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亚声速针栓燃气阀和超声速针栓燃气阀性能对比

黄楚九 魏志军 李志远 高紫晴 李大林

黄楚九, 魏志军, 李志远, 等. 亚声速针栓燃气阀和超声速针栓燃气阀性能对比[J]. 航空动力学报, 2026, 41(1):20240855 doi: 10.13224/j.cnki.jasp.20240855
引用本文: 黄楚九, 魏志军, 李志远, 等. 亚声速针栓燃气阀和超声速针栓燃气阀性能对比[J]. 航空动力学报, 2026, 41(1):20240855 doi: 10.13224/j.cnki.jasp.20240855
HUANG Chujiu, WEI Zhijun, LI Zhiyuan, et al. Performance comparison between subsonic and supersonic needle gas valves[J]. Journal of Aerospace Power, 2026, 41(1):20240855 doi: 10.13224/j.cnki.jasp.20240855
Citation: HUANG Chujiu, WEI Zhijun, LI Zhiyuan, et al. Performance comparison between subsonic and supersonic needle gas valves[J]. Journal of Aerospace Power, 2026, 41(1):20240855 doi: 10.13224/j.cnki.jasp.20240855

亚声速针栓燃气阀和超声速针栓燃气阀性能对比

doi: 10.13224/j.cnki.jasp.20240855
详细信息
    作者简介:

    黄楚九(2000-),男,博士生,主要从事姿轨控燃气阀研究。E-mail:3220235014@bit.edu.cn

    通讯作者:

    魏志军(1967-),男,教授,博士,主要从事固体火箭发动机研究。E-mail:wzj@bit.edu.cn

  • 中图分类号: V438

Performance comparison between subsonic and supersonic needle gas valves

  • 摘要:

    针栓燃气阀是固体姿轨控火箭发动机能量管理的关键部件。针栓燃气阀可以分为亚声速构型和超声速构型,两种阀门分别主要工作在亚声速段和超声速段,其工作特性和应用场合也各不相同。本文采用CFD数值计算方法,分析了多开度下两种阀门构型的流动损失、阀杆负载及热化学烧蚀等,并对比分析了两种结构阀门的优缺点。计算结果表明:两种阀门构型的流动损失都会随着开度的增大而减小,在工作条件相同的情况下超声速燃气阀流动损失更大。不同开度下,超声速阀的负载力更为稳定,并且大开度下超声速阀负载小,与此同时,阀杆结构尺寸对阀门负载具有很大影响。亚声速阀针栓阀杆处的热化学烧蚀率较超声速阀杆高,是超声速的5倍。超声速阀腔喉部处热化学烧蚀高,是亚声速阀的1.5倍。

     

  • 图 1  针栓式燃气阀

    Figure 1.  Needle-type gas valve

    图 2  燃气阀结构示意图

    Figure 2.  Schematic diagram of the gas valve structure

    图 3  出口压力与结果对比

    Figure 3.  Comparison of outlet pressure and results

    图 4  烧蚀率结果对比

    Figure 4.  Comparison of ablation rate results

    图 5  亚声速内流阀和超声速内流阀的数值计算模型

    Figure 5.  Numerical simulation models of subsonic and supersonic internal flow valves

    图 6  网格无关性验证

    Figure 6.  Grid independence verification

    图 7  亚声速阀马赫数云图

    Figure 7.  Mach number contour of the subsonic valve

    图 8  亚声速阀马赫数折线图

    Figure 8.  Streamwise Mach number variation in the subsonic valve

    图 9  超声速阀马赫数云图

    Figure 9.  Mach number contours of the supersonic valve

    图 10  超声速阀马赫数折线图

    Figure 10.  Mach number distributions under different valve openings

    图 11  亚声速阀总压损失特性

    Figure 11.  Total pressure loss characteristics of the subsonic valve

    图 12  超声速阀总压损失特性

    Figure 12.  Total pressure loss characteristics of the supersonic valve

    图 13  阀门总压损失

    Figure 13.  Total pressure loss of the valve

    图 14  阀门推力损失

    Figure 14.  Valve thrust loss characteristics

    图 15  亚声速阀压力分布曲线

    Figure 15.  Pressure distribution curve of subsonic valve

    图 16  超声速阀压力分布曲线

    Figure 16.  Pressure distribution in supersonic valve

    图 17  阀门针栓开闭过程负载

    Figure 17.  Load characteristics during needle valve opening/closing process

    图 18  阀门针栓关闭过程负载组成(胶圈力为阻力,动摩擦)

    Figure 18.  Load components during needle valve closing process (the rubber band force is the resistance, and the kinetic friction)

    图 19  阀门针栓开启过程负载组成(胶圈力为阻力,动摩擦)

    Figure 19.  Load components during needle valve opening process (the rubber band force is the resistance, and the kinetic friction)

    图 20  阀门稳定状态负载

    Figure 20.  Steady-state load characteristics of the valve

    图 21  阀门针栓稳定状态下负载组成(胶圈力为助力,静摩擦)

    Figure 21.  Steady-state load components of needle valve(the rubber band force is the driving force, and the static friction)

    图 22  亚声速阀不同开度针栓受力变化情况

    Figure 22.  Variation of needle force with opening degree in subsonic valve

    图 23  超声速阀不同开度针栓受力变化情况

    Figure 23.  Supersonic valve needle force variation across opening degrees

    图 24  不同尺寸阀杆开启过程负载力

    Figure 24.  Opening process load forces of different-sized valve stems

    图 25  阀杆壁面温度分布曲线

    Figure 25.  Wall temperature distribution curves of valve stems

    图 26  阀杆壁面热流密度分布曲线

    Figure 26.  Wall heat flux distribution curves of valve stems

    图 27  阀杆壁面烧蚀率分布曲线

    Figure 27.  Wall ablation rate distribution curves of valve stems

    表  1  亚超声速阀尺寸参数

    Table  1.   Dimensional parameters of subsonic and supersonic valve configurations mm

    参数亚声速阀超声速阀
    $ {L}_{\mathrm{a}1} $11.911.9
    $ {L}_{\mathrm{a}2} $44.844.8
    $ {d}_{\mathrm{a}1} $99
    $ {d}_{\mathrm{a}2} $99
    $ {d}_{\mathrm{a}3} $4.54.9
    $ {d}_{\mathrm{a}4} $1414
    $ {d}_{\mathrm{a}5} $10.814.3
    $ {d}_{\mathrm{a}6} $1414
    下载: 导出CSV

    表  2  烧蚀反应方程式及其动力参数

    Table  2.   Ablation reaction equations and associated kinetic parameters

    反应类型 A/($ {{\mathrm{m}}}^{2}\cdot {\mathrm{s}}\cdot {{\mathrm{Pa}}}^{0.5}/{\mathrm{kg}} $) $ \beta $ E/$ {10}^{5} $ (J/mol) n
    $ {{\rm{C}}}_{ ({{\mathrm{s}}}) }+{{\mathrm{H}}}_{2}{\mathrm{O}}\to {\mathrm{CO}}+{{\mathrm{H}}}_{2} $ 1.51×103 0 2.88 0.5
    $ {{\mathrm{C}}}_{ ({\mathrm{s}}) }+{{\mathrm{CO}}}_{2}\to 2{\mathrm{CO}} $ 28.27 0 2.88 0.5
    下载: 导出CSV

    表  3  亚声速阀不同开度下各个区域总压损失百分比

    Table  3.   Total pressure loss percentage in different regions of the subsonic valve configuration at various opening levels %

    开度/mm亚声速区亚声速转弯区喉部区膨胀区
    20.001340.00348.3914.4
    30.003230.04636.046.4
    40.004500.06720.125.5
    全开0.022720.0725.914.3
    下载: 导出CSV

    表  4  超声速阀不同开度下各个区域总压损失百分比

    Table  4.   Total pressure loss percentage in different regions of the supersonic valve configuration at various opening levels %

    开度/mm亚声速区喉部区阀腔区转弯区膨胀区
    20.014925.7667.3950.990.435
    30.088313.1267.1711.612.000
    40.12209.19961.5081.673.010
    全开0.18492.79160.0541.733.550
    下载: 导出CSV

    表  5  亚声速阀与超声速阀关键结构尺寸取值

    Table  5.   Key structural dimensions of subsonic and supersonic valve configurations mm

    尺寸编号 亚声速阀 超声速阀
    $ {d}_{{\mathrm{a}}1} $ $ {d}_{{\mathrm{a}}2} $ $ {d}_{{\mathrm{a}}1} $ $ {d}_{{\mathrm{a}}2} $
    1 9 9 9 9
    2 9 7 9 7
    3 9 5 9 5
    4 9 11 9 11
    5 9 13 9 13
    下载: 导出CSV
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  • 收稿日期:  2024-12-25
  • 网络出版日期:  2025-04-28

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