TY - JOUR
T1 - Low-velocity impact responses and failure mechanisms of CFRP after fire exposure
AU - Lei, Zuxiang
AU - Cheng, Chunyu
AU - Yin, Binbin
AU - Tong, Lihong
AU - Wan, Yun
PY - 2022/10
Y1 - 2022/10
N2 - Damage to composite laminates in a fire will significantly affect their structural integrity and post-fire performance. Here, we investigate the low-velocity impact (LVI) responses and failure mechanisms of CFRP with normal and flame-retardant epoxy resin after exposure to fire. When exposed to fire, the cases with normal resin lose more mass than those with flame retardant. Especially at 600 °C and 800 °C, the mass loss increases sharply, resulting in the visibility of fibers on the surface. Then LVI tests are conducted to evaluate the effects of the post-fire on the impact resistance. According to the experimental results, the specimens with normal resin have better impact resistance. When burning on both types of specimens, a higher ultimate contact force is observed later in the force-time curves. As a result of fire, the stiffness of the laminates degraded, changing their energy absorption mechanism. Nevertheless, when the temperature reaches 800 °C, more interfacial delamination and a new shear failure mode are observed in both types of specimens. Besides, the specimens with flame-retardant epoxy resin show excellent performance on the LVI testing after flaming of 800 °C.
AB - Damage to composite laminates in a fire will significantly affect their structural integrity and post-fire performance. Here, we investigate the low-velocity impact (LVI) responses and failure mechanisms of CFRP with normal and flame-retardant epoxy resin after exposure to fire. When exposed to fire, the cases with normal resin lose more mass than those with flame retardant. Especially at 600 °C and 800 °C, the mass loss increases sharply, resulting in the visibility of fibers on the surface. Then LVI tests are conducted to evaluate the effects of the post-fire on the impact resistance. According to the experimental results, the specimens with normal resin have better impact resistance. When burning on both types of specimens, a higher ultimate contact force is observed later in the force-time curves. As a result of fire, the stiffness of the laminates degraded, changing their energy absorption mechanism. Nevertheless, when the temperature reaches 800 °C, more interfacial delamination and a new shear failure mode are observed in both types of specimens. Besides, the specimens with flame-retardant epoxy resin show excellent performance on the LVI testing after flaming of 800 °C.
KW - CFRP
KW - Failure mechanism
KW - Fire exposure
KW - Low-velocity impact
UR - http://www.scopus.com/inward/record.url?scp=85135794253&partnerID=8YFLogxK
UR - https://www.scopus.com/record/pubmetrics.uri?eid=2-s2.0-85135794253&origin=recordpage
U2 - 10.1016/j.coco.2022.101277
DO - 10.1016/j.coco.2022.101277
M3 - RGC 21 - Publication in refereed journal
SN - 2452-2139
VL - 34
JO - Composites Communications
JF - Composites Communications
M1 - 101277
ER -