Carbon fiber unmanned aerial vehicle wing forming mold

Abstract

The utility model discloses a carbon fiber unmanned plane wing forming die relates to unmanned plane wing forming die technical field. This carbon fiber unmanned plane wing forming die, including support frame, be provided with upper die holder on the support frame, be provided with first track board in the support frame, be provided with second track board between the support frame, the fixedly connected with lower die holder on the support frame, the water tank is fixedly connected with the support frame bottom. This carbon fiber unmanned plane wing forming die adopts the structure of setting up two lower die holders and an upper die holder on the support frame, and the cooperation between them can effectively reduce the equipment downtime, and the water supply unit can guide the cold water into the cooling layer in the upper die holder and the lower die holder, accelerates the wing cooling after forming, guarantees the stable cooperation between two lower die holders and an upper die holder, effectively promotes the wing production efficiency.

Description

Technical Field

[0001] This utility model relates to the field of unmanned aerial vehicle (UAV) wing forming mold technology, specifically a carbon fiber UAV wing forming mold. Background Technology

[0002] In the field of modern drone manufacturing, carbon fiber has become an ideal material for making wings due to its excellent properties such as high specific strength, high specific modulus, corrosion resistance and fatigue resistance. The carbon fiber drone wing forming mold is the key. The mold needs to have high precision and good surface finish. The material is mostly stainless steel. It is strictly customized according to the wing design requirements. The surface is evenly coated with release agent to lay the foundation for creating high-performance drone wings.

[0003] Existing carbon fiber drone wing forming molds mostly rely on the coordinated operation of an upper and lower mold base to complete the extrusion forming of the wing. However, the temperature after wing extrusion is high, and the time required for natural cooling is long. Furthermore, the operation of a single upper and lower mold base results in extended equipment downtime and low production efficiency. To address the shortcomings of existing technologies, this invention provides a carbon fiber drone wing forming mold to solve the aforementioned problems. Utility Model Content

[0004] To address the shortcomings of existing technologies, this utility model provides a carbon fiber drone wing forming mold, which solves the problems of high temperature after wing extrusion molding, long time required for natural cooling, and long downtime and low production efficiency caused by the working configuration of a single upper and lower mold base.

[0005] To achieve the above objectives, this utility model provides the following technical solution: a carbon fiber unmanned aerial vehicle (UAV) wing forming mold, comprising a support frame, an upper mold base on the support frame, a first track plate inside the support frame, a second track plate between the support frames, a lower mold base fixedly connected to the support frame, a water tank fixedly connected to the bottom of the support frame, a water supply unit on the water tank for providing cold water, and a second track plate on the support frame;

[0006] The support frame is provided with a first drive unit, which is used to drive the second track plate. The second track plate is provided with a second drive unit, which is used to drive the upper mold base.

[0007] Preferably, the water supply unit includes:

[0008] A high-pressure water pump is located on the front of the water tank;

[0009] The main body of the water pipe is fixedly connected at one end to the high-pressure water pump, and the other end of the main body of the water pipe is fixedly connected to the lower mold base.

[0010] Preferably, the first driving unit includes:

[0011] The first servo motor is mounted on the support frame;

[0012] The first threaded rod has one end fixedly connected to the output end of the first servo motor.

[0013] Preferably, the second driving unit includes:

[0014] The second servo motor is installed inside the second track plate;

[0015] The second threaded rod has one end fixedly connected to the output end of the second servo motor.

[0016] Preferably, a second track block is fixedly connected to the upper mold base, the second threaded rod is threadedly connected to the second track block, a second cooling layer is provided inside the upper mold base, and a drain pipe is fixedly connected to the bottom of the upper mold base.

[0017] Preferably, a first cooling layer is provided inside the lower mold base, a water drain hole is provided at the bottom of the first cooling layer, and a water inlet pipe is fixedly connected to the lower mold base.

[0018] Preferably, the second track plate has a first track block fixedly connected to both ends, and the first track block is threadedly connected to the first threaded rod.

[0019] This utility model discloses a carbon fiber drone wing forming mold, which has the following beneficial effects: The carbon fiber drone wing forming mold adopts a structure with two lower mold bases and one upper mold base set on a support frame. The cooperation between them can effectively reduce equipment downtime. At the same time, the water supply unit can introduce cold water into the cooling layer inside the upper and lower mold bases to accelerate the cooling of the formed wing and ensure stable cooperation between the two lower mold bases and one upper mold base, effectively improving the wing production efficiency. Attached Figure Description

[0020] To more clearly illustrate the technical solutions in the embodiments of this utility model or the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments of this utility model. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0021] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0022] Figure 2 This is a schematic diagram of the second drive unit structure of this utility model;

[0023] Figure 3 This is a schematic diagram of the upper mold base structure of this utility model;

[0024] Figure 4 This is a schematic diagram of the lower mold base structure of this utility model.

[0025] In the diagram: 1. Water tank; 11. Support frame; 12. First track plate; 13. Lower mold base; 131. Water inlet pipe; 132. First cooling layer; 133. Drain hole; 2. Water supply unit; 21. High-pressure water pump; 22. Water pipe body; 3. First drive unit; 31. First servo motor; 32. First threaded rod; 4. Second track plate; 41. First track block; 5. Second drive unit; 51. Second servo motor; 52. Second threaded rod; 6. Upper mold base; 61. Second cooling layer; 62. Drain pipe; 63. Second track block. Detailed Implementation

[0026] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions in the embodiments of this utility model are described clearly and completely. Obviously, the described embodiments are only some embodiments of this utility model, not all embodiments. Based on the embodiments of this utility model, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of this utility model.

[0027] This application provides a carbon fiber drone wing forming mold, which solves the problems of high temperature after wing extrusion molding, long natural cooling time, and long downtime and low production efficiency caused by the operation of a single upper mold base 6 and lower mold base 13. The mold adopts a structure with two lower mold bases 13 and one upper mold base 6 on the support frame 11. Their coordinated operation can effectively reduce equipment downtime. At the same time, the water supply unit 2 can introduce cold water into the cooling layer inside the upper mold base 6 and lower mold base 13 to accelerate the cooling of the wing after molding, and ensure stable coordination between the two lower mold bases 13 and one upper mold base 6, effectively improving the wing production efficiency.

[0028] To better understand the above technical solutions, the following will provide a detailed explanation of the technical solutions in conjunction with the accompanying drawings and specific implementation methods.

[0029] Example 1;

[0030] This utility model discloses a carbon fiber drone wing forming mold, according to the attached... Figure 1-4As shown, it includes a support frame 11, an upper mold base 6 is provided on the support frame 11, a first track plate 12 is provided inside the support frame 11, a second track plate 4 is provided between the support frames 11, a lower mold base 13 is fixedly connected to the support frame 11, a water tank 1 is fixedly connected to the bottom of the support frame 11, a water supply unit 2 is provided on the water tank 1, the water supply unit 2 is used to provide cold water, and the second track plate 4 is provided on the support frame 11.

[0031] A first drive unit 3 is provided on the support frame 11. The first drive unit 3 is used to drive the second track plate 4. A second drive unit 5 is provided inside the second track plate 4. The second drive unit 5 is used to drive the upper mold base 6.

[0032] The first drive unit 3 includes:

[0033] The first servo motor 31 is mounted on the support frame 11;

[0034] The first threaded rod 32 has one end fixedly connected to the output end of the first servo motor 31.

[0035] The second drive unit 5 includes:

[0036] The second servo motor 51 is installed inside the second track plate 4;

[0037] The second threaded rod 52 has one end fixedly connected to the output end of the second servo motor 51.

[0038] The second track plate 4 has a first track block 41 fixedly connected to both ends, and the first track block 41 is threadedly connected to the first threaded rod 32.

[0039] After the model is placed in the lower mold base 13, the first drive unit 3 and the second drive unit 5 work together to control the upper mold base 6 to move on the support frame 11. The upper mold base 6 can accurately press down on the lower mold base 13 to achieve the purpose of extruding and forming the wing. First, the first servo motor 31 drives the first threaded rod 32 to rotate. The first threaded rod 32 is threadedly connected to the first track block 41, which drives the second track plate 4, which is fixedly connected to it, to move. The second servo motor 51 drives the second threaded rod 52 to rotate. The second threaded rod 52 is threadedly connected to the second track block 63, which facilitates the movement of the upper mold base 6, which is fixedly connected to it, to achieve the purpose of accurately controlling the position of the upper mold base 6.

[0040] Example 2;

[0041] This utility model discloses a carbon fiber drone wing forming mold, according to the attached... Figure 1-4As shown, it includes a support frame 11, an upper mold base 6 is provided on the support frame 11, a first track plate 12 is provided inside the support frame 11, a second track plate 4 is provided between the support frames 11, a lower mold base 13 is fixedly connected to the support frame 11, a water tank 1 is fixedly connected to the bottom of the support frame 11, a water supply unit 2 is provided on the water tank 1, the water supply unit 2 is used to provide cold water, and the second track plate 4 is provided on the support frame 11.

[0042] A first drive unit 3 is provided on the support frame 11. The first drive unit 3 is used to drive the second track plate 4. A second drive unit 5 is provided inside the second track plate 4. The second drive unit 5 is used to drive the upper mold base 6.

[0043] Water supply unit 2 includes:

[0044] High-pressure water pump 21 is located on the front of water tank 1;

[0045] The water pipe body 22 has one end fixedly connected to the high-pressure water pump 21, and the other end fixedly connected to the lower mold base 13.

[0046] A second track block 63 is fixedly connected to the upper mold base 6, and the second threaded rod 52 is threadedly connected to the second track block 63. A second cooling layer 61 is provided inside the upper mold base 6, and a drain pipe 62 is fixedly connected to the bottom of the upper mold base 6.

[0047] A first cooling layer 132 is provided inside the lower mold base 13, and a water drain hole 133 is provided at the bottom of the first cooling layer 132. A water inlet pipe 131 is fixedly connected to the lower mold base 13.

[0048] After the wing is extruded, it is easy to cool down quickly through the water supply unit 2. First, the high-pressure water pump 21 introduces the cold water in the water tank 1 into the first cooling layer 132 of the lower mold base 13 through the water pipe body 22. The upper water pipe 131, which is fixedly connected to it, introduces the cold water into the second cooling layer 61 of the upper mold base 6, so as to cool down the model inside the mold base. The water in the second cooling layer 61 flows back to the first cooling layer 132 through the lower water pipe 62. The water in the first cooling layer 132 flows back to the water tank 1 through the lower water hole 133. The water tank 1 is equipped with a cooling circulation system to facilitate the cooling of the used cooling water.

[0049] The foregoing has shown and described the basic principles, main features, and advantages of this utility model. Those skilled in the art should understand that this utility model is not limited to the above embodiments. The embodiments and descriptions in the specification are merely illustrative of the principles of this utility model. Various changes and modifications can be made to this utility model without departing from its spirit and scope, and all such changes and modifications fall within the scope of the claims. The scope of protection of this utility model is defined by the appended claims and their equivalents.

Claims

1. A carbon fiber unmanned aerial vehicle (UAV) wing forming mold, comprising a support frame (11), wherein an upper mold base (6) is provided on the support frame (11), characterized in that, The support frame (11) is provided with a first track plate (12), and the support frames (11) are provided with a second track plate (4). The support frame (11) is fixedly connected with a lower mold base (13), and the support frame (11) is fixedly connected with a water tank (1). The water tank (1) is provided with a water supply unit (2), which is used to provide cold water. The support frame (11) is provided with a second track plate (4). The support frame (11) is provided with a first drive unit (3), which is used to drive the second track plate (4). The second track plate (4) is provided with a second drive unit (5), which is used to drive the upper mold base (6).

2. The carbon fiber UAV wing forming mold according to claim 1, characterized in that, The water supply unit (2) includes: A high-pressure water pump (21) is located on the front of the water tank (1); The water pipe body (22) is fixedly connected at one end to the high-pressure water pump (21), and the other end of the water pipe body (22) is fixedly connected to the lower mold base (13).

3. The carbon fiber UAV wing forming mold according to claim 1, characterized in that, The first driving unit (3) includes: The first servo motor (31) is mounted on the support frame (11); The first threaded rod (32) has one end fixedly connected to the output end of the first servo motor (31).

4. The carbon fiber UAV wing forming mold according to claim 1, characterized in that, The second drive unit (5) includes: The second servo motor (51) is located inside the second track plate (4); The second threaded rod (52) has one end fixedly connected to the output end of the second servo motor (51).

5. A carbon fiber UAV wing forming mold according to claim 4, characterized in that, The upper mold base (6) is fixedly connected to a second track block (63), and the second threaded rod (52) is threadedly connected to the second track block (63). The upper mold base (6) is provided with a second cooling layer (61), and the bottom of the upper mold base (6) is fixedly connected to a drain pipe (62).

6. The carbon fiber UAV wing forming mold according to claim 1, characterized in that, The lower mold base (13) is provided with a first cooling layer (132), and a water drain hole (133) is provided at the bottom of the first cooling layer (132). A water inlet pipe (131) is fixedly connected to the lower mold base (13).

7. A carbon fiber UAV wing forming mold according to claim 3, characterized in that, The second track plate (4) has a first track block (41) fixedly connected to both ends, and the first track block (41) is threadedly connected to the first threaded rod (32).

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