Curing process and quasi-static compression monitoring of stiffened composite panels with embedded FBG sensors

被引:1
作者
Zhou Yu-jing [1 ,2 ]
Gang, Liu [2 ,4 ]
Hu Xiao-lan [3 ]
Ren Ming-wen [1 ]
Fan Guang-hong [1 ]
机构
[1] Beijing Natl Innovat Inst Lightweight Co Ltd, State Key Lab Adv Forming Technol & Equipment, Beijing 100083, Peoples R China
[2] AECC Beijing Inst Aeronaut Mat, Natl Key Lab Adv Composites, Beijing 100095, Peoples R China
[3] Xiamen Univ, Coll Mat, Fujian Prov Key Lab Fire Retardant Mat, Xiamen 361005, Fujian, Peoples R China
[4] Donghua Univ, Ctr Adv Low Dimens Mat, Shanghai 201620, Peoples R China
来源
CAILIAO GONGCHENG-JOURNAL OF MATERIALS ENGINEERING | 2021年 / 49卷 / 10期
关键词
FBG sensor; composite; curing process; compression; real-time monitoring;
D O I
10.11868/j.issn.1001-4381.2019.001208
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The FBG sensors, embedded in triangle region of composite T-stiffened panels, were used to monitor the strain change during curing process and quasi-static compression real-timely. The results show that the compression load of stiffened panels with the FBG sensor embedded along the stiffener is the same as that without the FBG sensor. The FBG sensor embedded in the triangular area of the stiffened panels can effectively monitor during the curing process, and it can also be used to monitor the temperature and strain changes real-timely after curing process. In the quasi-static compression process, the strain curve measured by the FBG sensor is the same as the force-displacement curve. The FBG sensors can monitor accurately the damage such as lamination and cracking in the stiffened panels without affecting the property of the stiffened panels.
引用
收藏
页码:132 / 137
页数:6
相关论文
共 24 条
[1]   Strain monitoring of composite elements by fibre Bragg grating sensors during a quasi-static indentation [J].
Antonucci, V. ;
Esposito, M. ;
Ricciardi, M. R. ;
Giordano, M. ;
Zarrelli, M. .
COMPOSITES PART B-ENGINEERING, 2014, 56 :34-41
[2]   Thermal isolation of FBG optical fibre sensors for composite cure monitoring [J].
Boateng, E. K. G. ;
Schubel, P. ;
Umer, R. .
SENSORS AND ACTUATORS A-PHYSICAL, 2019, 287 :158-167
[3]  
Chang Xinlong, 2010, Chinese Journal of Sensors and Actuators, V23, P748
[4]   Structural health monitoring techniques for aircraft composite structures [J].
Diamanti, K. ;
Soutis, C. .
PROGRESS IN AEROSPACE SCIENCES, 2010, 46 (08) :342-352
[5]   Predicting low-velocity impact damage on a stiffened composite panel [J].
Faggiani, A. ;
Falzon, B. G. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2010, 41 (06) :737-749
[6]  
Feng Yu, 2014, Journal of Aerospace Power, V29, P2905, DOI 10.13224/j.cnki.jasp.2014.12.017
[7]  
[高琳琳 Gao Linlin], 2016, [复合材料学报, Acta Materiae Compositae Sinica], V33, P2485
[8]  
[耿湘宜 Geng Xiangyi], 2016, [复合材料学报, Acta Materiae Compositae Sinica], V33, P1615
[9]   Monitoring the gelation and effective chemical shrinkage of composite curing process with a novel FBG approach [J].
Hu, Haixiao ;
Li, Shuxin ;
Wang, Jihui ;
Zu, Lei ;
Cao, Dongfeng ;
Zhong, Yucheng .
COMPOSITE STRUCTURES, 2017, 176 :187-194
[10]  
[黄飞生 Huang Feisheng], 2015, [玻璃钢/复合材料, Fiber Reinforced Plastics/Composites], P42