人工智能驱动的复合材料结构超声导波损伤监测技术
ULTRASONIC GUIDED WAVE DAMAGE MONITORING TECHNOLOGY FOR COMPOSITE STRUCTURES DRIVEN BY ARTIFICIAL INTELLIGENCE
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摘要: 复合材料结构在已广泛应用于航空航天等领域的重大装备, 及时发现复合材料结构中的损伤与破坏, 对避免造成突发性破坏与结构失效具有非常重要的意义, 探索具有高鲁棒性的复合材料结构损伤定量化监测理论与方法是结构健康监测领域的当务之急. 针对现有结构健康监测技术损伤识别精度低、跨场景泛化能力弱及小样本适应能力差等局限性, 本文凝练作者团队在人工智能驱动的复合材料结构超声导波损伤监测领域提供的解决方案. 首先, 针对复杂复合材料结构中超声导波信号特征提取难的问题, 构建基于深度学习的多源信息特征提取与融合方法, 实现复合材料结构损伤位置与尺寸的高精度辨识. 其次, 针对不同监测区域、不同传感器布局及不同结构下模型泛化性能差的挑战, 提出基于迁移学习与域自适应的跨域损伤识别方法, 通过参数迁移与特征分布对齐相结合, 实现损伤特征的有效迁移与鲁棒表征. 然后, 针对样本稀缺问题, 引入生成模型驱动的数据扩展策略, 并结合数字孪生开展小样本损伤监测研究, 提升有限样本条件下的识别性能. 作者团队相关研究结果表明, 所提方法在复合材料结构损伤定位与量化评估中具有较高的精度与鲁棒性, 为复杂服役环境下复合材料结构健康监测提供了理论依据与技术途径. 最后分析了飞行器复合材料结构健康监测在实际服役环境中应用仍面临的主要挑战, 并展望了飞行器复合材料结构健康监测技术未来的发展趋势.Abstract: Composite structures have been extensively applied in critical equipment within aerospace and other engineering industries. The timely detection of damage and failure is essential for preventing sudden damage and structural failure. It is urgent to explore the theory and method for quantitative monitoring of damage in composite structures in complex service environment. Aiming at the limitations of the existing structural health monitoring technology, such as low damage identification accuracy, weak cross-domain generalization, and poor performance under small-sample conditions, this paper summarizes the solutions provided by the author's team in the field of ultrasonic guided wave damage monitoring of composite structures driven by artificial intelligence. Firstly, aiming at the challenge of feature extraction from ultrasonic guided wave signals in complex composite structures, a deep learning-based multi-source information feature extraction and fusion method is constructed to achieve high-precision identification of damage location and size in composite structures. Secondly, to address the challenge of poor model generalization performance in different monitoring areas, different sensor layouts and different structures, a cross-domain damage identification method based on transfer learning and domain adaptation is proposed, and the effective transfer and robust characterization of damage features are realized by combining parameter transfer with feature distribution alignment. Then, in view of the scarcity of samples, a data expansion strategy driven by generation model is introduced, and damage monitoring research for limited samples is developed by integrating the digital twin method to improve the prediction performance. The research results of the author's team demonstrate that the proposed method has high accuracy and robustness in damage localization and quantification assessment of composite structures, which provides theoretical basis and technical approach for structural health monitoring of composite structures in complex service environment. Finally, the main challenges of aircraft composite structural health monitoring in actual service environment are analyzed, and the future development trend of aircraft composite structural health monitoring technology is prospected.
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