Impact response in polymer composites from embedded optical fibers

被引:15
作者
Batte, Lorianne K. [1 ]
Sullivan, Rani W. [1 ]
Ranatunga, Vipul [2 ]
Brown, Kevin [2 ]
机构
[1] Mississippi State Univ, Dept Aerosp Engn, Mississippi State, MS 39762 USA
[2] Air Force Res Lab, Wright Patterson AFB, OH USA
关键词
Optical strain sensing; delamination; low-velocity impact; DIAMETER FBG SENSORS; DELAMINATION DETECTION; SENSING TECHNIQUE; DAMAGE; EDGE;
D O I
10.1177/0021998318763274
中图分类号
TB33 [复合材料];
学科分类号
摘要
This study investigates the feasibility of using embedded optical fibers in polymer matrix composite laminates to characterize delaminations caused by low-velocity impacts with energies between 30J and 50J. Impact damage can occur in composite structures during manufacture, in-service, storage and routine maintenance. Because of their small size and light weight, optical fibers can be embedded in composite structures during the manufacture of composite parts, allowing the structure to be monitored for impact-induced delaminations without being removed from service. In this study, optical fibers are embedded in a grid configuration at four selected locations (one-third from impact surface, midplane, two-thirds from impact surface, and farthest ply from impact) in thick autoclave-cured graphite/epoxy laminates. Low-velocity impact testing is performed at four energy levels. Manufacturing procedures for embedding the optical fibers within the composite laminates are investigated. The strain distribution from the optical fibers is correlated with ultrasonic C-scans of the laminates in which they are embedded. X-ray computed tomography scan images are also compared to those from ultrasonic C-scans. Results indicate that embedded optical fibers can provide post-impact strain responses and delamination area from each embedded site within the impacted laminates.
引用
收藏
页码:3415 / 3427
页数:13
相关论文
共 20 条
[1]  
ASTM, 2015, ASTMD7136
[2]   OPTICAL-FIBER SENSING TECHNIQUE FOR EDGE-INDUCED AND INTERNAL DELAMINATION DETECTION IN COMPOSITES [J].
BHATIA, V ;
SCHMID, CA ;
MURPHY, KA ;
CLAUS, RO ;
TRAN, TA ;
GREENE, JA ;
MILLER, MS .
SMART MATERIALS & STRUCTURES, 1995, 4 (03) :164-169
[3]   Non-Destructive Inspection of Impact Damage in Composite Aircraft Panels by Ultrasonic Guided Waves and Statistical Processing [J].
Capriotti, Margherita ;
Kim, Hyungsuk E. ;
di Scalea, Francesco Lanza ;
Kim, Hyonny .
MATERIALS, 2017, 10 (06)
[4]   High-speed 3D digital image correlation of low-velocity impacts on composite plates [J].
Flores, Mark ;
Mollenhauer, David ;
Runatunga, Vipul ;
Beberniss, Timothy ;
Rapking, Daniel ;
Pankow, Mark .
COMPOSITES PART B-ENGINEERING, 2017, 131 :153-164
[5]   OPTICAL FIBER DAMAGE DETECTION FOR AN AIRCRAFT COMPOSITE LEADING-EDGE [J].
GLOSSOP, NDW ;
DUBOIS, S ;
TSAW, W ;
LEBLANC, M ;
LYMER, J ;
MEASURES, RM ;
TENNYSON, RC .
COMPOSITES, 1990, 21 (01) :71-80
[6]   OPTICAL-FIBER SENSING TECHNIQUE FOR IMPACT DETECTION AND LOCATION IN COMPOSITES AND METAL SPECIMENS [J].
GREENE, JA ;
TRAN, TA ;
BHATIA, V ;
GUNTHER, MF ;
WANG, A ;
MURPHY, KA ;
CLAUS, RO .
SMART MATERIALS AND STRUCTURES, 1995, 4 (02) :93-99
[7]   Damage of composite materials [J].
Jollivet, Thomas ;
Peyrac, Catherine ;
Lefebvre, Fabien .
FATIGUE DESIGN 2013, INTERNATIONAL CONFERENCE PROCEEDINGS, 2013, 66 :746-758
[8]  
Meadows L., 2016, 57 AIAA ASCE AHS ASC
[9]   Distributed optical sensing in composite laminates [J].
Meadows, Leeanna ;
Sullivan, Rani W. ;
Brown, Kevin ;
Ranatunga, Vipul ;
Vehorn, Keith ;
Olson, Steven .
JOURNAL OF STRAIN ANALYSIS FOR ENGINEERING DESIGN, 2017, 52 (07) :410-421
[10]  
Ranatunga V., 2015, 56 AIAA ASCE AHS ASC