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Observations of Fatigue Slip-Band Growth and Crack Initiation in alpha-Brass under Cyclic Shear Stresses by Means of Atomic-Force Microscopy

机译:循环剪切应力下的抗疲劳滑带生长和裂纹引发的观察借助原子力显微镜

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摘要

Slip-band formation and crack-initiation processes in a-brass under cyclic shear stress were examined by means of atomic force microscopy (AFM), and the slip-direction was identified with orientation imaging microscope (OIM). From AFM observations, it was found that slip-bands were not always formed along the maximum resolved shear stress directions, and slip-systems could be activated in the direction whose angles from the surface were larger than 22 deg. The depth of an intrusion increased linearly with the logarithm of the number of cycles, and the increasing rate of the intrusion depth drastically increased with its outgrowth to a crack. By combining the intrusion depth and the slip direction, those were measured with AFM and OIM, respectively, the value of slip distance could be evaluated, and the critical values of the slip distance for the initiation of transgranular crack was found to be constant for all crack initiation sites, while the intrusion depth was not constant. The critical value of the slip distance for cyclic shear stress (torsion) was identical for cyclic normal stress (bending). A unique relationship between shear stress amplitude in the slip direction and number of cycles to failure was obtained for cyclic torsion and bending loadings.
机译:通过原子力显微镜(AFM)检查循环剪切应力下的循环剪切应力下的防滑带形成和裂纹引发过程,并用取向成像显微镜(OIM)鉴定滑动方向。从AFM观察结果,发现滑动带并不总是沿着最大分辨的剪切应力方向形成,并且可以在从表面角度大于22°的方向上启动滑动系统。侵入的深度随着循环次数的对数而线性增加,并且入侵深度的增加率随着其远离裂缝而大大增加。通过组合入侵深度和滑动方向,分别用AFM和OIM测量那些,可以评价滑移距离的值,并且发现对旋转裂纹开始的滑移距离的临界值是恒定的裂缝起始位点,而入侵深度不是恒定的。循环剪切应力(扭转)的滑移距离的临界值与循环正常应力(弯曲)相同。获得了滑动方向上的剪切应力幅度与失效循环数之间的独特关系,用于循环扭转和弯曲载荷。

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