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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Interlaminar Crack Growth Resistances of Various Ceramic Matrix Composites in Mode I and Mode II Loading
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Interlaminar Crack Growth Resistances of Various Ceramic Matrix Composites in Mode I and Mode II Loading

机译:I和II模式下各种陶瓷基复合材料的层间裂纹扩展阻力

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摘要

Interlaminar crack growth resistances were evaluated for five different SiC fiber-reinforced ceramic matrix composites (CMCs) including three gas-turbine grade melt-infiltrated SiC/SiC composites. Modes Ⅰ andⅡ crack growth resistances, G_Ⅰand G_Ⅱ were determined at ambient temperature using double cantilever beam and end notched flexure methods, respectively. The CMCs exhibited G_1=200-500 J/m~2 and G_Ⅱ=200-900 J/m~2. All the composites (except for one SiC/CAS composite) showed a rising R-curve behavior either in modeⅠor in modeⅡ, presumably attributed to fiber bridging (in modesⅠandⅡ) and frictional constraint (modeⅡ) in the wake region of a propagating crack. A glass fiber-reinforced epoxy polymer matrix composite showed typically two to three times greater G_Ⅰ and eight times greater G_Ⅱ, compared to the CMCs. An experimental error analysis regarding the effect of the off-the-center of a crack plane on G_Ⅰ and GⅡ was also made.
机译:评价了五种不同的SiC纤维增强陶瓷基复合材料(CMC)的层间抗裂纹扩展性,其中包括三种燃气轮机级熔渗SiC / SiC复合材料。在室温下分别采用双悬臂梁和端部切口挠曲法测定了Ⅰ,Ⅱ型裂纹扩展阻力G_Ⅰ和G_Ⅱ。 CMC的G_1 = 200-500 J / m〜2和G_Ⅱ= 200-900 J / m〜2。所有复合材料(除了一种SiC / CAS复合材料)在模式Ⅰ或模式Ⅱ中均表现出R曲线的升高,可能归因于纤维裂纹(在模式Ⅰ和Ⅱ中)和摩擦约束(模式Ⅱ)在裂纹扩展的尾波区。与CMC相比,玻璃纤维增​​强的环氧聚合物基质复合材料的G_Ⅰ值通常大两到三倍,G_Ⅱ值大八倍。还对裂纹面偏心对G_Ⅰ和GⅡ的影响进行了实验误差分析。

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