A Modified Time Reversal Based Probabilistic Imaging Method for Composite Plate Delamination Detection

Yang Nan, Maoling Yue, Haodong Fan, Fei Du, L. Wen, Chao Xu
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Abstract

Composite materials have been widely used in aerospace manufacturing because of their low mass, high specific strength, high specific stiffness and good fatigue resistance. However, composite structures are susceptible to damage such as debonding and delamination due to various impacts, vibrations and other external loads. Therefore, it is crucial to regularly monitor composite structures in real-time during spacecraft service to ensure the safety and reliability of the structures. Ultrasonic guided wave is an effective means of monitoring the health of composite plate structures. Delamination, debonding and other damages of composite materials can be imaged and localized using ultrasonic guided wave signals and probabilistic imaging methods. However, due to the large damping of composite materials, the traditional probabilistic imaging method has the problem of low accuracy in damage localization. Therefore, in this paper, we propose a probabilistic imaging method based on a modified time reversal for damage localization and imaging of delamination damage. The proposed method was experimentally validated using a composite plate as a test piece and compared with the conventional method. A fully automated falling hammer impact tester was used to create low-velocity impact damage on specimens to compare the localization accuracy of the time-free reverse method and the modified time reversal method for delamination damage. The results show that the modified time reversal method can better localize and image the delamination damage of composite structures with higher localization accuracy and more sensitive to damage, which verifies the feasibility and accuracy of the method in the localization of debonding damage of composite structures.
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一种改进的基于时间反转的概率成像方法用于复合材料板分层检测
复合材料以其低质量、高比强度、高比刚度和良好的抗疲劳性能在航空航天制造中得到了广泛的应用。然而,由于各种冲击、振动和其他外部载荷,复合材料结构容易受到诸如脱粘和分层等损伤。因此,在航天器服役期间,对复合结构进行定期实时监测,以保证结构的安全可靠是至关重要的。超声导波是监测复合板结构健康状况的有效手段。利用超声导波信号和概率成像方法可以对复合材料的分层、脱粘等损伤进行成像和定位。然而,由于复合材料阻尼大,传统的概率成像方法存在损伤定位精度低的问题。因此,本文提出了一种基于改进时间反演的损伤定位与分层损伤成像概率成像方法。以复合材料板为试件进行了实验验证,并与传统方法进行了比较。采用全自动落锤冲击试验机对试件进行低速冲击损伤模拟,比较无时间反演法和改进时间反演法对分层损伤的定位精度。结果表明,改进的时间反演方法能较好地对复合材料结构脱层损伤进行定位和成像,具有较高的定位精度和对损伤的敏感性,验证了该方法在复合材料结构脱层损伤定位中的可行性和准确性。
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