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Fatigue and fracture behavior of (Zr_(58)Ni_(13.6)Cu_(18)Al_(10.4))_(99)Nb_1 bulk-amorphous alloy

机译:(Zr_(58)Ni_(13.6)Cu_(18)Al_(10.4))_(99)Nb_1大块非晶合金的疲劳和断裂行为

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摘要

The fatigue and fracture behaviors of the (Zr_(58)Ni_(13.6)Cu_(18)Al_(10.4))_(99)Nb_1 bulk amorphous alloy are investigated by four-point-bend fatigue tests. The material shows a fatigue-endurance limit and fatigue ratio of 559 MPa and approx 0.328, respectively. The fracture toughness is estimated to be about 26-43 MPa m~(1/2). Shear bands were found to be oriented greater than 45 deg on the tension surface and smaller than 45 deg on the compression surface, with respect to the outer fiber-stress direction of the sample. The density of the shear bands on the tension side is greater than that on the compression side. Many wavy shear bands perpendicular to the outer fiber-stress direction also formed on the tension and compression surfaces during the fatigue process. The fracture surface can be divided into four regions: crack initiation, crack propagation, fast fracture, and melting regions. The fracture mechanism is discussed.
机译:通过四点弯曲疲劳试验研究了(Zr_(58)Ni_(13.6)Cu_(18)Al_(10.4))_(99)Nb_1大块非晶合金的疲劳和断裂行为。该材料的疲劳极限和疲劳比分别为559 MPa和约0.328。断裂韧性估计为约26-43MPa m〜(1/2)。相对于样品的外部纤维应力方向,发现剪切带在拉伸表面上的取向大于45度,在压缩表面上的取向小于45度。拉伸侧的剪切带密度大于压缩侧的剪切带密度。在疲劳过程中,在拉伸和压缩表面上还形成了许多垂直于外部纤维应力方向的波浪形剪切带。断裂面可分为四个区域:裂纹萌生,裂纹扩展,快速断裂和熔化区域。讨论了断裂机理。

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