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首页> 外文期刊>Проблемы прочностиПроблемы прочности: на рус.укр.и анг.языках >Regularities of main-crack propagation and evolution of dislocation structure in the fracture zone of a VT22 alloy at various cyclic loading frequencies
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Regularities of main-crack propagation and evolution of dislocation structure in the fracture zone of a VT22 alloy at various cyclic loading frequencies

机译:不同循环加载频率的VT22合金裂缝区主裂纹传播与脱位结构的规律

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摘要

A relation between the dislocation structure in the fracture zone and fractographic features of main-crack propagation was studied for a Ti-5%Al-5%V alloy upon cyclic crack-propagation resistance tests with symmetrical tension-compression loading with frequencies of 140 Hz, 600 Hz, 3 kHz, and 10 kHz. Honeycomb and band-type dislocation structures were demonstrated to prevail in the near-threshold region of the ΔK values and in the remaining region of the stress-intensity factor, respectively. The structure this type features the fracture micromechanism by forming fatigue striations, characteristic of the alloy studied. Over the range of low values of ΔK, substructures of the indicated types and thus fatigue striations are most often formed along certain crystallographic planes and directions. With an increase in the ΔK values crystallographic sensitivity of a crack decreases. The influence of loading frequency on the regularities and mechanisms of fatigue crack growth is determined by two basic factors, namely, the processes of plastic deformation at the crack tip during the preparation of a material to fracture and interaction of the crack front with the initial and formed structural and substructural elements. The occurrence of elements of brittle fracture when increasing loading frequency is explained here by an increased sensitivity of the fl-phase to loading rate.
机译:在循环裂纹 - 传播电阻试验时,研究了裂缝区裂缝区和主要裂纹繁殖的裂缝繁殖的裂纹传播的裂缝传播的裂缝特征之间的关系,其具有对称拉伸压缩载荷,频率为140Hz ,600 Hz,3 kHz和10 kHz。蜂窝状和带式脱位结构分别在ΔK值的近阈值区域和应力强度因子的剩余区域中占上足。该结构通过形成疲劳条纹,采用疲劳纹理,对研究的特性进行了裂缝微观机制。在ΔK的低值范围内,所示类型的子结构以及因此疲劳突发件通常沿着一定的晶片和方向形成。随着ΔK值的增加,裂缝的晶体敏感性降低。加载频率对疲劳裂纹生长规律和机制的影响是由两个基本因素确定的,即裂纹尖端在制备物料中的裂纹尖端在裂缝和裂缝前方与初始和突出的相互作用过程中的塑性变形的过程形成的结构和子结构元件。这里通过增加FL相与装载速率的增加时,在此处解释脆性断裂元件的发生。

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