2.5D交织铺层结构复合材料抗低速冲击性能研究
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1.航天材料及工艺研究所,北京 100076;2.功能性碳纤维复合材料国家工程研究中心,北京 100076

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TB332

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2.5D Interleaved Laminated Composite for Low-speed Impact Resistance
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1.Aerospace Research Institute of Materials & Processing Technology,Beijing 100076;2.National Engineering Research Center for Functional Carbon Fiber Composites,Beijing 100076

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    摘要:

    为探究2.5D交织铺层结构复合材料的抗低速冲击性能,制备了2.5D交织铺层结构试样、常规交织铺层结构试样及相同铺层层合试样,通过落锤试验及冲击后压缩探究了两种交织铺层复合材料结构及层合结构复合材料低速冲击损伤下的性能表现。结果表明:落锤冲击下,2.5D交织铺层结构相较于层合结构其表面冲击变形面积缩小了73.79%,内部损伤投影区域缩小了21.66%,冲击后压缩强度提升了10.53%,表现出优异的抵抗低速冲击变形及损伤的能力。

    Abstract:

    In order to explore the low-velocity impact resistance of 2.5D interleaved laminated structure composites,2.5D interleaved laminated structure test panels,conventional interleaved laminated structure test panels and same laminate laminate test panels were prepared.The performance of two interleaved laminated composite structures and laminated composites under low-velocity impact damage was investigated by drop weight test and post-impact compression.The results show that under the impact of the falling weight,compared with the laminated structure,the surface impact deformation area of the 2.5D interleaved laminated structure is reduced by 73.79%,the internal damage projection area is reduced by 21.66%,and the compressive strength after impact is increased by 10.53%.The 2.5D interleaved laminated structure exhibits excellent resistance to low-speed impact deformation and damage.

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张昊,孙宏杰,张建宝,刘永佼,赵忠祥.2.5D交织铺层结构复合材料抗低速冲击性能研究[J].宇航材料工艺,2025,55(3):55-61.

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历史
  • 收稿日期:2023-01-04
  • 最后修改日期:2025-06-12
  • 录用日期:2023-04-20
  • 在线发布日期: 2025-06-27
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