The influence of wedge diffuser blade number and divergence angle on the performance of a high pressure ratio centrifugal compressor

被引:0
作者
Yi Wang
Ge Han
Xingen Lu
Junqiang Zhu
机构
[1] Central South University,School of Aeronautics and Astronautics
[2] Chinese Academy of Sciences,Institute of Engineering Thermophysics
来源
Journal of Thermal Science | 2018年 / 27卷
关键词
Wedge diffuser; Blade number; Diffuser angle; High pressure ratio; Centrifugal compressor;
D O I
暂无
中图分类号
学科分类号
摘要
Wedge diffuser is widely used in centrifugal compressors due to its high performance and compact size. This paper is aimed to research the influence of wedge diffuser blade number and divergence angle on centrifugal compressor performance. The impact of wedge diffuser blade number on compressor stage performance is investigated, and then the wedge diffusers with different divergence angle are studied by varying diffuser wedge angle and blade number simultaneously. It is found that wedge diffuser with 27 blades could have about 0.8% higher adiabatic efficiency and 0.14 higher total pressure ratio than the wedge diffuser with 19 blades and the best compressor performance is achieved when diffuser divergence angle is 8.3°.These results could give some advices on centrifugal compressor design.
引用
收藏
页码:17 / 24
页数:7
相关论文
共 13 条
[1]  
Palmer D. L.(1995)Design and Development of an Advanced Two-Stage Centrifugal Compressor ASME Journal of Turbomachinery 117 118-126
[2]  
Watermann W. F.(2004)Approach to High Performance Transonic Centrifugal Compressor Journal of Propulsion and Power 20 164-170
[3]  
Oana M.(2000)Effects of Inlet Flow Field Conditions on the Performance of Centrifugal Compressor Diffusers: Part 1- Discrete Passage Diffuser Journal of Turbomachinery 122 1-10
[4]  
Filipenco V. G.(1967)Performance and Design of Straight, 2D Diffusers Journal of Basic Engineering 89 1412-282
[5]  
Deniz S.(1980)Straight-walled Twodimensional Diffusers-transitory Stall and Peak Pressure Recovery Trans ASME Journal of Fluids Engineering 102 275-384
[6]  
Johnston J. M.(1973)Further Data on the Pressure Recovery of Straight-channel, Single-plane Divergence Diffusers at High Subsonic Mach Numbers ASME Journal of Fluids Engineering 95 373-undefined
[7]  
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[8]  
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[9]  
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[10]  
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