期刊文献+

高低齿汽封与蜂窝汽封及孔式阻尼汽封密封性能的比较 被引量:11

Comparison of Seal Performance Among Stepped Labyrinth, Honeycomb and Hole-pattern Damper Seal
下载PDF
导出
摘要 使用商用CFD软件Fluent对高低齿汽封、蜂窝汽封及孔式阻尼汽封进行了三维数值模拟,得到三种汽封在不同压比、轴转速和汽封相对间隙时的密封性能,并将高低齿汽封和蜂窝汽封计算值与试验数据进行了对比.结果表明:高低齿汽封流量系数随压比增大而增大,随转速加快而略有减小,随相对间隙的增大而减小;蜂窝汽封与孔式阻尼汽封的流量系数均随压比增大而减小,随转速加快而略有减小,基本呈直线变化规律,随相对间隙的增大而增大;在相同的条件下,蜂窝汽封的漏汽量比高低齿汽封的漏气量减少10%,而孔式阻尼汽封的漏汽量比蜂窝汽封漏汽量减少6%. A 3D numerical simulation was performed on the stepped labyrinth, honeycomb and hole pattern damper seal using the commercial CFD software Fluent, during which the seal performance of above 3 seals was respectively obtained at different pressure ratios, rotating speeds and relative clearances, while a com- parison made between calculated results and experimental data for the stepped labyrinth seal and honeycomb seal. Results show that for the stepped labyrinth seal, the flow coefficient increases with rising pressure ratio and reducing relative clearance, and drops slightly with rising rotating speed; whereas for both the honeycomb and hole-pattern damper seal, the flow coefficient increases with reducing pressure ratio and rising relative clearance, and drops slightly with rising rotating speed, indicating basi- cally a linear variation law. Under same conditions, the steam leakage of a honeycomb seal is 10% less than that of a labyrinth seal, and 6% higher than that of a hole-pattern damper seal.
出处 《动力工程学报》 CAS CSCD 北大核心 2012年第7期508-512,共5页 Journal of Chinese Society of Power Engineering
关键词 高低齿汽封 蜂窝汽封 孔式阻尼汽封 密封性能 stepped labyrinth seal honeycomb seal hole-pattern damper seal seal performance
  • 相关文献

参考文献7

二级参考文献15

  • 1王旭,张文平,马胜远,诸振友.转子蜂窝密封封严特性的试验研究[J].热能动力工程,2004,19(5):521-525. 被引量:25
  • 2李军,邓清华,丰镇平.蜂窝汽封和迷宫式汽封流动性能比较的数值研究[J].中国电机工程学报,2005,25(16):108-111. 被引量:70
  • 3张延蜂,王绍民.蜂窝式密封及汽轮机相关节能技术的研究与应用[M].北京:中国电力出版社,2007.
  • 4Schramm V, Willenborg K, Kim S, et al. Influence of a hone;ycombfacing on the flow through a stepped labyrinth seal [J]. ASME J, Eng. Gas Turbine Power, 2000, 124: 140-146.
  • 5Schlienger J, Pfau A, Kalfas A L, et al. Effects of labyrinth seal variation on multistage axial turbine flow [c]. GT2003 - 38270, Proceedings of ASME turbo Expo 2003,Power for Land, Sea, and Air, June 16 - 19,2003 Atlanta, Georgia, USA.
  • 6Schlienger J, Pfau A, Kalfas A L et al. Effects of labyrinth seal variation on multistage axial turbine flow[C]. GT2003-38270,Proceedings of ASME Turbo Expo 2003, Power for Land, Sea, and Air, June 16-19, 2003Atlanta, Georgia, USA.
  • 7Schramm V, Willenborg K, Kim S et al. Influence of a honeycomb-facing on the flow through a stepped labyrinth seal[J]. ASME J. Eng. GasTurbine Power, 2000, 124: 140-146.
  • 8FLUENT User's Guide[S]. Version 6.0, Fluent Inc., Centerra Resource Park, Lebanon, NH, 2001.
  • 9梁小兵,冯增国,孔祥林,张粉.汽轮机级间吸漏气量对级性能影响的研究[J].东方电气评论,2008,22(2):7-9. 被引量:5
  • 10黄典贵,李雪松.大型旋转机械中汽封间隙流激振力的分析——非定常N-S解[J].中国电机工程学报,2000,20(6):75-78. 被引量:21

共引文献78

同被引文献69

引证文献11

二级引证文献36

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部