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A molding process of prepreg/smc composite material

A molding process and composite material technology, which is applied in the field of material processing, can solve the problems of low overall molding rate of composite material parts and structural damage of parts, and achieve the effects of improving interlayer shear strength, realizing structural weight reduction, and reducing production costs

Active Publication Date: 2021-06-08
LEIKEDE MACROMOLECULE TIANJIN CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem of extremely low overall molding rate of composite material parts, the invention discloses a molding process of prepreg / SMC composite material, which can combine the composite material with good fluidity but low performance with the composite material with poor fluidity but high performance Composite materials are co-molded to solve the problem of damage to the component structure due to punching during the assembly process of composite parts, and improve the overall molding rate of composite parts

Method used

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  • A molding process of prepreg/smc composite material
  • A molding process of prepreg/smc composite material
  • A molding process of prepreg/smc composite material

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Experimental program
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preparation example Construction

[0034] The preparation method of the modified carbon fiber described in the present invention: (1) ultrasonically vibrate 50g of carbon fiber in 2L of acetone for 2h, and dry it for later use; (2) disperse the product of step (1) in 2L of 45% concentrated nitric acid, Reflux and oxidize at 90°C for 60min, cool down naturally, wash with water until the pH is about 7, and dry for later use; (3) Disperse the product of step (2) in 2L tetrahydrofuran, add 15g lithium aluminum hydride, stir at 60°C for 2h, add 2L2mom / L of hydrochloric acid, stirred for 1.5h, filtered out the carbon fiber, soaked and washed in tetrahydrofuran for 18h, and dried for later use; (4) Take 720g of ethanol and 80g of alcohol solution, add 200g of silane coupling agent into it, stir and mix well To obtain the hydrolyzate of the silane coupling agent, disperse the product of step (3) in it, stir or ultrasonically vibrate for 30-60min, filter out the fiber and dry it.

[0035] A modified carbon fiber prepre...

Embodiment 1

[0038] Prepreg: Solvay Cytec MTM 23 (vinyl type), SMC sheet: Polynt- 24-12K (vinyl type, fiber content 50%).

[0039] (1) Paving: Cut the prepreg according to the layup design, cut and weigh the SMC sheet, and then place it at the designed position on the prepreg layup;

[0040] (2) Mold preparation: evenly coat the mold with release agent, fix the mold on the hot press, and heat the mold and the hot press to 130-135°C;

[0041] (3) Co-molding: put the prepreg + SMC sheet laid in step (1) quickly into the predetermined position in the mold, operate the hot press to close the mold and pressurize, the minimum pressure is 140kPa, and keep warm for 10min. The material is fully cured at 130-135°C;

[0042] (4) Demoulding: open the mold, keep the mold at 130-135°C, and use tools to take out the pressed parts.

[0043] The weighing in step (1) is based on the design requirements. When using SMC for corner filling, the required weight is calculated according to the thickness and a...

Embodiment 2

[0046] Prepreg: Solvay Cytec MTM 23 (vinyl type), SMC sheet: Polynt- 24-12K (vinyl type, fiber content 50%).

[0047] (1) Paving: Cut the prepreg according to the layup design, cut and weigh the SMC sheet, and then place it at the designed position on the prepreg layup;

[0048] (2) Mold preparation: evenly coat the mold with release agent, fix the mold on the hot press, and heat the mold and the hot press to 120-125°C;

[0049] (3) Co-moulding: quickly put the prepreg + SMC sheet laid in step (1) into the predetermined position in the mold, operate the hot press to close the mold, pressurize, the minimum pressure is 140kPa, and keep warm for 14min. The material is fully cured at 120-125°C;

[0050] (4) Demoulding: open the mold, keep the mold at 120-125°C, and use tools to take out the pressed parts.

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Abstract

The invention belongs to the field of composite materials, and specifically relates to a molding process of prepreg / SMC composite materials, specifically: (1) laying: cutting the prepreg according to the layup design, and cutting the SMC sheet , weighed, and then placed at the designed position on the prepreg layup; (2) mold preparation: evenly coat the release agent on the mold, and fix the mold on the hot press, and put the mold and the hot press Heat together to the predetermined molding temperature; (3) Co-molding: quickly put the prepreg + SMC sheet laid in step (1) into the predetermined position in the mold, operate the hot press to close the mold and pressurize, so that the material Fully solidify at the preset molding temperature; (4) Demoulding: open the mold, keep the mold at the preset molding temperature in step (3), and use tools to take out the pressed parts. The high structural strength of the product is conducive to realizing structural weight reduction, and the cycle is greatly shortened, which is conducive to forming components with complex structures, and is conducive to reducing production costs and energy consumption.

Description

technical field [0001] The invention belongs to the field of material processing, and in particular relates to a forming process of a prepreg / SMC composite material. Background technique [0002] Using resin-based composite materials instead of metal (aluminum alloy, steel) as the structure of automobiles, drones and other components can reduce the weight of the overall structure by more than 30%, which is one of the important directions for the development of structural components such as automobiles and drones. one. [0003] Composite materials have material characteristics such as anisotropy, and the forming method is significantly different from that of metal. In the process of component structure design, the design concept of metal components cannot be copied. The overall forming rate of components is extremely low, and screwing or riveting is used in the assembly process , will destroy the structural integrity of composite parts due to problems such as punching, reduc...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B29C70/34B29B15/08C08J5/24C08L63/10C08L63/00C08K9/06C08K7/06
CPCB29B15/08B29C70/34B29K2105/0872B29K2105/12B29K2105/256C08J5/24C08J2363/00C08J2363/10C08K7/06C08K9/06
Inventor 吕金艳张庆辉杨鹏飞
Owner LEIKEDE MACROMOLECULE TIANJIN CO LTD