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Stress-life fatigue behavior and fracture-surface morphology of a Cu-based bulk-metallic glass

机译:铜基大块金属玻璃的应力寿命疲劳行为和断口形貌

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The stress-life fatigue behavior and fracture morphology of a (Cu_(60)Zr_(30)Ti_(10))_(99)Sn_1 bulk-metallic glass alloy was investigated under both three-point and four-point bending conditions. For all stress levels tested, the fatigue lifetimes tended to be higher for the three-point loading condition. The fatigue endurance limits (defined as 10~7 cycles without failure), based on the applied stress range, for three-point and four-point loading conditions were approximately 475 MPa and 350 MPa, respectively. All fracture surfaces were found to be composed of four main regions: a crack-initiation site, a stable crack-growth region, an unstable fast-fracture region, and a melting region. Finely spaced parallel marks, similar to fatigue striations found in crystalline alloys, oriented somewhat perpendicular to the direction of crack propagation were observed in the stable crack-growth region. Analyses of these marks found that their spacing increased with increasing stress-intensity-factor range. Damage was found to initiate from preexisting defects present on or near the surface.
机译:研究了(Cu_(60)Zr_(30)Ti_(10))_(99)Sn_1大块金属玻璃合金在三点和四点弯曲条件下的应力寿命疲劳行为和断裂形态。对于所有测试的应力水平,三点载荷条件下的疲劳寿命趋于更高。基于施加的应力范围,三点和四点载荷条件下的疲劳耐久性极限(定义为10到7个循环,无故障)分别约为475 MPa和350 MPa。发现所有断裂表面均由四个主要区域组成:裂纹形成部位,稳定的裂纹扩展区域,不稳定的快速断裂区域和熔化区域。在稳定的裂纹扩展区域中观察到细间距的平行标记,类似于在结晶合金中发现的疲劳条纹,其取向略微垂直于裂纹扩展的方向。对这些标记的分析发现,它们的间距随着应力强度因子范围的增加而增加。发现损坏是由表面上或表面附近存在的预先存在的缺陷引起的。

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