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Investigation of the fatigue crack propagation behaviour in the Al alloy/Hybrid MMC Bi-layer material

机译:Al合金/杂交MMC双层材料中疲劳裂纹繁殖行为的研究

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In this study, the fatigue crack propagation behaviour in the Al alloy-hybrid MMC bi-material system has been investigated. Three-point bending fatigue test is carried out on the Shimadzu servopulser machine. The plastic replica technique is used to observe the crack growth during cyclic loading. The crack growth rate is analyzed at different stress intensity factor range, ΔK. The experimental results showed that the crack growth decelerates in the MMC layer side and maximum crack retardation occurs on the boundary of the bi-material system. Near the boundary of the bi-material, the crack tip becomes curved, which reduces the crack growth rate in the vicinity of the boundary of the bi-material even at higher ΔK. The particle-matrix interfacial debonding, as well as particle fracture, is observed in the hybrid MMC layer during fatigue loading.
机译:在该研究中,研究了Al合金 - 杂交MMC双材料系统中的疲劳裂纹繁殖行为。在Shimadzu Servpucker机器上进行三点弯曲疲劳试验。塑料复制品技术用于观察循环载荷期间的裂纹生长。在不同的应力强度因子范围内分析裂缝生长速率ΔK。实验结果表明,在双层材料系统的边界上发生MMC层侧和最大裂缝延迟的裂缝生长。在双材料的边界附近,裂纹尖端变为弯曲,这使得即使在较高ΔK处也降低了双层材料的边界附近的裂纹生长速率。在疲劳负载期间,在杂交MMC层中观察到颗粒基质界面剥离和颗粒骨折。

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