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ENHANCING THE THROUGH-THICKNESS THERMAL CONDUCTIVITY OF CARBON FIBER POLYMER-MATRIX COMPOSITES

机译:提高碳纤维聚合物 - 基质复合材料的贯穿厚度导热系数

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The thermal load of aircraft is increasing [1]. Carbon fiber composites have high in-plane thermal conductivity, but low through-thickness conductivity. Because a carbon fiber is anisotropic, the thermal conductivity of a lamina is much higher in the fiber direction of the lamina than in the transverse direction. A structural composite involves fibers in different directions for different laminae. Therefore, the thermal conductivity of a structural composite is high in all in-plane directions, such that the conductivity is limited by the axial thermal conductivity of the fiber. On the other hand, the through-thickness thermal conductivity is much lower.
机译:飞机的热负荷增加[1]。碳纤维复合材料具有高面内导热率,但贯穿厚度的导电性低。因为碳纤维是各向异性的,所以薄层的导热率在薄层的纤维方向上比横向升高得多。结构复合材料涉及不同薄层的不同方向的纤维。因此,在所有面内方向上的结构复合材料的导热率高,使得导电性受到纤维的轴向导热率的限制。另一方面,贯穿厚度的导热率低得多。

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