Reliability assessment of pulsed thermography and ultrasonic testing for impact damage of CFRP panels

被引：58

作者：

Duan, Yuxia ^{[1
]}

Zhang, Hai ^{[2
]}

Maldague, Xavier P. V. ^{[2
]}

Ibarra-Castanedo, Clemente ^{[2
]}

Servais, Pierre ^{[3
]}

Genest, Marc ^{[4
]}

Sfarra, Stefano ^{[5
,6
]}

Meng, Jianqiao ^{[1
]}

机构：

[1] Cent S Univ, Sch Phys & Elect, 932 Lushan South Rd, Changsha 410083, Hunan, Peoples R China

[2] Univ Laval, Dept Elect & Comp Engn, Comp Vis & Syst Lab, 1065 Av Med, Quebec City, PQ G1V 0A6, Canada

[3] Soc NDT Pro, Entreprise BE 0883-019-209,Le Grand Enclos 18, B-6800 Libramont, Belgium

[4] Natl Res Council Canada, 1200 Montreal Rd,Bldg M-14, Ottawa, ON K1A 0R6, Canada

[5] Univ Aquila, Dept Ind & Informat Engn & Econ, Piazzale E Pontieri 1, I-67100 Roio Poggio, AQ, Italy

[6] Tomsk Polytech Univ, Lenin Av 30, Tomsk 634050, Russia

来源：

NDT & E INTERNATIONAL | 2019年 / 102卷

基金：

中国国家自然科学基金;

关键词：

Thermography; Ultrasonic testing; CFRP; Impact damage; Probability of detection; LASER LINE THERMOGRAPHY; LOCK-IN; INSPECTION; PROBABILITY; CAPABILITY;

D O I：

10.1016/j.ndteint.2018.11.010

中图分类号：

TB3 [工程材料学];

学科分类号：

0805 ; 080502 ;

摘要：

In order to quantitatively compare the reliability of pulsed thermography and ultrasonic testing techniques, a set of thirty-five Carbon Fiber Reinforced Plastic (CFRP) composite panels with impact damages are inspected by pulsed thermography and ultrasonic C-scan. The comparative experimental results and Probability of Detection (PoD) analysis results are presented. The quantitative comparison shows that pulsed thermography testing has smaller defect size at 90% PoD with 95% confidence level, i.e. a(90/95) values than ultrasonic testing for the parameters and setup used in the inspections of these thirty-five CFRP composite panels.

引用

页码：77 / 83

页数：7

共 37 条

[1]

[Anonymous], 2009, NONDESTRUCTIVE EVALU

[2] 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

[3] Rapid thermal non-destructive testing of aircraft components [J].

Bates, D ;

Smith, G ;

Lu, D ;

Hewitt, J .

COMPOSITES PART B-ENGINEERING, 2000, 31 (03) :175-185

[4]

Berens A. P, 1989, ASM METALS HDB, V17, P1389

[5]

Birks AS, NONDESTRUCTIVE TESTI, V7

[6] Sizing of impact damages in composite materials using ultrasonic guided waves [J].

Castaings, Michel ;

Singh, Dilbag ;

Viot, Philippe .

NDT & E INTERNATIONAL, 2012, 46 :22-31

[7]

DiMambro J, 2007, AIP CONF PROC, V894, P463, DOI 10.1063/1.2718008

[8]

DiMambro J, 2005, REV PROGR QUANTITATI, V24, P536

[9]

DiMambro J., 2006, ULTRASONIC ADV METHO, P349

[10]

DiMambro J, 2006, 49 ANN AIR TRANSP AS

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