Experimental Analysis of the Low-Velocity Impact and CAI Properties of 3D Four-Directional Braided Composites after Hygrothermal Aging

• Published in: Materials Vol. 17; no. 13; p. 3151
• Main Authors: Zhang, Yuxuan, Li, Hanhua, Yan, Shi, Wang, Xin, Guan, Yue, Du, Changmei, Jiang, Lili, Zhai, Junjun
• Format: Journal Article
• Language: English
• Published: Switzerland MDPI AG 27.06.2024
• Subjects: 3D four-directional braided composites; Aging; Braided composites; C-scan; Carbon fibers; Composite materials; compression after impact (CAI); Compression tests; Compressive strength; Energy absorption; Epoxy resins; Experiments; Failure; Humidity; hygrothermal aging; Impact analysis; Impact loads; Impact strength; Interfacial properties; low-velocity impact (LVI); Mechanical properties; Moisture; Polymers; Seawater; SEM; Temperature; Three dimensional analysis; Three dimensional composites; C-scan; compression after impact (CAI); low-velocity impact (LVI); 3D four-directional braided composites; SEM; DIC; TGA; hygrothermal aging
• ISSN: 1996-1944; 1996-1944
• DOI: 10.3390/ma17133151

Three-dimensional braided composites (3D-BCs) have better specific strength and stiffness than two-dimensional planar composites (2D-PCs), so they are widely used in modern industrial fields. In this paper, two kinds of 3D four-directional braided composites (3D4d-BCs) with different braided angles (15°, denoted as H15, and 30°, denoted as H30) were subjected to hydrothermal aging treatments, low-velocity impact (LVI) tests, and compression after impact (CAI) tests under different conditions. This study systematically studied the hygroscopic behavior and the effect of hygrothermal aging on the mechanical properties of 3D4d-BC. The results show that higher temperatures and smaller weaving angles can significantly improve the moisture absorption equilibrium content. When the moisture absorption content is balanced, the energy absorption effect of 3D4d-BC is better, but the integrity and residual compression rate will be reduced. Due to the intervention of oxygen molecules, the interface properties between the matrix and the composite material will be reduced, so the compressive strength will be further reduced. In the LVI test, the peak impact load of H15 is low. In CAI tests, the failure of H15 mainly occurs on the side, and the failure form is buckling failure. The main failure direction of H30 is 45° shear failure.