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压比和雷诺数对压气机级间篦齿封严流动特性的影响

刘高文 陈凯 刚铁 郑海亮

刘高文, 陈凯, 刚铁, 郑海亮. 压比和雷诺数对压气机级间篦齿封严流动特性的影响[J]. 航空动力学报, 2015, 30(7): 1554-1560. doi: 10.13224/j.cnki.jasp.2015.07.003
引用本文: 刘高文, 陈凯, 刚铁, 郑海亮. 压比和雷诺数对压气机级间篦齿封严流动特性的影响[J]. 航空动力学报, 2015, 30(7): 1554-1560. doi: 10.13224/j.cnki.jasp.2015.07.003
LIU Gao-wen, CHEN Kai, GANG Tie, ZHENG Hai-liang. Influences of pressure ratio and Reynolds number on flow characteristics of labyrinth seal in compressor stator well[J]. Journal of Aerospace Power, 2015, 30(7): 1554-1560. doi: 10.13224/j.cnki.jasp.2015.07.003
Citation: LIU Gao-wen, CHEN Kai, GANG Tie, ZHENG Hai-liang. Influences of pressure ratio and Reynolds number on flow characteristics of labyrinth seal in compressor stator well[J]. Journal of Aerospace Power, 2015, 30(7): 1554-1560. doi: 10.13224/j.cnki.jasp.2015.07.003

压比和雷诺数对压气机级间篦齿封严流动特性的影响

doi: 10.13224/j.cnki.jasp.2015.07.003
详细信息
    作者简介:

    刘高文(1974-),男,四川广安人,副教授,博士,研究领域为发动机空气系统和旋转盘腔中的流动传热.

  • 中图分类号: V231

Influences of pressure ratio and Reynolds number on flow characteristics of labyrinth seal in compressor stator well

  • 摘要: 为了解压气机级间封严的流动特性,以某航空发动机压气机为研究对象,对带有进出口旋转盘腔的级间篦齿结构进行了数值模拟.在压比范围为1.05~1.30,雷诺数范围为100~50000下,研究了压比和雷诺数对篦齿泄漏特性、旋流特性和风阻温升特性的影响,对比了包括篦齿和进出口旋转盘腔的系统参数与仅含篦齿的直齿参数的不同.计算结果表明进出口旋转盘腔对篦齿的流动特性有较大的影响;随着压比的增大,流量系数增加,封严效果下降,出口旋转比和风阻温升减小;随着雷诺数的增大,流量系数明显增大,出口旋转比和风阻温升也显著减小;在高雷诺数时,流量系数、出口旋转比和风阻温升变化幅度微小.

     

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出版历程
  • 收稿日期:  2014-01-22
  • 刊出日期:  2015-07-28

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