Integrated forming die for aircraft adapter

By designing an integrated mold for aircraft adapters and using upper and lower molds to form a single mold, the problems of cumbersome molding processes and inconsistent quality were solved, achieving efficient and precise adapter production.

CN224145197UActive Publication Date: 2026-04-21GUIZHOU AEROSPACE TIANMA ELECTRICAL TECH
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
GUIZHOU AEROSPACE TIANMA ELECTRICAL TECH
Filing Date
2025-03-12
Publication Date
2026-04-21

AI Technical Summary

Technical Problem

Existing aircraft adapter molding processes are cumbersome, have poor quality consistency, and are prone to molding defects such as dents, bubbles, softening, and whitening. Furthermore, the molding molds are complex in structure and costly, and cannot adapt to the rapid foaming of rigid polyurethane foam.

Method used

Design an integrated mold for an aircraft adapter, which adopts an upper and lower mold structure, with the molding grooves symmetrically distributed in a grid pattern, and is equipped with vent holes and positioning pins. Combined with a disassembly cover plate and a triangular notch step, it achieves integrated molding and avoids the problems of glue adhesion and rapid foaming.

Benefits of technology

It improves product quality consistency, reduces molding defects, simplifies operation processes, reduces costs, and improves production efficiency and precision.

✦ Generated by Eureka AI based on patent content.

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Abstract

An aircraft adapter integral forming die comprises an upper die and a lower die, the upper die and the lower die are both provided with forming grooves, the forming grooves are symmetrically distributed in a shape like a Chinese character'tian ', the upper die comprises an upper die upper portion and an upper die lower portion, and the lower die comprises a lower die upper portion and a lower die lower portion. The forming groove of the upper die is formed in the lower portion of the upper die, the forming groove of the lower die is formed in the upper portion of the lower die, the forming groove structures of the upper die and the lower die correspond to each other, the upper portion of the upper die is a flat face, and the lower portion of the lower die is a flat face. The lower portion of the upper die and the upper portion of the lower die are connected to form a closed cavity, and four identical adapters can be formed at the same time. The problem that the overall thickness of the adapter is inconsistent due to the fact that glue is used for pasting in the later period is avoided through mold closing integrated forming, the quality consistency of products is improved, the number of mold accessories is small, the structure is simple, and the production efficiency of the products can be effectively improved while the product precision is guaranteed.
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Description

Technical Field

[0001] This utility model belongs to the field of foam material molding mold technology, and in particular relates to an integrated molding mold for an aircraft adapter. Background Technology

[0002] An aircraft adapter is an auxiliary device inside an aircraft that serves as a connection, playing a crucial role in the aircraft's storage, transportation, and launch. An aircraft adapter typically consists of a metal shell, a rubber-plastic sheet, a rigid polyurethane foam layer, and an anti-static cloth. The adapter is generally manufactured as follows: first, the rigid polyurethane foam is cured and molded; then, the rubber-plastic sheet is adhered to the surface of the rigid polyurethane foam; finally, the anti-static cloth is attached.

[0003] The aforementioned molding methods are not only cumbersome, but the bonding of the rigid polyurethane foam layer to the rubber-plastic board is mostly done manually. The thickness of the adhesive layer affects the overall thickness of the adapter, making it impossible to guarantee the consistency of the final product's quality. Furthermore, existing molding dies have complex structures, high processing costs, and are prone to molding defects such as dents, bubbles, softening, and whitening on the product surface during the molding process. In addition, rigid polyurethane foam expands rapidly, and some foaming dies, due to the large number of parts, cannot be assembled in time during foaming, resulting in partial overflow of polyurethane foam, severely impacting product quality.

[0004] For example, patent document CN111645248A discloses a mold for integrally molding an irregularly shaped adapter, including a base plate, a mold frame vertically fixed to the base plate, and an upper mold rotatably fixed in the middle of the mold frame. The upper mold, mold frame, and base plate form a hollow cavity. The top surface of the upper mold is parallel to the plane of the adapter guide groove to be molded, and the top surface of the upper mold is not parallel to the upper surface of the base plate. This effectively prevents the PTFE film from falling off, ensures the integrity of the adapter, meets the requirements for wear resistance, high temperature resistance, and anti-adhesion performance, and conforms to the integrated design of structure and function. However, it cannot avoid molding defects such as dents, bubbles, softening, and whitening during molding. Moreover, this mold is only suitable for molding this irregularly shaped adapter and is not suitable for molding other non-irregularly shaped adapters.

[0005] Therefore, it is necessary to design a one-piece molding mold specifically for aircraft adapters that has a simple process, fewer manual operations, high product quality consistency, and can adapt to the fast foaming speed of rigid polyurethane foam, in order to improve the quality and production efficiency of aircraft adapters and avoid molding defects such as dents, bubbles, softening and whitening during the molding process. Utility Model Content

[0006] To address the problems existing in the prior art, this utility model provides an integrated mold for an aircraft adapter.

[0007] This invention is implemented as follows: an integrated mold for an aircraft adapter includes an upper mold and a lower mold. Both the upper and lower molds are provided with molding grooves, which are symmetrically distributed in a grid pattern. The upper mold includes an upper part and a lower part, and the lower mold includes an upper part and a lower part. The molding groove of the upper mold is located in the lower part, and the molding groove of the lower mold is located in the upper part. The molding groove structures of the upper and lower molds correspond to each other. The upper part of the upper mold is a flat surface, and the lower part of the lower mold is a flat surface. The lower part of the upper mold and the upper part of the lower mold are connected to form a closed cavity, which can simultaneously mold four identical adapters.

[0008] Furthermore, the bottom of the forming groove of the upper mold is set as a concave semi-circular shape and is provided with multiple vent holes, which are evenly distributed around the perimeter and center of the forming groove of the upper mold; the edges of the forming groove of the upper mold in the width direction are set as the same concave semi-circular shape.

[0009] Furthermore, two pull ring holes are provided on both sides of the upper mold in the width direction, and the pull ring holes are symmetrically distributed along the two axes of the upper mold.

[0010] Furthermore, the upper mold has a boss at the center of the outer long edge of the four forming grooves, and the outer side of the boss is aligned with the long edge of the upper mold.

[0011] Furthermore, the upper mold has multiple threaded holes A on its four sides at the bottom, and the lower mold has the same threaded holes B at corresponding positions on its upper part. The upper mold and the lower mold are connected by screws installed in the threaded holes A and B.

[0012] Furthermore, the bottom of the forming groove of the lower mold is set as an outwardly convex semi-circular shape, and the edge of the forming groove of the lower mold in the width direction is set as the same outwardly convex semi-circular shape as the bottom, and matches the inwardly concave semi-circular shape of the edge of the upper mold.

[0013] Furthermore, the bottom of the forming groove of the lower mold is equipped with a positioning pin and a disassembly cover plate. The positioning pin passes through the disassembly cover plate from the lower part of the lower mold and is located at the center of the bottom of the forming groove of the lower mold. Two adjacent positioning pins in the width direction of the lower mold are installed on the same disassembly cover plate. The disassembly cover plate is installed on the lower part of the lower mold by screws.

[0014] Furthermore, the bottom of the two adjacent forming grooves in the width direction of the lower mold is provided with a through groove, and the disassembly cover plate is set in the through groove. A total of two disassembly cover plates are provided in the lower part of the lower mold.

[0015] Furthermore, the four corners of the upper part of the lower mold are all set with the same triangular notch step, and the edges of the upper part of the lower mold along the length direction are provided with grooves that cooperate with the boss of the upper mold.

[0016] Furthermore, handle holes are provided on both sides of the lower mold in the width direction, and the handle holes are symmetrically distributed along the two axes of the lower mold.

[0017] In summary, the beneficial effects of this utility model are as follows:

[0018] (1) The present invention uses the upper mold and lower mold to make the adapter product, which avoids the problem of inconsistent overall thickness of the final adapter caused by glue bonding in the later stage, and improves the quality consistency of the product.

[0019] (2) By setting vent holes in the molding groove of the upper mold, this utility model effectively reduces the molding defects such as depressions, bubbles, softness and whitening on the surface of the adapter after molding.

[0020] (3) This utility model improves the positioning accuracy of each material used in the adapter by setting positioning pins in the lower mold, thereby improving the overall accuracy of the product.

[0021] (4) By setting a detachable cover plate and a triangular notch step in the lower mold, the demolding and disassembly of the upper mold and the lower mold are simple and convenient. The integrated molding mold has high positioning accuracy, uses fewer accessories and has a simple structure. While ensuring product accuracy, it can effectively improve product production efficiency. Attached Figure Description

[0022] To more clearly illustrate the technical solutions of the embodiments of this utility model, the accompanying drawings used in the description of the embodiments will be briefly introduced below.

[0023] Figure 1 This is a schematic diagram of the upper part of the upper mold of the integrated mold for the aircraft adapter described in this utility model;

[0024] Figure 2 This is a schematic diagram of the upper part of the lower mold of the integrated molding mold for the aircraft adapter of this utility model;

[0025] Figure 3 This is a schematic diagram of the lower part of the integrated molding mold for the aircraft adapter of this utility model;

[0026] Explanation of icon numbers:

[0027] 1-Upper mold, 11-Vent hole, 12-Pull ring hole, 13-Boss, 14-Threaded hole A, 15-Upper part of upper mold, 16-Lower part of upper mold;

[0028] 2-Lower mold, 21-Handle hole, 22-Positioning insert, 23-Removable cover plate, 24-Through groove, 25-Threaded hole B, 26-Triangular notch step, 27-Upper part of lower mold, 28-Lower part of lower mold. Detailed Implementation

[0029] 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.

[0030] like Figures 1-3 As shown in the figure, this utility model embodiment provides an integrated molding mold for an aircraft adapter, including an upper mold 1 and a lower mold 2. Both the upper mold 1 and the lower mold 2 are provided with molding grooves, which are symmetrically distributed in a grid pattern. The upper mold 1 includes an upper part 15 and an upper part 16, and the lower mold 2 includes an upper part 27 and a lower part 28. The molding groove of the upper mold 1 is located in the lower part 16, and the molding groove of the lower mold 2 is located in the upper part 27. The molding groove structures of the upper mold 1 and the lower mold 2 correspond to each other. The upper part 15 of the upper mold is a flat surface, and the lower part 28 of the lower mold is a flat surface. The lower part 16 of the upper mold and the upper part 27 of the lower mold are connected to form a closed cavity, which can simultaneously mold four identical adapters. By setting the upper mold 1 and the lower mold 2, the adapter can be integrally molded in the closed cavity formed by the upper mold 1 and the lower mold 2, avoiding the problem of inconsistent overall thickness of the final adapter caused by later gluing, thus improving the consistency of product quality.

[0031] In this embodiment, the bottom of the forming groove of the upper mold 1 is set as a concave semi-circular shape and is provided with a plurality of vent holes 11. The vent holes 11 are evenly distributed around the periphery and center of the forming groove of the upper mold 1. The edges of the forming groove of the upper mold 1 in the width direction are set as the same concave semi-circular shape. By setting the vent holes 11, the problems of forming defects such as dents, bubbles, softness and whitening on the surface of the adapter after forming can be effectively reduced.

[0032] In this embodiment, two pull ring holes 12 are provided on both sides of the upper mold 1 in the width direction. The pull ring holes 12 are symmetrically distributed along the two axes of the upper mold 1 and are used to install pull rings. When using pull rings, the one-piece mold is subjected to uniform force.

[0033] In this embodiment, the upper mold 1 has a boss 13 at the middle of the outer long edge of the four forming grooves. The outer side of the boss 13 is aligned with the long edge of the upper mold 1 for positioning and to cooperate with the structural features of the lower mold.

[0034] In this embodiment, the lower part 16 of the upper mold is provided with a plurality of threaded holes A14 on its four sides, and the upper part 27 of the lower mold is provided with the same threaded holes B25 at corresponding positions. The upper mold 1 and the lower mold 2 are connected by screws provided in the threaded holes A14 and the threaded holes B25. The lower part 16 of the upper mold is provided with an average of 3 threaded holes A14 on each side to ensure the tightness of the upper mold 1 and the lower mold 2 when they are closed.

[0035] In this embodiment, the bottom of the forming groove of the lower mold 2 is set as an outwardly convex semi-circular shape, and the edge of the forming groove of the lower mold 2 in the width direction is set as the same outwardly convex semi-circular shape as the bottom, and matches the inwardly concave semi-circular shape of the edge of the upper mold 1, so as to match the structural features corresponding to the upper mold.

[0036] In this embodiment, a positioning pin 22 and a disassembly cover plate 23 are installed at the bottom of the forming groove of the lower mold 2. The positioning pin 22 passes through the disassembly cover plate 23 from the lower part 28 of the lower mold and is located at the center of the bottom of the forming groove of the lower mold 2. Two adjacent positioning pins 22 in the width direction of the lower mold 2 are installed on the same disassembly cover plate 23. The disassembly cover plate 23 is installed on the lower part 28 of the lower mold by screws. By setting the positioning pin 22 and the disassembly cover plate 23, an interface for connection with the aircraft is reserved for the adapter during the forming process, which facilitates the use of the adapter. The installation of two adjacent positioning pins 22 in the width direction of the lower mold on the same disassembly cover plate 23 simplifies the structure of the mold, facilitates disassembly and assembly, and reduces the difficulty of processing the mold and the cost of components.

[0037] In this embodiment, the bottom of the two adjacent forming grooves in the width direction of the lower mold 28 is provided with a through groove 24, and the disassembly cover plate 23 is disposed in the through groove 24. A total of two disassembly cover plates 23 are provided in the lower mold 28, which improves the reliability of the installation of the disassembly cover plate 23.

[0038] In this embodiment, the four corners of the upper part 27 of the lower mold are all set with the same triangular notch step 26. The edge of the upper part 27 of the lower mold along the length direction is provided with a groove that cooperates with the boss 13 of the upper mold 1. The triangular notch step 26 facilitates the demolding after the mold is closed, and makes it easy to separate the upper mold 1 and the lower mold 2.

[0039] In this embodiment, handle holes 21 are provided on both sides of the lower mold 2 in the width direction. The handle holes 21 are symmetrically distributed along the two axes of the lower mold 2, which makes the installation of the handle simple and the lower mold 2 is evenly stressed when using the handle.

[0040] In use, first separate the upper mold 1 from the lower mold 2, install and fix the positioning pin 22 and the disassembly cover plate 23 from the lower mold. Then, lay the materials required for the aircraft adapter in sequence at the bottom of the lower mold forming groove. For example, first lay the rubber sheet flat at the bottom of the lower mold forming groove and compact it, with the smooth side of the rubber sheet facing down and the mushroom head column facing up, and the mushroom head pointing towards the upper mold. Then, pour the mixed rigid polyurethane foam material into the lower mold forming groove. Then, connect the upper mold 1 and the lower mold 2 with screws to close the mold. After curing, separate the upper mold 1 from the lower mold 2 from the triangular notch step 26, then remove the disassembly cover plate 23 and the positioning pin 22. Then, use a wooden stick to gently tap the cured adapter in the lower mold 2 through the channel of the positioning pin 22 to remove it and obtain the one-piece molded adapter.

[0041] This invention manufactures the adapter product using a combined upper and lower mold, avoiding the problem of inconsistent overall thickness caused by subsequent glue bonding, thus improving product quality consistency. Venting holes in the upper mold's forming groove effectively reduce molding defects such as dents, bubbles, softening, and whitening on the adapter's surface after molding. Positioning pins in the lower mold improve the placement accuracy of the materials used in the adapter, enhancing the overall product precision. A detachable cover plate and triangular notch step in the lower mold simplify demolding and disassembly of the upper and lower molds. This integrated molding die features high positioning accuracy, fewer components, and a simple structure, effectively improving production efficiency while ensuring product precision.

[0042] The quality and dimensions of the aircraft adapters manufactured using the integrated mold of the aircraft adapter described in this embodiment were tested. Four adapters manufactured by the integrated mold of this embodiment were randomly tested, and the test data are shown in Table 1. The test data in Table 1 shows that the quality and dimensions of the adapter products manufactured using the integrated mold of this embodiment meet the requirements.

[0043] Table 1

[0044]

[0045] The above description is only a preferred embodiment of the present utility model and does not limit the patent scope of the present utility model. All equivalent structural transformations made under the concept of the present utility model and using the contents of the present utility model specification and drawings, or direct / indirect applications in other related technical fields, are included in the patent protection scope of the present utility model.

Claims

1. A one-piece mold for an aircraft adapter, characterized in that: The upper mold (1) and the lower mold (2) are provided with forming grooves. The forming grooves are symmetrically distributed in a grid pattern. The upper mold (1) includes an upper part (15) and a lower part (16). The lower mold (2) includes an upper part (27) and a lower part (28). The forming groove of the upper mold (1) is located in the lower part (16). The forming groove of the lower mold (2) is located in the upper part (27). The forming groove structures of the upper mold (1) and the lower mold (2) are corresponding. The upper part (15) of the upper mold is a flat surface. The lower part (28) of the lower mold is a flat surface. The lower part (16) of the upper mold and the upper part (27) of the lower mold are connected to form a closed cavity, which can simultaneously form 4 identical adapters. The bottom of the forming groove of the upper mold (1) is set as a concave semi-circular shape and is provided with multiple vent holes (11). The vent holes (11) are evenly distributed around and in the center of the forming groove of the upper mold (1); the edges of the forming groove of the upper mold (1) in the width direction are set to the same concave semi-circular shape; the bottom of the forming groove of the lower mold (2) is equipped with positioning pins (22) and disassembly cover plates (23). The positioning pins (22) pass through the disassembly cover plates (23) from the lower part (28) of the lower mold and are set in the center of the bottom of the forming groove of the lower mold (2). Two adjacent positioning pins (22) in the width direction of the lower mold (2) are installed on the same disassembly cover plate (23). The disassembly cover plate (23) is installed in the lower part (28) of the lower mold by screws; the four corners of the upper part (27) of the lower mold are all set to the same triangular notch steps (26). The edges of the upper part (27) of the lower mold in the length direction are provided with grooves that cooperate with the bosses (13) of the upper mold (1).

2. The aircraft adapter integrally formed mold of claim 1, wherein: Two pull ring holes (12) are provided on both sides of the upper mold (1) in the width direction. The pull ring holes (12) are symmetrically distributed along the two axes of the upper mold (1).

3. The aircraft adapter integrally formed mold of claim 1, wherein: The upper mold (1) has a boss (13) in the middle of the long edge of the four forming grooves on the outside. The side of the boss (13) facing outward is aligned with the long edge of the upper mold (1).

4. The aircraft adapter integrally formed mold of claim 1, wherein: The lower part (16) of the upper mold has multiple threaded holes A (14) on its four sides, and the upper part (27) of the lower mold has the same threaded holes B (25) at the corresponding positions. The upper mold (1) and the lower mold (2) are connected by screws in the threaded holes A (14) and B (25).

5. The aircraft adapter integrally formed mold of claim 1, wherein: The bottom of the forming groove of the lower mold (2) is set as an outwardly convex semi-circular shape, and the edge of the forming groove in the width direction of the lower mold (2) is set as the same outwardly convex semi-circular shape as the bottom, and matches the concave semi-circular shape of the edge of the upper mold (1).

6. The aircraft adapter integrally formed mold of claim 1, wherein: The bottom of the two adjacent forming grooves in the width direction of the lower part (28) of the lower mold is provided with a through groove (24), and the disassembly cover plate (23) is provided in the through groove (24). A total of two disassembly cover plates (23) are provided in the lower part (28) of the lower mold.

7. The integrated mold for the aircraft adapter as described in claim 1, characterized in that: The lower mold (2) is provided with handle holes (21) on both sides in the width direction, and the handle holes (21) are symmetrically distributed along two axes of the lower mold (2).

Citation Information

Patent Citations

  • Special-shaped adapter integrated forming die and method

    CN111645248A