Nondestructive testing of fiber reinforced polymer-steel interfacial defects based on eddy current thermography
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摘要: 纤维增强树脂(Fiber reinforced polymer,FRP)复合材料已在钢结构加固中得到有效应用,但FRP-钢界面脱粘可能触发结构破坏,需无损检测以保证安全运营。基于自研涡流热成像(Eddy current thermography,ECT)系统对FRP-钢界面缺陷成像规律进行试验,并通过多物理场数值模拟揭示其内部生热和传热机制。试验测试了1个带缺陷试件在ECT下的温度响应,同时模拟了多个不同形状、位置和深度的界面缺陷对热成像的影响。试验表明:ECT系统能在80 s内精确检测试件中328 mm2的界面缺陷;边缘效应影响试件边缘和角部在加热阶段的检测精度,但在冷却阶段由于热量重分布而影响变小;热量沿深度方向传导造成的模糊效应降低了深层缺陷检测精度。本文的多物理场数值模型与试验结果吻合较好,并重现了ECT的边缘效应和模糊效应。基于数值模型的参数化分析,揭示了变化加热速率在一定范围内可克服边缘效应和模糊效应,提高FRP-钢内部缺陷探测精确度。Abstract: Fiber reinforced polymer (FRP) has been effectively used in strengthening steel structures, but FRP-steel interfacial debonding may trigger structural failure. Hence nondestructive testing is required to ensure structural safety. Herein one specimen with FRP-steel interfacial debonding was detected based on a self-developed eddy current thermography (ECT) system, and its heat generation and heat transferring mechanism was revealed through multi-physical numerical simulation. The effect of different shapes, locations and shapes of the defect on the temperature response under ECT was investigated through simulation. The results show that the ECT system can accurately detect 328 mm2 in the specimen within 80 s. The edge effect affects the detection accuracy of the edges and corners of the specimen in the heating stage, but it has little effect due to heat redistribution in the sample in the cooling stage. The blur effect caused by heat conduction along the depth direction reduces the detection accuracy of deep defects. Numerical simulation shows good agreement with the experimental tempera-ture response, and reproduces the edge effect and blur effect of ECT. Parametric study using numerical simulation reveals that the heating rate can overcome the edge effect and blur effect in a certain range and improve the accuracy of FRP-steel interfacial defect detection.
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Material Electromagnetic
properties$ k $/(W·(m·K)−1) $ c $/(J·(g·K)−1) $ \rho $/(kg·m−3) Foam $ {\varepsilon _{\text{r}}} = 1 $ 0.026 1.005 1.204 Epoxy ${\varepsilon _{\text{r} } } \approx 6-0.6{\rm{j} }$ 1.000 3.700 1100 Steel $ {\varepsilon _{\text{r}}} \approx 4.7 - 0.7{\rm{j}} $ 1.700 0.800 2400 CFRP$ \parallel $ $ \sigma = {10^4} $ 7.000 1.200 1600 CFRP$ \perp $ $ {\varepsilon _{\text{r}}} \approx 7 - 2.5{\rm{j}} $ 0.800 1.200 1600 Notes: j—Imaginary unit; $ k $—Thermal conductivity; $ c $—Specific heat; ρ—Density; $ {\varepsilon _{\text{r}}} $—Relative permittivity; $ \sigma $—Electrical conductance; $ \parallel $ and $ \perp $ represent the horizontal and vertical directions of the fibers, respectively. 表 2 试件缺陷详细尺寸
Table 2. Specimen detail size
Specimen Defect types Location Area/mm2 OC Octagon Center 328 OC-M-1 Octagon Center 656 OC-M-2 Octagon Center 216 OC-M-3 Octagon Center 56 OC-W-1 Octagon Right 328 OC-W-2 Octagon Lower right 328 SQ Square Center 400 RH Rhombus Center 100 CI Circle Center 314 -
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