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与0°取向层混合后提高螺旋层压板低速冲击后的抗压强度及其分析

Increasing the Compressive Strength of Helicoidal Laminates after Low-Velocity Impact upon Mixing with 0° Orientation Plies and Its Analysis.

作者信息

Yu Zhefeng, Du Xin, Liu Rui, Xie Qiwu, Zhang Xiaojing, Zhu Qiao

机构信息

Aerospace Structure Research Center, School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai 200240, China.

出版信息

Materials (Basel). 2023 Jun 26;16(13):4599. doi: 10.3390/ma16134599.

Abstract

The helicoidal laminate is a kind of nature inspired fiber reinforced polymer, and the ply orientation affects their mechanical properties for engineering structural applications. A variety of helicoidal laminates with uniform and non-linear pitch angles mixed with additional 0° plies are fabricated to investigate the impact resistance through low-velocity impact and after-impact compression tests. Additionally, helicoidal laminates with constant pitch angles, quasi-isotropic laminate, and cross-ply laminates are also fabricated for a comparative study. The impact characteristics and the compressive strength are analyzed in view of the impact model, shear stress distribution, and fracture toughness. The results suggest that 10° or 20° are the better basic pitch angles before mixing 0° orientation plies. The 0° orientation plies may affect the contact stiffness, bending stiffness, damage extent, and compressive modulus. The compressive strength reaches the highest in tests on two samples with different percentages of 0° orientation plies and ply setups. Bending stiffness also dominates the impact response. The analysis on the laminate parameters provides ideas to improve the residual strength of helicoidal laminate.

摘要

螺旋层合板是一种受自然启发的纤维增强聚合物,铺层方向会影响其在工程结构应用中的力学性能。制造了各种具有均匀和非线性螺距角并混合额外0°铺层的螺旋层合板,通过低速冲击和冲击后压缩试验来研究其抗冲击性。此外,还制造了具有恒定螺距角的螺旋层合板、准各向同性层合板和正交层合板用于对比研究。从冲击模型、剪应力分布和断裂韧性的角度分析了冲击特性和抗压强度。结果表明,在混合0°取向铺层之前,10°或20°是较好的基本螺距角。0°取向铺层可能会影响接触刚度、弯曲刚度、损伤程度和压缩模量。在对具有不同0°取向铺层百分比和铺层设置的两个样品的测试中,抗压强度达到最高。弯曲刚度也主导着冲击响应。对层合板参数的分析为提高螺旋层合板的残余强度提供了思路。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/18bb/10342965/d0f243231cb6/materials-16-04599-g001.jpg

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