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Fatigue Fracture Characteristics of Ti6Al4V Subjected to Ultrasonic Nanocrystal Surface Modification

机译:超声纳米晶表面改性对Ti6Al4V的疲劳断裂特性

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The influence of ultrasonic nanocrystal surface modification (UNSM) on the fatigue fracture characteristics of Ti6Al4V was investigated. Two groups of specimens were separated due to different heat treatment conditions. Group one was stress-relief annealed at 650 °C, and group two was then treated with solid solution-aging. UNSM with the conditions of a static load of 25 N, vibration amplitude of 30 μm, and 36,000 strikes per unit produced about 40 μm surface severe plastic deformation (SPD) layers on both groups of specimens. UNSM improved the microhardness and the compressive residual stress. UNSM also helped achieve a neat surface, almost without changing the surface roughness. The fatigue strengths of these two groups were improved by 7% and 11.7%, respectively. After UNSM, fatigue cracks mainly initiated from the surface of the specimen before the fatigue life of 10 6 cycles, while they appeared at the internal compress deformed α-phase at the zone between the SPD layer and the core after the fatigue life of 106 cycles. The cracks usually extended along the deformation overflow bands and the process traces on the surface. Through the change of micro-dimples in the fatigue final rupture region, nanocrystals were achieved in the SPD layer. The crystal slip and the surface remodeling together influenced the energy field of crack evolution.
机译:研究了超声纳米晶体表面改性(UNSM)对Ti6Al4V疲劳断裂特性的影响。由于热处理条件的不同,将两组样品分开。第一组在650°C下进行应力消除退火,然后第二组进行固溶时效处理。在25 N的静载荷,30μm的振动幅度和每单位36,000次冲击的条件下,UNSM在两组样品上产生约40μm的表面严重塑性变形(SPD)层。 UNSM改善了显微硬度和压缩残余应力。 UNSM还帮助实现了整洁的表面,几乎不改变表面粗糙度。两组的疲劳强度分别提高了7%和11.7%。在UNSM之后,疲劳裂纹主要在10 6个循环的疲劳寿命之前从试样表面开始,而在106个循环的疲劳寿命之后,它们出现在SPD层与铁心之间区域的内部压缩变形α相中。 。裂纹通常沿着变形溢出带延伸,并且表面上出现过程痕迹。通过改变疲劳最终断裂区域中的微凹坑,在SPD层中获得了纳米晶体。晶体滑移和表面重塑一起影响了裂纹扩展的能量场。

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