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Fully Non-Contact Laser Excitation and Reception Ultrasonic Propagation Imaging System with Repeat Scanning Technique

机译:具有重复扫描技术的完全非接触激光激发和接收超声波传播成像系统

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A reliable nondestructive evaluation technique is essential to detect any possible damage at the initiation phase to allow preventive measures to be taken for failure prevention. Composites are used in aerospace structures e.g., aircraft wing-box, which are highly susceptible to impact damages. Ultrasound has been widely used, but conventional contact ultrasonic inspection techniques are often difficult or not accessible in hard to reach locations and generally require disassembly of the structure for inspection, which limits in-field applicability. A novel fully non-contact hybrid ultrasonic propagation imaging (UPI) system that uses Q-switched laser (QL) ultrasonic scanning excitation and laser Doppler vibrometer (LDV) sensing has been devised and implemented. The problem of the lower sensitivity of LDV than those of contact sensors was solved by time domain averaging through repetitive scanning technique. Since not LDV but QL is used for scanning, LDV can be fixed into its own maximum sensitive status. Multiple 3D imaging processing such as ultrasonic wave propagation imaging (UWPI) and wavelet-transformed ultrasonic propagation imaging (WUPI) algorithms were used to extract reliable damage features without overlook. The pure laser hybrid system enables remote and fully non-contact automatic one-sided inspection for temporal reference-free damage evaluation, and is also applicable to in-field structures. Experimental analyses were conducted for impact damage on carbon fiber reinforced polymer composite wing-box specimen. The proposed laser excitation and sensing UPI system provided enhanced results for damage visibility, and accuracy in determining damage location and size. The results demonstrated the possibility of quantitative, fast and automatic damage evaluation for in-field application as well.
机译:可靠的非破坏性评估技术对于检测起始阶段的任何可能损坏至关重要,以允许预防性措施进行预防。复合材料用于航空航天结构,例如,飞机翼盒,这极易受影响损害的影响。超声波已被广泛使用,但常规的接触超声检查技术通常难以达到或不可达到位置,并且通常需要拆卸结构进行检查,这限制了现场适用性。采用Q开关激光(QL)超声波扫描激励和激光多普勒振动计(LDV)感测的新型完全非接触式混合超声波传播成像(UPI)系统已经设计并实施。通过重复扫描技术的时域平均解决了LDV比接触传感器较低的较低灵敏度的问题。由于不是LDV但QL用于扫描,因此LDV可以固定为其自己的最大敏感状态。诸如超声波传播成像(UWPI)和小波变换的超声波传播成像(WUPI)算法的多个3D成像处理用于提取可靠的损坏功能而不会俯视。纯激光混合系统使远程和完全非接触的自动单面检测能够进行时间参考损伤评估,也适用于现场结构。对碳纤维增强聚合物复合翼箱样品进行冲击损伤进行了实验分析。所提出的激光激发和感测UPI系统提供了增强的损坏可视性结果,以及确定损坏位置和尺寸的准确性。结果表明,对现场应用的定量,快速和自动损伤评估的可能性。

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