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Experimental investigation of fatigue crack growth in the welding nugget of FSW joints of a 6060 Aluminum Alloy

机译:6060铝合金FSW接头焊接熔核疲劳裂纹扩展的实验研究。

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The work investigates the fatigue behavior of friction stir welded butt joints by means of fracture mechanics techniques. FSW joints of artificially aged AA6060 T6 aluminum alloy were studied. The welding was performed on 8 mm thick butt joined sheets by means of a CNC machine tool. Welding speed in the range between 117 and 683 mm/min and tool rotational speed between 838 and 1262 rpm were considered. Fatigue crack growth tests were performed according to ASTM E647 standard on CT specimens, under constant load amplitude conditions, at 0.1 minimum to maximum load ratio, with the notch placed in the dynamic recrystallization zone of weld nugget, oriented along the welding direction. The comparison of results demonstrates the crack growth rate is always equal or lower than the base material at low values of stress intensity range. At △K. values above 12 MPa√m, crack growth rate was found to be higher than base material for high feed, low speed and high feed/speed ratio.
机译:这项工作通过断裂力学技术研究了搅拌摩擦对接焊缝的疲劳行为。研究了人工时效AA6060 T6铝合金的FSW接头。借助于CNC机床在8mm厚的对接接合板上进行焊接。考虑的焊接速度为117至683 mm / min,工具转速为838至1262 rpm。根据ASTM E647标准,在恒定载荷振幅条件下,以最小与最大载荷比为0.1的条件,对CT试样进行疲劳裂纹扩展测试,将缺口置于沿焊接方向定向的焊点熔核动态再结晶区中。结果比较表明,在较低的应力强度范围内,裂纹扩展速率始终等于或低于基础材料。在△K。当高进给,低速和高进给/速比时,当值大于12MPa√m时,发现裂纹扩展速率高于基础材料。

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