Investigation of Suction Flow Control on Centrifugal Compressor with Vaned Diffuser

被引:2
作者
Ak, Suleyman Emre [1 ,2 ]
Cadirci, Sertac [1 ]
机构
[1] Istanbul Tech Univ, Dept Mech Engn, TR-34437 Istanbul, Turkey
[2] Numesys Inc, TR-34758 Istanbul, Turkey
关键词
centrifugal compressor; CFD; suction flow control; stall; operation range; AIR INJECTION; STABILIZATION; STALL;
D O I
10.3390/en15020583
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
In this study, the effect of suction flow control on a centrifugal compressor at operation and stall flow rates was investigated using computational fluid dynamics (CFD). The compressor geometry was reconstructed from available open source profile data and the CFD analyses have been performed on this geometry using the appropriate mesh. To validate the CFD results, the compressor performance line was acquired and compared with the experimental results obtained at the design rotational speed. Then, suction flow control was employed at various suction slot positions with different suction flow rates to improve the performance of the compressor at operation and stall flow rates. As a result of the suction flow control trials, 0.85% increase in pressure ratio and 0.8% increase in adiabatic efficiency were achieved while the compressor was running at operation flow rate. The performance improvements corresponding to the stall flow rate of the compressor were 2.5% increase in pressure ratio and 2% increase in adiabatic efficiency.
引用
收藏
页数:12
相关论文
共 27 条
[1]  
Ansys Inc, 2020, ANSYS CFX SOLV THEOR
[2]   Assessment of Turbulence Model Predictions for an Aero-Engine Centrifugal Compressor [J].
Bourgeois, Jason A. ;
Martinuzzi, Robert J. ;
Savory, Eric ;
Zhang, Chao ;
Roberts, Douglas A. .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2011, 133 (01)
[3]  
Carretta M, 2017, PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2017, VOL 2C
[4]  
Cumpsty N.A., 1989, COMPRESSOR AERODYNAM
[5]   Optimization of Return Channels of High Flow Rate Centrifugal Compressor Stages Using CFD Methods [J].
Galerkin, Yuri ;
Rekstin, Aleksey ;
Marenina, Lyubov ;
Drozdov, Aleksandr ;
Solovyeva, Olga ;
Semenovskiy, Vasiliy .
ENERGIES, 2020, 13 (22)
[6]   Experimental and numerical investigations of surge extension on a centrifugal compressor with vaned diffuser using steam injection [J].
Gao, Chuang ;
Huang, Weiguang ;
Zheng, Tianhua ;
Yang, Kang ;
Yang, Haosen ;
Cao, Yun .
International Journal of Rotating Machinery, 2017, 2017
[7]   Assessment of some stall-onset criteria for centrifugal compressors [J].
Ghenaiet, Adel ;
Khalfallah, Smail .
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 88 :193-207
[8]  
Gibson L., 2017, Journal of the Global Power and Propulsion Society, V1, P142, DOI [10.22261/2ii890, DOI 10.22261/2II890]
[9]   Optimization of the Efficiency of Stall Control Using Air Injection for Centrifugal Compressors [J].
Halawa, Taher ;
Gadala, Mohamed S. ;
Alqaradawi, Mohamed ;
Badr, Osama .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2015, 137 (07)
[10]   Effect of Double Air Injection on Performance Characteristics of Centrifugal Compressor [J].
Hirano, Toshiyuki ;
Takano, Mizuki ;
Tsujita, Hoshio .
JOURNAL OF THERMAL SCIENCE, 2015, 24 (01) :10-16