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作 者:Yi-tong Liu Wu-qi Gong Ya Li Yi-tian Wang 刘一彤;宫武旗;李亚;王仪田
机构地区:[1]School of Energy and Power Engineering,Xi’an Jiaotong University [2]Xi'an Shaangu Power Co.,Ltd.
出 处:《风机技术》2024年第6期85-96,共12页Chinese Journal of Turbomachinery
基 金:National Science and Technology Major Project of China No.2017-V-0012-0064。
摘 要:The accurate parameters measurement of the flow field between the stages for axial compressors is a significant demand.This paper proposes an axial compressor inter-stage flow field high-precision test system,which mainly consists of a probe motion scanning mechanism,fully automated test control software,and data processing methods.Iterative correction is applied to the original readings obtained from the scanning tests to enhance testing accuracy.Using this test system,detailed tests are conducted on a 1.5-stage subsonic axial compressor under different operating conditions.The test results effectively captured the impact of surface roughness and tip clearance variations on compressor performance.The distribution characteristics of parameters measured in inter-stage sections can characterize the effects of blade wake area and changes in aerodynamic performance at different blade heights.The developed test system can be extended to multi-stage compressors.
关 键 词:Axial Compressor Test Method CALIBRATION Pneumatic Probe Flow Field
分 类 号:TH453[机械工程—机械制造及自动化]
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