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环下润滑供油通道流量分配特性的数值研究

朱泽韬 吕亚国 朱鹏飞 曹逸韬 刘振侠

朱泽韬, 吕亚国, 朱鹏飞, 等. 环下润滑供油通道流量分配特性的数值研究[J]. 航空动力学报, 2025, 40(1):20230255 doi: 10.13224/j.cnki.jasp.20230255
引用本文: 朱泽韬, 吕亚国, 朱鹏飞, 等. 环下润滑供油通道流量分配特性的数值研究[J]. 航空动力学报, 2025, 40(1):20230255 doi: 10.13224/j.cnki.jasp.20230255
ZHU Zetao, LYU Yaguo, ZHU Pengfei, et al. Numerical study on flow distribution characteristics of under-race lubrication oil passage[J]. Journal of Aerospace Power, 2025, 40(1):20230255 doi: 10.13224/j.cnki.jasp.20230255
Citation: ZHU Zetao, LYU Yaguo, ZHU Pengfei, et al. Numerical study on flow distribution characteristics of under-race lubrication oil passage[J]. Journal of Aerospace Power, 2025, 40(1):20230255 doi: 10.13224/j.cnki.jasp.20230255

环下润滑供油通道流量分配特性的数值研究

doi: 10.13224/j.cnki.jasp.20230255
基金项目: 国家科技重大专项(J2019-Ⅲ-0023-0067)
详细信息
    作者简介:

    朱泽韬(1997-),男,博士生,主要从事航空发动机润滑系统两相流研究

    通讯作者:

    吕亚国(1980-),男,副教授,博士,主要从事航空发动机润滑系统研究。E-mail:yglu@nwpu.edu.cn

  • 中图分类号: V233.4

Numerical study on flow distribution characteristics of under-race lubrication oil passage

  • 摘要:

    为探究环下润滑供油通道滑油流量分配特性,采用volume of fluid(VOF)方法对轴心射流收油环内部两相流动进行了计算,获得了供油通道内油膜形成过程与流场特征,重点讨论了供油温度、主轴转速、供油流量及供油孔径组合对流量分配的影响规律,建立了临界孔径比的无量纲关联式。结果表明:滑油射流冲击收油环中心后形成油膜,其边缘断裂形成油带、油矢甩至侧壁面,最终油膜铺满整个端面;计算工况范围内,滑油分配主要受供油流量及孔径影响,各出口流量随供油流量上升均呈线性增加,滑油分配比随供油流量增加而平均降低15.05%;滑油分配比随下游孔径与孔径比的增加而上升;当无量纲供油流量越大且下游无量纲孔径越小时,临界孔径比越高并趋近于1,当无量纲供油流量降低或下游无量纲孔径增大时,临界孔径比则下降。

     

  • 图 1  环下润滑结构模型

    Figure 1.  Under-race lubrication structure model

    图 2  计算模型及网格

    Figure 2.  Computational model and mesh

    图 3  时间步长独立性验证

    Figure 3.  Independence verification of time step

    图 4  旋转流道网格

    Figure 4.  Mesh of rotating tube

    图 5  流量实验值与计算值的比较

    Figure 5.  Comparison of experimental and calculative results of volume flow rate

    图 6  供油孔编号说明

    Figure 6.  Oil hole number description

    图 7  收油环壁面滑油迁移过程

    Figure 7.  Oil migration process at end surface of oil receiving scoop

    图 8  供油通道内滑油分布

    Figure 8.  Distribution of oil in the oil passage

    图 9  供油通道内速度分布

    Figure 9.  Distribution of velocity in the oil passage

    图 10  不同供油流量下温度对1号孔流量的影响

    Figure 10.  Effects of oil temperature on volume flow rate of outlet 1 at different oil volume flow rates

    图 11  不同供油流量下滑油温度对滑油分配比的影响

    Figure 11.  Effects of oil temperature on oil distribution ratio at different oil volume flow rates

    图 12  不同孔径比下转速对1号孔流量的影响

    Figure 12.  Effects of rotating speed on volume flow rate of outlet 1 at different aperture ratios

    图 13  不同孔径比下转速对滑油分配比的影响

    Figure 13.  Effects of rotating speed on oil distribution ratio at different aperture ratios

    图 14  不同孔径比下供油流量对各孔流量的影响

    Figure 14.  Effects of oil volume flow rate on oil volume flow rate of each outlet at different aperture ratios

    图 15  不同孔径比下供油流量对滑油分配比的影响

    Figure 15.  Effects of oil volume flow rate on oil distribution ratio at different aperture ratios

    图 16  不同流量下孔径比对各孔流量的影响

    Figure 16.  Effects of aperture ratio on oil volume flow rate of each outlet at different oil volume flow rates

    图 17  不同流量下孔径比对滑油分配比的影响

    Figure 17.  Effects of aperture ratio on oil distribution ratio at different oil volume flow rates

    图 18  不同下游孔径下孔径比对各孔流量的影响

    Figure 18.  Effects of aperture ratio on oil volume flow rate of each outlet at different downstream apertures

    图 19  不同孔径比下下游孔径对分配比的影响

    Figure 19.  Effects of downstream aperture on oil distribution ratio at different aperture ratios

    图 20  临界孔径比拟合面

    Figure 20.  Fitting surface of critical aperture ratio

    图 21  各无量纲孔径下无量纲流量对临界孔径比的影响

    Figure 21.  Effects of dimensionless oil volume flow rate on critical aperture ratio at different dimensionless apertures

    表  1  收油环结构参数

    Table  1.   Structure parameters of oil receiving scoop mm

    参数数值
    收油环内径40
    收油环外径50
    供油孔间距10
    供油孔直径1.0
    供油孔长度5.0
    下载: 导出CSV

    表  2  滑油物性参数

    Table  2.   Oil physical parameters

    温度/℃密度/(kg/m3运动黏度/(mm2/s)
    60968.812.94
    75957.19.05
    90945.66.24
    105932.84.42
    120920.43.30
    下载: 导出CSV

    表  3  旋转流道主要尺寸

    Table  3.   Main dimensions of rotating tube mm

    位置 直径 长度
    入口 6.35 25.4
    分支出口 A 6.35 25.4
    分支出口B 6.35 25.4
    旋流通道 12.7 469.9
    下载: 导出CSV

    表  4  不同参数组合下的临界孔径比

    Table  4.   Critical aperture ratio at different parameter combinations

    Nq $ {R'_{\text{d}}} $
    Nd=1.0 Nd=1.2 Nd=1.5 Nd=2.0
    1.0 0.836 0.773 0.705 0.621
    1.2 0.878 0.809 0.746 0.665
    1.3 0.885 0.835 0.761 0.687
    1.5 0.901 0.851 0.776 0.706
    1.6 0.922 0.862 0.799 0.723
    1.8 0.944 0.887 0.809 0.745
    2.0 0.951 0.893 0.832 0.757
    下载: 导出CSV
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  • 收稿日期:  2023-04-17
  • 网络出版日期:  2024-09-14

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