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Carbon fiber composite material fatigue damage probability imaging method based on ToF damage factor

A damage factor and composite material technology, which is applied in the analysis of materials, the use of sonic/ultrasonic/infrasonic waves for material analysis, and the processing of response signals from detection. problems such as poor performance, to achieve the effect of improving clarity, improving visualization, and reducing the amount of data

Inactive Publication Date: 2021-01-05
KUNMING UNIV OF SCI & TECH
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  • Abstract
  • Description
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  • Application Information

AI Technical Summary

Problems solved by technology

Although the existing damage probability imaging method can effectively identify damage, its visualization effect and damage location accuracy are poor, the imaging resolution is not high, and there is a common situation that the damage probability is high for the position without damage.

Method used

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  • Carbon fiber composite material fatigue damage probability imaging method based on ToF damage factor
  • Carbon fiber composite material fatigue damage probability imaging method based on ToF damage factor
  • Carbon fiber composite material fatigue damage probability imaging method based on ToF damage factor

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Embodiment Construction

[0051] The present invention will be further described below in combination with the accompanying drawings and specific embodiments.

[0052] Such as image 3 As shown, the specific embodiment of the present invention takes the damage detection and positioning of the fatigue damage of the carbon fiber composite material plate as an example. The small gap of 5.08mm*19.3mm is designed for concentrated load.

[0053] Such as figure 1 As shown, a carbon fiber composite material fatigue damage probability imaging method based on ToF damage factor, the steps of damage probability imaging based on ToF damage factor in the area to be detected include:

[0054] Step1: Evenly divide the monitored area in the piezoelectric sensor network into 600*360 small grids, and regard each small grid as a pixel;

[0055] Step1.1: Arrange a set of one-dimensional linear piezoelectric sensor arrays composed of six piezoelectric sensors on the upper and lower edges of the carbon fiber composite mat...

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Abstract

The invention relates to a carbon fiber composite material fatigue damage probability imaging method based on a ToF damage factor, and belongs to the technical field of engineering structure health monitoring. The method comprises the steps of firstly, uniformly dividing a monitored area in a piezoelectric sensor network into N small grids, and taking each small grid as a pixel point; then calculating a ToF damage factor of each excitation-sensing channel; secondly, calculating the damage existence probability of each pixel point in each excitation-sensing channel according to the ToF damage factor; and finally, superposing the damage probability of each pixel point in each excitation-sensing channel, mapping the damage existence probability of each pixel point into a pixel value and imaging, and taking the position with high damage probability in an imaging image as the possible damage existence position. Compared with a traditional damage probability imaging method, damage can be accurately recognized and positioned, the visualization effect of damage imaging can be effectively improved, and the approximate shape and size of the damage can be obtained.

Description

technical field [0001] The invention relates to a fatigue damage probability imaging method of a carbon fiber composite material based on a ToF damage factor, and belongs to the technical field of engineering structure health monitoring. Background technique [0002] Compared with metal materials, carbon fiber composite materials are widely used in the aerospace field because of their advantages such as high specific stiffness, high specific strength, high temperature resistance, corrosion resistance, fatigue resistance, and light weight. However, composite materials will continue to produce various defects and damages during material processing, component manufacturing and service, among which fatigue damage is a common and typical type of damage. Fatigue damage is caused by continuous load cycles that cause tiny damage inside the material at the initial stage. With repeated loads, the internal damage gradually expands until it breaks. However, the formation process of inte...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N29/06G01N29/44
CPCG01N29/069G01N29/44
Inventor 叶波孔琼英邓为权王丹宏陈宸
Owner KUNMING UNIV OF SCI & TECH
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