TY - JOUR
T1 - 2D Plain and 3D Needle-punched C/SiC Composites
T2 - Low-velocity Impact Damage Behavior and Failure Mechanism
AU - Luan, Xingang
AU - He, Dianwei
AU - Tu, Jianyong
AU - Cheng, Laifei
N1 - Publisher Copyright:
© 2025 Science Press. All rights reserved.
PY - 2025/2
Y1 - 2025/2
N2 - Continuous carbon fiber reinforced silicon carbide (C/SiC) composites are often subjected to low-velocity impacts when utilized as structural materials for thermal protection. However, research on in-plane impact damage and multiple impact damage of C/SiC composites is limited. To investigate the in-plane impact damage behavior of C/SiC composites, a drop-weight impact test method was developed for strip samples, and these results were subsequently compared with those of C/SiC composite plates. Results show that the in-plane impact behavior of C/SiC strip samples is similar to that of C/SiC composite plates. Variation of the impact load with displacement is characterized by three stages: a nearly linear stage, a severe load drop stage, and a rebound stage where displacement occurs after the impact energy exceeds its peak value. Impact damage behavior under single and multiple impacts on 2D plain and 3D needled C/SiC composites was investigated at different impact energies and durations. Crack propagation in C/SiC composites was studied by computerized tomography (CT) technique. In the 2D plain C/SiC composite, load propagation between layers is hindered during impact, leading to delamination and 90° fiber brittle fracture. The crack length perpendicular to the impact direction increases with impact energy increases, resulting in more serious 0° fiber fracture and a larger area of fiber loss. In the 3D needled C/SiC composite, load propagates between the layers during impact through the connection of needled fibers. The fibers continue to provide substantial structural support, with notable instances of fiber pull-off and debonding. Consequently, the impact resistance is superior to that of 2D plain C/SiC composite. When the 3D needled C/SiC composite undergoes two successive impacts of 1.5 J, the energy absorption efficiency of the second impact is significantly lower, accompanied by a smaller impact displacement. Moreover, the total energy absorption efficiency of these two impacts of 1.5 J is lower than that of a single 3.0 J impact.
AB - Continuous carbon fiber reinforced silicon carbide (C/SiC) composites are often subjected to low-velocity impacts when utilized as structural materials for thermal protection. However, research on in-plane impact damage and multiple impact damage of C/SiC composites is limited. To investigate the in-plane impact damage behavior of C/SiC composites, a drop-weight impact test method was developed for strip samples, and these results were subsequently compared with those of C/SiC composite plates. Results show that the in-plane impact behavior of C/SiC strip samples is similar to that of C/SiC composite plates. Variation of the impact load with displacement is characterized by three stages: a nearly linear stage, a severe load drop stage, and a rebound stage where displacement occurs after the impact energy exceeds its peak value. Impact damage behavior under single and multiple impacts on 2D plain and 3D needled C/SiC composites was investigated at different impact energies and durations. Crack propagation in C/SiC composites was studied by computerized tomography (CT) technique. In the 2D plain C/SiC composite, load propagation between layers is hindered during impact, leading to delamination and 90° fiber brittle fracture. The crack length perpendicular to the impact direction increases with impact energy increases, resulting in more serious 0° fiber fracture and a larger area of fiber loss. In the 3D needled C/SiC composite, load propagates between the layers during impact through the connection of needled fibers. The fibers continue to provide substantial structural support, with notable instances of fiber pull-off and debonding. Consequently, the impact resistance is superior to that of 2D plain C/SiC composite. When the 3D needled C/SiC composite undergoes two successive impacts of 1.5 J, the energy absorption efficiency of the second impact is significantly lower, accompanied by a smaller impact displacement. Moreover, the total energy absorption efficiency of these two impacts of 1.5 J is lower than that of a single 3.0 J impact.
KW - ceramic-matrix composite
KW - computerized tomography analysis
KW - fracture
KW - low-velocity impact
UR - http://www.scopus.com/inward/record.url?scp=85218345834&partnerID=8YFLogxK
U2 - 10.15541/jim20240269
DO - 10.15541/jim20240269
M3 - 文章
AN - SCOPUS:85218345834
SN - 1000-324X
VL - 40
SP - 205
EP - 214
JO - Wuji Cailiao Xuebao/Journal of Inorganic Materials
JF - Wuji Cailiao Xuebao/Journal of Inorganic Materials
IS - 2
ER -