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Factors Influencing the Formation of ODA in Ultralong Fatigue Regime

机译:影响超龙疲劳制度中臭臭作取的因素

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The mechanism of fatigue failure in the ultra-high cycle regime was studied using a bearing steel, JIS SUJ2 (SAE 52100). In the case of tension-compression fatigue testing, the S-N curve for high strength steels consisted of a single straight line in contrast to the dual S-N curve observed in rotating bending. The effect of internal hydrogen trapped by nonmetallic inclusions on high cycle fatigue behavior has been discussed by Murakami et al. In order to investigate further the influence of hydrogen trapped by various types of inclusions, four materials of different chemical compositions were prepared. Those specimens having a longer fatigue life had a particular morphology designated as ODA (Optically Dark Area) surrounding the inclusion at the fracture origin. In order to investigate the growth of ODA with cycling, fatigue tests involving multi-step loading were carried out, and the appearance of the ODA was compared with that of specimens tested under a constant amplitude loading. A specimen which endured N = 2 X 10~8 under a stress was fractured by tensile test at -190 deg C. The fracture origin in this tensile test was at a subsurface, nonmetallic inclusion. If the fatigue test had not been interrupted, the potential fatigue life of the specimen was estimated from the size of the inclusion and the ODA using the area~(1/2) parameter model. The model was also used to estimate the fatigue limit in the ultra-high cycle range. The condition for the critical size of ODA for the start of conventional fatigue crack growth was analyzed using fracture mechanics. The critical stress intensity factor range DELTA K_(ODA) for the critical size of the ODA can be correlated with the threshold stress intensity factor range DELTA K_(th) expressed by the area~(1/2) parameter model for small cracks. A fatigue design method for ultra-high fatigue life regime was proposed based upon the growth behavior of the ODA, the statistics of extremes of inclusions, and the area~(1/2) parameter model.
机译:使用轴承钢,JIS SUJ2(SAE 52100)研究了超高循环状态下的疲劳失效机理。在张力压缩疲劳测试的情况下,高强度钢的S-N曲线与单个直线组成,与在旋转弯曲中观察到的双S-N曲线形成对比。 Murakami等人讨论了非金属夹杂物捕获的内部氢气对高循环疲劳行为的影响。为了进一步探讨各种类型的夹杂物捕获的氢气的影响,制备了四种不同化学组合物的材料。具有较长疲劳寿命的那些标本具有指定为围绕裂缝起源的ODA(光学暗区)的特定形态。为了探讨循环的官方OA的生长,进行了涉及多步装载的疲劳试验,并将ODA的外观与在恒定幅度载荷下测试的样品进行比较。通过在-190℃的拉伸试验处破裂在应力下忍受损伤n = 2×10〜8的样品。该拉伸试验中的裂缝起源是在地下的,非金属夹杂物中。如果疲劳试验未被中断,则使用该区域〜(1/2)参数模型从包含和ODA的尺寸估计样本的潜在疲劳寿命。该模型还用于估计超高循环范围内的疲劳极限。使用骨折力学分析了用于开始常规疲劳裂纹裂纹生长的临界大小的临界大小的条件。 ODA的临界大小的临界应力强度因子范围Δk_(oda)可以与由小裂纹的区域〜(1/2)参数模型表示的阈值应力强度因子范围Δk_(th)相关。基于ODA的生长行为,夹杂物极端统计和面积〜(1/2)参数模型提出了一种疲劳设计方法。

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