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组合式弹性金属密封泄漏特性数值与实验研究

黄婵媛 温帅方 孙丹 李玉 杨泽敏 张晓林 吴丽军

黄婵媛, 温帅方, 孙丹, 等. 组合式弹性金属密封泄漏特性数值与实验研究[J]. 航空动力学报, 2025, 40(5):20230484 doi: 10.13224/j.cnki.jasp.20230484
引用本文: 黄婵媛, 温帅方, 孙丹, 等. 组合式弹性金属密封泄漏特性数值与实验研究[J]. 航空动力学报, 2025, 40(5):20230484 doi: 10.13224/j.cnki.jasp.20230484
HUANG Chanyuan, WEN Shuaifang, SUN Dan, et al. Numerical and experimental study on leakage characteristics of combined elastic metal seal[J]. Journal of Aerospace Power, 2025, 40(5):20230484 doi: 10.13224/j.cnki.jasp.20230484
Citation: HUANG Chanyuan, WEN Shuaifang, SUN Dan, et al. Numerical and experimental study on leakage characteristics of combined elastic metal seal[J]. Journal of Aerospace Power, 2025, 40(5):20230484 doi: 10.13224/j.cnki.jasp.20230484

组合式弹性金属密封泄漏特性数值与实验研究

doi: 10.13224/j.cnki.jasp.20230484
基金项目: 国家自然科学基金(52075346); 辽宁省教育厅面上项目(LJKZ0179); 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:

    黄婵媛(1999-),女,硕士生,主要从事接触式封严密封性能研究。E-mail:2583204198@qq.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 and experimental study on leakage characteristics of combined elastic metal seal

  • 摘要:

    为研究组合式弹性金属密封泄漏特性,针对接触泄漏通道、间隙泄漏通道建立两种泄漏特性数值计算模型,在宏观力学特性数值计算结果的基础上,基于分形理论建立了考虑实际粗糙接触表面的组合式弹性金属密封泄漏特性求解模型,并设计搭建了组合式弹性金属密封泄漏特性实验装置,在实验验证数值求解模型准确性的基础上,研究了组合式弹性金属密封在不同内外腔压差、压缩量下的力学特性与泄漏特性,并分析表面粗糙度影响下的密封机理。研究结果表明:等效应力随着内外腔压差的增大、压缩量的增加而不断增大;而泄漏量随压缩量的增加、温度的增加而逐渐减小,在最大压比、最大压缩量条件下泄漏量较初始条件减少24.12%;表面粗糙度对组合式弹性金属密封的泄漏量影响较大,表面粗糙度以及压缩量会影响接触处泄漏通道间隙进而影响其流场分布,本文提出的考虑表面粗糙度的数值计算方法较传统方法误差较小,可较为准确计算组合式弹性金属密封的泄漏量,为组合式弹性金属密封泄漏特性分析提供理论依据。

     

  • 图 1  组合式弹性金属密封位置图

    Figure 1.  Schematic diagram of the position for combined elastic metal seal

    图 2  组合式弹性金属密封泄漏通道表征图

    Figure 2.  Schematic diagram of leakage passage for combined elastic metal seal

    图 3  粗糙接触表面接触示意图

    Figure 3.  Schematic diagram of the contact between rough and smooth surface

    图 4  间隙泄漏几何模型

    Figure 4.  Gap leakage geometric model

    图 5  组合式弹性金属密封实物图

    Figure 5.  Physical diagram of the combined elastic metal seal

    图 6  简化后的组合式弹性金属密封模型

    Figure 6.  Simplified combined elastic metal seal

    图 7  力学特性求解模型网格划分

    Figure 7.  Meshing of the mechanical properties solving model

    图 8  泄漏模型建模流程

    Figure 8.  Leakage modeling process

    图 9  泄漏特性求解模型网格划分

    Figure 9.  Meshing of the leakage model

    图 10  网格无关性验证

    Figure 10.  Grid independence verification

    图 11  实验装置示意图

    Figure 11.  Diagram of experimental device

    图 12  实验装置实物图

    Figure 12.  Physical diagram of the experimental device

    图 13  准确性验证

    Figure 13.  Accuracy verification

    图 14  接触应力随压缩量变化关系

    Figure 14.  Relationship between contact stress and compression amount

    图 15  弹性片等效应力分布

    Figure 15.  Equivalent stress distribution of elastic plate

    图 16  弹性片变形图

    Figure 16.  Elastic sheet deformation diagram

    图 17  泄漏量随压比变化关系

    Figure 17.  Relationship between leakage and pressure ratio

    图 18  泄漏量随压缩量变化关系

    Figure 18.  Relationship between leakage and compression

    图 19  泄漏量随温度变化关系

    Figure 19.  Relationship between leakage and compression

    图 20  接触泄漏模型流体速度矢量图

    Figure 20.  Contact leakage model fluid velocity vector diagram

    图 21  接触泄漏模型压力分布云图

    Figure 21.  Contact leakage model pressure distribution cloud

    图 22  不同接触泄漏间隙速度矢量图

    Figure 22.  Velocity vector diagram of different leakage gaps

    图 23  不同压缩量下速度变化关系

    Figure 23.  Relationship of velocity change under different compression

    表  1  材料参数

    Table  1.   Material parameters

    温度
    T/K
    抗拉强度
    σb/MPa
    屈服强度
    σs/MPa
    弹性模量
    E/GPa
    29314651265203
    92311801030167
    下载: 导出CSV

    表  2  力学特性求解模型边界条件

    Table  2.   Boundary conditions of the mechanical properties solving model

    部件接触设置模块
    内、外封严片Bond
    外封严片与顶块Rough
    弹性片与封严片Frictional
    封严片与底座Frictional
    下载: 导出CSV

    表  3  泄漏模型工况参数

    Table  3.   Operating parameters of the leakage model

    参数数值
    出口压力/MPa0.1
    进口压比1~4
    接触应力/MPa60~160
    表面粗糙度/μm0.8~3.2
    下载: 导出CSV
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  • 收稿日期:  2023-07-26
  • 网络出版日期:  2024-08-29

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