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Development of matrix cracks in cross-ply laminates under bending and their detection using FBG sensors.

机译:弯曲下交叉层压板中基体裂纹的产生以及使用FBG传感器的检测。

摘要

The development of matrix cracking damage in a double cross-ply laminate under four-point bending has been investigated for both quasi-static and fatigue loading. Under quasi-static loading, crack onset was found to develop at the interface between the outer 0° ply and the adjacent 90° ply on the tension side of the laminate. The cracks initiated at coupon edges and then extended across both the thickness and width of the 90° ply, crack growth occurring In a "stick-slip" manner. Under fatigue loading, additional damage in the form of delaminations developed, especially under "high" fatigue loads and splits developed in the outer 0° ply. The delaminations initiated at the point where the matrix cracks met the outer 0/90 interface. For both quasi-static and fatigue loading, the modulus reduction due to matrix cracking damage was in good agreement with the predictions of a model based on a onedimensional shear-lag analysis. A system for monitoring the output from a fibre Bragg grating sensor located within a 0° ply and near a 0/90 interface was developed, using a broad-band laser source and an optical spectrum analyser. The strain output from the sensors was correlated with measurements of strain in both tension and bending tests, and there was found to be good agreement between the measurements employing the sensor and those using the extensometer. The change in the spectrum recorded using the sensor when matrix cracks developed has been investigated for both tensile tests and bending tests. The reflected signal showed additional peaks on the long wavelength side when a matrix crack developed. These changes have been interpreted qualitatively in terms of the strain magnification experienced locally in the 0° ply due to the presence of the matrix crack. It has thus been shown that fibre Bragg grating sensors can both monitor strain and detect matrix crack development when the matrix cracks develop in the ply adjacent to the position of the sensor.
机译:对于准静态载荷和疲劳载荷,已经研究了在四点弯曲下双交叉层压板中基体开裂损伤的发展。在准静态载荷下,发现在层压板拉伸侧的外部0°帘布层和相邻的90°帘布层之间的界面处出现裂纹开始。裂纹在试样块边缘开始,然后在90°帘布层的厚度和宽度上延伸,裂纹以“粘滑”方式发生。在疲劳载荷下,会产生分层形式的附加损坏,特别是在“高”疲劳载荷下和在0°外侧帘布层产生裂缝的情况下。在基质裂纹与外部0/90界面相遇的点开始分层。对于准静态载荷和疲劳载荷,由于基体裂纹损伤而导致的模量降低与基于一维剪切滞后分析的模型预测非常吻合。开发了一种使用宽带激光源和光谱分析仪来监测位于0°层内且接近0/90接口的光纤布拉格光栅传感器输出的系统。传感器输出的应变与拉伸和弯曲测试中的应变测量值相关,发现使用传感器的测量值与使用引伸计的测量值之间具有良好的一致性。对于拉伸试验和弯曲试验,已经研究了当基质出现裂纹时使用传感器记录的光谱变化。当基体裂纹发展时,反射信号在长波长一侧显示出额外的峰值。这些变化已根据存在基体裂纹的0°层局部经历的应变放大率进行了定性解释。因此已经表明,当基体裂纹在邻近传感器位置的层中发展时,光纤布拉格光栅传感器既可以监测应变又可以检测基体裂纹的发展。

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  • 作者

    Ussorio Mauro.;

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  • 年度 2004
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  • 原文格式 PDF
  • 正文语种 en
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