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减压腔宽度对刷式密封泄漏特性和滞后效应的影响

李朋飞 胡娅萍 陈文洋

李朋飞, 胡娅萍, 陈文洋. 减压腔宽度对刷式密封泄漏特性和滞后效应的影响[J]. 航空动力学报, 2020, 35(7): 1473-1481. doi: 10.13224/j.cnki.jasp.2020.07.015
引用本文: 李朋飞, 胡娅萍, 陈文洋. 减压腔宽度对刷式密封泄漏特性和滞后效应的影响[J]. 航空动力学报, 2020, 35(7): 1473-1481. doi: 10.13224/j.cnki.jasp.2020.07.015
LI Pengfei, HU Yaping, CHEN Wenyang. Influence of axial wide of pressure relief chamber on leakage characteristics and hysteresis of brush seals[J]. Journal of Aerospace Power, 2020, 35(7): 1473-1481. doi: 10.13224/j.cnki.jasp.2020.07.015
Citation: LI Pengfei, HU Yaping, CHEN Wenyang. Influence of axial wide of pressure relief chamber on leakage characteristics and hysteresis of brush seals[J]. Journal of Aerospace Power, 2020, 35(7): 1473-1481. doi: 10.13224/j.cnki.jasp.2020.07.015

减压腔宽度对刷式密封泄漏特性和滞后效应的影响

doi: 10.13224/j.cnki.jasp.2020.07.015

Influence of axial wide of pressure relief chamber on leakage characteristics and hysteresis of brush seals

  • 摘要: 对减压腔轴向宽度分别为0、04 mm和06 mm的基本型和两种低滞后刷式密封结构进行了静态和动态下压差升降和转子转速升降循环试验,并对其泄漏特性和滞后效应进行了研究。研究结果表明:压差大于02 MPa后,同一压差下的动态泄漏系数比静态降低约14%~20%;低滞后结构的密封性能优于基本型,其泄漏系数最高比基本型降低约20%;静态压差升降循环中,减压腔轴向宽度为06 mm的低滞后结构的滞后效应最强;动态的压差升降循环中,基本型结构的滞后效应最强。转子转速升降循环前后,w为06 mm结构泄漏系数减小约15%,滞后效应最强,减压腔轴向宽度为04 mm结构几乎不存在滞后效应;三种结构中,减压腔轴向宽度为04 mm的结构密封性能最优,滞后效应也最弱。

     

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出版历程
  • 收稿日期:  2019-11-19
  • 刊出日期:  2020-07-28

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