Carbon fiber compression molding device for manufacturing unmanned aerial vehicle parts

Abstract

The utility model provides a carbon fiber compression molding device for manufacturing parts of an unmanned aerial vehicle, and particularly relates to the technical field of compression molding devices, the carbon fiber compression molding device comprises two frame bodies, an alternate conduction assembly arranged between the two frame bodies and a sliding assembly matched with the conduction assembly of the frame bodies, and the compression molding assembly is arranged on the two frame bodies; the alternate conduction assembly comprises a first conduction assembly arranged on one side between the two frame bodies and a second conduction assembly arranged on the other side between the two frame bodies, and the second conduction assembly is located below the first conduction assembly; the alternating conduction assembly can be used for replacing the working panel, specifically, the first conduction assembly and the second conduction assembly can achieve the switching work of the working panel, and the first placing plate and the second placing plate alternately work to achieve the replacement work of the carbon fiber plate to be processed. And the processing efficiency of the carbon fiber plate is improved to a certain extent.

Description

Technical Field

[0001] The utility model relates to the technical field of compression molding devices, in particular to a carbon fiber compression molding device for manufacturing UAV parts. Background Art

[0002] A carbon fiber board is formed by infiltrating and hardening carbon fibers arranged in the same direction with resin to form a carbon fiber board, which can effectively solve the problems of difficult construction and large engineering quantity of multi-layer carbon fiber cloth, has good reinforcement effect and convenient construction; it uses high-quality carbon fiber raw materials and good basic resin as raw materials, has good properties such as high tensile strength, corrosion resistance, seismic resistance, and impact resistance, and is commonly used in the production of multi-rotor UAV fuselages; the carbon fiber board is formed by laying the raw materials layer by layer in a mold and then hot pressing it through a press.

[0003] The existing carbon fiber thermoplastic setting, for example, a hot pressing device for UAV carbon fiber board production disclosed in the patent with the publication number CN217622305U includes a hydraulic cylinder, an upper mold, a lower mold, and a cold and hot integrated machine. A hydraulic cylinder is arranged on the upper side of the upper mold, a hydraulic oil cylinder is arranged on the upper side of the hydraulic cylinder, a lower mold is arranged on the lower side of the upper mold, a bottom plate is arranged on the lower side of the lower mold, a water pipe is arranged inside the bottom plate, a cold and hot integrated machine is arranged on the lower side of the water pipe, a servo motor is arranged on one side of the lower mold, a threaded shaft is arranged on the side of the servo motor close to the lower mold, a slider is arranged on the outer side of the threaded shaft, an electric heater is arranged on the front side of the slider, an electric heating tube is arranged on the rear side of the slider, a fixing rod is arranged on the inner side of the electric heating tube, a roller is arranged on the outer side of the electric heating tube, and a chute is arranged on the rear side of the fixing rod; when the thermoplastic equipment in this patent processes the carbon fiber board, it is necessary to wait for the previous carbon fiber board to cool down after processing before new carbon fiber board laying work can be carried out, and the manufacturing efficiency is poor.

[0004] Therefore, it is necessary to design a carbon fiber compression molding device that can improve the processing efficiency of carbon fiber boards. Summary of the Utility Model

[0005] In order to solve the above problems, the utility model proposes a carbon fiber compression molding device for manufacturing UAV parts to more precisely solve the above problems.

[0006] The utility model is realized through the following technical solutions:

[0007] The present utility model provides a carbon fiber compression molding device for manufacturing UAV components, which includes two frames and an alternating conduction assembly arranged between the two frames, as well as a sliding assembly cooperating with the frame conduction assembly. A compression molding assembly is arranged on the two frames; the alternating conduction assembly includes a first conduction assembly arranged on one side between the two frames and a second conduction assembly arranged on the other side between the two frames. The second conduction assembly is located below the first conduction assembly. The first conduction assembly includes two first cylinder members connected to the inner sides of the two frames, and the output ends of the two first cylinder members are connected with a first placement plate for placing a carbon fiber mold. The second conduction assembly includes second cylinder members connected to the inner sides of the two frames, and the output ends of the two second cylinder members are connected with a second placement plate.

[0008] Further, the compression molding assembly of the present utility model includes four guide rods arranged on the two frames, a hot pressing end sleeved with the four guide rods, and a top plate arranged at the tops of the four guide rods. A hydraulic cylinder is connected to the top of the top plate, and the output end of the hydraulic cylinder passes through the top plate and is connected with the hot pressing end.

[0009] Further, a heating element is arranged inside the hot pressing end, and a closed end cooperating with the mold is detachably arranged at the bottom of the hot pressing end.

[0010] Further, the closed end includes a conduction part and a pressing part arranged at the bottom of the conduction part.

[0011] Further, the sliding assembly includes a first sliding rail cooperating with the first placement plate, and first sliding blocks are arranged on both sides of the first placement plate and cooperate with the first sliding rail.

[0012] Further, the sliding assembly further includes a second sliding rail cooperating with the second placement plate, and second sliding blocks are arranged on both sides of the second placement plate and cooperate with the second sliding rail.

[0013] Further, both the first sliding block and the second sliding block are arranged in a T shape.

[0014] The beneficial effects of the present utility model:

[0015] The setting of the alternating conduction assembly can be used to replace the working panel. Specifically, the setting of the first conduction assembly and the second conduction assembly can realize the switching of the working panel, and the alternating work of the first placement plate and the second placement plate can realize the replacement of the carbon fiber board to be processed, which increases the processing efficiency of the carbon fiber board to a certain extent. Description of the Drawings

[0016] Figure 1 It is a schematic diagram of the overall structure in the present utility model;

[0017] Figure 2 It is a schematic diagram of the frame body, the first conduction component and the second conduction component in the present utility model;

[0018] Figure 3 It is a schematic diagram of the frame body and the sliding component in the present utility model;

[0019] Figure 4 It is a schematic diagram of the compression molding component in the present utility model;

[0020] Figure 5 It is a schematic diagram of the cross-section structure of the hot pressing end in the present utility model;

[0021] Figure 6 It is a schematic diagram of the bottom view structure of the hot pressing end in the present utility model.

[0022] In the figure, 1 is the frame body; 2 is the alternating conduction component; 21 is the first conduction component; 211 is the first cylinder part; 212 is the first placing plate; 22 is the second conduction component; 221 is the second cylinder part; 222 is the second placing plate; 3 is the sliding component; 31 is the first slide rail; 32 is the first slider; 33 is the second slide rail; 34 is the second slider; 4 is the compression molding component; 41 is the guide rod; 42 is the hot pressing end; 421 is the heating part; 422 is the closed end; 4221 is the conduction part; 4222 is the pressing part; 43 is the top plate; 44 is the hydraulic cylinder. Specific embodiments

[0023] In order to make the objectives, technical solutions and advantages of the embodiments of the present utility model clearer, the technical solutions in the embodiments of the present utility model will be clearly and completely described below. Obviously, the described embodiments are part of the embodiments of the present utility model, rather than all of them. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present utility model.

[0024] Embodiment

[0025] Refer to Figure 1-6, A carbon fiber compression molding device for manufacturing UAV parts, including two frames 1 and an alternating conduction component 2 arranged between the two frames 1, and a sliding component 3 cooperating with the conduction component of the frame 1. A compression molding component 44 is arranged on the two frames 1; The alternating conduction component 2 includes a first conduction component 21 arranged on one side between the two frames 1 and a second conduction component 22 arranged on the other side between the two frames 1. The second conduction component 22 is located below the first conduction component 21. The first conduction component 21 includes two first cylinder parts 211 connected to the inner sides of the two frames 1. The output ends of the two first cylinder parts 211 are connected with a first placement plate 212 for placing a carbon fiber mold. The second conduction component 22 includes second cylinder parts 221 connected to the inner sides of the two frames 1. The output ends of the two second cylinder parts 221 are connected with a second placement plate 222;

[0026] The setting of the alternating conduction component 2 can be used to replace the working panel. Specifically, the settings of the first conduction component 21 and the second conduction component 22 can realize the switching of the working panel. That is, the two first cylinder parts 211 can drive the first placement plate 212 to slide. And when the two first cylinder parts 211 extend the first placement plate 212, the compression molding component 44 will perform compression molding on the mold and the carbon fiber board on the first placement plate 212. At this time, the two second cylinder parts 221 will drive the second placement plate 222 to be in a retracted state. During the use of the first placement plate 212, the staff can lay the mold and the carbon fiber board on the second placement plate 222. When the mold carbon fiber board on the first placement plate 212 is processed, the two first cylinder parts 211 will drive the first placement plate 212 to perform a retraction movement. At this time, the two second cylinders will drive the second placement plate 222 to perform an extension movement and move the mold and the carbon fiber board to below the compression molding component 44. And the staff can disassemble and lay the carbon fiber board of the first placement plate 212. The alternating work of the first placement plate 212 and the second placement plate 222 can realize the replacement of the carbon fiber board to be processed, which increases the processing efficiency of the carbon fiber board to a certain extent;

[0027] In this embodiment, the setting of the sliding component 3 can provide a basis for the sliding work of the first placement plate 212 and the second placement plate 222, so as to ensure the switching work of the first placement plate 212 and the second placement plate 222.

[0028] Preferably, refer to Figure 4 , The compression molding component 44 includes four guide rods 41 arranged on the two frames 1, a hot pressing end 42 sleeved on the four guide rods 41, and a top plate 43 arranged on the tops of the four guide rods 41. A hydraulic cylinder 44 is connected to the top of the top plate 43. The output end of the hydraulic cylinder 44 passes through the top plate 43 and is connected to the hot pressing end 42;

[0029] The setting of the hydraulic cylinder 44 can drive the hot pressing end 42 to move up and down, so that the hot pressing end 42 can perform compression molding on the mold and the carbon fiber board on the mold. The setting of the guide rod 41 can limit the moving direction of the hot pressing end 42, so that the movement of the hot pressing end 42 is more accurate;

[0030] Among them, the extending height of the hot pressing end 42 is two heights. Specifically, when the first placing plate 212 is in use, that is, when the first placing plate 212 is located below the hot pressing end 42, when the hydraulic cylinder 44 drives the hot pressing end 42 to move downward, when the hot pressing end 42 contacts the top of the first placing plate 212, there is a certain distance between the bottom of the hot pressing end 42 and the top of the frame body 1. And when the second placing plate 222 is located below the hot pressing end 42, when the hot pressing end 42 contacts the top of the second placing plate 222, the bottom of the hot pressing end 42 will contact the top of the frame body 1.

[0031] Preferably, refer to Figure 5 , a heating element 421 is arranged in the hot pressing end 42, and a closed end 422 matching the mold is detachably arranged at the bottom of the hot pressing end 42. The closed end 422 includes a conduction part 4221 and a pressing part 4222 arranged at the bottom of the conduction part 4221; the setting of the conduction part can conduct the heat generated by the heating element 421 into the pressing part 4222, so as to realize the thermoplastic work of the carbon fiber board. The setting of the pressing part 4222 can be attached to the mold, so as to realize the pressing work of the carbon fiber board;

[0032] The advantage of the detachable setting of the closed end 422 and the hot pressing end 42 is that it is convenient for the staff to replace different styles of the closed end 422, so as to realize the manufacturing work of different types of UAV parts;

[0033] In this embodiment, the pressing part 4222 includes an inner groove matching the mold; among them, the inner groove styles on different closed ends 422 are different; further increasing the applicable range of the equipment;

[0034] Optionally, the closed end 422 and the bottom of the hot pressing end 42 are connected by screw fixation.

[0035] Preferably, refer to Figure 3 , the sliding assembly 3 includes a first sliding rail 31 matching the first placing plate 212. First sliding blocks 32 matching the first sliding rail 31 are arranged on both sides of the first placing plate 212. The sliding assembly 3 further includes a second sliding rail 33 matching the second placing plate 222. Second sliding blocks 34 matching the second sliding rail 33 are arranged on both sides of the second placing plate 222; the settings of the first sliding rail 31 and the first sliding blocks 32 and the second sliding rail 33 and the second sliding blocks 34 can respectively provide a basis for the sliding work of the first placing plate 212 and the second placing plate 222;

[0036] In this embodiment, both the first slider 32 and the second slider 34 are arranged in a T shape. The first slider 32 and the second slider 34 arranged in a T shape can also bear the pressure received by the first placing plate 212 and the second placing plate 222. To a certain extent, it can avoid the bending phenomenon at the connection between the first placing plate 212 and the second placing plate 222 and the first cylinder member 211 and the second cylinder member 221 respectively, thereby ensuring the stability of the first placing plate 212 and the second placing plate 222 during the sliding process and ensuring the quality of the carbon fiber board after processing is completed.

[0037] It should be noted that the present utility model only protects the mechanical part, and the functions realized through the software control part related thereto are not within the protection scope of the present utility model.

[0038] Of course, the present utility model can also have many other implementation manners. Based on this implementation manner, other implementation manners obtained by those of ordinary skill in the art without any creative work belong to the protection scope of the present utility model.

Claims

1. A carbon fiber compression molding device for manufacturing UAV components, characterized in that, It includes two frame bodies, an alternating conduction component arranged between the two frame bodies, and a sliding component cooperating with the frame body conduction component. A compression molding component is arranged on the two frame bodies; the alternating conduction component includes a first conduction component arranged on one side between the two frame bodies and a second conduction component arranged on the other side between the two frame bodies. The second conduction component is located below the first conduction component. The first conduction component includes two first cylinder parts connected to the inner sides of the two frame bodies. The output ends of the two first cylinder parts are connected with a first placement plate for placing a carbon fiber mold. The second conduction component includes second cylinder parts connected to the inner sides of the two frame bodies. The output ends of the two second cylinder parts are connected with a second placement plate.

2. The carbon fiber compression molding device for manufacturing UAV parts according to claim 1, characterized in that, The compression molding component includes four guide rods arranged on the two frame bodies, a hot pressing end sleeved on the four guide rods, and a top plate arranged at the tops of the four guide rods. A hydraulic cylinder is connected to the top of the top plate. The output end of the hydraulic cylinder passes through the top plate and is connected with the hot pressing end.

3. The carbon fiber compression molding device for manufacturing UAV components according to claim 2, characterized in that, A heating element is arranged inside the hot pressing end. A closed end cooperating with the mold is detachably arranged at the bottom of the hot pressing end.

4. The carbon fiber compression molding device for manufacturing UAV components according to claim 3, characterized in that, The closed end includes a conduction part and a pressing part arranged at the bottom of the conduction part.

5. A carbon fiber compression molding device for manufacturing UAV components according to claim 1, characterized in that, The sliding component includes a first slide rail cooperating with the first placement plate. First sliders cooperating with the first slide rail are arranged on both sides of the first placement plate.

6. The carbon fiber compression molding device for manufacturing UAV parts according to claim 5, characterized in that, The sliding component further includes a second slide rail cooperating with the second placement plate. Second sliders cooperating with the second slide rail are arranged on both sides of the second placement plate.

7. A carbon fiber compression molding device for manufacturing UAV components according to claim 6, characterized in that, Both the first slider and the second slider are arranged in a T shape.

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