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

浅槽动压整体式浮环密封静力与动力特性数值研究

赵欢 姜金裕 孙丹 王双 李延鹏

赵欢, 姜金裕, 孙丹, 等. 浅槽动压整体式浮环密封静力与动力特性数值研究[J]. 航空动力学报, 2024, 39(9):20220697 doi: 10.13224/j.cnki.jasp.20220697
引用本文: 赵欢, 姜金裕, 孙丹, 等. 浅槽动压整体式浮环密封静力与动力特性数值研究[J]. 航空动力学报, 2024, 39(9):20220697 doi: 10.13224/j.cnki.jasp.20220697
ZHAO Huan, JIANG Jinyu, SUN Dan, et al. Numerical study on static and dynamic characteristics of an integral floating ring seal with shallow groove dynamic pressure[J]. Journal of Aerospace Power, 2024, 39(9):20220697 doi: 10.13224/j.cnki.jasp.20220697
Citation: ZHAO Huan, JIANG Jinyu, SUN Dan, et al. Numerical study on static and dynamic characteristics of an integral floating ring seal with shallow groove dynamic pressure[J]. Journal of Aerospace Power, 2024, 39(9):20220697 doi: 10.13224/j.cnki.jasp.20220697

浅槽动压整体式浮环密封静力与动力特性数值研究

doi: 10.13224/j.cnki.jasp.20220697
基金项目: 国家自然科学基金(52075346); 先进航空动力创新工作站(依托中国航空发动机研究院设立)项目(HKC2020-02-030); 中国航空发动机集团产学研合作项目(HFZL2021CXY012)
详细信息
    作者简介:

    姜金裕(1998-),男,硕士生,主要研究方向为密封静力与动力特性。E-mail:18842822199@163.com

    通讯作者:

    孙丹(1981-),男,教授,博士,主要从事航空发动机先进密封技术研究。E-mail:phd_sundan@163.com

  • 中图分类号: V233.5

Numerical study on static and dynamic characteristics of an integral floating ring seal with shallow groove dynamic pressure

  • 摘要:

    建立了浅槽动压整体式浮环密封静力与动力特性多频椭圆涡动求解模型,在验证数值计算方法准确性的基础上,分析了无槽、矩形槽、螺旋槽及T型槽4种结构整体式浮环密封的静力与动力特性,研究了不同结构与工况参数下的整体式浮环密封泄漏量、浮升力以及动力特性的变化规律,分析了槽型对整体式浮环密封转子稳定性的影响,揭示了动压槽型对整体式浮环密封动力特性的影响机理。研究结果表明,泄漏量与浮升力随着偏心率的增加而增大,相较于无槽浮环密封,矩形槽泄漏量最大,T型槽的浮升力最大,为无槽浮升力的434.7%;在同一涡动频率下,矩形槽的有效阻尼最大且为正值,切向气流力与转子涡动方向相反,从而抑制转子的涡动,提高转子稳定。

     

  • 图 1  整体式浮环密封装置

    Figure 1.  Integral floating ring seal device

    图 2  整体式浮环密封槽型结构

    Figure 2.  Integral floating ring seal groove structures

    图 3  椭圆轨迹涡动模型

    Figure 3.  Vortex model of elliptical trajectory

    图 4  整体式浮环密封三维结构示意图

    Figure 4.  Three-dimensional structure diagram of the integral floating ring seal

    图 5  网格示意图

    Figure 5.  Grid diagram

    图 6  数值计算结果对比验证

    Figure 6.  Comparison and verification of numerical results

    图 7  浮环密封压力分布云图

    Figure 7.  Pressure distribution contour of floating ring seal

    图 8  浮环密封压力差大小柱状图

    Figure 8.  Pressure difference bar diagram of floating ring seal

    图 9  泄漏量随不同工况变化图

    Figure 9.  Variation of leakage with different working conditons

    图 10  整体式浮环密封浮环受力分析图

    Figure 10.  Force analysis diagram of integral floating ring seal floating ring

    图 11  浮升力随不同工况变化图

    Figure 11.  Diagram of lifting force variation with different working conditions

    图 12  直接刚度变化图

    Figure 12.  Variation diagram of direct stiffness

    图 13  交叉刚度变化图

    Figure 13.  Variation diagram of cross stiffness

    图 14  直接阻尼变化图

    Figure 14.  Variation diagram of direct damping

    图 15  交叉阻尼变化图

    Figure 15.  Variation diagram of cross damping

    图 16  有效阻尼的变化图

    Figure 16.  Variation diagram of effective damping

    图 17  有效刚度变化图

    Figure 17.  Variation diagram of effective stiffness

    图 18  整体式浮环密封转子面流体激振力矢量图

    Figure 18.  Fluid excitation force vector diagram of integral floating ring seal rotor surface

    表  1  密封模型几何尺寸

    Table  1.   Dimension of seal model

    参数 数值
    转子直径ϕr/mm 53.0
    浮环内表面直径ϕf/mm 53.2
    密封间隙h/mm 0.10
    密封环长度L/mm 8.0
    密封环高度E/mm 4.5
    槽种类/种 3
    槽数量/个 16
    槽深τ/mm 0.10
    槽长l/mm 5.50
    下载: 导出CSV

    表  2  边界条件

    Table  2.   Boundary conditions

    参数 数值及说明
    转速/(r/min) 0~40000
    壁面属性 无滑移绝热
    工质 理想空气
    湍流模型 标准k-ε
    涡动模型 多频椭圆涡动
    进口压力/MPa 0.3~0.7
    出口压力/MPa 0.1
    总温/K 298
    偏心率 0~0.7
    涡动频率/Hz 40~320
    下载: 导出CSV
  • [1] 马也,王庆锋,施任杰,等. 航空发动机气膜浮环密封上浮性能研究[J]. 润滑与密封,2021,46(1): 38-44,50. MA Ye,WANG Qingfeng,SHI Renjie,et al. Research on floating performance of aeroengine air film floating ring seal[J]. Lubrication Engineering,2021,46(1): 38-44,50. (in Chinese

    MA Ye, WANG Qingfeng, SHI Renjie, et al. Research on floating performance of aeroengine air film floating ring seal[J]. Lubrication Engineering, 2021, 46(1): 38-44, 50. (in Chinese)
    [2] ALLEN G. Self-acting lift-pad geometry for circumferential seals: a noncontacting concept[R]. NASA TP-1583,1980.
    [3] BURCHAM R. High speed cryogenic self-acting,shaft seals for liquid rocket turbopumps[R]. NASA CR-168194,1983.
    [4] OIKE M,NAGAO R,NOSAKA M,et al. Characteristics of a shaft seal system for the LE-7 liquid oxygen turbopump[R]. AIAA 95-3102,1995.
    [5] PESCOSOLIDO A,DOBEK L. Development of high misalignment carbon seals[R]. AIAA 2001-3625,2001.
    [6] 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
    [7] KIRK R G,BAHETI S K. Evaluation of floating ring seals for centrifugal compressors using the finite element method[J]. Journal of Vibration and Acoustics,1999,121(1): 131-136. doi: 10.1115/1.2893940
    [8] DUAN Wenbo,CHU Fulei,KIM C H,et al. A bulk-flow analysis of static and dynamic characteristics of floating ring seals[J]. Tribology International,2007,40(3): 470-478. doi: 10.1016/j.triboint.2006.04.010
    [9] CHOI C H,NOH J G,KIM D J,et al. Effects of floating-ring seal clearance on the pump performance for turbopumps[J]. Journal of Propulsion and Power,2009,25(1): 191-195. doi: 10.2514/1.36806
    [10] 王飞,刘向锋,刘莹. 浅槽环瓣型浮动环密封的性能分析[J]. 润滑与密封,2005,30(6): 74-76,85. WANG Fei,LIU Xiangfeng,LIU Ying. Performance analysis of the shallow slot split floating ring seal[J]. Lubrication Engineering,2005,30(6): 74-76,85. (in Chinese doi: 10.3969/j.issn.0254-0150.2005.06.024

    WANG Fei, LIU Xiangfeng, LIU Ying. Performance analysis of the shallow slot split floating ring seal[J]. Lubrication Engineering, 2005, 30(6): 74-76, 85. (in Chinese) doi: 10.3969/j.issn.0254-0150.2005.06.024
    [11] 王伟,赵宗坚,张振生. 单环圆周密封装置设计和应用研究[J]. 航空发动机,2009,35(4): 7-11. WANG Wei,ZHAO Zongjian,ZHANG Zhensheng. Design and application of single circumferential seal[J]. Aeroengine,2009,35(4): 7-11. (in Chinese doi: 10.3969/j.issn.1672-3147.2009.04.002

    WANG Wei, ZHAO Zongjian, ZHANG Zhensheng. Design and application of single circumferential seal[J]. Aeroengine, 2009, 35(4): 7-11. (in Chinese) doi: 10.3969/j.issn.1672-3147.2009.04.002
    [12] 马利军,李双喜,马也,等. 气膜浮环密封特性参数的影响因素分析[J]. 流体机械,2018,46(10): 6-10,34. MA Lijun,LI Shuangxi,MA Ye,et al. Analysis of factors influencing characteristic parameters of gas film floating ring seal[J]. Fluid Machinery,2018,46(10): 6-10,34. (in Chinese doi: 10.3969/j.issn.1005-0329.2018.10.002

    MA Lijun, LI Shuangxi, MA Ye, et al. Analysis of factors influencing characteristic parameters of gas film floating ring seal[J]. Fluid Machinery, 2018, 46(10): 6-10, 34. (in Chinese) doi: 10.3969/j.issn.1005-0329.2018.10.002
    [13] 胡廷勋,周坤,王晓燕,等. 浮环密封泄漏特性数值计算与试验[J]. 航空动力学报,2020,35(4): 888-896. HU Tingxun,ZHOU Kun,WANG Xiaoyan,et al. Numerical calculation and experiment on leakage characteristics of floating ring seal[J]. Journal of Aerospace Power,2020,35(4): 888-896. (in Chinese doi: 10.13224/j.cnki.jasp.2020.04.022

    HU Tingxun, ZHOU Kun, WANG Xiaoyan, et al. Numerical calculation and experiment on leakage characteristics of floating ring seal[J]. Journal of Aerospace Power, 2020, 35(4): 888-896. (in Chinese) doi: 10.13224/j.cnki.jasp.2020.04.022
    [14] 马也. 整体式气膜浮环密封的开启性能与泄漏特性研究[D]. 北京: 北京化工大学,2020. MA Ye. Research on opening performance and leakage performance of tntergral gas film floating ring seal[D]. Beijing: Beijing University of Chemical Technology,2020. (in Chinese

    MA Ye. Research on opening performance and leakage performance of tntergral gas film floating ring seal[D]. Beijing: Beijing University of Chemical Technology, 2020. (in Chinese)
    [15] 郑娆,陈潇竹,李双喜,等. 高速气膜镶装式浮环密封的开启特性[J]. 北京航空航天大学学报,2022,48(11): 2111-2120. ZHENG Rao,CHEN Xiaozhu,LI Shuangxi,et al. Opening characteristics of inlaid floating ring seal with high-speed gas film[J]. Journal of Beijing University of Aeronautics and Astronautics,2022,48(11): 2111-2120. (in Chinese

    ZHENG Rao, CHEN Xiaozhu, LI Shuangxi, et al. Opening characteristics of inlaid floating ring seal with high-speed gas film[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(11): 2111-2120. (in Chinese)
    [16] CHILDS D W,RODRIGUEZ L E,CULLOTTA V,et al. Rotordynamic-coefficients and static (equilibrium loci and leakage) characteristics for short,laminar-flow annular seals[J]. Journal of Tribology,2006,128(2): 378-387. doi: 10.1115/1.2164468
    [17] CHILDS D W,GRAVISS M,RODRIGUEZ L E. Influence of groove size on the static and rotordynamic characteristics of short,laminar-flow annular seals[J]. Journal of Tribology,2007,129(2): 398-406. doi: 10.1115/1.2647471
    [18] ANDRÉS L S,DELGADO A. A novel bulk-flow model for improved predictions of force coefficients in grooved oil seals operating eccentrically[J]. Journal of Engineering for Gas Turbines and Power,2012,134(5): 0525091-05250910.
    [19] HA T W,LEE Y B,KIM C H. Leakage and rotordynamic analysis of a high pressure floating ring seal in the turbo pump unit of a liquid rocket engine[J]. Tribology International,2002,35(3): 153-161. doi: 10.1016/S0301-679X(01)00110-4
    [20] 王乐勤,周文杰,邢桂坤,等. 小锥度环形密封转子动特性[J]. 排灌机械工程学报,2013,31(6): 517-522,539. WANG Leqin,ZHOU Wenjie,XING Guikun,et al. Dynamic coefficients of small cone-shaped annular seal rotor[J]. Journal of Drainage and Irrigation Machinery Engineering,2013,31(6): 517-522,539. (in Chinese doi: 10.3969/j.issn.1674-8530.2013.06.012

    WANG Leqin, ZHOU Wenjie, XING Guikun, et al. Dynamic coefficients of small cone-shaped annular seal rotor[J]. Journal of Drainage and Irrigation Machinery Engineering, 2013, 31(6): 517-522, 539. (in Chinese) doi: 10.3969/j.issn.1674-8530.2013.06.012
    [21] 刘占生,夏鹏,张广辉,等. 浮环密封运动机理及对轴系稳定性的影响[J]. 振动与冲击,2016,35(9): 110-116. LIU Zhansheng,XIA Peng,ZHANG Guanghui,et al. Floating ring seals movement mechanism and its influence on stability of a rotor system[J]. Journal of Vibration and Shock,2016,35(9): 110-116. (in Chinese doi: 10.13465/j.cnki.jvs.2016.09.017

    LIU Zhansheng, XIA Peng, ZHANG Guanghui, et al. Floating ring seals movement mechanism and its influence on stability of a rotor system[J]. Journal of Vibration and Shock, 2016, 35(9): 110-116. (in Chinese) doi: 10.13465/j.cnki.jvs.2016.09.017
    [22] 苏令. 新型浅槽环瓣型浮动环密封综合性能分析及软件开发[D]. 北京: 清华大学,2006. SU Ling. Performance analysis and software development of a new shallow-slot split floating ring seal[D]. Beijing: Tsinghua University,2006. (in Chinese

    SU Ling. Performance analysis and software development of a new shallow-slot split floating ring seal[D]. Beijing: Tsinghua University, 2006. (in Chinese)
    [23] 方昌德. 世界航空发动机手册[M]. 北京: 航空工业出版社,1996.
    [24] CHILDS D W. Turbomachinery rotor-dynamics: phenomena,modeling,and analysis[J]. Turbomachinery Rotor-dynamics Phenomena Modeling & Analysis,1993,28: 262-263.
    [25] 孙丹,王双,艾延廷,等. 阻旋栅对密封静力与动力特性影响的数值分析与实验研究[J]. 航空学报,2015,36(9): 3002-3011. SUN Dan,WANG Shuang,AI Yanting,et al. Numerical and experimental research on performance of swirl brakes for the static and dynamic characteristics of seals[J]. Acta Aeronautica et Astronautica Sinica,2015,36(9): 3002-3011. (in Chinese

    SUN Dan, WANG Shuang, AI Yanting, et al. Numerical and experimental research on performance of swirl brakes for the static and dynamic characteristics of seals[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(9): 3002-3011. (in Chinese)
    [26] ERTAS B H,DELGADO A,VANNINI G. Rotordynamic force coefficients for three types of annular gas seals with inlet preswirl and high differential pressure ratio[J]. Journal of Engineering for Gas Turbines and Power,2012,134(4): 42501-42503.
    [27] 李志刚. 袋型阻尼密封泄漏特性和转子动力特性的研究[D]. 西安: 西安交通大学,2017. LI Zhigang. Investigations on the leakage flow and rotordynamic characteristics of the pocket damper seal[D]. Xi’an: Xi’an Jiaotong University,2017. (in Chinese

    LI Zhigang. Investigations on the leakage flow and rotordynamic characteristics of the pocket damper seal[D]. Xi’an: Xi’an Jiaotong University, 2017. (in Chinese)
  • 加载中
图(18) / 表(2)
计量
  • 文章访问数:  51
  • HTML浏览量:  29
  • PDF量:  6
  • 被引次数: 0
出版历程
  • 收稿日期:  2022-09-16
  • 网络出版日期:  2023-12-26

目录

    /

    返回文章
    返回