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转速对压气机级间篦齿封严影响的实验
引用本文:孔晓治,刘高文,雷昭,畅然,刘阳.转速对压气机级间篦齿封严影响的实验[J].航空动力学报,2016,31(7):1575-1582.
作者姓名:孔晓治  刘高文  雷昭  畅然  刘阳
作者单位:西北工业大学 动力与能源学院, 西安 710072
摘    要:对压气机级间篦齿封严进行了实验研究.不同压比下(1.05~1.3),研究转速(1500~8100r/min)对压气机级间篦齿封严的工作间隙变化、泄漏特性、温升特性和旋流特性的影响.结果表明:随转速的增大,工作间隙减小,流量降低;小压比时流量系数降低,较大压比时流量系数变化微小.系统风阻温升随转速增大而增大,转速越大时,其温升越明显.另外,随转速的增大,出口盘腔同一径向位置的旋转比增大;同一转速下,随出口盘腔径向位置的增大,旋转比降低. 

关 键 词:级间    篦齿封严    流量系数    风阻温升    旋转比
收稿时间:2015/11/2 0:00:00

Experiment on influence of rotational speeds on labyrinth seal in compressor stator well
KONG Xiao-zhi,LIU Gao-wen,LEI Zhao,CHANG Ran and LIU Yang.Experiment on influence of rotational speeds on labyrinth seal in compressor stator well[J].Journal of Aerospace Power,2016,31(7):1575-1582.
Authors:KONG Xiao-zhi  LIU Gao-wen  LEI Zhao  CHANG Ran and LIU Yang
Institution:School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072, China
Abstract:A rotating experiment rig with high rotational speeds was designed for the experiment of labyrinth seal in a compressor stator well. The influences of rotational speed (1500-8100r/min) on the working tip clearance, leakage characteristic, windage heating and swirl characteristics at different pressure ratios (1.05-1.30) were studied. Results show that the working tip clearance decreases and the mass flow rate declines with the increasing of the rotational speed. For low pressure ratios, increasing the rotational speed results in falling discharge coefficient, while the variation of discharge coefficient is relatively small for high pressure ratios. The windage heating of system increases as the rotational speed increases. Higher rotational speed gives much larger temperature rise. In addition, it is obvious that increasing the rotational speed leads to an increase of the swirl ratio at a specific radial location. However, the swirl ratio shows a decrease with increasing radius in the outlet cavity.
Keywords:stator well  labyrinth seal  discharge coefficient  windage heating  swirl ratio
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