Die for unmanned aerial vehicle production

Abstract

The utility model provides a die for unmanned aerial vehicle production, and particularly relates to the technical field of dies, the die comprises a seat body, a lower die connected with the top of the seat body, and an upper die arranged above the lower die and matched with the lower die, and the upper die and the lower die are both provided with manufacturing cavities; the base body comprises a bottom plate and a supporting plate arranged at the top of the bottom plate, an inner groove is formed in the lower mold and located below the manufacturing cavity, and a cooling piece used for cooling the lower mold is arranged in the inner groove; the first air cylinder part is arranged and can be used for jacking up a product in a manufacturing cavity in the lower die, so that a worker can conveniently unload the product; a second air cylinder part is arranged and can be used for jacking the upper mold, so that the upper mold is separated from the lower mold, and the disassembly work of the upper mold and the lower mold is realized; and through the arrangement of the cooling piece, heat of the product in the production process can be guided out, and therefore it is guaranteed that the product is cooled.

Description

Technical Field

[0001] The utility model relates to the technical field of molds, in particular to a mold for producing unmanned aerial vehicles. Background Art

[0002] Unmanned aircraft, also known as "drones", are unmanned aircraft that are controlled by radio remote control equipment and self-contained program control devices. There is no cockpit on board, but it is equipped with autopilot, program control devices and other equipment. Personnel on the ground, on ships or at the mother aircraft remote control station use radar and other equipment to track, locate, remotely control, telemeter and digitally transmit it. It can take off like a normal aircraft or be launched into the air with a booster rocket under radio remote control, or it can be taken to the air by the mother aircraft for flight. When recovering, it can land automatically in the same way as a normal aircraft landing process, or it can be recovered by remote control with a parachute or intercepting net. It can be used repeatedly many times. It is widely used in aerial reconnaissance, surveillance, communications, anti-submarine, electronic jamming, etc.

[0003] Existing drones and drone parts generally use molded composite materials to achieve the manufacturing of drone parts;

[0004] For example, the patent number CN220517311U discloses a mold for integrally forming a center cabin of a UAV, including an upper mold and a lower mold that are interlocked with each other and a core mold arranged between the upper mold and the lower mold; the upper mold includes an upper mold plate and an upper cavity mold connected to the lower surface of the upper mold plate, the lower surface of the upper cavity mold is provided with an upper mold cavity recessed inwardly, and an upper heat exchange tube is laid in the upper cavity mold; the lower mold includes a lower mold plate and a lower cavity mold connected to the lower mold plate, the lower cavity The upper surface of the mold is provided with a lower mold cavity which is concave inwards, and a lower heat exchange tube is laid in the lower mold cavity; the core mold comprises an upper core mold, an intermediate core mold and a lower core mold which are detachably connected; prepreg is laid on the surface of the core mold, and then the core mold with the prepreg laid is placed in the upper mold cavity and the lower mold cavity, and the pressure is provided by a molding press to realize the one-piece molding of the center cabin of the UAV, and the sealing requirements of the mold are relatively low; and the core mold adopts a split structure, and when demolding, the intermediate core mold can be pulled out first, and demolding is convenient;

[0005] However, the existing molds used to manufacture drone parts are heavy. If the molds are disassembled manually, not only will they take a long time to use, but they are also less safe. At the same time, the raw materials will generate high temperatures during the molding process, and the patent does not provide a heat dissipation mechanism. Therefore, when the parts are taken after manufacturing, it is necessary to wait for them to cool down before taking the parts after manufacturing, which takes a long time to use.

[0006] Therefore, it is necessary to design a UAV production mold that is easy to disassemble the mold and has the function of specifically cooling the mold. Utility Model Content

[0007] In order to solve the above problems, the utility model proposes a mold for UAV production to more accurately solve the above problems.

[0008] The utility model is realized by the following technical solutions:

[0009] The utility model proposes a mold for producing an unmanned aerial vehicle, comprising a seat body, a lower mold connected to the top of the seat body, and an upper mold arranged above the lower mold and matched with the lower mold, wherein a manufacturing cavity is provided on the upper mold and the lower mold; the seat body comprises a bottom plate, and two support plates arranged on the top of the bottom plate, an inner groove is provided in the lower mold and below the manufacturing cavity, a cooling member for cooling the lower mold is provided in the inner groove, a first cylinder member is provided on the inner side of the support plate, an output end of the first cylinder member passes through the inner groove and is located in the manufacturing cavity, and a second cylinder member for lifting the upper mold is provided on the top of the seat body and on both sides of the lower mold.

[0010] Furthermore, the utility model provides that the cooling component includes a water tank, and a cooling pipe connected to the output end of the water tank, the other end of the cooling pipe extends into the inner tank along one side of the inner side, and passes through the other side of the inner tank along to the outside of the inner tank, and is connected to the input end of the water tank.

[0011] Furthermore, in the utility model, the water tank comprises a normal temperature water tank or a refrigeration water tank.

[0012] Furthermore, the utility model provides that the inner groove is convexly arranged, and one side of the inner groove is connected to one side of the lower mold, and two barrier columns are arranged in the inner groove, and the barrier columns are arranged on a side close to the second cylinder member.

[0013] Furthermore, the utility model is provided with a plurality of supporting columns in the inner groove.

[0014] Furthermore, in the utility model, the second cylinder member includes a cylinder body, and a lifting member connected to the output end of the cylinder body, and the lifting member is arranged in an L shape.

[0015] Beneficial effects of the utility model:

[0016] The upper mold, the lower mold and the manufacturing cavity can cooperate to manufacture the molding production of drone parts;

[0017] The setting of the first cylinder member can be used to lift the product in the manufacturing cavity on the lower mold, so as to facilitate the staff to unload the product; the setting of the second cylinder member can be used to lift the upper mold to separate the upper mold from the lower mold, thereby realizing the disassembly of the upper mold and the lower mold; further, it is convenient for the staff to collect the product parts after manufacturing; and the setting of the cooling member can export the heat of the product during the production process, thereby ensuring the cooling of the product. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0019] Figure 2 It is a schematic diagram of the cooling element and the inner tank split structure in the utility model;

[0020] Figure 3 It is a schematic diagram of the manufacturing cavity structure in the utility model;

[0021] Figure 4 It is a schematic diagram of the internal cross-sectional structure of the inner tank in the utility model.

[0022] In the figure, 1, base body; 11, bottom plate; 12, support plate; 2, lower mold; 21, inner groove; 22, barrier column; 23, support column; 3, upper mold; 4, manufacturing cavity; 5, cooling part; 51, water tank; 52, cooling pipe; 6, first cylinder part; 7, second cylinder part; 71, cylinder body; 72, lifting part. DETAILED DESCRIPTION

[0023] In order to make the purpose, technical solution and advantages of the embodiments of the utility model clearer, the following will be combined with the technical solution in the embodiments of the utility model for a clear and complete description. Obviously, the described embodiments are partial embodiments of the utility model, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0024] Example

[0025] refer to Figure 1-4A mold for producing a drone comprises a seat body 1, a lower mold 2 connected to the top of the seat body 1, and an upper mold 3 arranged above the lower mold 2 and matched with the lower mold 2, and a manufacturing cavity 4 is provided on the upper mold 3 and the lower mold 2; the seat body 1 comprises a bottom plate 11, and two support plates 12 arranged on the top of the bottom plate 11, an inner groove 21 is provided in the lower mold 2 and below the manufacturing cavity 4, a cooling member 5 for cooling the lower mold 2 is provided in the inner groove 21, a first cylinder member 6 is provided on the inner side of the support plate 12, an output end of the first cylinder member 6 passes through the inner groove 21 and is located in the manufacturing cavity 4, and a second cylinder member 7 for lifting the upper mold 3 is provided on the top of the seat body 1 and on both sides of the lower mold 2;

[0026] The upper mold 3, the lower mold 2 and the manufacturing cavity 4 cooperate to manufacture the drone parts through the molding process;

[0027] The first cylinder 6 can be used to lift the product in the manufacturing cavity 4 on the lower mold 2, so that the staff can unload the product; the second cylinder 7 can be used to lift the upper mold 3 to separate the upper mold 3 from the lower mold 2, so as to realize the disassembly of the upper mold 3 and the lower mold 2; further, it is convenient for the staff to collect the parts of the product after manufacturing; and the cooling element 5 can be set to extract the heat of the product during the production process, so as to ensure the cooling of the product;

[0028] Specifically, first, the staff takes out the composite material to be used and puts the material into the manufacturing cavity 4, then places the upper mold 3 above the lower mold 2, and seals the two manufacturing cavities 4, and then performs compression molding on the raw materials in the two manufacturing cavities 4. When the raw materials are molded, the cooling member 5 located below the manufacturing cavity 4 will cool the temperature of the bottom of the manufacturing cavity 4, thereby accelerating the cooling of the raw materials after molding; when demolding is required, the second cylinder member 7 is started, and the second cylinder member 7 will lift the upper mold 3, and gradually separate the upper mold 3 from the lower mold 2, and expose the molded raw materials. At the same time, the exposed raw materials cooperate with the cooling member 5 to quickly realize the cooling of the manufacturing cavity 4. Finally, the first cylinder member 6 is started, and the first cylinder member 6 will lift the raw materials, thereby realizing the demolding of the raw materials;

[0029] In this embodiment, the mold compression molding process is an existing mature technology, so its specific process and principle are not described in detail in this application document.

[0030] The utility model further comprises a cooling member 5 including a water tank 51 and a cooling pipe 52 connected to the output end of the water tank 51, the other end of the cooling pipe 52 extends into the inner tank 21 along one side of the inner side, and extends to the outside of the inner tank 21 through the other side of the inner tank 21, and is connected to the input end of the water tank 51; the water tank 51, the input end of the water tank 51 (not shown in the figure), the cooling pipe 52 and the output end of the water tank 51 (not shown in the figure) cooperate, and water can be injected into the inner tank 21 through the cooling pipe 52, and the water will absorb the heat at the bottom of the manufacturing cavity 4, and the adsorbed heat will be injected into the output end of the water tank 51. Under the continuous flow of water, the effect of cooling the temperature in the manufacturing cavity 4 can be achieved. At the same time, the temperature of the water itself will also be conducted to the manufacturing cavity 4 through the inner tank 21;

[0031] In this embodiment, considering the continuous input of water, a water pump is provided in the water tank 51;

[0032] In the embodiment, optionally, a partition in the water tank 51 divides the water tank 51 evenly and forms a first water storage chamber and a second water storage chamber, the first water storage chamber is connected to the input end, and the second water storage chamber is connected to the output end.

[0033] Preferably, the water tank 51 includes a normal temperature water tank 51 or a refrigeration water tank 51; because the temperature value of the mold lamination process during the production process is relatively high, water at normal temperature also has the effect of cooling the manufacturing cavity 4;

[0034] The use of the refrigeration water tank 51 can further increase the cooling effect of the manufacturing cavity 4, and the principle of the refrigeration water tank 51 is to cool the water and inject the cooled water into the cooling pipe through the output end;

[0035] It should be noted that the process of cooling water is an existing technology, so it is not described in detail in this application document, such as using semiconductor cooling plates, etc.

[0036] Preferably, referring to the figure, the inner groove 21 is arranged in a convex shape, and one side of the inner groove 21 is connected to one side of the lower mold 2, and two barrier columns 22 are arranged in the inner groove 21, and the barrier columns 22 are arranged on the side close to the second cylinder component 7; the setting of the two barrier columns 22 can adjust the direction of the cooling pipe 52, and the two ends of the adjusted cooling pipe 52 will be located on both sides of the second cylinder component 7, providing a basis for the installation of the second cylinder component 7.

[0037] Furthermore, the utility model is provided with a plurality of support columns 23 in the inner groove 21; the provision of the support columns 23 can increase the force strength of the bottom of the manufacturing cavity 4, thereby ensuring the progress of the work of manufacturing the drone parts.

[0038] Furthermore, the utility model comprises a second cylinder member 7 including a cylinder body 71 and a lifting member 72 connected to the output end of the cylinder body 71, wherein the lifting member 72 is arranged in an L shape; the lifting member 72 arranged in an L shape can move upward synchronously with the movement of the second cylinder member 7, thereby realizing the lifting work of the upper mold 3, and the upper mold 3 gradually separates from the lower mold 2.

[0039] Of course, the present utility model may have many other implementations. Based on the present implementation, other implementations obtained by ordinary technicians in this field without any creative work are all within the scope of protection of the present utility model.

Claims

1. A mold for producing drones, characterized in that: The invention comprises a seat body, a lower mold connected to the top of the seat body, and an upper mold arranged above the lower mold and matched with the lower mold, wherein the upper mold and the lower mold are both provided with a manufacturing cavity; the seat body comprises a bottom plate, and two support plates arranged on the top of the bottom plate, an inner groove is provided in the lower mold and below the manufacturing cavity, a cooling member for cooling the lower mold is provided in the inner groove, a first cylinder member is provided on the inner side of the support plate, an output end of the first cylinder member passes through the inner groove and is located in the manufacturing cavity, and the top of the seat body , and second cylinder parts for lifting the upper mold are arranged on both sides of the lower mold; the cooling part includes a water tank, and a cooling pipe connected to the output end of the water tank, the other end of the cooling pipe extends into the inner groove along one side of the inner side, and passes through the other side of the inner groove along to the outside of the inner groove, and is connected to the input end of the water tank; the inner groove is convex, and one side of the inner groove is connected to one side of the lower mold, two blocking columns are arranged in the inner groove, and the blocking columns are arranged on the side close to the second cylinder part; a plurality of supporting columns are arranged in the inner groove.

2. A UAV production mold according to claim 1, characterized in that: The water tank comprises a normal temperature water tank or a refrigeration water tank.

3. A UAV production mold according to claim 1, characterized in that: The second cylinder member comprises a cylinder body, and a lifting member connected to the output end of the cylinder body, and the lifting member is arranged in an L shape.

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