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High cycle fatigue property of Ti-600 alloy at ambient temperature

机译:Ti-600合金在环境温度下的高循环疲劳性能

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摘要

Smooth axial fatigue tests were carried out at ambient temperature on one kind of near alpha titanium alloy named after Ti-600 at a frequency of 120-130 Hz and with two kinds of load ratios. The high cycle fatigue (HCF) strength for the solutioned and aged alloy is found to be 475 MPa fatigued with a load ratio R of 0.1, and which is 315 MPa with a load ratio R of -1. The observed high HCF strength for the samples fatigued with a load ratio R of 0.1 is attributed to its overlapping fine and thin plate like a+ (3 phase microstructure. During the crack propagation region, at the same stress of 600 MPa, the sample with a fatigue life of 1.78 x 106 cycles has a better fatigue resistance than that of the sample with a fatigue life of 8.61 x 105 cycles, because of its smaller striation distance, its well-developed secondary cracks, more wider and coarsened a lathes precipitated at grain boundaries, and the heavily arranged interlacing transformed (3 microsructures. The average grain size of rare earth phases varies from several micrometers to 0.2 (xm, no cracks corresponding to rare earth particles can be initiated.
机译:在环境温度下对一种以Ti-600命名的近α钛合金以120-130 Hz的频率和两种负载比进行了光滑的轴向疲劳测试。发现固溶和时效合金的高循环疲劳强度(HCF)为475 MPa,负载比R为0.1,疲劳强度为315 MPa,负载比R为-1。疲劳比为0.1的样品观察到的高HCF强度归因于其重叠的薄板和薄板,如a +(3相显微组织。在裂纹扩展区域,在600 MPa的相同应力下,具有1.78 x 106周期的疲劳寿命比8.61 x 105周期的样品具有更好的抗疲劳性,因为其条纹距离更小,二次裂纹发展良好,车削时晶粒更粗和更粗边界,并且交错排列的交错排列(3个微结构。稀土相的平均晶粒尺寸从几微米到0.2(xm)不等,无法引发与稀土颗粒相对应的裂纹。

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