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激光斜冲击对S1100型曲轴疲劳强度的影响
  • 期刊名称:农业机械学报
  • 时间:0
  • 页码:167-169
  • 语言:中文
  • 分类:TN249[电子电信—物理电子学]
  • 作者机构:[1]江苏大学机械工程学院,镇江市212013, [2]中国科技大学物理系研究员,合肥市230026
  • 相关基金:国家自然科学基金资助项目(项目编号:50705038)和江苏大学第六批学生科研课题立项(项目编号:06A133)
  • 相关项目:激光冲击飞机叶片的超高应变率再制造基础研究
中文摘要:

激光冲击加工连杆轴颈与曲柄连接处过渡区域曲面时,激光光束不能保证与曲面上每点切线方向始终垂直,为激光斜冲击强化。用Nd:glass激光器斜冲击强化连杆轴颈与曲柄连接处圆角区域。受冲击区域显微硬度比未冲击区域提高了65%~75%,残余应力提高了80%-100%,使用寿命提高了150%。激光斜冲击曲轴连杆轴颈与曲柄处圆角,残余应力和显微硬度提高最大处为圆角中心处,而这个位置正是易产生疲劳裂纹处,而圆角边缘处是疲劳强度非敏感区,对裂纹的产生影响不大。

英文摘要:

When laser shocks the connecting surface which is a circle angle area between crankshaft connecting rod and crank, it can't make the beam vertical to the tangency direction of each point on the surface, so it is called oblique laser shock processing. In the paper, the laser oblique shocking the connecting surface experiments were carried out via the Nd.glass laser machine at Jiangsu University. The results show that the micro-hardness of the laser shock area increases about 65%-75% than that of non-shock area, the residual stress increases about 80%-100%, and the using life increases about 150%. The biggest increasing area of micro-hardness and the residual stress is the center of the circle angle, which is the area of being easy to produce the fatigue crack. The edge of the circle angle is the non-sensitivity area of the fatigue intension that can't affect the crack producing.

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