Numerical Investigation of Base-Setting of Stator's Stagger Angles for a 15-stage Axial-Flow Compressor  

作　　者：CHANG Hao ZHAO Weiguang JIN Donghai PENG Zeyan GUI Xingmin 

机构地区：[1]Aero-Engine Simulation Research Center,School of Energy and Power Engineering,Beihang University 37

出　　处：《Journal of Thermal Science》2014年第1期36-44,共9页热科学学报（英文版）

摘　　要：A 15-stage axial-flow compressor utilized in steel industry was studied in this paper. All the stator's stagger angles of the compressor are variable to ensure the multistage compressor operate effectively within a wide range of flow rate and meanwhile satisfy the demand for sufficient pressure ratio, adiabatic efficiency and stall margin. Three in all different base-settings of stator's stagger angles were presented and commercial CFD software was applied to obtain the overall performance characteristics. The results showed that both of the optimized base-settings improved the performances both in summer and winter conditions, although the adiabatic efficiency was somewhat decreased. Taking incidence angle and stage loading into consideration, differences among the three cases were analyzed in detail. On the basis of numerical computations, the performance could be effectively improved through adjusting the base-setting of stator's stagger angles.

关 键 词：multistage compressor stagger angle incidence angle variable stator 

分 类 号：TH45[机械工程—机械制造及自动化]