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高转速对直通型篦齿封严特性影响的试验研究
引用本文:王鹏飞,刘玉芳,郭文,李江海,刘波.高转速对直通型篦齿封严特性影响的试验研究[J].燃气涡轮试验与研究,2007,20(2):45-48.
作者姓名:王鹏飞  刘玉芳  郭文  李江海  刘波
作者单位:中国燃气涡轮研究院,四川,成都,610500
摘    要:通过试验的方法研究了转速对篦齿封严特性的影响。分别在不考虑封严间隙变化和考虑封严间隙变化的情况下,在大转速和大压比变化范围内,详细地分析了篦齿流量参数随转速和压比的变化规律及变化大小,并对引起变化的主要原因进行了分析,得到了一些有价值的结论。

关 键 词:航空发动机  篦齿密封  旋转
文章编号:24488802
修稿时间:11 27 2006 12:00AM

Influence of High Rotational Speeds on the Labyrinth Sealing Characteristics
WANG Peng-fei,LIU Yu-fang,GUO Wen,LI Jiang-hai,LIU Bo.Influence of High Rotational Speeds on the Labyrinth Sealing Characteristics[J].Gas Turbine Experiment and Research,2007,20(2):45-48.
Authors:WANG Peng-fei  LIU Yu-fang  GUO Wen  LI Jiang-hai  LIU Bo
Institution:China Gas Turbine Establishment,Chengdu 610500 ,China
Abstract:Labyrinth seal was experimentally investigated to determine the effects of rotational speed and pressure ratio on the leakage through the seal.The effects of rotational speed on the flow parameter using dynamic clearance and static clearance were analyzed in detail respectively.The investigation encompasses a wide range of pressure ratio and rotational speed.The main reasons for flow parameter changes with rotational speed and pressure ratio were analyzed.A number of valuable conclusions have been drawn on the basis of analyses.
Keywords:aeroengine  labyrinth seal  rotation
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