Cristea George Cătălin, Deleanu Lorena, Chiracu Ioana Gabriela, Boțan Mihail, Ojoc George Ghiocel, Vasiliu Alexandru Viorel, Cantaragiu Ceoromila Alina
National Institute for Aerospace Research (INCAS) "Elie Carafoli", 220 Iuliu Maniu, 061126 Bucharest, Romania.
Center of Excellence in Polymer Processing (CE-PP), "Dunarea de Jos" University, 111 Domneasca, 800201 Galati, Romania.
Polymers (Basel). 2025 Jan 28;17(3):355. doi: 10.3390/polym17030355.
In this study, the composition and mechanical properties of composites designed for shipbuilding are described. Four different composites were designed and fabricated by the research team, using quadriaxial glass fiber fabric (eight layers in all composites), two different resins (the epoxy resin SikaBiresin CR82 with the hardener CH80-2 or the polyester resin Enydyne H 68372 TA with Metox-50 W as the accelerator), and a middle layer of Coremat Xi 3 (only applied in some composites). The experimental results of low-velocity impact tests are also discussed, including the graphics force (displacement) and absorbed energy (displacement and velocity). The displacement and composite quality were evaluated through several parameters, such as maximum force, absorbed energy, and maximum displacement. Impact tests were carried out using four impact energy values (50-200 J), with an average impact velocity in the range of 4.37 ± 0.05 m/s. Only partial penetrations were obtained for all tested composites. For the low energy tests (50 J), the four composite materials were not well differentiated by graph shapes and parameter values, but for the higher energy tests, the composites containing Coremat Xi 3 displayed better behavior, having F reduced with 10.8% to 29.08%. The higher absorbed energy of these composites can be explained by the plateau generated by the force from a longer impactor displacement in contact with the composite. The results generated in this study confirm the suitability of the designed composites for shipbuilding applications. Still, the composites have light differences in terms of energy absorption in low-velocity impact and a significant reduction in maximum force.
本研究描述了用于造船的复合材料的组成和力学性能。研究团队设计并制造了四种不同的复合材料,使用四轴玻璃纤维织物(所有复合材料共八层)、两种不同的树脂(环氧树脂西卡比树脂CR82与固化剂CH80 - 2或聚酯树脂恩迪恩H 68372 TA与作为促进剂的美托克斯 - 50 W),以及一层Coremat Xi 3中间层(仅应用于部分复合材料)。还讨论了低速冲击试验的实验结果,包括力(位移)和吸收能量(位移和速度)的图表。通过几个参数评估位移和复合材料质量,如最大力、吸收能量和最大位移。使用四个冲击能量值(50 - 200 J)进行冲击试验,平均冲击速度在4.37±0.05 m/s范围内。所有测试复合材料均仅出现部分穿透。对于低能量试验(50 J),四种复合材料在图表形状和参数值方面没有很好地区分,但对于较高能量试验,含有Coremat Xi 3的复合材料表现更好,F降低了10.8%至29.08%。这些复合材料较高的吸收能量可以通过较长冲击器位移与复合材料接触时力产生的平台来解释。本研究产生的结果证实了所设计的复合材料适用于造船应用。尽管如此,这些复合材料在低速冲击下的能量吸收方面存在轻微差异,并且最大力有显著降低。