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射流管伺服阀前置级压力特性

訚耀保 王玉

訚耀保, 王玉. 射流管伺服阀前置级压力特性[J]. 航空动力学报, 2015, 30(12): 3058-3064. doi: 10.13224/j.cnki.jasp.2015.12.032
引用本文: 訚耀保, 王玉. 射流管伺服阀前置级压力特性[J]. 航空动力学报, 2015, 30(12): 3058-3064. doi: 10.13224/j.cnki.jasp.2015.12.032
YIN Yao-bao, WANG Yu. Pressure characterization of the pre-stage of jet pipe servo valve[J]. Journal of Aerospace Power, 2015, 30(12): 3058-3064. doi: 10.13224/j.cnki.jasp.2015.12.032
Citation: YIN Yao-bao, WANG Yu. Pressure characterization of the pre-stage of jet pipe servo valve[J]. Journal of Aerospace Power, 2015, 30(12): 3058-3064. doi: 10.13224/j.cnki.jasp.2015.12.032

射流管伺服阀前置级压力特性

doi: 10.13224/j.cnki.jasp.2015.12.032
基金项目: 

国家自然科学基金(51175378,51275356)

航空科学基金(20120738001,20128038003)

详细信息
    作者简介:

    訚耀保(1965-),男,湖北麻城人,教授、博士生导师,博士,主要研究方向为极限环境下的液压与气动基础理论、飞行器能源与舵机、高速气动控制.E-mail:y-yin@tongji.edu.cn

  • 中图分类号: V233;TH138.52

Pressure characterization of the pre-stage of jet pipe servo valve

  • 摘要: 为分析射流管伺服阀射流管喷嘴高压射流区的特性,建立了射流管伺服阀前置级数学模型,得到了射流管偏移值、射流管喷嘴半径和接收孔半径对接收器压力分布、喷嘴出口流速及接收器的左右孔恢复压力的影响规律.流场分析发现射流管喷嘴的高速射流出口处容易产生旋涡,且存在环状负压效应.结果表明:高压射流状态下,射流管喷嘴半径增大,恢复压力增加;接收孔半径增大,恢复压力降低.接收孔半径与射流管喷嘴半径之比的最佳取值区间为[1.3,1.5].当射流管偏移值增大时,在偏移值增大一侧,射流管与接收孔之间的有效流体接收面积增大,射流管与接收孔之间的流体旋涡扩大,内部流场环状负压效应增加,接收孔恢复压力降低.

     

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出版历程
  • 收稿日期:  2014-05-06
  • 刊出日期:  2015-12-28

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