注胶法修复5228A/ CF3031 层压板力学性能研究
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西北工业大学

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Mechanical Properties of 5228A/ CF3031 LaminatesRepaired by The Glue-Injection Method
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    摘要:

    针对5228A/ CF3031 层压板生产过程中可能产生的缺陷,设计并制造了孔径超差、不圆孔、孔径
    分层、孔边打磨过分、边缘分层等5 种常见缺陷,并采用注胶法对5 种缺陷进行修复。采用ASTM 标准对无缺
    陷试样、缺陷试样、修复试样的拉伸、压缩、弯曲、纵横剪切和层间剪切强度进行了测试,并对试样进行了光学显
    微镜观察。研究表明孔径超差对拉伸、压缩、弯曲强度影响较大,缺陷试样强度分别下降了11. 1%、13. 8%、
    14.4%;孔边打磨过分对纵横剪切强度影响较大,缺陷试样纵横剪切强度下降了25. 6%;边缘分层对层间剪切
    强度影响较大,缺陷试样层间剪切强度下降了27. 3%。采用注胶法修复后,5 种缺陷试样的力学性能均有一定
    程度的提高。相比而言,修复后层压板抵抗拉伸、压缩、层间剪切等小形变破坏的效果显著;抵抗弯曲、纵横剪
    切等大形变破坏的效果不理想。

    Abstract:

    Based on damages probably caused by the process of production of 5228A/ CF3031 laminates, 5
    kinds of defective samples were designed and produced, including the exceeding standard aperture(ESA), the elliptical
    aperture(EA), the layering aperture(LA), the overly polishing aperture(OPA) and the layering fringe(LF),
    and glue-injection method was proposed for restoration. ASTM standard is used to test the strength of tensile, compression,
    inflexion, and longitudinal transverse and inter laminar shear of original, defective and repaired samples,
    and then optical microscope was used for the observation. The result indicated that ESA has more negative impact on
    the tensile strength, compression, inflexion of samples, and strength of these defective samples respectively decreased
    by 11. 1%, 13. 8%, 14. 4%; OPA creates more harmful effects on the longitudinal transverse sheared strength, and
    strength of these defective samples decreased by 25. 6%; inter laminar sheared strength is more vulnerable to the LF,
    and strength of these defective samples decreased by 27. 3%. Additionally, the strength of all the five samples is improved
    to a certain degree due to the application of glue-injection method. The improvement of laminates resistance to
    small deformation (tensile, compression and inter laminar shear) for laminates is more significant than large deformation
    (inflexion and longitudinal transverse shear).

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张万卿.注胶法修复5228A/ CF3031 层压板力学性能研究[J].宇航材料工艺,2013,43(6).

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  • 在线发布日期: 2016-11-28
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