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首页> 外文期刊>CERAMICS INTERNATIONAL >Effects of different loading methods on thermal expansion behaviors of 2D cross-ply carbon/carbon composites from 850 ℃ to 2300 ℃
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Effects of different loading methods on thermal expansion behaviors of 2D cross-ply carbon/carbon composites from 850 ℃ to 2300 ℃

机译:850℃至2300℃不同加载方式对二维交联碳/碳复合材料热膨胀行为的影响

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摘要

2D cross-ply carbon/carbon (C/C) composites were prepared by isothermal chemical vapor infiltration (ICVI) process. Thermal expansion behaviors of 2D cross-ply C/C composites and effects of static loading and fatigue loading conditions on coefficient of thermal expansion (CTE) of the C/C composites from 850 ℃ to 2300 ℃ were studied. In static test cases, different damage levels were produced inside samples by displacement-controlled three-point bending loading. Meanwhile, flexural fatigue experiments were conducted under stress level of 70%, cycling numbers (N) of 10~5 and 10~6 at a sinusoidal loading frequency of 15 Hz. Afterwards, the thermal expansion behaviors were investigated. It showed that CTE of the C/C composites after static loading and fatigue loading had a decrease compared with CTE of the as-prepared C/C composites. After static loading, there was a larger decrease in CTE for the C/C composites with more severe damage levels. Moreover, the influence of damage on CTE reached to the greatest at around 1550 ℃. The largest decline percentage of the C/C composites after static loading and fatigue loading was 30% and 85% in contrast to the as-prepared C/C composites, respectively. In addition, weakening interfacial strength of the C/C composites was the main effect on the large decrease of CTE after the fatigue loading.
机译:通过等温化学气相渗透(ICVI)工艺制备了二维交叉碳/碳(C / C)复合材料。研究了二维交联C / C复合材料的热膨胀行为以及静态载荷和疲劳载荷条件对C / C复合材料在850℃至2300℃之间的热膨胀系数(CTE)的影响。在静态测试案例中,通过位移控制的三点弯曲载荷在样品内部产生了不同的损伤水平。同时,在疲劳强度为70%,循环数(N)为10〜5和10〜6的正弦负载频率为15 Hz的情况下进行了弯曲疲劳实验。之后,研究了热膨胀行为。结果表明,与已制备的C / C复合材料相比,C / C复合材料在静载荷和疲劳载荷作用下的CTE有所降低。静载荷后,具有更严重破坏水平的C / C复合材料的CTE下降幅度更大。此外,损伤对CTE的影响在1550℃左右达到最大。与所制备的C / C复合材料相比,C / C复合材料在静态载荷和疲劳载荷之后的最大下降百分比分别为30%和85%。此外,C / C复合材料的界面强度减弱是疲劳载荷后CTE大幅降低的主要影响。

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