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Nonlinear air-coupled thermosonics for fatigue micro-damage detection and localisation

机译:非线性空气耦合热超声用于疲劳微损伤的检测和定位

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Over the years, traditional active infrared thermography has played a pivotal role in ensuring that a component is free of any damage. However, whilst optical thermography is still not sufficiently sensitive to the presence of material micro-flaws, current vibro-thermography requires inspection solutions that are not always feasible, such as the use of coupling materials between the sensing probe and the monitored structure. This paper presents a valid alternative to current thermographic systems by developing and experimentally validating nonlinear air-coupled thermosonics for a contactless, rapid and accurate detection of fatigue micro-cracks in an aero-engine turbine blade. The proposed thermographic method combines the high sensitivity to micro-damage of nonlinear ultrasonic techniques with non-contact air-coupled ultrasonic transducers and thermographic equipment. Narrowband frequency sweeps were performed to identify local damage resonance frequencies in order to generate large vibrational amplitudes at the damage location and compensate for signal losses caused by the high acoustic impedance mismatch between the air and the sample. An infrared camera was then used to acquire the thermal response generated by frictional heat at the crack interfaces. Moreover, an image processing method based on a combination of morphological opening and a Savitzky-Golay smoothing filter was employed to enhance the quality of thermal images affected by anisotropic heating and thermal noise effects. Nonlinear air-coupled thermosonics experiments were validated with laser Doppler vibrometry scan measurements and compared with both flash and pulsed phase thermography. Thermal imaging results showed that the proposed nonlinear air-coupled thermosonics was the only thermographic technique able to detect fatigue micro-cracks, thus demonstrating its potential as an efficient and sensitive inspection tool for micro-damage detection in geometrically complex components.
机译:多年来,传统的主动红外热成像技术在确保组件不受任何损坏方面发挥了关键作用。但是,尽管光学热成像技术对材料微瑕疵的存在仍然不够敏感,但是当前的振动热成像技术要求的检查解决方案并不总是可行的,例如在传感探头和被监测结构之间使用耦合材料。本文通过开发和实验验证非线性空气耦合热超声技术,以非接触式,快速而准确地检测航空发动机涡轮叶片中的疲劳微裂纹,提出了一种有效的替代当前热成像系统的方法。所提出的热成像方法将非线性超声技术对微损伤的高灵敏度与非接触式空气耦合超声换能器和热成像设备相结合。进行窄带扫频以识别局部损伤共振频率,以便在损伤位置产生较大的振动幅度,并补偿由空气与样品之间的高声阻抗失配引起的信号损失。然后,使用红外热像仪获取裂纹界面处的摩擦热产生的热响应。此外,采用基于形态学开口和Savitzky-Golay平滑滤波器的组合的图像处理方法来提高受各向异性加热和热噪声影响的热图像的质量。非线性空气耦合热超声实验已通过激光多普勒振动法扫描测量进行了验证,并与闪光相和脉冲相热成像法进行了比较。热成像结果表明,所提出的非线性空气耦合热超声技术是唯一能够检测疲劳微裂纹的热成像技术,从而证明了其作为有效且灵敏的检测工具的潜力,可用于检测几何复杂部件中的微损伤。

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