首页|厚/薄铺层混杂复合材料层合板低速冲击损伤及冲击后压缩特性研究

厚/薄铺层混杂复合材料层合板低速冲击损伤及冲击后压缩特性研究

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相对于传统厚铺层碳纤维增强树脂基复合材料,薄铺层复合材料具有明显的损伤抑制效应,在诸多力学性能方面表现更为优异.基于准各项同性厚铺层层合板,采用"离散"与"聚集"2 种薄层嵌入厚层的方式衍生出的 2 种厚/薄层混杂层合板,研究低能量冲击载荷作用下的复合材料结构的损伤程度和分布特征以及冲击后的剩余压缩性能.实验获取了冲击与准静态压缩实验过程的力学响应;超声C扫与热揭层实验揭示了 3 类含冲击损伤复合材料层合板的分层损伤形貌特征,量化了损伤尺寸大小.实验结果分析表明:薄层的"离散"与"聚集"2种嵌入厚层的方式,充分利用了薄铺层复合材料的损伤抑制效应,改变了复合材料结构分层损伤的中心对称分布特征与特征分层损伤沿厚度方向分布位置,改善了复合材料层合板的剩余压缩性能.
Investigation on Low-velocity Impact Damage and Characteristics of Compression after Impact of Thick-/thin-ply Composite Laminates
Comparing with the traditional thick layer carbon fiber reinforced resin matrix composites,the thin layer composites have obvious damage inhibition effect and better mechanical properties.Two kinds of thick/thin hybrid laminates were derived by using discrete and aggregation embedment methods based on thick-ply laminate,which were used to study the damage degree and distribution characteristics of composite structures under low energy impact loads,as well as the residual com-pression properties after impact.The delamination damage morphologies of three types of composite laminates with impact damage were revealed by ultrasonic C-scan and thermal peeling experiments,and the damage size was quantified.The experimental results showed that the"discrete"and"ag-gregate"modes of thin layer embedding into thick layer made full use of the damage suppression effect of thin layer composite,the centrosymmetric distribution of layered damage and the distribu-tion position of characteristic layered damage along the thickness direction were changed,and the re-sidual compression performance of composite laminates was improved.

low-speed impacthybrid effectDe-plydamage suppression

郑凯东、曹东风、胡海晓、李瑞奇、李书欣

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国家能源氢能及氨氢融合新能源技术重点实验室,佛山仙湖实验室,佛山 528200

武汉理工大学 材料复合新技术国家重点实验室,武汉 430070

武汉理工大学 先进材料制作装备与技术研究院,武汉 430070

武汉理工大学 新材料力学理论与应用湖北省重点实验室,武汉 430070

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低速冲击 混杂效应 热揭层 损伤抑制

先进能源科学与技术广东省实验室佛山分中心(佛山仙湖实验室)开放基金资助中央高校基本科研业务费专项资金湖北省对外科技合作项目

XHT2020-0022020Ⅲ066GX2013BHE008

2024

载人航天
中国载人航天工程办公室

载人航天

CSTPCD北大核心
影响因子:0.411
ISSN:1674-5825
年,卷(期):2024.30(4)
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