Fusion-based damage diagnostics for stiffened composite panels

被引:33
|
作者
Broer, Agnes [1 ]
Galanopoulos, Georgios [2 ]
Benedictus, Rinze [1 ]
Loutas, Theodoros [2 ]
Zarouchas, Dimitrios [1 ]
机构
[1] Delft Univ Technol, Struct Integr & Composites Grp, Fac Aerosp Engn, Kluyverweg 1, NL-2629 HS Delft, Netherlands
[2] Univ Patras, Dept Mech Engn & Aeronaut, Lab Appl Mech & Vibrat, Patras, Greece
基金
欧盟地平线“2020”;
关键词
Damage diagnostics; fusion; acoustic emission; distributed strain sensing; stiffened composite panel; fatigue; impact; EMISSION SOURCE LOCATION; BRAGG GRATING SENSORS; ACOUSTIC-EMISSION; LAMINATED COMPOSITES; MONITORING TECHNIQUE; DISTRIBUTED STRAIN; FATIGUE LIFE; CRACK-GROWTH; IDENTIFICATION; LOCALIZATION;
D O I
10.1177/14759217211007127
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Conducting damage diagnostics on stiffened panels is commonly performed using a single SHM technique. However, each SHM technique has both its strengths and limitations. Rather than straining the expansion of single SHM techniques going beyond their intrinsic capacities, these strengths and limitations should instead be considered in their application. In this work, we propose a novel fusion-based methodology between data from two SHM techniques in order to surpass the capabilities of a single SHM technique. The aim is to show that by considering data fusion, a synergy can be obtained, resulting in a comprehensive damage assessment, not possible using a single SHM technique. For this purpose, three single-stiffener carbon-epoxy panels were subjected to fatigue compression after impact tests. Two SHM techniques monitored damage growth under the applied fatigue loads: acoustic emission and distributed fiber optic strain sensing. Four acoustic emission sensors were placed on each panel, thereby allowing for damage detection, localization, type identification (delamination), and severity assessment. The optical fibers were adhered to the stiffener feet' surface, and its strain measurements were used for damage detection, disbond localization, damage type identification (stiffness degradation and disbond growth), and severity assessment. Different fusion techniques are presented in order to integrate the acoustic emission and strain data. For damage detection and severity assessment, a hybrid health indicator is obtained by feature-level fusion while a complementary and cooperative fusion of the diagnostic results is developed for damage localization and type identification. We show that damage growth can be monitored up until final failure, thereby performing a simultaneous damage assessment on all four SHM levels. In this manner, we demonstrate that by proposing a fusion-based approach toward SHM of composite structures, the intrinsic capacity of each SHM technique can be utilized, leading to synergistic effects for damage diagnostics.
引用
收藏
页码:613 / 639
页数:27
相关论文
共 50 条
  • [32] Damage tolerance predictions for stiffened composite panels .2. Application of a failure criteria
    Graesser, DL
    Tuttle, ME
    JOURNAL OF COMPOSITES TECHNOLOGY & RESEARCH, 1996, 18 (02): : 102 - 108
  • [33] Nonlinear progressive damage analysis of integral stiffened composite panels under compressive load
    Chang, Yuanyuan
    Xu, Xiwu
    Guo, Shuxiang
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2011, 28 (04): : 202 - 211
  • [34] Damage tolerance predictions for stiffened composite panels - Part II: Application of a failure criteria
    Graesser, Douglas L.
    Tuttle, Mark E.
    Journal of Composites Technology and Research, 1996, 18 (02): : 102 - 108
  • [35] Energy absorption and damage evaluation of grid stiffened composite panels under transverse loading
    Jadhav, P
    Mantena, PR
    Gibson, RF
    COMPOSITES PART B-ENGINEERING, 2006, 37 (2-3) : 191 - 199
  • [36] A Framework for Damage Tolerance and Optimization of Stiffened Panels
    Jrad, Mohamed
    Mulani, Sameer B.
    Kapania, Rakesh K.
    STRUCTURAL HEALTH MONITORING 2015: SYSTEM RELIABILITY FOR VERIFICATION AND IMPLEMENTATION, VOLS. 1 AND 2, 2015, : 3 - 10
  • [37] Reliability based buckling analysis of composite panels with tophat stiffened topology
    Xue, Xiaoguang
    Li, Guoxi
    Yang, Jingzhao
    Gong, Jingzhong
    ADVANCED MATERIALS AND PROCESS TECHNOLOGY, PTS 1-3, 2012, 217-219 : 91 - 95
  • [38] Vibrations of stiffened composite panels with smart materials
    Poulin, KC
    Vaicaitis, R
    JOURNAL OF VIBRATION AND ACOUSTICS-TRANSACTIONS OF THE ASME, 2004, 126 (03): : 370 - 379
  • [39] A fast procedure for the design of composite stiffened panels
    Vescovini, Riccardo
    Bisagni, Chiara
    AERONAUTICAL JOURNAL, 2015, 119 (1212): : 185 - 201
  • [40] Thermomechanical response variability of stiffened composite panels
    Noor, AK
    Starnes, JH
    Peters, JM
    JOURNAL OF AEROSPACE ENGINEERING, 2002, 15 (04) : 154 - 164