inclined bar; 19. Heat-conducting plate. Detailed Implementation

[0026] The technical solutions of the present invention will be described below with reference to the accompanying drawings. The described embodiments are only some embodiments of the present invention, and not all embodiments.

[0027] Example 1 Please see Figures 1-6 This invention relates to a copper-plated film covering for anti-interference core components of a drone, comprising a base plate 1, mounting blocks fixedly connected to all four sides of the base plate 1, bolts threaded into the inner cavity of the mounting blocks to facilitate the installation of the base plate 1 in the required position, and subsequent installation of a top cover 3. A component 2, the core component required by the drone, is located on the top of the base plate 1. A top cover 3 is also located on the top of the base plate 1. Circular insertion holes are provided on both sides of the bottom of the top cover 3 to allow insertion rods 7 to extend into the inner cavity of the top cover 3. A disassembly assembly is provided within the inner cavity of the base plate 1, including a rotating rod 4 movably connected to the inner cavity of the base plate 1. One end of the rotating rod 4 is rotatably connected to one side of the inner cavity of the base plate 1 via a rotating shaft, and the other end extends to the outside of the base plate 1, with a handwheel fixedly connected to this end. A limit pin is threadedly connected to one side of the inner cavity of the handwheel to limit the position of the rotating rod 4. Cams 5 are fixedly connected to both sides of the surface of the rotating rod 4. The slide block 6 can be rotated at a certain angle to facilitate its movement. The slide block 6 is slidably connected to both sides of the inner cavity of the base plate 1. Limiting strips are fixedly connected to the top and bottom of the base plate 1 to limit the movement of the slide block 6. A plug rod 7 is fixedly connected to one side of the slide block 6. One end of the plug rod 7 is angled so that when the top cover 3 is inserted, the plug rod 7 can automatically insert into the circular insertion hole of the top cover 3. The disassembly and assembly assembly is used for quick disassembly and assembly of the cover. The surface of the top cover 3 is provided with a composite assembly, which includes an energy-absorbing layer 8. A shielding layer 9 is fixedly connected to the surface of the energy-absorbing layer 8. An anti-collision layer 10 is fixedly connected to the surface of the shielding layer 9. The composite assembly is composed of the energy-absorbing layer 8, the shielding layer 9, and the anti-collision layer 10. The energy-absorbing layer 8 is located in the innermost layer of the top cover 3, the shielding layer 9 is in the middle layer of the top cover 3, and the anti-collision layer 10 is located in the outermost layer of the top cover 3 to provide different protections for the components 2 inside the top cover 3.

[0028] Example 2 Please see Figures 1-6Based on embodiment 1, a positioning groove 11 is provided on the top of the base plate 1. The size of the positioning groove 11 is set according to the size of the component 2 to facilitate the positioning of the component 2. Support bars 12 are fixedly connected to both sides of the top of the positioning groove 11. An inclined block 13 is slidably connected to one side of the inner cavity of the support bar 12. A limit opening is provided on the top of the support bar 12. The inclined block 13 slides in the inner cavity of the limit opening. A locking block is fixedly connected to one side of the inclined block 13 to prevent the inclined block 13 from separating from the inner cavity of the limit opening. A reinforcing plate 14 is fixedly connected to one side of the inclined block 13. The reinforcing plate 14 is used to clamp and position the components 2 on both sides. Positioning plates 15 are fixedly connected to both sides of the inner cavity of the base plate 1. A first spring 16 is sleeved on the surface of the insertion rod 7. One end of the first spring 16 is fixedly connected to one side of the positioning plate 15, and the other end of the first spring 16 is fixedly connected to one side of the slider 6. A second spring 17 is sleeved on the surface of the inclined block 13. A second spring 17 is fixedly connected to both sides of the inner cavity of the top cover 3. The top cover 3 is connected to a diagonal strip 18, and one side of the diagonal block 13 is slidably connected to the other side of the diagonal strip 18. When the top cover 3 is pressed down, the diagonal strip 18 squeezes the diagonal block 13, so that the reinforcing plate 14 on one side of the diagonal block 13 limits the component 2. A heat-conducting plate 19 is fixedly connected to the top of the top cover 3. The heat-conducting plate 19 is made of thermally conductive silicone grease, which has good thermal conductivity and can limit the top of the component 2. The bottom of the heat-conducting plate 19 is in contact with the top of the component 2. The energy-absorbing layer 8 is made of foamed silicone, which can absorb vibration energy and improve the shock resistance of the top cover 3. The shielding layer 9 is made of copper-plated film, which provides electromagnetic shielding and reduces the impact of external factors on the component 2. The anti-collision layer 10 is made of ultra-high molecular weight polyethylene, which is a high-strength material and can resist external physical impacts on the top cover 3. Slots are opened on both sides of the top of the bottom plate 1, and one side of the bottom of the top cover 3 is slidably connected to the inner cavity of the slot.

[0029] The working principle of this invention is as follows: During installation, the core component is first placed in the positioning groove 11 of the base plate 1 for initial positioning. Then, the top cover 3 is pressed down so that its bottom is inserted into the slot of the base plate 1. At this time, the inclined strip 18 inside the top cover 3 contacts the inclined surface of the inclined block 13, pushing the inclined block 13 to slide laterally and compress the second spring 17, which drives the reinforcing plate 14 to automatically clamp the two sides of the component to achieve reinforcement. At the same time, the downward pressure of the top cover 3 causes the inclined surface of the insertion rod 7 to retract and compress the first spring 16. After the top cover 3 is fully in place, the first spring 16 pushes the insertion rod 7 to insert into the insertion hole of the top cover 3 to complete the mechanical locking. Then, the rotating rod 4 drives the cam 5 to press the slider 6 for further fixation.

[0030] During drone operation, the copper-plated film shielding layer 9 effectively resists electromagnetic interference, the ultra-high molecular weight polyethylene anti-collision layer 10 resists physical impact, and the foamed silicone energy-absorbing layer 8 buffers vibration. At the same time, the heat-conducting plate 19 conducts the heat of the components to the surface of the cover to achieve efficient heat dissipation. When disassembling, simply rotate the rotating rod 4 in the opposite direction to release the pressure of the cam 5. The insertion rod 7 exits the insertion hole under the action of the first spring 16, and the top cover 3 can be lifted. The inclined block 13 resets under the action of the second spring 17 to release the clamp. The whole process realizes quick disassembly and maintenance.

[0031] The foregoing has only described certain exemplary embodiments of the present invention by way of illustration. Undoubtedly, those skilled in the art can modify the described embodiments in various ways without departing from the spirit and scope of the present invention. Therefore, the foregoing drawings and descriptions are illustrative in nature and should not be construed as limiting the scope of protection of the claims of the present invention.

Claims

1. A copper-plated film covering for anti-interference core components of a UAV, comprising a base plate (1), characterized in that: The bottom plate (1) is provided with a component (2) on its top and a top cover (3) on its top. The inner cavity of the base plate (1) is provided with a disassembly and assembly assembly, which includes a rotating rod (4) movably connected to the inner cavity of the base plate (1), a cam (5) fixedly connected to both sides of the surface of the rotating rod (4), a slider (6) slidably connected to both sides of the inner cavity of the base plate (1), and an insert rod (7) fixedly connected to one side of the slider (6). The disassembly and assembly assembly is used to quickly disassemble and assemble the cover. The top cover (3) is provided with a composite component, which includes an energy-absorbing layer (8), a shielding layer (9) is fixedly connected to the surface of the energy-absorbing layer (8), and an anti-collision layer (10) is fixedly connected to the surface of the shielding layer (9). The composite component is composed of the energy-absorbing layer (8), the shielding layer (9), and the anti-collision layer (10).

2. The anti-interference copper-plated film covering for a core component of a drone according to claim 1, characterized in that: The bottom plate (1) has a positioning groove (11) on the top. Support bars (12) are fixedly connected to both sides of the top of the positioning groove (11). An inclined block (13) is slidably connected to one side of the inner cavity of the support bar (12). A reinforcing plate (14) is fixedly connected to one side of the inclined block (13).

3. The anti-interference copper-plated film covering for a UAV core component according to claim 1, characterized in that: Positioning plates (15) are fixedly connected to both sides of the inner cavity of the base plate (1). A first spring (16) is sleeved on the surface of the insertion rod (7). One end of the first spring (16) is fixedly connected to one side of the positioning plate (15), and the other end of the first spring (16) is fixedly connected to one side of the slider (6).

4. The anti-interference copper-plated film covering for a UAV core component according to claim 2, characterized in that: The surface of the inclined block (13) is fitted with a second spring (17), and both sides of the inner cavity of the top cover (3) are fixedly connected with inclined strips (18). One side of the inclined block (13) is slidably connected to one side of the inclined strips (18).

5. The anti-interference copper-plated film covering for a UAV core component according to claim 1, characterized in that: A heat-conducting plate (19) is fixedly connected to the top of the top cover (3), and the bottom of the heat-conducting plate (19) is in contact with the top of the component (2).

6. The anti-interference copper-plated film covering for a UAV core component according to claim 1, characterized in that: The energy-absorbing layer (8) is made of foamed silicone, the shielding layer (9) is made of copper-plated film, and the anti-collision layer (10) is made of ultra-high molecular weight polyethylene.

7. The anti-interference copper-plated film covering for a core component of a drone according to claim 1, characterized in that: The bottom plate (1) has slots on both sides of its top, and the bottom side of the top cover (3) is slidably connected to the inner cavity of the slot.

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