复合材料基板电热除冰过程的数值模拟模型

Xiaofeng Guo, Zhiqiang Guo, Qiang Yang, W. Dong
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引用次数: 1

摘要

为研究碳纤维增强聚合物(CFRP)复合材料电热除冰过程中基材热性能对除冰过程的影响,建立了CFRP复合材料电热除冰过程的数值模拟模型。采用基于焓孔法的融冰模型,研究了融冰系统的瞬态融冰过程和换热过程。采用含不同纤维取向复合材料的多层电热除冰系统,分析了CFRP复合材料的正交各向异性导热系数对除冰过程和传热的影响。在三维电热除冰装置上研究了CFRP复合材料的冰-水界面运动、融化区厚度和融化区面积。分析了基板热性能对冰翼型界面温度分布的影响。计算结果表明,基板热性能对冰翼型界面温度、基板内温度分布、融冰面积、融冰速率和融冰体积有显著影响。CFRP基板上的冰开始融化的时间比金属基板上的冰开始融化的时间早。然而,冰-碳纤维布界面上的冰完全融化所需的时间比冰-金属界面上的要长。CFRP复合材料的正交各向异性导热性导致冰-CFRP界面上的熔化区具有很强的指向性。定义了一个比率参数来表示衬底材料与除冰系统几何模型的匹配程度。该仿真模型可用于研究复合材料翼型与机舱进气道的电热除冰系统。研究结果也有助于预测除冰过程中的温度变化,为根据复合材料的纤维结构优化电热除冰系统以降低功耗提供指导。
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Numerical Simulation Model of Electrothermal De-Icing Process on Composite Substrate
A numerical simulation model of electrothermal de-icing process on carbon fiber reinforced polymer (CFRP) composite is conducted to study the effect of thermal properties of the substrate on the ice melting process. A novel melting model which is based on the enthalpy-porosity method is applied to study the transient ice melting process and heat transfer of the de-icing sys-tem. Multi-layered electrothermal de-icing systems including composites with different fiber orientation are used to analyze the effects of orthotropic heat conductivity of the CFRP composite on the ice melting process and heat transfer. Movement of the ice-water interface, the melted zone thickness and the melted zone area on CFRP composite are investigated on the three-dimensional electrothermal de-icing unit. The effects of thermal properties of substrate on the temperature distribution of the ice-airfoil interface are analyzed. The computational results show that the thermal properties of substrates affect the temperature on the ice-airfoil interface, the temperature distribution in the substrate, ice melting area, ice melting rate and ice melting volume significantly. The time that ice starts to melt on the CFRP composite substrate is earlier than that on the metal substrate. However, it takes more time for the ice to melt completely on the ice-CFRP interface than that on the ice-metal inter-face. The orthotropic heat conductivity of CFRP composite results in strong directivity of the melting area on the ice-CFRP in-terface. A ratio parameter is defined to represent the matching degree of substrate materials and geometry model of de-icing system. The simulation model can be applied to study electrothermal de-icing system of nacelle inlet and airfoil made of composite. The results in present work is also helpful to predict the change of temperature during de-icing process and provide guidelines for the optimizing the electrothermal de-icing system to reduce power consumption according to the fiber structure of composite.
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