Forming method for variable cross-section hollow-structure composite part with high-precision inner surface

A composite material and molding method technology, applied in the field of autoclave molding of resin-based fiber-reinforced composite material prepreg, can solve the problems of vacuum leakage, expensive materials, and high cost, and achieve lower quality requirements, simple demoulding operation, and low cost low effect

Inactive Publication Date: 2019-06-07
成都联科航空技术有限公司
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0003] 1) The metal combined mandrel has many assembly relationships, high precision of the mating surface, difficult processing, high cost, and cannot guarantee the overall airtightness of the mold, and problems such as vacuum leakage are prone to occur during the curing process; when the shape is relatively When it is complex, metal combined mold processing cannot be realized;
[0004] 2) Water-soluble mandrel: There are two types of water-soluble mandrels, one is pouring mandrel, that is, the mandrel is obtained by pouring special water

Method used

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  • Forming method for variable cross-section hollow-structure composite part with high-precision inner surface
  • Forming method for variable cross-section hollow-structure composite part with high-precision inner surface
  • Forming method for variable cross-section hollow-structure composite part with high-precision inner surface

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Example Embodiment

[0036] Example

[0037] See Figure 1-Figure 7 . This embodiment provides a method for forming a composite material part 1 with a variable cross-section hollow structure with a high-precision inner surface. This method uses a forming core mold 3. See figure 2 and image 3 The molding core mold 3 includes a soft mold 31, a water-soluble core 32 and a support.

[0038] The soft mold 31 includes an outer rubber layer, an inner rubber layer, and a carbon fiber composite material layer between the outer rubber layer and the inner rubber layer. The space enclosed by the soft mold 31 is filled with a water-soluble core 32 made of a water-soluble material. In this embodiment, the water-soluble core 32 is made of a high-temperature-resistant water-soluble material, such as:

[0039] The number of support rods 33 is two. One support rod 33 is located at one end of the water-soluble core 32 and the other support rod 33 is located at the other end of the water-soluble core 32. One end of th...

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Abstract

The invention relates to the technical field of forming of resin-based fiber reinforced composite prepreg through an autoclave, in particular to a forming method for a variable cross-section hollow-structure composite part with a high-precision inner surface. A forming mandrel is adopted and comprises a sold mold and a water-soluble core, and the water-soluble core is located in the spaced formedby the soft mold. The forming method includes the following steps that composite prepreg is paved on the surface of the soft mold; the composite prepreg is cured; and the water-soluble core is removed, and the soft mold and the cured composite are separated. The forming method provided by the invention adopts the forming mandrel combining the soft mold and the water-soluble core, the soft mold isused for being attached to the composite, and therefore high surface quality can be provided. The water-soluble core is used for supporting the soft mold, so that the soft mold has a preset shape, andthe cost of the forming mandrel is low. In the machining process of the composite part, during demolding, the water-soluble core is removed firstly, the soft mold is deformed and removed, and therefore demolding is achieved, and demolding operation is simple.

Description

technical field [0001] The invention relates to the technical field of resin-based fiber-reinforced composite material prepreg autoclave forming technology, in particular to a high-precision internal surface variable cross-section hollow structure composite material part forming method. Background technique [0002] Due to its light weight, high specific strength and specific stiffness, and strong designability, composite materials are increasingly used in the field of aerospace vehicle structural parts; Aero-engine inlet with deformed cross-section; when forming this type of structural parts, the side with high surface quality and precision requirements is usually selected as the surface that fits the mold, referred to as the mold-fitting surface. When the inner shape surface of the part is the mold-fitting surface, the male mold lay-up and molding method can be used, and the demolding of the part after curing is more difficult. In order to achieve the purpose of forming p...

Claims

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Application Information

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IPC IPC(8): B29C70/34B29C70/54B29C33/00B29C33/52
Inventor 李书军陈剑尹军华李璐璐杨自燕周才超石小平任贵川谷雨
Owner 成都联科航空技术有限公司
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