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

刷式密封临界承压能力流固耦合数值研究

孙丹 刘伟 焦忠泽 赵欢 李玉

孙丹, 刘伟, 焦忠泽, 等. 刷式密封临界承压能力流固耦合数值研究[J]. 航空动力学报, 2023, 38(1):13-22 doi: 10.13224/j.cnki.jasp.20210404
引用本文: 孙丹, 刘伟, 焦忠泽, 等. 刷式密封临界承压能力流固耦合数值研究[J]. 航空动力学报, 2023, 38(1):13-22 doi: 10.13224/j.cnki.jasp.20210404
SUN Dan, LIU Wei, JIAO Zhongze, et al. Numerical study on fluid-structure interaction of critical pressure capacity of brush seal[J]. Journal of Aerospace Power, 2023, 38(1):13-22 doi: 10.13224/j.cnki.jasp.20210404
Citation: SUN Dan, LIU Wei, JIAO Zhongze, et al. Numerical study on fluid-structure interaction of critical pressure capacity of brush seal[J]. Journal of Aerospace Power, 2023, 38(1):13-22 doi: 10.13224/j.cnki.jasp.20210404

刷式密封临界承压能力流固耦合数值研究

doi: 10.13224/j.cnki.jasp.20210404
基金项目: 国家自然科学基金(52075346); 辽宁省教育厅基础研究项目(JYT2020047);辽宁省航发材料摩擦学重点实验室开放基金(LKLAMTF202103)
详细信息
    作者简介:

    孙丹(1981-),男,教授,博士,主要从事涡轮机械先进密封技术研究

    通讯作者:

    赵欢(1982-),女,副教授,博士,主要从事航空发动机新材料密封的制备技术及其特性研究。 E-mail:phd_zhaohuan@163.com

  • 中图分类号: V233;TK263.2

Numerical study on fluid-structure interaction of critical pressure capacity of brush seal

  • 摘要:

    采用以泄漏因子与有效间隙作为刷式密封临界承压能力的评价指标,基于ALE(arbitrary Lagrange-Euler)流固耦合方法建立刷式密封三维瞬态求解模型,分析三种不同结构的刷式密封模型在不同压差下的刷丝变形,研究临界承压能力对刷丝变形的影响。研究结果表明:随着上下游压差的增加,泄漏因子与有效间隙的值趋于稳定时的压差范围即为刷式密封的临界承压能力。所研究的基本型刷式密封临界承压能力为0.25~0.30 MPa,后挡板保护高度降低0.5 mm的刷式密封和轴向增加5排刷丝的刷式密封临界承压能力相对于基本型增加了16.7%~20.0%,降低后挡板保护高度和增加刷丝轴向排数可以提高刷式密封临界承压能力。随着上下游压差的增加,刷丝轴向最大变形量先增加,在上下游压差达到刷式密封临界承压能力时,刷丝之间间隙被压缩至接近最小,刷丝轴向最大变形量达到稳定。该研究成果为刷式密封的结构设计提供理论依据。

     

  • 图 1  刷式密封结构及工作示意图

    Figure 1.  Brush seal structure and work diagram

    图 2  流固耦合流程图

    Figure 2.  Flow chart of fluid-structure interaction

    图 3  刷式密封计算模型图

    Figure 3.  Brush seal calculation model diagram

    图 4  网格划分示意图

    Figure 4.  Meshing diagram

    图 5  边界条件

    Figure 5.  Boundary conditions

    图 6  刷式密封实验装置实物图

    Figure 6.  Diagram of brush seals test device

    图 7  刷式密封实验件

    Figure 7.  Test piece of brush seals

    图 8  泄漏特性测试原理图

    Figure 8.  Diagram of leakage characteristic test schematic

    图 9  计算值与实验值对比图

    Figure 9.  Comparison diagram of calculated values and test values

    图 10  三种不同结构刷式密封压力分布

    Figure 10.  Pressure distribution of brush seal with three different structures

    图 11  三种不同结构刷式密封速度分布

    Figure 11.  Speed distribution of brush seal with three different structures

    图 12  泄漏因子随上下游压差的变化

    Figure 12.  Variation of leakage factor with pressure difference between the upstream and downstream

    图 13  有效间隙随上下游压差的变化

    Figure 13.  Variation of effective clearance with pressure difference between the upstream and downstream

    图 14  三种刷式密封刷丝轴向变形图

    Figure 14.  Axial deformation diagram of three kinds of brush seal wire

    图 15  三种刷式密封刷丝轴向最大变形量

    Figure 15.  Maximum axial deformation of three kinds of brush seals

    表  1  刷式密封主要结构参数

    Table  1.   Main structural parameters of brush seal

    刷式密封主要结构参数数值
    刷丝直径/mm0.08
    刷丝之间间隙/mm0.008
    刷丝束厚度/mm1.80
    后挡板保护高度/mm3.00
    刷丝与转子表面间间隙/mm0
    末排刷丝与后挡板间轴向间隙/mm0
    下载: 导出CSV

    表  2  主要工况参数

    Table  2.   Main operating parameters

    参数数值
    入口总压/MPa0.15~0.60
    出口静压/MPa0.10
    刷丝之间摩擦因数0.3
    刷丝与挡板间摩擦因数0.3
    下载: 导出CSV
  • [1] 孙丹,刘宁宁,胡广阳,等. 考虑刷丝变形的刷式密封流场特性与力学特性流固耦合研究[J]. 航空动力学报,2016,31(10): 2544-2553.

    SUN Dan,LIU Ningning,HU Guangyang,et al. Fluid-structure investigation on the flow flied and mechanical characteristic in brush seals with bristle deflections[J]. Journal of Aerospace Power,2016,31(10): 2544-2553. (in Chinese)
    [2] 赵欢,焦忠泽,孙丹,等. 多级刷式密封级间压降分配影响因素数值与实验研究[J]. 航空学报,2020,41(10): 79-91.

    ZHAO Huan,JIAO Zhongze,SUN Dan,et al. Numerial and experimental research on interstage drop distribution affecting factors of multi-stage brush seals[J]. Acta Aeronautica et Astronautica Sinica,2020,41(10): 79-91. (in Chinese)
    [3] 孙丹,李国勤,艾延廷,等. 基于三维实体建模的刷式密封传热机理数值研究[J]. 航空动力学报,2019,34(8): 1633-1643.

    SUN Dan,LI Guoqin,AI Yanting,et al. Numerical study on heat transfer mechanism of brush seal based on three-dimensional solid modeling[J]. Journal of Aerospace Power,2019,34(8): 1633-1643. (in Chinese)
    [4] DINC S,DEMIROGLU M,TURNQUIST N,et al. Fundamental design issues of brush seals for industrial applications[R]. ASME Paper 2001-0400,2001.
    [5] SHORT F,BASU P,DATTA A.Advanced brush seal developmnet[R]. AIAA-1996-2907,1996.
    [6] CHUPP R E,HENDRICKS R C,LATTIME S B. Sealing in turbomachinery[J]. Journal of Propulsion and Power,2006,22(2): 313-349. doi: 10.2514/1.17778
    [7] CHUPP R E,PRIOR R,LOWENTHAL R. Update on brush seal development for large industrial gas turbines[R]. AIAA-1996-3306,1996.
    [8] CRUDGINGTON P. Brush seal performance evaluation[R]. AIAA-1998-3172,1998.
    [9] DINC S,DEMIROGLU M,TURNQUIST N,et al. Fundamental design issues of brush seals for industrial applications[J]. Journal of Turbomachinery,2002,124(2): 293-300. doi: 10.1115/1.1451847
    [10] TRIVEDI D,ROY B,DEMIROGLU M. Experimental characterization of variable bristle diameter brush seal leakage,stiffness and wear[R]. ASME Paper GT2013-95086,2013.
    [11] 孙晓萍. 刷式密封性能和耐久性试验研究[J]. 航空发动机,2002,28(3): 37-41. doi: 10.3969/j.issn.1672-3147.2002.03.009

    SUN Xiaoping. Experimental investigation of performance and durability of brush seal[J]. Aeroengine,2002,28(3): 37-41. (in Chinese) doi: 10.3969/j.issn.1672-3147.2002.03.009
    [12] 孙晓萍,李卫东,刘晓远. 刷式密封设计与试验研究[J]. 航空发动机,2005,31(2): 17-19. doi: 10.3969/j.issn.1672-3147.2005.02.007

    SUN Xiaoping,LI Weidong,LIU Xiaoyuan. Design and test of brush seal[J]. Aeroengine,2005,31(2): 17-19. (in Chinese) doi: 10.3969/j.issn.1672-3147.2005.02.007
    [13] 朱宗举. 刷式密封的设计与应用[J]. 燃气轮机技术,2005,18(3): 68-72. doi: 10.3969/j.issn.1009-2889.2005.03.014

    ZHU Zhongju. Design and application of brush seal[J]. Gas Turbine Technology,2005,18(3): 68-72. (in Chinese) doi: 10.3969/j.issn.1009-2889.2005.03.014
    [14] JAYESH M, GARY H. Rotating intershaft brush seal for sealing between rotating shafts: Part Ⅱ experimental data evaluation and modeling of the brush seal leakage flows[R]. AIAA-2007-5733,2007.
    [15] MEHTA J,HOLLOWAY G,ASKEW J. Innovative rotating intershaft brush seal for sealing between rotating shafts: Part Ⅱ modeling of brush seal leakage flows[R]. AIAA-2006-4752,2006.
    [16] BASU P,DATTA A,JOHNSON R. Hysteresis and bristle stiffening effects of conventional brush seals[R]. AIAA-1993-1996,1993
    [17] ADDY E J,HOWE H,FLOWERS J. Preliminary results of silicon carbide brush seal testing at NASA Lewis Research Center[R]. AIAA-1995-2763,1995.
    [18] CHUPP R E,HOLLE G F,DOWLER C A. Simple leakage flow model for brush seals[R]. AIAA-1991-1913,1991.
    [19] PUGACHEV A O. Aggregation of experimental and theoretical data for brush seal leakage evaluation[R]. AIAA-2014-3598,2014.
    [20] 张雄,王天舒,刘岩.计算动力学[M].2版.北京:清华大学出版社,2015.
    [21] 孙丹,杜宸宇,刘永泉,等. 基于ALE流固耦合方法的刷式密封刷丝接触变形特性理论与试验研究[J]. 机械工程学报,2020,56(9): 170-180. doi: 10.3901/JME.2020.09.170

    SUN Dan,DU Chenyu,LIU Yongquan,et al. Theoretical and experimental investigation on the bristle contact deflections characteristics of brush seals based on ALE fluid-structure interaction method[J]. Journal of Mechanical Engineering,2020,56(9): 170-180. (in Chinese) doi: 10.3901/JME.2020.09.170
    [22] CARLILE J A,HENDRICKS R C,YODER D A. Brush seal leakage performance with gaseous working fluids at static and low rotor speed conditions[J]. Journal of Engineering for Gas Turbines and Power,1993,115(2): 1-7.
    [23] 邱波,李军. 刷式密封传热特性研究[J]. 西安交通大学学报,2011,45(9): 94-100.

    QIU Bo,LI Jun. Investigation on the heat transfer characteristics of brush seals[J]. Journal of Xi’an Jiaotong University,2011,45(9): 94-100. (in Chinese)
  • 加载中
图(16) / 表(2)
计量
  • 文章访问数:  728
  • HTML浏览量:  290
  • PDF量:  298
  • 被引次数: 0
出版历程
  • 收稿日期:  2021-07-30
  • 网络出版日期:  2022-10-12

目录

    /

    返回文章
    返回