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Preparation method of intelligent composite material containing delamination damage

A composite material and intelligent technology, applied in the field of materials, can solve the problems of indistinguishable damage signal and noise signal, X-ray damage to human body, complicated experimental procedures, etc. Effect

Inactive Publication Date: 2019-11-08
XIDIAN UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The X-ray detection method has high sensitivity and intuitive detection results, but the rays are attenuated due to absorption and scattering during the process of penetrating the material, so there is a certain limit to the thickness of the detection workpiece, and X-rays are harmful to the human body, and the detection personnel need to do special work. protection, the cost of experiment is high; the ultrasonic testing method uses the characteristics of strong penetrating power and good directivity of ultrasonic waves to various materials to detect surface and internal defects of components. It is simple to operate, high in detection sensitivity, and can accurately determine the position and distribution, but using this method usually requires couplant, and different probes are used for different types of defects, and the experimental procedures are complicated; Detection methods are difficult or inaccessible, such as detection in high and low temperature, nuclear radiation, flammable and explosive environments. The acoustic emission detection method is sensitive to dynamic defects and only needs to receive sensors, but this method is not sensitive to static defects and damages the signal. Indistinguishable from noise signal

Method used

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  • Preparation method of intelligent composite material containing delamination damage
  • Preparation method of intelligent composite material containing delamination damage
  • Preparation method of intelligent composite material containing delamination damage

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0030] Example 1, prepare a prefabricated 22-layer carbon fiber epoxy resin-based composite laminate test piece with a damage area of ​​10mm×10mm and a surface size of 200mm×25mm.

[0031] Step 1: Prepare before making

[0032] 1.1) Prepare the basic materials used:

[0033] Basic materials include: disinfectant, fiber cloth, PTFE film, fully transparent epoxy resin glue, fiber grating sensor, high temperature silicone, high temperature tape, flat mold, isolation film, air felt, vacuum bag and high temperature sealant;

[0034] 1.2) Prepare the equipment used:

[0035] Equipment includes: fiber cloth cutting machine, autoclave

[0036] 1.3) Scrub the work surface with a disinfectant to ensure the surface of the material is clean.

[0037] Step 2: Cut the fiber cloth.

[0038] The main technical material of the present invention is carbon fiber epoxy resin-based composite material fiber cloth. First, a whole piece of carbon fiber epoxy resin-based composite material fiber c...

Embodiment 2

[0062] Embodiment 2, the preparation of a prefabricated damage area is 15mm * 15mm, and the surface size of the test piece is a 22-layer carbon fiber epoxy resin-based composite laminate test piece of 200mm * 25mm;

[0063] Step 1: Preparation before making.

[0064] The specific implementation of this step is the same as Step 1 of Example 1.

[0065] Step 2: Cut the fiber cloth.

[0066] The specific implementation of this step is the same as step 2 of embodiment 1.

[0067] Step 3: Lay the optical fiber layer.

[0068] The specific implementation of this step is the same as step 3 of embodiment 1.

[0069] Step 4: Make a prefabricated damage layer.

[0070] In this embodiment, a polytetrafluoroethylene film with an area of ​​15 mm×15 mm is used as the prefabricated damaged layer of the test piece, and the remaining implementation methods are the same as Step 4 of Embodiment 1.

[0071] Step 5: Overall compounding.

[0072] The specific implementation of this step is th...

Embodiment 3

[0073] Embodiment 3, the preparation of a prefabricated damage area is 10mm * 10mm, and the surface size of the test piece is a 44-layer carbon fiber epoxy resin-based composite laminate test piece of 200mm * 25mm;

[0074] Step A: Preparation before making.

[0075] The specific implementation of this step is the same as Step 1 of Example 1.

[0076] Step B: cutting the fiber cloth.

[0077] In this example, 16 pieces of fiber cloth strips with a ply angle of 0°, 12 pieces of fiber cloth strips with a ply angle of 45°, 8 pieces of fiber cloth strips with a ply angle of -45°, and 8 pieces of fiber strips with a ply angle of 90° Cloth strips, all the other implementations are the same as step 2 of embodiment 1.

[0078] Step C: laying the optical fiber layer.

[0079] The specific implementation of this step is the same as step 3 of embodiment 1.

[0080] Step D: making a prefabricated damage layer.

[0081] The specific implementation of this step is the same as step 4 of...

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Abstract

The invention discloses a preparation method of an intelligent composite material structure containing delamination damage and mainly solves the problems that influence on the material self is great when the intelligent composite material is prepared in the prior art and preparation cost is high. According to the scheme, the preparation method comprises the following steps: cutting fiber cloth byadopting a cutting machine, thus obtaining fiber cloth strips with different fiber ply angles; paving a fiber Bragg grating sensor on every two fiber cloth strips by adopting a trapezoid slide routingstructure, thus forming an optical fiber layer, placing two optical fiber layers back to back, and placing a polytetrafluoroethylene film in the middle as a prefabricated damaged layer; then taking the damaged layer as a starting point, respectively paving the same number of layers of the fiber cloth strips above and below the two optical fiber layers, thus forming a well-overlaid fiber cloth strip whole, then sequentially covering with an isolating membrane, a ventilated felt and a vacuum bag, and sealing with high temperature sealant; and finally transferring the well-sealed whole into a hot pressing tank, and curing at set technological conditions, thus obtaining the intelligent composite material containing the prefabricated damaged layer. The preparation method disclosed by the invention has small influence on the material self, is low in preparation cost and can be used for health detection on the composite material.

Description

technical field [0001] The invention belongs to the technical field of materials, and in particular relates to a preparation method of an intelligent composite material, which can be used to analyze the damage evolution process of a certain composite material in experiments. Background technique [0002] The delamination damage of composite laminates is the main damage mode that affects the structural bearing capacity. Composite laminate structures are easily subjected to low-energy impacts during processing, assembly and service, and delamination damage occurs between layers. Since delamination damage often occurs inside the laminate, it is difficult to observe visually on its surface, so delamination damage is a hidden safety hazard that cannot be ignored for composite laminate structures. To sum up, systematic research on the delamination damage of composite structures is of great significance to the actual engineering structure design, manufacture and maintenance of comp...

Claims

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Application Information

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IPC IPC(8): G01B11/16G01N3/06
CPCG01B11/165G01N3/068G01N2203/0075G01N2203/0282G01N2203/0641
Inventor 叶俊杰席佳乐蔡恒贾斐储辰辰张解语史宝全
Owner XIDIAN UNIV
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