Segmentation strengthening method for damage detection image of aerospace composite material

A composite material, damage detection technology, applied in image analysis, image enhancement, image data processing, etc., can solve the problems of large background noise, small damage defect size, and unfavorable image segmentation in infrared reconstructed images.

Active Publication Date: 2021-05-18
中国空气动力研究与发展中心超高速空气动力研究所
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AI Technical Summary

Problems solved by technology

On the one hand, if the defect detection rate is improved to a certain extent under the premise of fully satisfying the preservation of details, the noise is also retained, which is easy to cause misjudgment of defect recognition, resulting in an increase in the false detection rate
On the other hand, if only the overall denoising of the image is satisfied, the size of the damage defects caused by the impact of tiny debris is small and the number is large, and these tiny defects similar to the noise will be removed together with the denoising process, reducing the damage of defects. Detection rate and detection accuracy
Therefore, the above-mentioned conventional segmentation method is applied to the object of the present invention, that is, the in

Method used

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  • Segmentation strengthening method for damage detection image of aerospace composite material
  • Segmentation strengthening method for damage detection image of aerospace composite material
  • Segmentation strengthening method for damage detection image of aerospace composite material

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Embodiment

[0224] In this embodiment, the infrared thermal imaging camera collected 502 frames of images with a pixel size of 512×640. That is, there are 327,680 temperature points on each map, and the temperature value of each temperature point is recorded 502 times. This time-varying temperature condition constitutes the transient thermal response TTR of the temperature point. Step 1: After extracting the effective transient thermal response from the infrared thermal sequence, divide the area according to the defect type, and extract the typical transient thermal response from each type of divided area. When extracting the effective transient thermal response, set the parameter Re CL =0.92, 441 valid transient thermal responses containing complete defect information were extracted from 327,680 temperature points. According to the pixel points, the membership degree of each cluster center is softened, and 103, 196 and 142 thermal response curves are divided into corresponding categor...

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Abstract

The invention discloses a segmentation strengthening method for a damage detection image of an aerospace composite material. The segmentation strengthening method comprises the following steps: extracting typical transient thermal response of a defect; obtaining an infrared reconstruction image; utilizing multi-target to measure segmentation performance of three aspects ofnoise removal, detail reservation and edge maintenance, and solving the weight coefficient of each segmentation performance; constructing infrared image segmentation function data under the guidance of three purposes of noise removal, detail reservation and edge maintenance; obtaining a weight coefficient of the target function; carrying out image segmentation on the full-pixel infrared image obtained through reconstruction; and achieving infrared full-pixel image segmentation on the image segmentation layer to obtain a segmented image of the defect. According to the method, the multi-objective optimization theory is utilized to segment the damage defect area in the infrared reconstructed image, objective functions are respectively constructed for the noise problem and the edge blur problem, the area segmentation precision is improved, the false detection rate is reduced, the readability of the damage defect area is effectively enhanced, and quantitative research of complex defects is facilitated.

Description

technical field [0001] The invention belongs to the technical field of damage detection and maintenance support of aerospace vehicles, and more specifically, the invention relates to a method for segmenting and enhancing damage detection images of aerospace composite materials. Background technique [0002] With the urgent need for weight reduction of aerospace vehicles, lightweight structural materials with excellent mechanical properties, especially lightweight composite materials represented by high-strength / high-modulus carbon fiber composite materials and honeycomb structure materials, have increasingly become the focus of aerospace research. hotspot. At the same time, composite materials with special functional uses, such as stealth coating materials, carbon-based heat-resistant materials and other functional composite materials, are also more widely used in the aerospace field. However, in the process of manufacturing, assembly processing or real-time use of composit...

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Application Information

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IPC IPC(8): G06T7/00G06T7/11G06T7/194G06T7/62G06T7/90G06K9/62G06N3/12
CPCG06T7/0004G06T7/11G06T7/194G06T7/62G06T7/90G06N3/126G06T2207/10048G06T2207/20192G06T2207/30164G06F18/23G06F18/24
Inventor 黄雪刚石安华罗庆雷光钰谭旭彤赵君尧董文朴
Owner 中国空气动力研究与发展中心超高速空气动力研究所
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