Experimental study on bladeless turbine using incompressible working medium

被引:21
作者
Li, Ruixiong [1 ]
Wang, Huanran [1 ]
Yao, Erren [1 ]
Li, Meng [1 ]
Nan, Weigang [1 ]
机构
[1] Xi An Jiao Tong Univ, Dept Fluid Machinery & Engn, Xian 710049, Shaanxi, Peoples R China
基金
中国国家自然科学基金;
关键词
Bladeless turbine; experiment; numerical; entry and exit losses; loss model; ROTATING-DISKS; PERFORMANCE; FLOW; EFFICIENCY; FLUID;
D O I
10.1177/1687814016686935
中图分类号
O414.1 [热力学];
学科分类号
摘要
The bladeless turbine has a promising future as a new power generation system. To explore the operating characteristics of the turbine, a bladeless turbine experimental platform with an incompressible working medium was designed and built. The relationships among performance parameters were analysed in experiments, and studies were conducted on the flow characteristics of the working medium inside the turbine using numerical simulation software. The causes of entry and exit losses were analysed. The data acquired by simulation were consistent with the result of calculations using the partial loss model developed in this article, which means that this model is capable of calculating the partial loss of a bladeless turbine and is thus suitable for the design and optimization of bladeless turbines.
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页数:12
相关论文
共 34 条
[1]  
Armstrong J.H., 1952, THESIS
[2]  
Awasthi K, 2014, INT J ENG TRENDS TEC, V13, P98
[3]   LAMINAR INWARD FLOW OF AN INCOMPRESSIBLE FLUID BETWEEN ROTATING DISKS WITH FULL PERIPHERAL ADMISSION [J].
BOYD, KE ;
RICE, W .
JOURNAL OF APPLIED MECHANICS, 1968, 35 (02) :229-&
[4]   ENGINEERING APPLICATION OF EXPERIMENTAL UNCERTAINTY ANALYSIS [J].
COLEMAN, HW ;
STEELE, WG .
AIAA JOURNAL, 1995, 33 (10) :1888-1896
[5]  
Deam RT, 2008, J ENG GAS TURB POWER, V130, DOI [10.1115/1.2938516, 10.1115/1.293851]
[6]  
Deng Q, 2013, AM SOC MECH ENG, V6, pV6C
[7]  
Fuchs T, 2015, P 68 ANN M APS DIV F
[8]   A unified theory for the interpretation of total pressure and temperature in two-phase flows at subsonic and supersonic speeds [J].
Guha, A .
PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 1998, 454 (1970) :671-695
[9]   Effects of internal combustion and non-perfect gas properties on the optimum performance of gas turbines [J].
Guha, A .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2003, 217 (09) :1085-1099
[10]   Experiment and analysis for an improved design of the inlet and nozzle in Tesla disc turbines [J].
Guha, A. ;
Smiley, B. .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2010, 224 (A2) :261-277