不同针刺预制体结构对C/ C 复合材料力学性能的影响
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西安航天复合材料研究所

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Effect of Needled Preform Structure on Mechanical Properties of C/ C Composite
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    摘要:

    在斜纹碳布/ 碳纤维网胎、无纬布正交/ 碳纤维网胎针刺圆筒预制体的基础上,通过在其结构中增
    加角度缠绕连续纤维,设计和研制了新型结构针刺预制体,并对比研究了不同针刺预制体结构对圆筒C/ C 复
    合材料力学性能的影响。结果表明,无纬布正交铺层针刺C/ C 复合材料的层剪、轴向拉伸强度都高于斜纹碳
    布增强针刺C/ C 材料,其中轴向拉伸强度达到157. 0 MPa,提高了83. 0%;其层剪、轴向拉伸强度均有所提高,
    其最大分别可达到11. 68 和179郾0 MPa,分别提高了22. 6%和14%。

    Abstract:

    A new needled cylindrical preform was designed and fabricated in this paper by means of angle plies
    of continuous wound carbon fibers with a twill fabric and non鄄woven tapes needled preform as basements. The effects
    of needled preform structures on the mechanical properties of C/ C composites were compared and investigated. The
    results show that the orthogonal needled C/ C composite with the non鄄woven tapes has higher interlaminar shear
    strength(ILSS), and a higher axial tensile strength of 157. 0 MPa, being 83. 0% higher than that of the twill fabric
    reinforced. The non鄄woven tapes reinforced cylindrical C/ C composites with different angles have improved ILSS and
    axial tensile properties, the maximum ILSS and axial tensile strength reach 11. 68 MPa and 179. 0 MPa respectively,
    being 22. 6% and 14%,respectively,higher than that of the orthogonal C/ C composite.

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郑蕊.不同针刺预制体结构对C/ C 复合材料力学性能的影响[J].宇航材料工艺,2012,42(5).

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  • 在线发布日期: 2016-11-28
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