利用数字图像相关分析确定未固化单向 CF/Epoxy 预浸料的平面内剪切行为及其工艺影响

Hongfu Li, Haoxuan Zhang, Guangquan Yue, Boyu Guo, Ying Wu
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摘要

研究预浸料的面内剪切行为对于了解自动纤维铺放和热成型等先进复合材料制造工艺中预成型件皱纹的产生至关重要。尽管意义重大,但目前还没有用于表征未固化单向(UD)预浸料的标准化测试方法。本文介绍了一种 ±45° 离轴拉伸试验,旨在评估 UD 碳纤维增强环氧树脂预浸料(CF/环氧树脂)的面内剪切行为。采用数字图像相关技术(DIC)定量跟踪拉伸过程中的三维应变和剪切角演变。还进一步研究了温度和拉伸速率对预浸料平面内剪切行为的影响。研究结果表明,预浸料具有明显的四个剪切特征区和起皱行为。由于纤维在面内和面外两方面的限制,实际面内剪切角明显低于理论值。当离轴拉伸位移 (d) 小于 15.6 mm 时,±45° 试样主要表现出宏观的面内剪切行为,这是由 +45° 层和 -45° 层之间的层间界面剪切在中尺度上引起的。然而,当 d > 15.6 mm 时,开始出现纤维挤压和起皱。当 d > 29 mm 时,面内剪切在完全剪切区(A)消失。温度升高导致 CF/epoxy 预浸料的树脂粘度降低,被认为是降低面内剪切力阻力的主要因素,其次是树脂固化度升高的影响。较高的剪切速率会导致剪切力大幅增加,最终导致预浸料开裂失效。研究结果证明了预测和提取未固化预浸料平面内剪切行为以及材料响应的应变速率和温度依赖性的测试方法的可行性。
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Determination of the In-Plane Shear Behavior of and Process Influence on Uncured Unidirectional CF/Epoxy Prepreg Using Digital Image Correlation Analysis
The investigation of the in-plane shear behavior of prepreg is crucial for understanding the generation of wrinkles of preforms in advanced composite manufacturing processes, such as automated fiber placement and thermoforming. Despite this significance, there is currently no standardized test method for characterizing uncured unidirectional (UD) prepreg. This paper introduces a ±45° off-axis tensile test designed to assess the in-plane shear behavior of UD carbon fiber-reinforced epoxy prepreg (CF/epoxy). Digital image correlation (DIC) was employed to quantitatively track the strains in three dimensions and the shear angle evolution during the stretching process. The influences of the temperature and stretching rate on the in-plane shear behavior of the prepreg were further investigated. The results reveal that four shear characteristic zones and wrinkling behaviors are clearly distinguished. The actual in-plane shear angle is significantly lower than the theoretical value due to fiber constraints from both the in-plane and out-of-plane aspects. When the off-axis tensile displacement (d) is less than 15.6 mm, the ±45° specimens primarily exhibit macroscale in-plane shear behavior, induced by interlaminar interface shear between the +45° ply and −45° ply at the mesoscale. The shear angle increases linearly with the d. However, when d > 15.6 mm, fiber squeezing and wrinkling begin to occur. When d > 29 mm, the in-plane shear disappears in the completely sheared zone (A). The reduction in the resin viscosity of the CF/epoxy prepreg caused by increased temperature is identified as the primary factor in lowering the in-plane shear force resistance, followed by the effect of the increasing resin curing degree. Higher shear rates can lead to a substantial increase in shear forces, eventually causing cracking failure in the prepreg. The findings demonstrate the feasibility of the test method for predicting and extracting uncured prepreg in-plane shear behaviors and the strain-rate and temperature dependency of the material response.
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