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陶瓷栅板密封泄漏特性数值方法研究

金冠男 孙丹 张国臣 刘胜 满延进 李建辉

金冠男, 孙丹, 张国臣, 等. 陶瓷栅板密封泄漏特性数值方法研究[J]. 航空动力学报, 2024, 39(11):20220169 doi: 10.13224/j.cnki.jasp.20220169
引用本文: 金冠男, 孙丹, 张国臣, 等. 陶瓷栅板密封泄漏特性数值方法研究[J]. 航空动力学报, 2024, 39(11):20220169 doi: 10.13224/j.cnki.jasp.20220169
JIN Guannan, SUN Dan, ZHANG Guochen, et al. Study on numerical method of leakage characteristics of ceramic wafer seal[J]. Journal of Aerospace Power, 2024, 39(11):20220169 doi: 10.13224/j.cnki.jasp.20220169
Citation: JIN Guannan, SUN Dan, ZHANG Guochen, et al. Study on numerical method of leakage characteristics of ceramic wafer seal[J]. Journal of Aerospace Power, 2024, 39(11):20220169 doi: 10.13224/j.cnki.jasp.20220169

陶瓷栅板密封泄漏特性数值方法研究

doi: 10.13224/j.cnki.jasp.20220169
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)
详细信息
    作者简介:

    金冠男(1998-),男,硕士,主要从事陶瓷栅板密封泄漏特性研究

    通讯作者:

    张国臣(1984-),男,讲师,博士,主要从事航空发动机先进密封技术研究。E-mail:hngchzh@126.com

  • 中图分类号: V233.5

Study on numerical method of leakage characteristics of ceramic wafer seal

  • 摘要:

    理论分析了陶瓷栅板密封的泄漏特性,提出了考虑间隙泄漏与接触泄漏的陶瓷栅板密封泄漏特性的数值计算方法,在验证数值方法准确性基础上,通过分析进出口压比及温度等工况参数对闭合力、流量因子及泄漏量的影响,研究了工况参数下的陶瓷栅板密封流场、自密封效应及泄漏特性,揭示了自密封效应的变化规律,阐明了陶瓷栅板密封的泄漏机理。研究表明:陶瓷栅板密封闭合力随进出口压比的增加而增大,自密封效应随之增强,径向闭合力高于切向闭合力;气流温度对陶瓷栅板密封切向闭合力影响较小,径向闭合力随着气流温度的增加而平缓减小,径向自密封效应随之减弱;陶瓷栅板密封泄漏量随着进出口压比增加而增大,随着温度的增大而减小,且间隙泄漏在泄漏系统中占主要地位。提出的数值方法能准确计算陶瓷栅板密封泄漏量,为陶瓷栅板密封泄漏特性分析提供理论依据。

     

  • 图 1  空天飞机发动机尾喷管陶瓷栅板密封结构[4]

    Figure 1.  Structure of ceramic wafer seal in aerospace aircraft engine[4]

    图 2  陶瓷栅板密封结构示意图

    1 压缩弹簧;2 密封区域;3 陶瓷栅板;4 密封衬套;5 分隔板;6 供给气流;7 集气腔;8 装置主体。

    Figure 2.  Schematic diagram of structure of ceramic wafer seal

    图 3  陶瓷栅板密封受力分析图

    Figure 3.  Force analysis diagram of ceramic wafer seal

    图 4  陶瓷栅板密封间隙泄漏路径

    1 装置主体;2 分隔板;3 栅板前端;4 陶瓷栅板;5 栅板顶部;6 栅板底部;7 栅板末端。

    Figure 4.  Gap leakage path of ceramic wafer seal

    图 5  陶瓷栅板密封接触泄漏路径

    Figure 5.  Contact leakage path of ceramic wafer seal

    图 6  数值求解模型结构

    Figure 6.  Structure of solution model

    图 7  模型对比图

    Figure 7.  Model comparison diagram

    图 8  接触间隙泄漏数值模型建立过程

    Figure 8.  Process of establishing a numerical model of contact gap leakage

    图 9  陶瓷栅板密封网格划分

    Figure 9.  Grid division of ceramic wafer seal

    图 10  网格无关性验证

    Figure 10.  Grid independence verification

    图 11  模型准确性验证

    Figure 11.  Accuracy verification of model

    图 12  间隙泄漏流场分布云图

    Figure 12.  Flow field distribution cloud diagram of gap leakage

    图 13  接触泄漏流场分布云图

    Figure 13.  Flow field distribution cloud diagram of contact leakage

    图 14  工况参数对闭合力的影响规律

    Figure 14.  Influence law of working condition parameters on air force

    图 15  进出口压比对流量因子的影响规律

    Figure 15.  Influence law of pressure ratio of input and output on flow factor

    图 16  进出口压比对泄漏量的影响规律

    Figure 16.  Influence law of pressure ratio of input and output on leakage

    表  1  陶瓷栅板密封结构参数

    Table  1.   Structural parameters of ceramic wafer seal

    参数 数值
    密封出口长度l/mm 120
    泄漏路径1高长比h1/H1 7.9×10−4~9.8×10−4
    泄漏路径2高长比h2/H2 4.3×10−4~5.4×10−4
    密封腔底部宽高比b/h 0.7
    泄漏路径3宽长比b3/l3 1.8
    下载: 导出CSV

    表  2  陶瓷栅板密封边界条件

    Table  2.   Boundary conditions of ceramic wafer seal

    参数 数值或说明
    流体介质 理想空气
    湍流模型 Laminar
    流动区域 连续无滑移
    出口压力/MPa 0.1
    进出口压比 2~7
    进口温度/℃ 25~800
    下载: 导出CSV
  • [1] 薛俊川. 高超声速飞行器陶瓷栅板式密封设计研究[J]. 飞机设计,2016,36(2): 48-52. XUE Junchuan. Research of ceramic wafer seals for hypersonic vehicles[J]. Aircraft Design,2016,36(2): 48-52. (in Chinese

    XUE Junchuan. Research of ceramic wafer seals for hypersonic vehicles[J]. Aircraft Design, 2016, 36(2): 48-52. (in Chinese)
    [2] 廖龙文,曾鹏,陈军燕,等. 高超声速飞行器发展困境分析[J]. 飞航导弹,2019(12): 22-27. LIAO Longwen,ZENG Peng,CHEN Junyan,et al. Analysis of development dilemma of hypersonic vehicle[J]. Aerodynamic Missile Journal,2019(12): 22-27. (in Chinese

    LIAO Longwen, ZENG Peng, CHEN Junyan, et al. Analysis of development dilemma of hypersonic vehicle[J]. Aerodynamic Missile Journal, 2019(12): 22-27. (in Chinese)
    [3] 姜鹏,匡宇,谢小平,等. 国外高超声速飞行器研究现状及发展趋势[J]. 飞航导弹,2017(7): 19-24. JIANG Peng,KUANG Yu,XIE Xiaoping,et al. Research status and development trend of hypersonic vehicles abroad[J]. Aerodynamic Missile Journal,2017(7): 19-24. (in Chinese

    JIANG Peng, KUANG Yu, XIE Xiaoping, et al. Research status and development trend of hypersonic vehicles abroad[J]. Aerodynamic Missile Journal, 2017(7): 19-24. (in Chinese)
    [4] DUNLAP P,FINKBEINER J,STEINETZ B,et al. Design study of wafer seals for future hypersonic vehicles[R]. AIAA-2005-4153,2005.
    [5] STEINETZ B M. Evaluation of an innovative high-temperature ceramic wafer seal for hypersonic engine applications[D]. Cleveland,US: Case Western Reserve University,1991.
    [6] BISSON E E,ANDERSON W J. Advanced bearing technology[M]. Washington: Office of Scientific and Technical Information,National Aeronautics and Space Administration,1964.
    [7] 王昊辰. 几何可调超声速燃烧室热环境及热结构研究[D]. 哈尔滨: 哈尔滨工业大学,2017. WANG Haochen. The study on the thermal environment and thermal structure of ramjet variable geometry combustor[D]. Harbin: Harbin Institute of Technology,2017. (in Chinese

    WANG Haochen. The study on the thermal environment and thermal structure of ramjet variable geometry combustor[D]. Harbin: Harbin Institute of Technology, 2017. (in Chinese)
    [8] STEINETZ B M. Seal technology for hypersonic vehicle and propulsion: an overview[R]. NASA-E-16776, 2008.
    [9] 李鸿举,刘莹,黄伟峰,等. 栅板密封对流道侧壁变形的随动模型[J]. 机械工程学报,2020,56(23): 239-248. LI Hongju,LIU Ying,HUANG Weifeng,et al. Wafer seal servo model under distorted engine panel[J]. Journal of Mechanical Engineering,2020,56(23): 239-248. (in Chinese doi: 10.3901/JME.2020.23.239

    LI Hongju, LIU Ying, HUANG Weifeng, et al. Wafer seal servo model under distorted engine panel[J]. Journal of Mechanical Engineering, 2020, 56(23): 239-248. (in Chinese) doi: 10.3901/JME.2020.23.239
    [10] 徐洁. 微尺度器件及旋转干气密封微间隙内流体流动问题的研究[D]. 上海: 上海交通大学,2007. XU Jie. Research on flow in micro-device of mems and dry-gas seals[D]. Shanghai: Shanghai Jiao Tong University,2007. (in Chinese

    XU Jie. Research on flow in micro-device of mems and dry-gas seals[D]. Shanghai: Shanghai Jiao Tong University, 2007. (in Chinese)
    [11] CHILDS D W,WADE J. Rotordynamic-coefficient and leakage characteristics for hole-pattern-stator annular gas seals—measurements versus predictions[J]. Journal of Tribology,2004,126(2): 326-333. doi: 10.1115/1.1611502
    [12] 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

    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)
    [13] 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)
    [14] 包超英,孟祥铠,李纪云,等. 基于多孔介质模型的机械密封静压泄漏特性分析[J]. 润滑与密封,2015,40(3): 57-63. BAO Chaoying,MENG Xiangkai,LI Jiyun,et al. The leakage performance analysis of mechanical seals under hydrostatic pressures based on porous media model[J]. Lubrication Engineering,2015,40(3): 57-63. (in Chinese doi: 10.3969/j.issn.0254-0150.2015.03.012

    BAO Chaoying, MENG Xiangkai, LI Jiyun, et al. The leakage performance analysis of mechanical seals under hydrostatic pressures based on porous media model[J]. Lubrication Engineering, 2015, 40(3): 57-63. (in Chinese) doi: 10.3969/j.issn.0254-0150.2015.03.012
    [15] YAN W,KOMVOPOULOS K. Contact analysis of elastic-plastic fractal surfaces[J]. Journal of Applied Physics,1998,84(7): 3617-3624. doi: 10.1063/1.368536
    [16] 李伟平,贾占举,路茜,等. 金属封严环泄漏率预测方法[J]. 航空动力学报,2019,34(2): 368-375. LI Weiping,JIA Zhanju,LU Xi,et al. Method to predict leakage rate of metal seal ring[J]. Journal of Aerospace Power,2019,34(2): 368-375. (in Chinese

    LI Weiping, JIA Zhanju, LU Xi, et al. Method to predict leakage rate of metal seal ring[J]. Journal of Aerospace Power, 2019, 34(2): 368-375. (in Chinese)
    [17] 陶然,权晓波,徐建中. 微尺度流动研究中的几个问题[J]. 工程热物理学报,2001,22(5): 575-577. TAO Ran,QUAN Xiaobo,XU Jianzhong. Several questions in research of micro scale flow[J]. Journal of Engineering Thermophysics,2001,22(5): 575-577. (in Chinese doi: 10.3321/j.issn:0253-231X.2001.05.015

    TAO Ran, QUAN Xiaobo, XU Jianzhong. Several questions in research of micro scale flow[J]. Journal of Engineering Thermophysics, 2001, 22(5): 575-577. (in Chinese) doi: 10.3321/j.issn:0253-231X.2001.05.015
    [18] 闫寒. 随机粗糙表面效应下微流体器件中的流动特性研究[D]. 上海: 上海交通大学,2014. YAN Han. Investigation on characteristics of flow in different microfluidic devices with random surface roughness[D]. Shanghai: Shanghai Jiao Tong University,2014. (in Chinese

    YAN Han. Investigation on characteristics of flow in different microfluidic devices with random surface roughness[D]. Shanghai: Shanghai Jiao Tong University, 2014. (in Chinese)
    [19] 杨文健. 硬密封结构界面泄漏特性的数值分析及理论预测方法[D]. 武汉: 华中科技大学,2016. YANG Wenjian. Numerical analysis and theoretical prediction method of interface leakage characteristics of hard seal structure[D]. Wuhan: Huazhong University of Science and Technology,2016. (in Chinese

    YANG Wenjian. Numerical analysis and theoretical prediction method of interface leakage characteristics of hard seal structure[D]. Wuhan: Huazhong University of Science and Technology, 2016. (in Chinese)
    [20] 吕祥奎,杨文健,许国良,等. 密封结构中粗糙表面特征对其气密性的影响[J]. 机械工程学报,2015,51(23): 110-115. LÜ Xiangkui,YANG Wenjian,XU Guoliang,et al. The influence of characteristic of rough surface on gas sealing performance in seal structure[J]. Journal of Mechanical Engineering,2015,51(23): 110-115. (in Chinese doi: 10.3901/JME.2015.23.110

    LÜ Xiangkui, YANG Wenjian, XU Guoliang, et al. The influence of characteristic of rough surface on gas sealing performance in seal structure[J]. Journal of Mechanical Engineering, 2015, 51(23): 110-115. (in Chinese) doi: 10.3901/JME.2015.23.110
    [21] KE Yuchao,YAO Xuefeng,YANG Heng,et al. Gas leakage prediction of contact interface in fabric rubber seal based on a rectangle channel model[J]. Tribology Transactions,2017,60(1): 146-153. doi: 10.1080/10402004.2016.1154232
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  • 收稿日期:  2022-03-30
  • 网络出版日期:  2024-02-19

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