Investigation of carbon fiber reinforced polymer (CFRP) sheet with subsurface defects inspection using thermal-wave radar imaging (TWRI) based on the multi-transform technique

被引:67
作者
Gong, Jinlong [1 ]
Liu, Junyan [1 ]
Qin, Lei [1 ]
Wang, Yang [1 ]
机构
[1] Harbin Inst Technol, Sch Mechatron Engn, Harbin 150001, Peoples R China
关键词
Carbon fiber reinforced polymer; Linear frequency modulation; Thermal-wave radar imaging; Hilbert transform; Cross-correlation; MIRAGE EFFECT SPECTROMETER; TRANSIENT THERMOGRAPHY; INSTRUMENTATION; SPECTROSCOPIES;
D O I
10.1016/j.ndteint.2013.12.006
中图分类号
TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
A combined theoretical and experimental approach is reported using thermal-wave radar imaging (TRWI) for carbon fiber reinforced polymer (CFRP) with subsurface defects inspection. The multi-transform technique (Fourier transform, FT; Hilbert transform, HT; and cross-correlation, CC) is applied to extract the characteristics of thermal-wave signal. Experimental results indicate that the multi-transform technique of thermal-wave signal is available for detecting the subsurface defect. For the shallow defect (defect depth <= 1 mm), the delay time image of CC exhibits high contrast, and the phase image of FT has high SNR at the right frequency component. For the deep defect (defect depth 2.0 mm), the phase images of HT have both high contrast and large SNR value. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:130 / 136
页数:7
相关论文
共 36 条
[1]   Aircraft composites assessment by means of transient thermal NDT [J].
Avdelidis, NP ;
Almond, DP ;
Dobbinson, A ;
Hawtin, BC ;
Ibarra-Castanedo, C ;
Maldague, X .
PROGRESS IN AEROSPACE SCIENCES, 2004, 40 (03) :143-162
[2]   Through skin sensing assessment of aircraft structures using pulsed thermography [J].
Avdelidis, NP ;
Almond, DP .
NDT & E INTERNATIONAL, 2004, 37 (05) :353-359
[3]   Transient thermography as a through skin imaging technique for aircraft assembly: modelling and experimental results [J].
Avdelidis, NP ;
Almond, DP .
INFRARED PHYSICS & TECHNOLOGY, 2004, 45 (02) :103-114
[4]   Transient thermography in the assessment of defects of aircraft composites [J].
Avdelidis, NP ;
Hawtin, BC ;
Almond, DP .
NDT & E INTERNATIONAL, 2003, 36 (06) :433-439
[5]   The detection and measurement of impact damage in thick carbon fibre reinforced laminates by transient thermography [J].
Ball, RJ ;
Almond, DP .
NDT & E INTERNATIONAL, 1998, 31 (03) :165-173
[6]  
Brigham E. O., 1974, FAST FOURIER TRANSFO
[7]   THERMAL WAVE REMOTE AND NON-DESTRUCTIVE INSPECTION OF POLYMERS [J].
BUSSE, G ;
EYERER, P .
APPLIED PHYSICS LETTERS, 1983, 43 (04) :355-357
[8]   THERMAL WAVE IMAGING WITH PHASE SENSITIVE MODULATED THERMOGRAPHY [J].
BUSSE, G ;
WU, D ;
KARPEN, W .
JOURNAL OF APPLIED PHYSICS, 1992, 71 (08) :3962-3965
[9]  
Castanedo CI, 2007, P SOC PHOTO-OPT INS, V6541
[10]   Applications of Barker coded infrared imaging method for characterisation of glass fibre reinforced plastic materials [J].
Dua, G. ;
Mulaveesala, R. .
ELECTRONICS LETTERS, 2013, 49 (17) :1071-1072