Steady state performance evaluation of variable geometry twin-entry turbine

被引:43
作者
Romagnoli, A. [1 ]
Martinez-Botas, R. F. [1 ]
Rajoo, S. [2 ]
机构
[1] Univ London Imperial Coll Sci Technol & Med, Dept Mech Engn, London SW7 2AZ, England
[2] Univ Teknol Malaysia, Dept Automot Engn, Fac Mech Engn, Johor Baharu 81310, Malaysia
关键词
Turbochargers; Internal combustion engines; Turbomachinery; Radial turbines;
D O I
10.1016/j.ijheatfluidflow.2010.12.002
中图分类号
O414.1 [热力学];
学科分类号
摘要
This paper presents the results from an experimental investigation conducted on different turbine designs for an automotive turbocharger. The design progression was based on a commercial nozzleless unit that was modified into a variable geometry single and twin-entry turbine. The main geometrical parameters were kept constant for all the configurations and the turbine was tested under steady flow conditions. A significant depreciation in efficiency was measured between the single and twin-entry configuration due to the mixing effects. The nozzleless unit provides the best compromise in terms of performance at different speeds. The twin-entry turbine was also tested under partial and unequal admissions. Based on the test results a method to determine the swallowing capacity under partial admission given the full admission map is presented. The test results also showed that the turbine swallowing capacity under unequal admission is linked to the full admission case. (c) 2010 Elsevier Inc. All rights reserved.
引用
收藏
页码:477 / 489
页数:13
相关论文
共 16 条
[1]  
Abidat M., 1991, Ph.D. Thesis,
[2]  
ARCOUMANIS C, 1995, T ASME, V95, pGT210
[3]  
BAINES NC, 1990, C405005 I MECH ENG, P7
[4]  
BAINES NC, 1994, C48400694 I MECH ENG, P78
[5]  
CAPOBIANCO M, 1993, P ASME 93
[6]  
Ghassemi S, 2005, IRAN J SCI TECHNOL B, V29, P145
[7]   Flow and performance characteristics of twin-entry radial turbine under full and extreme partial admission conditions [J].
Hajilouy-Benisi, A. ;
Rad, M. ;
Shahhosseini, M. R. .
ARCHIVE OF APPLIED MECHANICS, 2009, 79 (12) :1127-1143
[8]  
HAKEEM I, 1995, THESIS IMPERIAL COLL
[9]  
Japikse D., 1994, INTRO TURBOMACHINERY
[10]  
Karamanis N., 2000, Ph.D. Thesis