Evaluating impact damage in CFRP using fibre optic sensors

被引:40
作者
Chambers, A. R. [1 ]
Mowlem, M. C.
Dokos, L.
机构
[1] Univ Southampton, Sch Engn Sci, Southampton SO17 1BJ, Hants, England
[2] Univ Southampton, NOC, Southampton SO17 1BJ, Hants, England
关键词
carbon fibres; impact behaviour; smart materials;
D O I
10.1016/j.compscitech.2006.05.023
中图分类号
TB33 [复合材料];
学科分类号
摘要
Damage in unidirectional carbon/fibre composite resulting from both low and high velocity/energy impacts was evaluated using embedded fibre Bragg grating (FBG) sensors, C-scan and microscopic analysis. It was found that the FBG sensors located 10 mm from the impact site could detect residual strains from a 0.33 J (1.3 m s(-1)) impact which was not detectable by C-scan or visual inspection. The measured residual strain increased with impact energy and damage changed from matrix cracking to severe delaminations. High velocity impacts (225 in s(-1) 11 J) resulted in test panel perforation and delaminations. FBG sensors located within a distance of 2-3 the damage radius detected residual strain from the impact. With an array of embedded sensors it is believed that it will be possible to identify the site of both low and high velocity energy impacts and predict the damage from the response of the adjacent sensors providing the sensors are located sufficiently close to the impact site. (c) 2006 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1235 / 1242
页数:8
相关论文
共 24 条
[1]  
BERT C, 1987, DAMAGE ASSESS MAT EV, P1
[2]   Damage detection in a radome sandwich material with embedded fiber optic sensors [J].
Bocherens, E ;
Bourasseau, S ;
Dewynter-Marty, V ;
Py, S ;
Dupont, M ;
Ferdinand, P ;
Berenger, H .
SMART MATERIALS & STRUCTURES, 2000, 9 (03) :310-315
[3]   POST-IMPACT FATIGUE PERFORMANCE OF CARBON-FIBER LAMINATES WITH NON-WOVEN AND MIXED-WOVEN LAYERS [J].
CANTWELL, W ;
CURTIS, P ;
MORTON, J .
COMPOSITES, 1983, 14 (03) :301-305
[4]  
CANTWELL W, 1987, COMPOS STRUCT, V3, P241
[5]   Impact-induced damage of laminated graphite/epoxy composites monitored using embedded in-line fiber etalon optic sensors [J].
Chang, CC ;
Sirkis, J .
JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 1997, 8 (10) :829-841
[6]   INVESTIGATION OF HYPERVELOCITY IMPACT DAMAGE TO SPACE STATION TRUSS TUBES [J].
CHRISTIANSEN, EL .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 1990, 10 (1-4) :125-133
[7]  
CRANE R, 1982, REV PROGR QUANT NO B, V2, P1419
[8]   In-situ process and condition monitoring of advanced fibre-reinforced composite materials using optical fibre sensors [J].
Doyle, C ;
Martin, A ;
Liu, T ;
Wu, M ;
Hayes, S ;
Crosby, PA ;
Powell, GR ;
Brooks, D ;
Fernando, GF .
SMART MATERIALS & STRUCTURES, 1998, 7 (02) :145-158
[9]  
Hale K. F., 1992, Smart Materials and Structures, V1, P156, DOI 10.1088/0964-1726/1/2/009
[10]   FIBER OPTIC DAMAGE DETECTION IN COMPOSITE STRUCTURES [J].
HOFER, B .
COMPOSITES, 1987, 18 (04) :309-316