针对微小孔周裂纹高精度检测的柔性旋转涡流检测探头及方法

By using a flexible array rotating eddy current detection probe and differential detection method, the problem of high-precision detection of micro-cracks around the cooling film holes of turbine blades was solved, and high-precision identification and location of micro-cracks were achieved.

CN116337994BActive Publication Date: 2026-07-17XI AN JIAOTONG UNIV
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
XI AN JIAOTONG UNIV
Filing Date
2023-04-06
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing technologies are insufficient for high-precision detection of minute cracks around the cooling film holes of turbine blades, and traditional rigid rotating eddy current probes have limited detection performance on complex curvature structures, resulting in easily obscured detection signals and a high rate of missed detections.

Method used

A flexible array rotating eddy current detection probe is designed, which uses a flexible silicone pad and an FPC flexible excitation coil, combined with differential phase and differential amplitude detection methods, to achieve high-precision detection of peripore cracks in the cooling film of turbine blades.

Benefits of technology

It achieves high-precision detection of cooling film hole peripore cracks in turbine blades within the range of 0.5×0.2mm2 to 1×0.2mm2, reduces detection noise, and improves detection accuracy and reliability.

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Abstract

一种针微小孔周裂纹高精度检测的柔性旋转涡流检测探头及方法,该检测探头由硅胶柔性垫板、FPC柔性激励线圈和饼式检出线圈组成;在探头工作时分别通入相位差为90°的正弦调制激励电流,产生周期性旋转的涡流场增加检测灵敏度;使用差分相位法对气膜孔周裂纹的存在性进行检测,极大提高了涡轮叶片冷却气膜孔周裂纹识别的精度;使用差分幅值法对气膜孔周裂纹的位置方向进行确认,实现对涡轮叶片冷却气膜孔周任意方向裂纹的检测;本发明可以实现对任意方向0.5×0.2mm2~1×0.2mm2大小范围内的涡轮叶片冷却气膜孔周裂纹的高精度检测,相比于传统探头和识别方法具有高灵敏度、高精度、高信噪比的技术优势。
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