Damage localization in geometrically complex aeronautic structures using canonical polyadic decomposition of Lamb wave difference signal tensors

被引:20
|
作者
Rebillat, Marc [1 ]
Mechbal, Nazih [1 ]
机构
[1] HESAM Univ, CNRS, CNAM, PIMM Lab,ENSAM, Paris, France
关键词
Structural health monitoring; damage localization; tensors; canonical polyadic decomposition; Lamb waves; piezoelectric elements;
D O I
10.1177/1475921719843453
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Monitoring in real time and autonomously the health state of aeronautic structures is referred to as structural health monitoring and is a process decomposed in four steps: damage detection, localization, classification, and quantification. In this work, the structures under study are aeronautic geometrically complex structures equipped with a bonded piezoelectric network. When interrogating such a structure, the resulting data lie along three dimensions (namely, the "actuator,""sensor," and "time" dimensions) and can thus be interpreted as three-way tensors. The fact that Lamb wave structural health monitoring-based data are naturally three-way tensors is here investigated for damage localization purpose. In this article, it is demonstrated that under classical assumptions regarding wave propagation, the canonical polyadic decomposition of rank 2 of the tensors build from the phase and amplitude of the difference signals between a healthy and damaged states provides direct access to the distances between the piezoelectric elements and damage. This property is used here to propose an original tensor-based damage localization algorithm. This algorithm is successfully validated on experimental data coming from a scale one part of an airplane nacelle (1.5 m in height for a semi circumference of 4 m) equipped with 30 piezoelectric elements and many stiffeners. Obtained results demonstrate that the tensor-based localization algorithm can locate a damage within this structure with an average precision of 10 cm and with a precision lower than 1 cm at best. In comparison with standard damage localization algorithms (delay-and-sum, reconstruction algorithm for probabilistic inspection of defects, and ellipse- or hyperbola-based algorithms), the proposed algorithm appears as more precise and robust on the investigated cases. Furthermore, it is important to notice that this algorithm only takes the raw signals as inputs and that no specific pre-processing steps or finely tuned external parameters are needed. This algorithm is thus very appealing as reliable and easy to settle damage localization timeliness with low false alarm rates are one of the key successes to shorten the gap between research and industrial deployment of structural health monitoring processes.
引用
收藏
页码:305 / 321
页数:17
相关论文
共 3 条
  • [1] Damage localization in composite plates using canonical polyadic decomposition of Lamb wave difference signals tensor
    Rebillat, Marc
    Mechbal, Nazih
    IFAC PAPERSONLINE, 2018, 51 (24): : 668 - 673
  • [2] Damage Localization of Composites Based on Difference Signal and Lamb Wave Tomography
    Su, Chenhui
    Jiang, Mingshun
    Liang, Jianying
    Tian, Aiqin
    Sun, Lin
    Zhang, Lei
    Zhang, Faye
    Sui, Qingmei
    MATERIALS, 2020, 13 (01)
  • [3] Lamb wave-based damage assessment for CFRP composite structures using a CHMM-based damage localization algorithm and a damage quantitative expression
    Zeng, Xianping
    Zhao, Bowen
    Liu, Xiao
    Yu, Yinghong
    Guo, Jiahui
    Qing, Xinlin
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2023, 184