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A springback deformation suppression method for laser-assisted in-situ formed thermoplastic composite structural parts

A technology of composite materials and in-situ forming, which is applied in the field of composite materials to achieve the effects of improving manufacturing precision, realizing localized adjustment, and improving springback problems

Active Publication Date: 2021-09-24
DALIAN UNIV OF TECH
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] In order to solve the springback problem that occurs during the forming process of thermoplastic composite lattice structures and other complex structures, this patent provides a method for suppressing springback deformation of thermoplastic composite structural parts with laser-assisted in-situ forming, which helps to realize automation integration Forming, can be used for laying and forming of thermoplastic composite structural parts with various shapes, easy to realize localized adjustment of springback deformation, and helps to realize high-precision manufacturing of thermoplastic composite aerospace vehicle parts

Method used

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  • A springback deformation suppression method for laser-assisted in-situ formed thermoplastic composite structural parts

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Embodiment Construction

[0026] The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.

[0027] Step 1: Set the laser power density to 15W / cm by adjusting beam adjuster 2 2 , the spot type is a circular spot laser heat source 1 with a diameter of 15mm, the forming speed is 1000mm / min, the forming temperature is 450°C, and the pressure of the pressing roller 3 is 30N; And heat and pressurize it, so that the prepreg is formed on the surface of the mold 5;

[0028] Step 2: Instead of laying new prepregs, laser and pressure rollers are used to heat and press the prepregs laid in step 1 twice;

[0029] Step 3: Repeat steps 1 and 2 until the sample preparation is completed.

[0030] The prepreg used in step 1 is a carbon fiber reinforced PEEK composite material with a thickness of 0.14mm and a width of 10mm, and a total of 5 layers are laid.

[0031] The second heating and pressing process conditions in step 2 are: the laser power de...

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Abstract

A method for suppressing springback deformation of laser-assisted in-situ formed thermoplastic composite structural parts. 1) Use laser and pressure roller to heat and press the laid prepreg for the first time; 2) Do not lay new prepreg, but heat and press the laid part in step 1) multiple times; 3 ) Repeat steps 1) and 2) until the sample preparation is complete. The first time of heating and pressing is to make the high-temperature molten resin in the adjacent layer of prepreg flow under the pressure of the pressure roller to form a good interlayer bond. Repeated heating and pressurization is to make the sample undergo multiple high temperature effects, release the internal stress caused by the viscoelasticity of the material and rapid cooling, and reduce the springback angle. The invention can realize online adjustment of springback deformation, which is helpful to realize automatic integrated forming; it can be used for laying and forming of thermoplastic composite structural parts with various shapes, and the operation is simple, which can significantly improve the geometric accuracy of structural parts; the laser heat source is accurate and can control, which can realize the localized adjustment of springback deformation.

Description

technical field [0001] The invention relates to a method for suppressing springback deformation of a laser-assisted in-situ forming thermoplastic composite material structural part, and belongs to the technical field of composite materials. Background technique [0002] Thermoplastic composite materials have the characteristics of high specific strength and good impact resistance, and have great application prospects in aerospace, transportation and other fields. The melting and solidification of thermoplastic composite materials is a physical change process, and the solidification process is the forming process, which can greatly improve the forming efficiency. Thermoplastic composite structural parts are the basis of lightweight and complex structures, and their high-quality manufacturing is the basic manufacturing technology to further improve the performance of aerospace vehicles. The angle springback of the formed sample is a major problem in the forming of thermoplast...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B29C70/34B29C70/54B29C35/08B29K105/08
CPCB29C35/0805B29C70/34B29C70/54B29C2035/0838B29K2105/0872
Inventor 吴东江苗秋玉戴智弘马广义牛方勇
Owner DALIAN UNIV OF TECH
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