首页> 外文期刊>Concurrency and computation: practice and experience >Experimental investigation of effect of tooth geometrical parameters to flow characteristics in slant labyrinth seals
【24h】

Experimental investigation of effect of tooth geometrical parameters to flow characteristics in slant labyrinth seals

机译:齿形参数对斜迷宫式密封流动特性影响的实验研究

获取原文
获取原文并翻译 | 示例

摘要

An experiment investigation was made to study the influence of the geometry parameters ofslant straight-through labyrinth seals on sealing characteristics. 22 models with different geometryparameters were designed, and the geometry parameters studied include seal clearance, finheight, fin pitch, fin tip thickness, and fin number. The results showed that, when p_0/p_n rangedfrom 1.2 to 1.8, the discharge coefficient increased with the drop pressure ratio, seal clearance,and fin tip thickness and decreased with fin height, fin pitch, and fin number. The rank of sensitivityof each parameter's variation in the unit size on sealing characteristics is seal clearance, fin tipthickness, fin pitch, back angle, fin height, and front angle. The correlation of different parameterswere summarized for the designing of advanced labyrinth seals.
机译:通过实验研究了 r nslant直通迷宫式密封件的几何参数对密封性能的影响。设计了22个具有不同几何参数的模型,所研究的几何参数包括密封间隙,散热片高度,散热片间距,散热片尖端厚度和散热片数量。结果表明,当p_0 / p_n的范围从1.2到1.8时,排放系数随着降压比,密封间隙,r和翅片尖端厚度的增加而增大,而随翅片高度,翅片间距和翅片数量的减小而减小。 。密封性能上,每个参数在单位尺寸上变化的灵敏度等级 r n为密封间隙,翅片尖端 r n厚度,翅片间距,后角,翅片高度和前角。总结了高级迷宫式密封件设计中不同参数的相关性。

著录项

  • 来源
    《Concurrency and computation: practice and experience》 |2018年第24期|e4951.1-e4951.9|共9页
  • 作者单位

    Jiangsu Province Key Laboratory of AerospacePower System, College of Energy and Power,Nanjing University of Aeronautics andAstronautics, Nanjing 210016, China;

    Jiangsu Province Key Laboratory of AerospacePower System, College of Energy and Power,Nanjing University of Aeronautics andAstronautics, Nanjing 210016, China;

    Jiangsu Province Key Laboratory of AerospacePower System, College of Energy and Power,Nanjing University of Aeronautics andAstronautics, Nanjing 210016, China;

    Jiangsu Province Key Laboratory of AerospacePower System, College of Energy and Power,Nanjing University of Aeronautics andAstronautics, Nanjing 210016, China;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    correlational function; discharge coefficient; geometry parameters; rank of sensitivity; slant labyrinth seals;

    机译:相关函数放电系数几何参数;敏感度等级斜迷宫式海豹;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号