留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

基于油气两相流的轴承腔封严系统泄漏流动特性研究

任国哲 李延鹏 赵欢 徐文峰 孙丹 燕阳

任国哲, 李延鹏, 赵欢, 等. 基于油气两相流的轴承腔封严系统泄漏流动特性研究[J]. 航空动力学报, 2025, 40(4):20230471 doi: 10.13224/j.cnki.jasp.20230471
引用本文: 任国哲, 李延鹏, 赵欢, 等. 基于油气两相流的轴承腔封严系统泄漏流动特性研究[J]. 航空动力学报, 2025, 40(4):20230471 doi: 10.13224/j.cnki.jasp.20230471
REN Guozhe, LI Yanpeng, ZHAO Huan, et al. Research on flow characteristics of bearing chamber sealing system based on oil-gas two-phase flow[J]. Journal of Aerospace Power, 2025, 40(4):20230471 doi: 10.13224/j.cnki.jasp.20230471
Citation: REN Guozhe, LI Yanpeng, ZHAO Huan, et al. Research on flow characteristics of bearing chamber sealing system based on oil-gas two-phase flow[J]. Journal of Aerospace Power, 2025, 40(4):20230471 doi: 10.13224/j.cnki.jasp.20230471

基于油气两相流的轴承腔封严系统泄漏流动特性研究

doi: 10.13224/j.cnki.jasp.20230471
基金项目: 国家自然科学基金(52075346); 辽宁省“兴辽英才计划”资助项目(XLYC2007077); 通航专项(LJKMZ20220565)
详细信息
    作者简介:

    任国哲(1987-),男,副教授,博士,主要从事航空发动机轴承腔两相流及封严技术研究。E-mail:renguozhe7917@163.com

    通讯作者:

    赵欢(1982-),女,教授,博士,主要从事航空发动机石墨密封技术研究。E-mail:phd_zhaohuan@163.com

  • 中图分类号: V233.5

Research on flow characteristics of bearing chamber sealing system based on oil-gas two-phase flow

  • 摘要:

    为研究航空发动机轴承腔封严系统油气两相流动特性及滑油封严与泄漏特性,建立了基于欧拉-欧拉两相流方法的封严腔-石墨密封-轴承腔封严系统和封严腔-石墨密封-反螺纹结构-轴承腔封严系统非定常求解模型。设计搭建了轴承腔油气两相流动实验装置,通过滑油封严特性实验,验证了求解方法的准确性。在此基础上,研究了不同工况条件下常规轴承腔封严系统和带有反螺纹结构轴承腔封严系统的油气两相泄漏流动特性。研究结果表明:针对常规轴承腔封严系统,转速越高,滑油泄漏量越大。压差越大,滑油泄漏量越小。反螺纹结构可以有效降低轴承腔封严系统滑油泄漏量,转速为15000 r/min,压差为5 kPa时,相对无反螺纹结构的轴承腔封严系统,带有反螺纹结构滑油泄漏量减小95%以上;反螺纹结构的间隙对滑油封严与泄漏特性影响不明显。

     

  • 图 1  实验装置

    Figure 1.  Experimental facility

    图 2  密封长度对临界封油压差影响

    Figure 2.  Length of the seal has an effect on the differential pressure of the critical seal oil

    图 3  常规轴承腔封严系统

    Figure 3.  Conventional bearing chamber sealing system

    图 4  常规轴承腔封严系统网格划分

    Figure 4.  Meshing of conventional bearing chamber sealing system

    图 5  初始油位

    Figure 5.  Initial oil level

    图 6  滑油体积分数随时间变化(常规结构)

    Figure 6.  Volume fraction of oil varies over time(conventional structure)

    图 7  油气两相分布随时间变化 (常规结构,Δp=5 kPa、n=15000 r/min)

    Figure 7.  Effect of time on oil and gas distribution(conventional structure, Δp =5 kPa,n=15000 r/min)

    图 8  滑油体积分数为80%等值面(常规结构, Δp=5 kPa、n=15000 r/min)

    Figure 8.  Isosurface of oil volume fraction is 80% (conventional structure, Δp=5 kPa,n=15000 r/min)

    图 9  轴承腔封严系统二维示意图

    Figure 9.  Two-dimensional schematic diagram of bearing chamber sealing system

    图 10  转速对滑油分布的影响

    Figure 10.  Effect of rotational speed on oil distribution

    图 11  转速对滑油无量纲泄漏量影响 (Δp=1 kPa)

    Figure 11.  Effect of rotational speed on dimensionless oil leakage (Δp=1 kPa)

    图 12  转速对滑油无量纲泄漏量影响 (Δp=5 kPa)

    Figure 12.  Effect of rotational speed on dimensionless oil leakage (Δp=5 kPa)

    图 13  压差对滑油无量纲泄漏量影响(n=0 r/min)

    Figure 13.  Effect of pressure difference on dimensionless oil leakage (n=0 r/min)

    图 14  压差对滑油无量纲泄漏量影响(n=7500 r/min)

    Figure 14.  Effect of pressure difference on dimensionless oil leakage (n=7500 r/min)

    图 15  压差对滑油无量纲泄漏量影响(n=15000 r/min)

    Figure 15.  Effect of pressure difference on dimensionless oil leakage (n=15000 r/min)

    图 16  带有反螺纹结构轴承腔封严系统

    Figure 16.  Bearing chamber sealing system with reverse thread structure

    图 17  滑油体积分数随时间变化(反螺纹结构)

    Figure 17.  Volume fraction of oil varies over time(anti-screw structure)

    图 18  油气两相分布随时间变化(反螺纹结构, Δp=5 kPa、n=15000 r/min)

    Figure 18.  Effect of time on oil and gas distribution(anti-screw structure, Δp=5 kPa, n=15000 r/min)

    图 19  滑油体积分数为80%等值面(反螺纹结构, Δp=5 kPa、n=15000 r/min)

    Figure 19.  Isosurface of oil volume fraction is 80% (anri-screw structure, Δp=5 kPa,n=15000 r/min)

    图 20  滑油体积分数为1%等值面图(Δp=5 kPa、n=15000 r/min)

    Figure 20.  Isosurface of oil volume fraction is 1% (Δp=5 kPa,n=15000 r/min)

    图 21  反螺纹结构对滑油无量纲泄漏量的影响

    Figure 21.  Effect of anti-screw structure on dimensionless oil leakage

    图 22  反螺纹间隙对滑油无量纲泄漏量影响

    Figure 22.  Effect of anti-screw clearance on dimensionless oil leakage

    表  1  试验件结构参数

    Table  1.   Structural parameters of the test piece mm

    参数 数值
    油腔、气腔直径 155
    密封间隙 0.05
    油腔高度 155
    气腔高度 90
    进气口直径 8
    下载: 导出CSV

    表  2  边界条件

    Table  2.   Boundary conditions MPa

    参数数值
    进气口压力0.1~0.2
    通风口压力0.1
    下载: 导出CSV

    表  3  常规轴承腔封严系统结构参数

    Table  3.   Structural parameters of conventional bearing chamber sealing system

    参数 数值
    内径Di/mm 78
    外径Do/mm 98
    密封间隙H1/μm 50
    封严腔宽度L1/mm 25
    轴承腔宽度L2/mm 25
    腔室高度e/mm 10
    密封长度l2/mm 15
    下载: 导出CSV

    表  4  边界设置参数

    Table  4.   Boundary setting parameters

    参数数值
    进气口压力/MPa0.101,0.103,0.105
    进油口流量/(kg/s)0.06
    通风口压力/MPa0.1
    回油口压力/MPa0.1
    转速/(r/min)0,750015000
    下载: 导出CSV

    表  5  反螺纹结构参数

    Table  5.   Structure parameters of anti-screw mm

    参数数值
    齿高2.0
    螺距0.5
    螺纹间隙0.3,0.4,0.5
    下载: 导出CSV
  • [1] 王莉娜,陈国定,孙恒超. 轴承腔油滴沉积特性及油膜流动特征分析[J]. 航空学报,2016,37(10): 3159-3169. WANG Lina,CHEN Guoding,SUN Hengchao. Characteristics analysis of oil droplet deposition and oil film flow in a bearing chamber[J]. Acta Aeronautica et Astronautica Sinica,2016,37(10): 3159-3169. (in Chinese

    WANG Lina, CHEN Guoding, SUN Hengchao. Characteristics analysis of oil droplet deposition and oil film flow in a bearing chamber[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(10): 3159-3169. (in Chinese)
    [2] 孙恒超,陈国定,王莉娜,等. 轴承腔油滴含率及油滴相与空气能量传递分析[J]. 航空学报,2016,37(3): 1060-1073. SUN Hengchao,CHEN Guoding,WANG Lina,et al. Oil droplets fractions and oil droplets/air energy transfer analysis in bearing chamber[J]. Acta Aeronautica et Astronautica Sinica,2016,37(3): 1060-1073. (in Chinese

    SUN Hengchao, CHEN Guoding, WANG Lina, et al. Oil droplets fractions and oil droplets/air energy transfer analysis in bearing chamber[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3): 1060-1073. (in Chinese)
    [3] 王莉娜,陈国定,孙恒超. 轴承腔油滴碰撞腔壁沉积特性分析[J]. 哈尔滨工业大学学报,2017,49(1): 144-149. WANG Lina,CHEN Guoding,SUN Hengchao. Deposition characteristic of the oil droplet on housing in a bearing chamber[J]. Journal of Harbin Institute of Technology,2017,49(1): 144-149. (in Chinese doi: 10.11918/j.issn.0367-6234.2017.01.021

    WANG Lina, CHEN Guoding, SUN Hengchao. Deposition characteristic of the oil droplet on housing in a bearing chamber[J]. Journal of Harbin Institute of Technology, 2017, 49(1): 144-149. (in Chinese) doi: 10.11918/j.issn.0367-6234.2017.01.021
    [4] 方龙,陈国定. 轴承腔油滴/固体壁面斜碰撞的试验及理论研究[J]. 西北工业大学学报,2016,34(4): 627-634. FANG Long,CHEN Guoding. The experimental and theoretical study of oil droplet behaviors after oblique collision in bearing chamber[J]. Journal of Northwestern Polytechnical University,2016,34(4): 627-634. (in Chinese

    FANG Long, CHEN Guoding. The experimental and theoretical study of oil droplet behaviors after oblique collision in bearing chamber[J]. Journal of Northwestern Polytechnical University, 2016, 34(4): 627-634. (in Chinese)
    [5] 李坤,高文君,李宛蓉,等. 锥形轴承腔油气两相流动与换热数值研究[J]. 推进技术,2022,43(11): 210611. LI Kun,GAO Wenjun,LI Wanrong,et al. Numerical study of oil-air two-phase flow and heat transfer in tapered bearing chamber[J]. Journal of Propulsion Technology,2022,43(11): 210611. (in Chinese

    LI Kun, GAO Wenjun, LI Wanrong, et al. Numerical study of oil-air two-phase flow and heat transfer in tapered bearing chamber[J]. Journal of Propulsion Technology, 2022, 43(11): 210611. (in Chinese)
    [6] LU Peng,YE Qihang,FANG Lulu,et al. Research on the air-oil two-phase flow regime in an aeroengine bearing chamber based on Hilbert-Huang transform[J]. Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering,2022,236(1): 24-32. doi: 10.1177/09544100211002956
    [7] 李伟. 轴承腔油气两相流动特性的数值研究[D]. 南京: 南京航空航天大学,2017. LI Wei. Numerical simulation and research on the characteristics of oil/gas two-phase flow in bearing chamber[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2017. (in Chinese

    LI Wei. Numerical simulation and research on the characteristics of oil/gas two-phase flow in bearing chamber[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2017. (in Chinese)
    [8] 任国哲. 基于油气两相流的航空发动机轴承腔流动换热研究及回油结构改进设计[D]. 西安: 西北工业大学,2016. REN Guozhe. Study on flow and heat transfer and optimization of scavenge structure in bearing chamber based on oil/air two-phase flow[D]. Xi'an: Northwestern Polytechnical University,2016. (in Chinese

    REN Guozhe. Study on flow and heat transfer and optimization of scavenge structure in bearing chamber based on oil/air two-phase flow[D]. Xi'an: Northwestern Polytechnical University, 2016. (in Chinese)
    [9] 胡剑平,任国哲,易军,等. 轴承腔内壁与油膜换热的数值模拟与试验[J]. 航空学报,2017,38(9): 521013. HU Jianping,REN Guozhe,YI Jun,et al. Numerical simulation and experiment for heat transfer between oil film and inner wall of bearing chamber[J]. Acta Aeronautica et Astronautica Sinica,2017,38(9): 521013. (in Chinese

    HU Jianping, REN Guozhe, YI Jun, et al. Numerical simulation and experiment for heat transfer between oil film and inner wall of bearing chamber[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(9): 521013. (in Chinese)
    [10] 任国哲,燕阳,郑莞霏,等. 航空发动机轴承腔油气两相流动特性及改进研究[J]. 推进技术,2023,44(11): 2302011. REN Guozhe,YAN Yang,ZHENG Guanfei,et al. Oil-gas two-phase flow characteristics and improvement of bearing chamber for an aeroengine[J]. Journal of Propulsion Technology,2023,44(11): 2302011. (in Chinese

    REN Guozhe, YAN Yang, ZHENG Guanfei, et al. Oil-gas two-phase flow characteristics and improvement of bearing chamber for an aeroengine[J]. Journal of Propulsion Technology, 2023, 44(11): 2302011. (in Chinese)
    [11] WEI Lie,PAN Liangming,ZHAO Yanming,et al. Numerical study of adiabatic two-phase flow patterns in vertical rectangular narrow channels[J]. Applied Thermal Engineering,2017,110: 1101-1110. doi: 10.1016/j.applthermaleng.2016.09.007
    [12] LEE C W,PALMA P C,SIMMONS K,et al. Comparison of computational fluid dynamics and particle image velocimetry data for the airflow in an aeroengine bearing chamber[J]. Journal of Engineering for Gas Turbines and Power,2005,127(4): 697-703. doi: 10.1115/1.1924635
    [13] AIDARINIS J,GOULAS A. Enhanced computational fluid dynamics modeling and laser Doppler anemometer measurements for the air-flow in an aero-engine front bearing chamber: Part Ⅱ[J]. Journal of Engineering for Gas Turbines and Power,2015,137(8): 082502. doi: 10.1115/1.4029365
    [14] ARGHIR M,MARIOT A. Theoretical analysis of the static characteristics of the carbon segmented seal[J]. Journal of Tribology,2017,139(6): 062202. doi: 10.1115/1.4036272
    [15] 胡廷勋,王晓燕,周坤,等. 温度对浮环密封泄漏特性的影响[J]. 推进技术,2022,43(4): 200846. HU Tingxun,WANG Xiaoyan,ZHOU Kun,et al. Effects of temperature on leakage characteristics of floating ring seal[J]. Journal of Propulsion Technology,2022,43(4): 200846. (in Chinese

    HU Tingxun, WANG Xiaoyan, ZHOU Kun, et al. Effects of temperature on leakage characteristics of floating ring seal[J]. Journal of Propulsion Technology, 2022, 43(4): 200846. (in Chinese)
    [16] 马文杰. 高转速环瓣式浮环密封性能研究[D]. 北京: 北京化工大学,2019. MA Wenjie. Research on sealing performance of high speed ring-shaped floating ring[D]. Beijing: Beijing University of Chemical Technology,2019. (in Chinese

    MA Wenjie. Research on sealing performance of high speed ring-shaped floating ring[D]. Beijing: Beijing University of Chemical Technology, 2019. (in Chinese)
    [17] 王佳星. 分瓣式浮环密封性能研究[D]. 北京: 北京化工大学,2020. WANG Jiaxing. Study on the sealing performance of split-floating ring[D]. Beijing: Beijing University of Chemical Technology,2020. (in Chinese

    WANG Jiaxing. Study on the sealing performance of split-floating ring[D]. Beijing: Beijing University of Chemical Technology, 2020. (in Chinese)
    [18] MCGREW J M,MCHUGH J D. Analysis and test of the screw seal in laminar and turbulent operation[J]. Journal of Basic Engineering,1965,87(1): 153-162. doi: 10.1115/1.3650492
    [19] 伊格·叶斯曼. 泵[M]. 黄宗鑫,译. 北京: 石油工业出版社,1956. ESMAN I. Pump[M]. Translated by HUANG Zongxin. Beijing: Petroleum Press,1956. (in Chinese

    ESMAN I. Pump[M]. Translated by HUANG Zongxin. Beijing: Petroleum Press, 1956. (in Chinese)
  • 加载中
图(22) / 表(5)
计量
  • 文章访问数:  489
  • HTML浏览量:  374
  • PDF量:  72
  • 被引次数: 0
出版历程
  • 收稿日期:  2023-07-19
  • 网络出版日期:  2024-10-04

目录

    /

    返回文章
    返回