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动压型分瓣式浮环密封泄漏特性流固热耦合数值研究

任国哲 李延鹏 孙丹 赵欢 温帅方 王鑫宇

任国哲, 李延鹏, 孙丹, 等. 动压型分瓣式浮环密封泄漏特性流固热耦合数值研究[J]. 航空动力学报, 2025, 40(3):20230261 doi: 10.13224/j.cnki.jasp.20230261
引用本文: 任国哲, 李延鹏, 孙丹, 等. 动压型分瓣式浮环密封泄漏特性流固热耦合数值研究[J]. 航空动力学报, 2025, 40(3):20230261 doi: 10.13224/j.cnki.jasp.20230261
REN Guozhe, LI Yanpeng, SUN Dan, et al. Numerical study on leakage characteristics of dynamic pressure split floating ring seal with fluid-solid-thermal coupling[J]. Journal of Aerospace Power, 2025, 40(3):20230261 doi: 10.13224/j.cnki.jasp.20230261
Citation: REN Guozhe, LI Yanpeng, SUN Dan, et al. Numerical study on leakage characteristics of dynamic pressure split floating ring seal with fluid-solid-thermal coupling[J]. Journal of Aerospace Power, 2025, 40(3):20230261 doi: 10.13224/j.cnki.jasp.20230261

动压型分瓣式浮环密封泄漏特性流固热耦合数值研究

doi: 10.13224/j.cnki.jasp.20230261
基金项目: 国家自然科学基金(52075346); 中国航空发动机集团产学研合作项目(HFZL2021CXY012); 辽宁省自然科学基金(2022-MS-301)
详细信息
    作者简介:

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

    通讯作者:

    孙丹(1981-),男,教授,博士,主要从事透平机械先进密封技术研究。E-mail:phd_sundan@163.com

  • 中图分类号: V233.5

Numerical study on leakage characteristics of dynamic pressure split floating ring seal with fluid-solid-thermal coupling

  • 摘要:

    分析了分瓣式浮环密封流固热耦合理论,建立了有槽和无槽这3种结构分瓣式浮环密封流固热耦合数值求解模型,在验证数值方法准确性的基础上,研究了无浅槽、矩形槽和三角槽这3种结构的分瓣式浮环密封在高温高压气体耦合作用下随不同入口压力、温度和转速下的流场特性、力学特性以及泄漏特性。结果表明:3种浅槽结构的分瓣式浮环密封流固热耦合数值求解模型,可准确求解流场特性、力学特性和泄漏特性。流体在高速剪切力的作用下沿周向运动,由于挤压使浅槽结构产生局部高压区,形成动压效应;同一入口压力工况下,具有三角槽结构的分瓣式浮环密封开启力最大,入口压力为600 kPa时相比于无浅槽结构增加9.6%,且泄漏量保持相对较小;温度对浮环开启力影响很小,且温度越高泄漏量越小,最大减小6%;转速对矩形槽和三角槽结构浮环开启力影响较大,且最大增加3.2%,对闭合力和泄漏量影响很小。

     

  • 图 1  分瓣式浮环密封结构示意图

    Figure 1.  Schematic diagram of sealing structure of split floating ring

    图 2  动压型分瓣式浮环密封示意图

    Figure 2.  Schematic diagram of dynamic pressure split floating ring seal

    图 3  浮环受力示意图

    Figure 3.  Schematic diagram of floating ring force

    图 4  分瓣式浮环密封流固热耦合计算流程图

    Figure 4.  Fluid-solid-thermal coupling calculation flow chart of split floating ring seal

    图 5  浮环密封结构示意图

    Figure 5.  Schematic diagram of floating ring seal structure

    图 6  无浅槽模型

    Figure 6.  Model without slot

    图 7  矩形槽模型

    Figure 7.  Rectangular slot model

    图 8  三角槽模型

    Figure 8.  Triangular groove model

    图 9  网格无关性验证

    Figure 9.  Grid independence verification

    图 10  无浅槽结构网格划分

    Figure 10.  Meshing of structure without slot

    图 11  矩形槽结构网格划分

    Figure 11.  Meshing of rectangular slot structure

    图 12  三角槽结构网格划分

    Figure 12.  Meshing of triangular groove structure

    图 13  几何模型二维示意图(单位:mm)[8]

    Figure 13.  Two-dimension schematic diagram of geometric model (unit:mm)[8]

    图 14  流场压力分布云图

    Figure 14.  Pressure distribution cloud of flow field

    图 15  流场温度分布云图

    Figure 15.  Temperature distribution cloud of flow field

    图 16  入口压力对开启力的影响

    Figure 16.  Influence of inlet pressure on opening force

    图 17  入口温度对开启力的影响

    Figure 17.  Influence of inlet temperature on opening force

    图 18  开启力和闭合力随转速变化

    Figure 18.  Opening force and closing force changing with rotational speed

    图 19  入口压力对泄漏量的影响

    Figure 19.  Influence of inlet pressure on leakage

    图 20  入口温度对泄漏量的影响

    Figure 20.  Influence of inlet temperature on leakage

    图 21  转速对泄漏量的影响

    Figure 21.  Influence of speed on leakage

    表  1  浮环结构参数

    Table  1.   Structure parameters of floating ring

    参数 数值
    气膜厚度hm/μm 10
    横槽深度h1/mm 0.8
    浅槽深度h3/mm 0.3
    环槽宽度b2/mm 2
    三角槽轴向间距b4/mm 1.5
    横槽宽度L2/mm 16
    顶角θ/(°) 50
    环槽深度h2/mm 0.8
    主密封面坝区宽度b1/mm 0.7
    单侧密封台宽度b3/mm 100
    浅槽宽度L1/mm 0.3
    封严半径/mm 104.5
    下载: 导出CSV

    表  2  材料属性

    Table  2.   Material properties

    参数 数值
    石墨 结构钢
    密度/(kg/m3 1930 7800
    弹性模量/GPa 14 206
    泊松比 0.25 0.3
    下载: 导出CSV

    表  3  浮环密封数值模型和工况参数

    Table  3.   Numerical model and working condition parameters of floating ring seal

    参数 数值或说明
    流体属性 理想气体
    入口压力/kPa 200~600
    入口温度/℃ 300~500
    湍流模型 k-ε
    出口压力/kPa 20
    转速/(r/min) 12000
    下载: 导出CSV

    表  4  边界条件参数

    Table  4.   Boundary condition parameters

    参数 数值或说明
    流体属性 理想气体
    入口压力/kPa 345
    入口温度/℃ 21
    湍流模型 k-ε
    出口压力/kPa 100
    转速/(rad/s) 3140
    下载: 导出CSV

    表  5  准确性验证

    Table  5.   Accuracy verification

    浅槽槽深/
    μm
    泄漏量/(g/s) 相对误差/%
    文献[8] 本文
    20 0.631 0.614 2.7
    25 0.805 0.816 1.1
    30 0.959 0.969 1.04
    下载: 导出CSV
  • [1] 郑大勇,陶瑞峰,张玺,等. 大推力氢氧发动机关键技术及解决途径[J]. 火箭推进,2014,40(2): 22-27,35. ZHENG Dayong,TAO Ruifeng,ZHANG Xi,et al. Key technology and solution of high thrust hydrogen and oxygen engine[J]. Journal of Rocket Propulsion,2014,40(2): 22-27,35. (in Chinese doi: 10.3969/j.issn.1672-9374.2014.02.004

    ZHENG Dayong, TAO Ruifeng, ZHANG Xi, et al. Key technology and solution of high thrust hydrogen and oxygen engine[J]. Journal of Rocket Propulsion, 2014, 40(2): 22-27, 35. (in Chinese) doi: 10.3969/j.issn.1672-9374.2014.02.004
    [2] SOROKINA N E,REDCHITZ A V,IONOV S G,et al. Different exfoliated graphite as a base of sealing materials[J]. Journal of Physics and Chemistry of Solids,2006,67(5/6): 1202-1204.
    [3] SONG Yongzhong,ZHAI Gengtai,SONG Jinren,et al. Seal and wear properties of graphite from MCMBs/pitch-based carbon/phenolic-based carbon composites[J]. Carbon,2006,44(13): 2793-2796. doi: 10.1016/j.carbon.2006.03.028
    [4] 闫玉涛,张博,胡广阳,等. 石墨圆周密封热-结构耦合分析[J]. 航空动力学报,2018,33(2): 273-281. YAN Yutao,ZHANG Bo,HU Guangyang,et al. Analysis on thermal-structure coupling for graphite circumferential seal[J]. Journal of Aerospace Power,2018,33(2): 273-281. (in Chinese

    YAN Yutao, ZHANG Bo, HU Guangyang, et al. Analysis on thermal-structure coupling for graphite circumferential seal[J]. Journal of Aerospace Power, 2018, 33(2): 273-281. (in Chinese)
    [5] 闫玉涛,魏荣,胡广阳,等. 考虑热流固多物理场耦合的圆周密封特性[J]. 航空动力学报,2020,35(2): 305-317. YAN Yutao,WEI Rong,HU Guangyang,et al. Circumferential seal characteristics with thermal-fluid-structure multi-physics field coupling[J]. Journal of Aerospace Power,2020,35(2): 305-317. (in Chinese

    YAN Yutao, WEI Rong, HU Guangyang, et al. Circumferential seal characteristics with thermal-fluid-structure multi-physics field coupling[J]. Journal of Aerospace Power, 2020, 35(2): 305-317. (in Chinese)
    [6] ALLEN G P. Self-acting lift-pad geometry for circumferential seals: a noncontacting concept[R]. NASA-1980-1583,1980.
    [7] BURCHAM R E. High-speed cryogenic self-acting shaft seals for liquid rockrt turbopumps[R]. NASA-1983-168194,1983.
    [8] 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
    [9] OIKE M,NAGAO R. Characteristics of a shaft seal system for the LE-7 liquid oxygen turbopump[R]. AIAA 95-3102,1995.
    [10] 仰宏伟,白少先. 环瓣式浮环密封表面瑞利台阶型槽气体润滑动压特性[J]. 推进技术,2022,43(2): 142-148. YANG Hongwei,BAI Shaoxian. Gas hydrodynamic lubrication performance of split floating ring seals with Rayleigh step grooves[J]. Journal of Propulsion Technology,2022,43(2): 142-148. (in Chinese

    YANG Hongwei, BAI Shaoxian. Gas hydrodynamic lubrication performance of split floating ring seals with Rayleigh step grooves[J]. Journal of Propulsion Technology, 2022, 43(2): 142-148. (in Chinese)
    [11] 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
    [12] 王飞,刘向锋,刘莹. 浅槽环瓣型浮动环密封的参数优化[J]. 润滑与密封,2006,31(2): 105-107. WANG Fei,LIU Xiangfeng,LIU Ying. Parameters optimization of the shallow-slot split floating ring seal[J]. Lubrication Engineering,2006,31(2): 105-107. (in Chinese doi: 10.3969/j.issn.0254-0150.2006.02.033

    WANG Fei, LIU Xiangfeng, LIU Ying. Parameters optimization of the shallow-slot split floating ring seal[J]. Lubrication Engineering, 2006, 31(2): 105-107. (in Chinese) doi: 10.3969/j.issn.0254-0150.2006.02.033
    [13] 李小芬,周芮,涂霆. 圆周分段式密封动压浮起力数值仿真计算[J]. 火箭推进,2019,45(5): 45-51. LI Xiaofeng,ZHOU Rui,TU Ting. Numerical simulation of dynamic pressure floating force of circular segmented seal[J]. Journal of Rocket Propulsion,2019,45(5): 45-51. (in Chinese

    LI Xiaofeng, ZHOU Rui, TU Ting. Numerical simulation of dynamic pressure floating force of circular segmented seal[J]. Journal of Rocket Propulsion, 2019, 45(5): 45-51. (in Chinese)
    [14] 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. Comprehensive performance analysis and software development of a new type of shallow groove ring flap floating ring seal[D]. Beijing: Tsinghua University,2006. (in Chinese

    SU Ling. Comprehensive performance analysis and software development of a new type of shallow groove ring flap floating ring seal[D]. Beijing: Tsinghua University, 2006. (in Chinese)
    [15] 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. Study on sealing performance of high speed annular flap floating ring[D]. Beijing: Beijing University of Chemical Technology,2019. (in Chinese

    MA Wenjie. Study on sealing performance of high speed annular flap floating ring[D]. Beijing: Beijing University of Chemical Technology, 2019. (in Chinese)
    [16] 马润梅,赵祥,李双喜,等. 动压式环瓣浮环密封特性及摩擦磨损研究[J]. 推进技术,2022,43(8): 210099. MA Runmei,ZHAO Xiang,LI Shuangxi,et al. Dynamic pressure type ring disc floating ring seal properties and friction and wear studies[J]. Propulsion technology: 2022,43(8): 210099. (in Chinese

    MA Runmei, ZHAO Xiang, LI Shuangxi, et al. Dynamic pressure type ring disc floating ring seal properties and friction and wear studies[J]. Propulsion technology: 2022, 43(8): 210099. (in Chinese)
    [17] 赵超越. 鼓泡支撑T型槽柱面气膜密封流固耦合分析[D]. 昆明: 昆明理工大学,2021. ZHAO Chaoyue. Fluid-solid coupling analysis of T-groove cylindrical gas film seal with bubble support[D]. Kunming: Kunming University of Science and Technology,2021. (in Chinese

    ZHAO Chaoyue. Fluid-solid coupling analysis of T-groove cylindrical gas film seal with bubble support[D]. Kunming: Kunming University of Science and Technology, 2021. (in Chinese)
    [18] 白超斌,刘美红,孙军锋,等. 基于流固耦合的柱面气膜密封支撑结构性能研究[J]. 润滑与密封,2020,45(9): 64-70. BAI Chaobin,LIU Meihong,SUN Junfeng,et al. Research on support structure performance of cylindrical gas film seal based on fluid-structure interaction[J]. Lubrication Engineering,2020,45(9): 64-70. (in Chinese doi: 10.3969/j.issn.0254-0150.2020.09.011

    BAI Chaobin, LIU Meihong, SUN Junfeng, et al. Research on support structure performance of cylindrical gas film seal based on fluid-structure interaction[J]. Lubrication Engineering, 2020, 45(9): 64-70. (in Chinese) doi: 10.3969/j.issn.0254-0150.2020.09.011
    [19] 王婷,刘美红,孙军锋,等. 一字槽柱面气膜密封性能的仿真分析[J]. 流体机械,2020,48(5): 55-60. WANG Ting,LIU Meihong,SUN Junfeng,et al. Simulation analysis of the sealing performance of cylinder gas film[J]. Fluid Machinery,2020,48(5): 55-60. (in Chinese doi: 10.3969/j.issn.1005-0329.2020.05.010

    WANG Ting, LIU Meihong, SUN Junfeng, et al. Simulation analysis of the sealing performance of cylinder gas film[J]. Fluid Machinery, 2020, 48(5): 55-60. (in Chinese) doi: 10.3969/j.issn.1005-0329.2020.05.010
    [20] 运睿德,陈志英,刘勇,等. 周向弹簧力分布对圆周密封装置密封性能的影响[J]. 推进技术,2021,42(6): 1361-1371. YUN Ruide,CHEN Zhiying,LIU Yong,et al. Effects of circumferential spring force distribution on sealing performance of circumferential seal[J]. Journal of Propulsion Technology,2021,42(6): 1361-1371. (in Chinese

    YUN Ruide, CHEN Zhiying, LIU Yong, et al. Effects of circumferential spring force distribution on sealing performance of circumferential seal[J]. Journal of Propulsion Technology, 2021, 42(6): 1361-1371. (in Chinese)
    [21] 何川. CFD基础及应用[M]. 重庆: 重庆大学出版社,2015.
    [22] 任弘,李范春,杜玲. 流固耦合作用对螺旋桨强度影响的数值计算[J]. 武汉理工大学学报(交通科学与工程版),2015,39(1): 144-147,152. REN Hong,LI Fanchun,DU Ling. Numerical calculation for the effect of FSI on marine propeller strength[J]. Journal of Wuhan University of Technology (Transportation Science & Engineering),2015,39(1): 144-147,152. (in Chinese

    REN Hong, LI Fanchun, DU Ling. Numerical calculation for the effect of FSI on marine propeller strength[J]. Journal of Wuhan University of Technology (Transportation Science & Engineering), 2015, 39(1): 144-147, 152. (in Chinese)
    [23] 魏炫宇,马咏梅,丁万,等. 机械密封摩擦副界面热流固耦合分析[J]. 机械设计与制造工程,2017,46(6): 89-94. WEI Xuanyu,MA Yongmei,DING Wan,et al. The thermal fluid and solid coupling analysis on the friction surface of mechanical seal[J]. Machine Design and Manufacturing Engineering,2017,46(6): 89-94. (in Chinese doi: 10.3969/j.issn.2095-509X.2017.06.021

    WEI Xuanyu, MA Yongmei, DING Wan, et al. The thermal fluid and solid coupling analysis on the friction surface of mechanical seal[J]. Machine Design and Manufacturing Engineering, 2017, 46(6): 89-94. (in Chinese) doi: 10.3969/j.issn.2095-509X.2017.06.021
    [24] 孟璐. 复合材料水翼流固耦合数值计算研究[D]. 北京: 北京理工大学,2018. MENG Lu. Study on numerical calculation of fluid-solid coupling of composite hydrofoil[D]. Beijing: Beijing Institute of Technology,2018. (in Chinese

    MENG Lu. Study on numerical calculation of fluid-solid coupling of composite hydrofoil[D]. Beijing: Beijing Institute of Technology, 2018. (in Chinese)
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  • 收稿日期:  2023-04-21
  • 网络出版日期:  2024-11-04

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