Integral forming die for unmanned aerial vehicle shell

Abstract

An unmanned aerial vehicle shell integrated forming mold comprises a lower mold plate and an upper mold plate corresponding to the lower mold plate, a profiled groove matched with an unmanned aerial vehicle shell is formed in the lower mold plate, a protrusion corresponding to the profiled groove is formed in the upper mold plate, and vertically-formed upper fixing through holes are formed in the four corners of the top end of the upper mold plate; lower fixing through holes corresponding to the upper fixing through holes in a one-to-one mode are formed in the lower die plate, a lower inclined plane inclining downwards is arranged on the right side of the lower die plate, and an upper inclined plane corresponding to the lower inclined plane is arranged at the right end of the upper die plate. Four conical positioning blocks are arranged on the lower die plate and fixed to the two ends of the profiled groove respectively. And positioning grooves in one-to-one correspondence with the positioning blocks are formed in the upper template. The device is simple in structure and convenient to use.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicle production, and particularly relates to an integrally formed mold for an unmanned aerial vehicle housing. Background Art

[0002] An unmanned aerial vehicle, abbreviated as UAV, has the advantages of being flexible, fast in response, capable of unmanned flight, and having low operation requirements. It is widely used in the fields of electric power, communication, meteorology, agriculture, ocean, exploration, photography, disaster prevention and reduction, crop yield estimation, etc. Due to the characteristics of UAVs, the materials used to make UAVs are required to have high strength and light weight. Therefore, many UAV propellers are made of carbon fiber materials. Carbon fiber reinforced composite material is one of the most advanced high-performance composite materials at present, with the characteristics of light weight, high strength, high temperature resistance, corrosion resistance, and excellent thermodynamic properties. When producing the UAV housing, it is necessary to wrap the carbon fiber material on the foam board, and then place the board coated with the carbon fiber material into the upper mold and the lower mold, and place the mold on the hot press for heating and pressing to form. However, in the prior art, it is inconvenient to close and open the mold for unloading the UAV housing. It is not easy to position the upper mold and the lower mold, and they are prone to dislocation under high pressure. Summary of the Utility Model

[0003] In order to solve the technical problem that it is inconvenient to close and open the mold for unloading during the production of the existing UAV housing, the utility model provides an integrally formed mold for an unmanned aerial vehicle housing, which includes a lower template and an upper template corresponding to the lower template. A mold cavity matching the UAV housing is provided on the lower template, and a protrusion corresponding to the mold cavity is provided on the upper template. Vertically arranged upper fixing through holes are respectively provided at the four corners of the top end of the upper template, and lower fixing through holes corresponding to the upper fixing through holes one by one are provided on the lower template. During use, a pin is passed through the upper fixing through hole and enters the lower fixing through hole to fix the upper template and the lower template together, avoiding dislocation of the upper template and the lower template under the action of pressure. An inclined downwardly arranged lower inclined plane is provided on the right side of the lower template, and an upper inclined plane corresponding to the lower inclined plane is provided at the right end of the upper template. The settings of the upper inclined plane and the lower inclined plane facilitate the positioning of the upper template and the lower template and facilitate the unloading of the produced UAV housing from the mold cavity, improving the working efficiency. Four conical positioning blocks are provided on the lower template, and the positioning blocks are respectively fixed at both ends of the mold cavity; positioning grooves corresponding to the positioning blocks one by one are provided on the upper template. The settings of the positioning blocks and the positioning grooves can quickly adjust the position of the upper template in place during mold closing, improving the mold closing efficiency.

[0004] Preferably, two symmetrically arranged lower fixing through holes are also provided at the middle of the top end of the lower template, and the two lower fixing through holes are respectively located on the lower template on both sides of the mold cavity. An upper fixing through hole corresponding to the lower template one by one is provided at the middle of the upper template.

[0005] Preferably, notches for facilitating demolding are provided at the four corners of the top end of the upper template, which are convenient for removing the upper template and act like handles.

[0006] Preferably, the notches are rectangular.

[0007] Preferably, fixing slot holes for fixing and supporting are provided on the sides of both the upper template and the lower template. The fixing slot holes are provided to fix the upper template and the lower template on the fixture when manufacturing the upper template and the lower template.

[0008] Adopting the above solution has the following advantages:

[0009] The provision of the upper fixing through-hole and the lower fixing through-hole facilitates fixing the upper template and the lower template together with a pin. Under the pressure of the hot press, misalignment between the upper die and the lower die is avoided, improving the quality of the product; the provision of the positioning block and the positioning groove facilitates quickly and accurately buckling the upper template on the lower template, reducing the positioning time and improving the die-closing efficiency; the provision of the upper inclined plane and the lower inclined plane facilitates the positioning of the upper template and the lower template and facilitates removing the produced drone housing from the mold cavity, improving the working efficiency. Description of the Drawings

[0010] Figure 1 is a schematic three-dimensional structure of the present utility model Figure 1 ;

[0011] Figure 2 is a schematic three-dimensional structure of the present utility model Figure 2 ;

[0012] Figure 3 is an exploded view of the present utility model;

[0013] Figure 4 is a schematic diagram of the structure of the upper template;

[0014] Figure 5 is a schematic diagram of the structure of the lower template.

[0015] Reference numerals: 1, lower template; 2, upper template; 3, fixing slot hole; 11, mold cavity; 12, lower fixing through-hole; 13, positioning block; 14, lower inclined plane; 21, protrusion; 22, upper fixing through-hole; 23, positioning groove; 24, upper inclined plane. Detailed Embodiments

[0016] As Figure 1-2As shown in the figure, a one-piece molding die for a drone housing includes a lower template 1 and an upper template 2 arranged corresponding to the lower template 1. A molding groove 11 matching the drone housing is provided on the lower template 1, and a protrusion 21 corresponding to the molding groove 11 is provided on the upper template 2. Vertical upper fixing through holes 22 are provided at the four corners of the top end of the upper template 2, and lower fixing through holes 12 corresponding to the upper fixing through holes 22 one by one are provided on the lower template 1. During use, a pin is passed through the upper fixing through hole 22 and enters the lower fixing through hole 12 to fix the upper template 2 and the lower template 1 together, preventing the upper template 2 and the lower template 1 from being misaligned under pressure. A downwardly inclined lower inclined plane 14 is provided on the right side of the lower template 1, and an upper inclined plane 24 corresponding to the lower inclined plane 14 is provided at the right end of the upper template 2. The settings of the upper inclined plane 24 and the lower inclined plane 14 facilitate the positioning of the upper template 2 and the lower template 1 and the unloading of the produced drone housing from the molding groove 11, improving work efficiency. Four conical positioning blocks 13 are provided on the lower template 1, and the positioning blocks 13 are respectively fixed at both ends of the molding groove 11; positioning grooves 23 corresponding to the positioning blocks 13 one by one are provided on the upper template 2. The settings of the positioning blocks 13 and the positioning grooves 11 can quickly adjust the position of the upper template 2 in place during mold closing, improving the mold closing efficiency.

[0017] Preferably, two symmetrically arranged lower fixing through holes 12 are also provided at the middle of the top end of the lower template 1, and the two lower fixing through holes 12 are respectively located on the lower template 1 on both sides of the molding groove 11. An upper fixing through hole 22 corresponding to the lower template 1 one by one is provided at the middle of the upper template 2.

[0018] Preferably, notches 25 for facilitating mold unloading are provided at the four corners of the top end of the upper template 2, which are convenient for unloading the upper template 2 and act like handles.

[0019] Preferably, the notch 25 is rectangular.

[0020] Preferably, fixing slot holes 3 for fixing and supporting are provided on the sides of both the upper template 2 and the lower template 1. The setting of the fixing slot holes 3 is for fixing the upper template 2 and the lower template 1 on a fixture during the production of the upper template 2 and the lower template 1.

[0021] Usage process:

[0022] When the utility model is in use, it is necessary to wrap the carbon fiber material on the foam board, and then place the foam board wrapped with the carbon fiber material in the mold groove 11 on the lower template 1. The staff transports the upper template 2 above the lower template 1 through the notch 25, and then slowly lowers it until the positioning block 13 on the lower template 1 enters the positioning groove 23 on the upper template 2. After the upper template 2 drops to the specified position, the pins are sequentially placed into the upper fixing through holes 22, and the lower ends of the pins are inserted into the lower fixing through holes 12 on the lower template 1. Then, the device is transported under the hot press for the hot pressing treatment process. After the drone shell is hot-pressed and formed, each pin is pulled out in sequence, the upper template 2 is removed, and the drone shell product is removed from the mold groove 11 on the lower template 1.

[0023] In the description of the present utility model, it should be understood that the orientation or positional relationship indicated by the terms "upper", "lower", "left", "right", "top", "bottom", "horizontal", "vertical", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as a limitation to the present utility model.

[0024] The above embodiments are illustrative of the present utility model, rather than limiting the present utility model. Any solution obtained by simply transforming the present utility model belongs to the protection scope of the present utility model.

Claims

1. An integrally formed mold for a drone housing, comprising a lower template and an upper template arranged corresponding to the lower template, characterized in that: The lower template is provided with a shaped groove matching the drone housing, and the upper template is provided with a protrusion corresponding to the shaped groove. Moreover, vertical upper fixing through holes are provided at the four corners of the top end of the upper template, and lower fixing through holes corresponding to the upper fixing through holes one by one are provided on the lower template. An inclined downward lower inclined plane is provided on the right side of the lower template, and an upper inclined plane corresponding to the lower inclined plane is provided at the right end of the upper template.

2. The one-piece forming mold for the drone housing according to claim 1, wherein: Four conical positioning blocks are provided on the lower template, and the positioning blocks are respectively fixed at both ends of the shaped groove; positioning grooves corresponding to the positioning blocks one by one are provided on the upper template.

3. The one-piece molding die for the drone housing according to claim 1, wherein: Two symmetrically arranged lower fixing through holes are also provided at the middle of the top end of the lower template, and the two lower fixing through holes are respectively located on the lower template on both sides of the shaped groove. An upper fixing through hole corresponding to the lower template one by one is provided at the middle of the upper template.

4. A one-piece molding die for a drone housing according to claim 1, characterized in that: Notches facilitating mold unloading are provided at the four corners of the top end of the upper template.

5. The one-piece forming mold for a drone housing according to claim 4, characterized in that: The notches are rectangular.

6. The one-piece molding die for the drone housing according to claim 1, characterized in that: Fixing slot holes for fixing and supporting are provided on the sides of both the upper template and the lower template.

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