A composite device forming mold for securing a rudder.

Abstract

The utility model discloses a kind of composite material device forming die for fixing rudder engine, belong to mould pressing technical field, including lower mould, the side of lower mould is equipped with temperature measuring hole, the top surface of lower mould is equipped with positioning guide column respectively, the top surface of lower mould is equipped with positioning pin, positioning pin is installed with first module, second module and third module are respectively installed on first module, the side of first module close to temperature measuring hole is equipped with first movable block, the side of first module away from temperature measuring hole is equipped with second movable block and third movable block respectively, positioning guide column is installed with upper mould. First, first module, second module and third module are separately individually pasted inner skin, place fiber outside inner skin, after pasting outer skin, perform mould closing. The carbon fiber composite material manufactured by the utility model using mould pressing mode can guarantee the interlaminar bond degree of composite material, improve the production quality and size requirement of fixing device.

Description

Technical Field

[0001] This utility model belongs to the field of molding technology, and in particular relates to a molding die for a composite material device for fixing a servo motor. Background Technology

[0002] Servo mechanisms play a crucial role in aircraft, controlling key components such as the rudder and horizontal stabilizer. Precise control of the servo's rotation angle enables flight maneuvers such as pitch and roll. Using carbon fiber composite materials to mount the servo fully leverages the excellent mechanical properties of carbon fiber, its extreme lightweight nature, and outstanding fatigue resistance, corrosion resistance, and dimensional stability, significantly improving the overall system performance. However, existing methods for manufacturing carbon fiber composite devices are complex, difficult to demold, and produce products with relatively low dimensional accuracy. Utility Model Content

[0003] The purpose of this invention is to provide a molding die for a composite material device used to fix a servo motor, so as to solve the problems existing in the prior art.

[0004] To achieve the above objectives, this utility model provides the following solution: This utility model provides a molding die for a composite material device used to fix a servo motor, including a lower die. A temperature measuring hole is provided on one side of the lower die. Positioning guide posts are provided at the four corners of the top surface of the lower die. Positioning pins are provided on the top surface of the lower die. A first module is installed on the positioning pins. A second module and a third module are respectively installed on the first module. A first movable block is provided on the side of the first module near the temperature measuring hole. A second movable block and a third movable block are respectively provided on the side of the first module away from the temperature measuring hole. An upper die is installed on the positioning guide posts.

[0005] Preferably, the outer sides of the first module, the second module and the third module are respectively covered with inner skins, the inner skins are filled with fibers, and the outer skins are provided on the outside of the fibers.

[0006] Preferably, the first module, the second module, and the third module are fixed to the lower mold by screws.

[0007] Preferably, the lower mold is provided with a lifting ring hole.

[0008] Preferably, the lower mold has mold release grooves on both sides.

[0009] Preferably, the second live block abuts against both the first live block and the second live block.

[0010] This utility model discloses the following technical effects: First, the inner skin of the first, second, and third modules is laid separately. Then, the three laid modules are installed on the lower mold. Fibers are placed outside the inner skin, and then the outer skin is laid before the mold is closed. During the laying process, the mold can be used for assistance, and multiple vacuum pre-compaction can be performed to ensure the size and density of the laid product. This utility model uses a molding method to manufacture carbon fiber composite materials, which can ensure the interlayer bonding of the composite material and improve the production quality and dimensional requirements of the fixing device. Attached Figure Description

[0011] The accompanying drawings, which form part of this application, are used to provide a further understanding of this application. The embodiments of this application and their descriptions are used to explain this application and do not constitute an undue limitation of this application. In the drawings:

[0012] Figure 1 This is a structural diagram showing the placement of each module in the lower module of this utility model;

[0013] Figure 2 This is a schematic diagram of the structure of the lower module where each movable block is placed;

[0014] Figure 3 This is a schematic diagram of the mold assembly structure of this utility model.

[0015] In the diagram: 1. Lower mold; 2. Temperature measuring hole; 3. Positioning guide post; 4. Positioning pin; 5. First module; 6. Second module; 7. Third module; 8. First movable block; 9. Second movable block; 10. Third movable block; 11. Screw; 12. Lifting eye hole; 13. Ejection groove. Detailed Implementation

[0016] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0017] To make the above-mentioned objectives, features and advantages of this utility model more apparent and understandable, the utility model will be further described in detail below with reference to the accompanying drawings and specific embodiments.

[0018] Reference Figures 1 to 3As shown, this embodiment provides a composite material device molding die for fixing a servo motor, including a lower die 1. A temperature measuring hole 2 is provided on one side of the lower die 1. Positioning guide posts 3 are provided at the four corners of the top surface of the lower die 1. Positioning pins 4 are provided on the top surface of the lower die 1. A first module 5 is installed on the positioning pins 4. A second module 6 and a third module 7 are respectively installed on the first module 5. A first movable block 8 is provided on the side of the first module 5 near the temperature measuring hole 2. A second movable block 9 and a third movable block 10 are respectively provided on the side of the first module 5 away from the temperature measuring hole 2. An upper die is installed on the positioning guide posts 3.

[0019] First, the inner skins of modules 5, 6, and 7 are individually laid. Then, the three laid modules are installed on the lower mold 1. Fibers are placed outside the inner skins, and the outer skins are then laid before the molds are closed. During the laying process, mold assistance and multiple vacuum pre-compaction processes can be used to ensure the size and density of the laid product. This utility model uses a molding process to manufacture carbon fiber composite materials, which can ensure the interlayer bonding of the composite material and improve the production quality and dimensional requirements of the fixing device.

[0020] Temperature sensor 2 is mainly used to detect the temperature of the mold, which facilitates the control of the pressing time, pressing pressure and temperature control in the compression molding process, thereby reducing internal quality problems of the product.

[0021] The scheme was further optimized by laying inner skin on the outer side of the first module 5, the second module 6 and the third module 7 respectively, filling the inner skin with fibers, and providing an outer skin on the outer side of the fibers.

[0022] The design was further optimized, with the first module 5, the second module 6, and the third module 7 each fixed to the lower mold 1 using screws 11. This ensures accurate positioning of each module on the lower mold.

[0023] The design was further optimized by adding a lifting ring hole 12 to the lower mold 1. This hole is used to assist in mold closing.

[0024] The design was further optimized by adding mold release grooves 13 on both sides of the lower mold 1. This facilitates demolding after the mold is closed.

[0025] The scheme is further optimized so that the second live block 9 abuts against the first live block 8 and the second live block 9 respectively.

[0026] During molding, inner skins can be laid on each module separately, followed by the placement of movable blocks. During molding, pressure can be applied to the outer surface of the composite material using 95° movable blocks, ensuring the integrity of the product's inner and outer surfaces and improving product performance. Demolding is simple and convenient, minimizing the risk of product damage. During demolding, the positioning pins 4 and bolts can be removed gradually, dismantling each module without damaging the product surface. The upper and lower mold structure 1, composed of multiple movable blocks, ensures the surface quality of the product, reduces molding difficulty, and guarantees product precision requirements through the molding process. By designing the mold gap and controlling the movable block positioning method, the risk of poor bonding between multi-curved layers is reduced.

[0027] A method of using a composite material device molding die for fixing a servo motor includes the following steps:

[0028] S1. First, lay the inner skin of the first module 5, the second module 6 and the third module 7 separately. Then, place the first module 5 on the positioning pin 4 and tighten the screws on each module to ensure that each module is accurately positioned on the lower mold 1.

[0029] S2. Check the gap between modules on the modules installed in step S1, fill them with fiber, then lay the outer skin as a whole, and place the first movable block 8, the second movable block 9 and the third movable block 10 respectively to limit the product size and protect the product's outer surface.

[0030] S3. Perform mold closing, align the positioning guide post 3, and close the upper and lower molds 1 together, with the lifting ring assisting in mold closing;

[0031] S4. After the mold is closed, the product enters the press to cure. Using temperature measuring hole 2, the temperature is measured when the mold is heated to near the gel point. The temperature is then maintained for 30 minutes. At this time, the resin on the product has good fluidity.

[0032] S5. Continue heating and heat preservation for curing;

[0033] S6. Cool to room temperature, demold and trim to obtain a product that meets the requirements.

[0034] In the description of this utility model, it should be understood that the terms "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc., indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this utility model and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limitations on this utility model.

[0035] The embodiments described above are merely preferred embodiments of the present utility model and are not intended to limit the scope of the present utility model. Various modifications and improvements made to the technical solutions of the present utility model by those skilled in the art without departing from the spirit of the present utility model should fall within the protection scope defined by the claims of the present utility model.

Claims

1. A molding die for a composite material device for fixing a servo motor, characterized in that: The device includes a lower mold (1), a temperature measuring hole (2) on one side of the lower mold (1), positioning guide posts (3) at the four corners of the top surface of the lower mold (1), a positioning pin (4) on the top surface of the lower mold (1), a first module (5) installed on the positioning pin (4), a second module (6) and a third module (7) installed on the first module (5), a first movable block (8) on the side of the first module (5) close to the temperature measuring hole (2), a second movable block (9) and a third movable block (10) on the side of the first module (5) away from the temperature measuring hole (2), and an upper mold installed on the positioning guide post (3).

2. The molding die for a composite material device for fixing a servo motor according to claim 1, characterized in that: The outer sides of the first module (5), the second module (6) and the third module (7) are respectively covered with inner skins, the inner skins are filled with fibers, and the outer skins are provided on the outside of the fibers.

3. The molding die for a composite material device for fixing a servo motor according to claim 1, characterized in that: The first module (5), the second module (6) and the third module (7) are respectively fixed to the lower mold (1) by screws (11).

4. The molding die for a composite material device for fixing a servo motor according to claim 1, characterized in that: The lower mold (1) is provided with a lifting ring hole (12).

5. The molding die for a composite material device for fixing a servo motor according to claim 1, characterized in that: The lower mold (1) is provided with mold release grooves (13) on both sides.

6. The molding die for a composite material device for fixing a servo motor according to claim 1, characterized in that: The second movable block (9) abuts against the first movable block (8) and the second movable block (9) respectively.

Images