Analysis of barely visible impact damage severity with ultrasonic guided Lamb waves

被引:43
作者
Dafydd, Ifan [1 ]
Sharif Khodaei, Zahra [1 ]
机构
[1] Imperial Coll London, Dept Aeronaut, South Kensington Campus, London SW7 2AZ, England
来源
STRUCTURAL HEALTH MONITORING-AN INTERNATIONAL JOURNAL | 2020年 / 19卷 / 04期
基金
英国工程与自然科学研究理事会;
关键词
Lamb waves; structural health monitoring; laser Doppler vibrometer; barely visible impact damage; ultrasonics; non-destructive inspection; damage severity; PIEZOELECTRIC SENSOR/ACTUATOR NETWORK; SCANNING LASER VIBROMETRY; LOCALIZATION; PLATES; MODE; IDENTIFICATION; PROPAGATION; SCATTERING;
D O I
10.1177/1475921719878850
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Barely visible impact damage is one of the most common types of damage in carbon-fibre-reinforced polymer composite structures. This article investigates the potential of using ultrasonic guided Lamb waves to characterise the through thickness severity of barely visible impact damage in thin carbon-fibre-reinforced polymer structures. In the first step, a laser Doppler vibrometer was used to capture the full damage interaction of the wavefield excited by a piezoelectric actuator. Damage-scattered wavefield for four different severities were studied to find the best parameters for characterising the severity of damage. To reduce the overall acquisition time and size of data collected using the laser Doppler vibrometer, the measured signals were reconstructed from a singular broadband chirp response using a post-processing algorithm. From the full wavefield analysis obtained at a wide range of toneburst frequencies, the results showed that barely visible impact damage severity could be characterised using ultrasonic guided Lamb waves and that theA0mode, dominant at lower frequencies, gave better results than theS0mode. In the second step, the parameters for characterising the damage severity were applied to a sparse network of transducers as an in-service structural health monitoring methodology. The damage was successfully detected and located. In addition, the transducer path close to the predicted damage location was utilised to successfully quantify the damage severity based on the proposed damage index.
引用
收藏
页码:1104 / 1122
页数:19
相关论文
共 53 条
[31]   Computational aspects of guided wave based damage localization algorithms in flat anisotropic structures [J].
Moll, Jochen ;
Torres-Arredondo, Miguel Angel ;
Fritzen, Claus-Peter .
SMART STRUCTURES AND SYSTEMS, 2012, 10 (03) :229-251
[32]   Analytical prediction of large mass impact damage in composite laminates [J].
Olsson, R .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2001, 32 (09) :1207-1215
[33]   Visualization of hidden delamination and debonding in composites through noncontact laser ultrasonic scanning [J].
Park, Byeongjin ;
An, Yun-Kyu ;
Sohn, Hoon .
COMPOSITES SCIENCE AND TECHNOLOGY, 2014, 100 :10-18
[34]   Damage detection in composite panels based on mode-converted Lamb waves sensed using 3D laser scanning vibrometer [J].
Pieczonka, Lukasz ;
Ambrozinski, Lukasz ;
Staszewski, Wieslaw J. ;
Barnoncel, David ;
Peres, Patrick .
OPTICS AND LASERS IN ENGINEERING, 2017, 99 :80-87
[35]   On quantifying damage severity in composite materials by an ultrasonic method [J].
Pillarisetti, Lalith Sai Srinivas ;
Talreja, Ramesh .
COMPOSITE STRUCTURES, 2019, 216 :213-221
[36]   Characterization of impact damage in composite laminates using guided wavefield imaging and local wavenumber domain analysis [J].
Rogge, Matthew D. ;
Leckey, Cara A. C. .
ULTRASONICS, 2013, 53 (07) :1217-1226
[37]   Frequency-wavenumber domain filtering for improved damage visualization [J].
Ruzzene, M. .
SMART MATERIALS & STRUCTURES, 2007, 16 (06) :2116-2129
[38]  
Ruzzene M, 2005, AIP CONF PROC, V760, P172, DOI 10.1063/1.1916675
[39]  
Rytter A, 1993, VIBRATIONAL BASED IN
[40]   Guided wave temperature correction methods in structural health monitoring [J].
Salmanpour, M. S. ;
Khodaei, Z. Sharif ;
Aliabadi, M. H. .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2017, 28 (05) :604-618