空心芯棒服役过程温度场及热疲劳有限元分析

    Finite Element Analysis on Temperature Field and Thermal Fatigue of Hollow Mandrel in Servicing Process

    • 摘要: 针对Φ340 mm MPM机组芯棒服役过程建立三维有限元模型,设计空心芯棒内径尺寸,分析空心芯棒服役过程温度场和空心芯棒表面热疲劳。分析认为:对于外径为358.1 mm的空心芯棒来说,内径在200~240 mm时能较好地平衡减重和控制变形;内径为214 mm的空心芯棒,在轧制、第1次空冷、第1次水冷3个阶段的温度场与实心芯棒相同区域的温度场基本一致,而在其他各服役阶段时的内表面温度比实心芯棒相同位置处高13~18℃。空心芯棒与实心芯棒的热应力的差别,导致空心芯棒的环向和轴向裂纹比实心芯棒萌生更早、扩展速度更快。

       

      Abstract: Based on the servicing process of the hollow mandrel of the Φ340 mm MPM,a 3-D FE mathematic model is set up.with which the ID dimensions of the mandrel is designed,and the temperature field and surface thermal fatigue of it in servicing process are analyzed.The analysis result reveals the facts as follows.For the hollow mandrel with OD as 358.1 mm,in case of ID as 200~240 mm,balance weight reduction and deformation control are better obtained,while in case of ID as 214 mm,the temperature fields of the hollow mandrel at the three phases i.e.,rolling,the first air cooling and the first water cooling are almost the same as those of the solid mandrel at the same phases.However at the other servicing phases the inner surface temperatures of the former are 13~18 ℃ higher than those of the solid mandrel at the same positions.It is also revealed that the difference between the thermal stress of the hollow mandrel and that of the solid one leads to the result that both the circular and axial cracks of the former are developed earlier,and extended faster than those of the latter.

       

    /

    返回文章
    返回