一种基于机器视觉的MIM涡轮叶片表面微裂纹识别方法

By employing machine vision-based methods, utilizing photometric stereo vision and topological singularity index analysis, microcracks in MIM turbine blades are accurately identified, solving the detection challenges under complex curvature and porosity interference, and achieving efficient and accurate microcrack identification and quality assessment.

CN121937455BActive Publication Date: 2026-07-17LIANYUNGANG FUTURE HIGH TECH CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
LIANYUNGANG FUTURE HIGH TECH CO LTD
Filing Date
2026-03-31
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies struggle to accurately identify microcracks in MIM turbine blades under complex curvature and porosity interference, leading to false positives and false negatives, which impacts aero-engine safety.

Method used

A machine vision-based approach is adopted to acquire the original image sequence through multi-angle light source illumination. By combining photometric stereo vision solution and model projection alignment, a normal residual map is obtained. Global statistical analysis and differential operator operations are performed to calculate the topological singularity index and crack significance index. The maximum entropy threshold method is used for segmentation and skeletonization extraction to generate a defect heat map and perform quality rating and data binding.

Benefits of technology

It enables accurate identification of microcracks under complex curvature and porosity interference, reduces the false judgment rate, improves detection accuracy and stability, supports automated sorting and full life cycle data management, and meets production needs.

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Abstract

本发明属于图像处理技术领域,具体涉及一种基于机器视觉的MIM涡轮叶片表面微裂纹识别方法,其方法包括:获得表征涡轮叶片微观形貌特征的法向残差图;获得二阶边缘强度;计算拓扑奇异指数;计算用于表征缺陷综合显著程度的裂纹显著性指数;获得裂纹长度、裂纹平均宽度及裂纹区域投影面积;计算断裂风险指数;获得质量评级及缺陷热力图;生成质量追溯报表;基于断裂风险指数、法向残差图、质量评级结果,执行全生命周期数据绑定。本发明一定程度上解决了现有技术在复杂曲率及孔隙干扰下难以精准识别MIM涡轮叶片微裂纹的技术问题。
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