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    超声滚压静压力对20CrNiMo钢表面完整性及疲劳性能的影响

    Effect of Ultrasonic Rolling Static Pressure on Surface Integrity and Fatigue Property of 20CrNiMo Steel

    • 摘要: 采用超声滚压工艺对渗碳+淬回火态20CrNiMo钢试样进行表面强化处理,研究了不同静压力(700,800,900,1 000 N)下试样的表面粗糙度、硬度、残余压应力分布以及旋转弯曲疲劳性能。结果表明:超声滚压后,试样的表面粗糙度明显降低,且随着静压力的增加呈先降低后增加的趋势,当静压力为900 N时,表面粗糙度Ra最低,为0.17 μm。超声滚压后,试样的硬度提高,且随着静压力的增加呈升高趋势。超声滚压在试样表层引入梯度分布的残余压应力;随着静压力的增加,残余压应力最大值先增后降,在静压力为900 N时达到最大,为1 128 MPa。超声滚压后试样的旋转弯曲疲劳寿命显著提高,且随着静压力的增加先增后降。当静压力为900 N时,疲劳寿命最高,达到697.3×104周次,此时疲劳裂纹源为单裂纹源,位于次表层。试样表层残余压应力最大值的变化趋势与疲劳寿命具有高度相关性,是影响疲劳寿命的关键因素。

       

      Abstract: The surface strengthening treatment was carried out on the carburized, quenched and tempered 20CrNiMo steel sample by ultrasonic rolling process. The surface roughness, hardness, residual compressive stress distribution and rotary bending fatigue properties of the sample under different static pressures (700,800,900,1 000 N) were investigated. The results show that the surface roughness of the sample decreased significantly after ultrasonic rolling, and first decreased and then increased with the increase of static pressure. When the static pressure was 900 N, the surface roughness Ra was the lowest (0.17 μm). After ultrasonic rolling, the microhardness of the sample increased, and increased with the increase of static pressure. The residual compressive stress with gradient distribution was introduced into the surface layer of the sample by ultrasonic rolling. With the increase of static pressure, the maximum value of the residual compressive stress first increased and then decreased, reaching the largest value of 1 128 MPa when the static pressure was 900 N. The rotary bending fatigue life of the sample after ultrasonic rolling was significantly improved, and with the increase of static pressure, the fatigue life first increased and then decreased. When the static pressure was 900 N, the fatigue life was the highest, which was 697.3×104 cycles. Under 900 N, the fatigue crack source was a single crack source located in the subsurface. The variation trend of the maximum residual compressive stress in surface layer of the sample was highly correlated with the fatigue life, which was the key factor influencing the fatigue life.

       

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