端面变形锥角对干气密封性能影响的数值模拟
Numerical Simulation of the Influence of the Angle of End Face Gap on the Performance of Dry Gas Seal
作者:陈志(四川大学 化学工程学院, 四川 成都 610065);赵鹏(四川大学 化学工程学院, 四川 成都 610065);王金红(四川大学 化学工程学院, 四川 成都 610065);吉华(四川大学 化学工程学院, 四川 成都 610065)
Author:CHEN Zhi(College of Chemical Eng., Sichuan Univ., Chengdu 610065, China);ZHAO Peng(College of Chemical Eng., Sichuan Univ., Chengdu 610065, China);WANG Jinhong(College of Chemical Eng., Sichuan Univ., Chengdu 610065, China);JI Hua(College of Chemical Eng., Sichuan Univ., Chengdu 610065, China)
收稿日期:2017-07-23 年卷(期)页码:2018,50(1):203-210
期刊名称:工程科学与技术
Journal Name:Advanced Engineering Sciences
关键字:干气密封;楔形间隙;螺旋槽;气膜流场;数值模拟
Key words:dry gas seal;wedge gap;spiral groove;gas film flow field;numerical simulation
基金项目:无
中文摘要
多数干气密封端面流场分析是在假设平行间隙的前提下进行的,而工作状态下由于力变形和热变形的共同作用,两密封环的端面呈近似线性收敛型的楔形间隙。作者对平行及不同锥角的收敛型气膜流场进行了模拟分析,讨论了端面变形锥角对干气密封性能的影响。使用ANSYS软件对气膜流场模型进行前处理,对于流场中气体密度和黏度的变化,采用用户自定义函数(UDF)将密封介质的密度和黏度定义为压力的函数,再利用Fluent软件对气膜流场进行数值模拟计算。发现本文采用的变密度变黏度方法对干气密封楔形气膜流场的模拟是可行的。收敛型气膜锥角β使气膜径向压力分布发生改变,压力分布为连续光滑的上凸曲线。与平行间隙对比,发现其螺旋槽槽根处的压力明显下降,但随着β的增大,压力下降速度越来越缓。在相同的工况下,随着β的增大,总体气膜厚度增加,而端面内径处膜厚先减小后增加,外径处膜厚和泄漏量随着锥角的增大一直增加,并且在某一锥角后泄漏量增加明显。在0≤ β≤ 0.000 50 rad的范围内得出膜厚和泄漏率与β的关系式,并建议0≤ β≤0.000 30 rad。随着β的增大,端面螺旋槽产生的气体动压效应作用减弱,而端面径向楔形效应作用增强并起到使端面开启的主导作用。
英文摘要
The flow field analysis of most dry gas seal end faces is carried out on the assumption of parallel gap for end faces.But because of the force deformation and thermal deformation working together,the gap between the end faces of two sealing rings is almost linearly convergent.The gas film flow fields for parallel gap and convergent wedge gaps with different angles were simulated and analyzed.ANSYS is used to pretreat the gas film flow field model.For the changes of gas density and viscosity in the flow field,the user-defined function (UDF) was used to define the density and viscosity of sealing medium as pressure functions.Fluent software was used for numerical simulation of the flow field of gas film.It was found that the variable density viscosity method used is feasible for the simulation of wedge flow field for a dry gas seal.The change of the convergent angleβof gas film alteres the radial pressure profile.The pressure profile was a continuous and smooth convex curve.The peak pressure at the spiral groove root decreases obviously comparing with that for the parallel film gap.With the increase of gas film taper angle,the decreasing speed of peak pressure became slower and slower.Under the same working conditions,with the increase ofβ,the total film thickness increases,the film thickness at the inner end of the face first decreases and then increases and the film thickness at the outside diameter and leakage increases.The leakage increases obviously whenβis greater than the given value.When 0≤β≤0.000 50 rad,the relationships between film thickness and leakage rate withβwere given,respectively.It was suggested that 0≤β≤0.000 30 rad.With the increase ofβ,the dynamic pressure effect of the gas in the helical groove is weakened and the radial wedge effect between the end faces is enhances,which causes both end faces to open.
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