Manufacturing process for carbon fiber composite forming membrane disk

A composite material and manufacturing process technology, which is applied in the field of carbon fiber composite material forming membrane disc manufacturing process, can solve the problems of strong wear resistance, high strength, and inability to produce quality, and achieve good corrosion resistance, fatigue resistance, and The effect of small thermal expansion coefficient

Inactive Publication Date: 2018-05-11
刘长喜
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to clarify a carbon fiber composite material forming membrane disk manufacturing process, in order to solve the problem in the prior art that carbon fiber co

Method used

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  • Manufacturing process for carbon fiber composite forming membrane disk
  • Manufacturing process for carbon fiber composite forming membrane disk
  • Manufacturing process for carbon fiber composite forming membrane disk

Examples

Experimental program
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Example Embodiment

Specific embodiment one:

[0023] The carbon fiber composite material forming membrane disc manufacturing process of this embodiment, the carbon fiber composite material forming membrane disc manufacturing process, involves the slitting method of the resin-based carbon fiber prepreg, that is, the roll prepreg is first assembled on the rack Above, fix the edge of the prepreg with the mechanical structure of position alignment, use a vibrating cutter to cut the prepreg into multiple prepregs of specified size, collect the cut prepreg, repeat the above steps Until all the prepregs are cut.

[0024] The prepreg prepared by the slitting method of the resin-based carbon fiber prepreg has uniform thickness and accurate size, which significantly improves the compactness, uniformity and dimensional accuracy of the product.

[0025] The manufacturing process of the carbon fiber composite material forming membrane disc involves a preheating process method, that is, a heating device is used nea...

Example Embodiment

Specific implementation manner two:

[0038] The difference from the first embodiment is that in the manufacturing process of the carbon fiber composite material forming membrane disc in this embodiment, the cutting is performed according to the graphics drawn by the cutting machine as described in step 1, and the above steps are repeated until all the prepregs are cut. In the process, the prepreg is cut by the cutting method of the coordinate cutting machine vibrating cutting knife.

Example Embodiment

Specific implementation manner three:

[0039] The difference from the first or second embodiment is that in the manufacturing process of the carbon fiber composite material molded film tray of this embodiment, the heating device described in step 2 is used to preheat and heat the prepreg obtained in step 1 The heating device is a digital heating platform device.

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Abstract

The invention discloses a manufacturing process for a carbon fiber composite forming membrane disk. The manufacturing process comprises the steps that a prepreg is slit into a prepreg body in a certain shape and angle; a mold is cleaned and coated with a mold releasing agent; a heating platform is used for carrying out preheating treatment on the cut prepreg body; the prepreg body is laid to forma carbon fiber composite layer in a regular shape; a vacuum membrane bag is used for carrying out sealing treatment, and vacuumizing is carried out to form negative pressure; an oven is used for heating and solidifying the carbon fiber composite layer; the cooled carbon fiber composite layer is separated from the mold; the carbon fiber composite layer is cut and polished, and a finished product ofthe carbon fiber composite forming membrane disk is obtained. The membrane disk manufactured through the method has high-content fiber, the surface is bright without bubbles, the interlayer bonding intensity achieves an effect of a compression molding process, and the requirement for carbon fiber composite product production in the fields of aerospace and navigation.

Description

Technical field: [0001] The invention relates to a manufacturing process of a carbon fiber composite material forming membrane disc, in particular to a closed mold internal pressure forming process of a prepreg carbon fiber composite material. Background technique: [0002] Resin-based carbon fiber reinforced phase composite material is lighter than metal aluminum, but its strength is higher than steel, and it has the characteristics of corrosion resistance and high modulus. With many excellent properties, carbon fiber has high axial strength and modulus, low density, high specific performance, no creep, ultra-high temperature resistance in non-oxidizing environment, good fatigue resistance, specific heat and electrical conductivity between non-metal and metal Among them, the coefficient of thermal expansion is small and anisotropic, with good corrosion resistance and good ray transparency. Good electrical and thermal conductivity, good electromagnetic shielding, etc. [0...

Claims

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Application Information

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IPC IPC(8): B29C70/34B29C70/54
CPCB29C70/345B29C70/545
Inventor 刘长喜
Owner 刘长喜
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