热残余应力松弛和物理老化引起的CFRP准各向同性层合板的时效变形

Tomoyuki Niwa, Y. Arao, H. Kawada
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引用次数: 1

摘要

本文用经典层合理论预测了由热残余应力松弛和物理老化引起的准各向同性层合板的时变尺寸变化。选择沥青基碳纤维和氰酸酯树脂复合的CFRP材料进行研究。通过横向拉伸蠕变试验研究了单向层合板的粘弹性。此外,还通过测量单向层合板的应变变化,研究了物理时效引起的收缩应变。采用坐标变换法计算了离轴层的收缩应变。测量了60°和45°层合板的收缩应变,并与计算结果进行了比较。通过比较发现,可以用坐标变换法计算离轴层的收缩应变。为了预测准各向同性层合板尺寸随时间的变化,将实验结果应用于经典理论。实验得到了准各向同性层合板的应变变化,并与预测结果进行了比较。结果表明,所提出的预测方法可以用- 2022阶来预测准各向同性层合板的随时间变形。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Time-dependent deformation of CFRP quasi-isotropic laminates caused by relaxation of thermal residual stress and physical aging
In this paper, time-dependent dimensional change in quasi-isotropic laminates induced by relaxation of thermal residual stress and physical aging was predicted by the classical lamination theory. CFRP with pitch-based carbon fiber and cyanate ester resin was chosen for the study. Viscoelastic properties were investigated by performing tensile creep test for unidirectional laminates in the transverse direction. In addition, shrinkage strain induced by physical aging was studied by measuring the strain change of unidirectional laminates as well. Shrinkage strain in off–axis layers was calculated by using the coordinate-transform method. Shrinkage strain in 60° and 45° laminates were measured and the results were compared with the calculation. From the comparison, it was found that shrinkage strain of off-axis layers can be calculated by using the coordinate-transform method. Experimental results were applied to the classical theory in order to predict the time-dependent dimensional change of quasi-isotropic laminates. The strain change in quasi-isotropic laminates was obtained experimentally, and the result was compared with the prediction. It was verified that the time-dependent deformation of quasi-isotropic laminates can be predicted with a -order by using proposed prediction method.
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