Experimental investigations into damage mechanism in the low-velocity impact and tension-after-impact testing of z-pin reinforced curved CFRP composite

被引:6
作者
Liu, Weiwei [1 ]
Sang, Chen [1 ]
Jin, Kexin [1 ]
Hou, Jiahao [1 ]
Yin, Mingxin [1 ]
机构
[1] Northwestern Polytech Univ, Sch Mech Engn, Xian 710072, Shaanxi, Peoples R China
关键词
3-dimensional reinforcement; impact behavior; tension-after-impact testing; INTERLAMINAR FRACTURE-TOUGHNESS; DELAMINATION; COMPRESSION; PERFORMANCE; RESISTANCE; FAILURE;
D O I
10.1002/pc.28109
中图分类号
TB33 [复合材料];
学科分类号
摘要
This paper studies the influence of z-pins on the impact resistance and residual tensile properties of composite large curvature components through low velocity impact and tension-after-impact tests to explore the damage mechanism. Unpinned and z-pinned specimens with different diameters (0.3 and 0.5 mm) and spacing (3, 4, and 5 mm) were impacted at energies of 28 J and 14 J + 14 J and were stretched until failure. The theoretical models were used to predict impact dent depth and tensile strength, and the effectiveness of z-pins and damage patterns were characterized by force-time/displacement curves and through visual observation. The agreement between the experiments and predictions can thus validate the presented approach. Through the low-velocity impact test, it is found that z-pins with higher density and smaller diameter make the impact dent shallower and the surface damage less, thus showing better performance. Later, the impacted specimens mainly show delamination, explosion, breakage, and splitting after tension. During the first stage of the force-displacement curves, since z-pins mitigate the delamination, tensile strength shows a 29.58%-59.17% increase while in the third stage, a decrease of 3.95%-15.12% occurs due to initial damage caused by z-pins. Highlights center dot Different impact energies are implemented on large curved CFRP laminates of z-pins with different diameters and spacing to explore the damage mechanism.center dot Low-velocity impact and tension-after-impact (TAI) tests are used to simulate the centrifugal force of the blade subjected to impact and rotation after impact.center dot Z-pinned group with a small diameter and high density causes less damage and tensile strength in the first stage increases while decreasing in the third stage compared with the unpinned group.
引用
收藏
页码:5051 / 5067
页数:17
相关论文
共 50 条
[41]   IN-SITU DAMAGE PROGRESSION OBSERVATIONS IN CROSS-PLY CFRP COMPOSITE BEAMS UNDER LOW-VELOCITY IMPACT AND QUASI-STATIC INDENTATION LOADING [J].
Batmaz, Onur Ali ;
Coker, Demirkan .
PROCEEDINGS OF ASME 2023 INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, IMECE2023, VOL 11, 2023,
[42]   Compressive Residual Load Testing and Analysis of Composite Stiffened Panels With Delamination Damage Due to Low-Velocity Impact [J].
Park, Chan Yik ;
Eom, Sohyeon ;
Joo, Young Sik ;
Kim, Min Sung ;
Seo, Bohwi .
JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2024, 52 (07) :521-527
[43]   Experimental and numerical studies on low-velocity impact damage of composite laminates toughened by nickel-coated carbon fiber veil [J].
Liu, Hui ;
Qu, Peng ;
Guo, Yunli ;
Zhou, Yong ;
Wan, Guoshun ;
Jia, Yuxi .
POLYMER COMPOSITES, 2022, 43 (04) :2460-2476
[44]   Damage Prediction of Integrated Composite T-Joint with Fixed Support Subjected to Low-Velocity Impact: An Experimental and Numerical Study [J].
Zhu, Rujian ;
Xu, Xiwu ;
Mao, Chunjian .
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2019, 20 (01) :90-99
[45]   Experimental and numerical analysis of low-velocity impact damage of CFRP laminates with negative Poisson ratio (NPR) rubber protective layer [J].
Li, Ximing ;
Liu, Ping ;
Cheng, Hui ;
Liu, Chinan ;
Zhu, Yuchen ;
Zhang, Kaifu .
THIN-WALLED STRUCTURES, 2023, 191
[46]   Experimental and Numerical Study of Low-Velocity Impact and Tensile after Impact for CFRP Laminates Single-Lap Joints Adhesively Bonded Structure [J].
Hu, Chunxing ;
Huang, Guibin ;
Li, Cheng .
MATERIALS, 2021, 14 (04) :1-24
[47]   Noncontact inspection of impact damage properties of woven fabric-reinforced composites after low-velocity impact by using air-coupled ultrasonic technique [J].
Ahmed, Azzam ;
Mohmmed, Ramadan ;
Bingjie, Zhou ;
Wei, Li .
JOURNAL OF INDUSTRIAL TEXTILES, 2016, 46 (03) :809-832
[48]   Methodology of residual strength prediction of composite structures with low-velocity impact damage based on NDT inspections and numerical-experimental CAI testing [J].
Katunin, Andrzej ;
Danek, Wojciech ;
Wronkowicz, Angelika ;
Dragan, Krzysztof .
INTERNATIONAL JOURNAL OF IMPACT ENGINEERING, 2023, 181
[49]   Experimental and numerical investigation of Low-Velocity impact on steel wire reinforced foam Core/Composite skin sandwich panels [J].
Mohammadkhani, P. ;
Jalali, S. S. ;
Safarabadi, M. .
COMPOSITE STRUCTURES, 2021, 256
[50]   Experimental damage tolerance evaluation of thick fabric carbon/epoxy laminates under low-velocity and high-velocity impact and compression-after-impact [J].
van Hoorn, Niels ;
Kassapoglou, Christos ;
Turteltaub, Sergio ;
van den Brink, Wouter .
JOURNAL OF COMPOSITE MATERIALS, 2022, 56 (05) :761-778