碳纳米管膜层间增韧对碳纤维复合材料力学性能的影响
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航天材料及工艺研究所

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TB332

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Effect of Carbon Nanotube Film Interlayer Toughening on MechanicalProperties of Carbon Fiber Reinforced Composite
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    摘要:

    分别采用两种碳纳米管膜进行层间增韧,应用热压罐工艺成型了碳纳米管膜/ 碳纤维增强树脂基
    复合材料,研究了碳纳米管膜的成型工艺、取向、面密度对复合材料力学性能和层间韧性的影响。结果表明:
    CNT 膜平行于碳纤维铺放时复合材料的压缩强度、90毅弯曲强度和层剪强度均高于CNT 膜垂直于碳纤维铺放
    时的复合材料性能。面密度较小的CNT 膜对复合材料的增韧效果较好。喷涂法成型的碳纳米管膜层间改性
    的复合材料层间断裂韧性明显优于拉膜法碳纳米管膜层间改性的。CNT 无规膜的面密度为0. 75 g/ m2 时,复
    合材料的GIC和GIIC最优,相比改性前分别提高了21%和42%。

    Abstract:

    Carbon nanotube film(CNTF) / carbon fiber reinforced resin composite were fabricated via autoclave
    process with two kinds of carbon nanotube film interlayer toughening respectively. Effect of the molding process, ori鄄
    entation and planar density of the carbon nanotube film on the mechanical properties and interlaminar toughness of
    composite were investigated. The result reveals that compared to the vertical direction, when the CNTF were layed
    paralleling to the carbon fiber, the compression strength,90毅flexural strength and interlaminar shear strength of com鄄
    posite were better. The toughening effect of the composite enhanced as the planar density of the carbon nanotube film
    decrease. The interlaminar fracture toughness of composite interlayer toughened by carbon nanotube film sprayed is
    more outstanding evidently than carbon nanotube film drawed. When the planar density of the carbon nanotube ran鄄
    dom film was 0. 75 g/ m2, GIC and GIIC of composite were optimum, increased by 21% and 42%, respectively,com鄄
    pared to composite before toughening.

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邓火英.碳纳米管膜层间增韧对碳纤维复合材料力学性能的影响[J].宇航材料工艺,2015,45(5).

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  • 在线发布日期: 2016-11-28
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