Investigation on effect of anti-cavitation edge on performance and leakage vortex characteristics of tubular turbine for ocean power generation

被引:5
作者
Li, Chenhao [1 ]
Luo, Xingqi [1 ,2 ]
Wu, Guangkuan [2 ]
Fu, Yongyuan [2 ]
Feng, Jianjun [1 ,2 ]
Zhu, Guojun [2 ]
机构
[1] Xian Univ Technol, State Key Lab Ecohydraul Northwest Arid Reg, Xian 710048, Peoples R China
[2] Xian Univ Technol, Inst Water Resources & Hydroelect Engn, Dept Power Engn, Xian 710048, Peoples R China
基金
中国国家自然科学基金;
关键词
Tubular turbine; Anti-cavitation edge of runner blade; Tip clearance; Leakage vortex; Hydraulic loss; TIP; CLEARANCE; FLOW;
D O I
10.1016/j.oceaneng.2023.114797
中图分类号
U6 [水路运输]; P75 [海洋工程];
学科分类号
0814 ; 081505 ; 0824 ; 082401 ;
摘要
Anti-cavitation edge directly affects turbine runner performance and clearance leakage flow. This paper takes a tubular turbine as the object of study and uses the numerical simulation method of SST-CC turbulence model based on rotation and curvature correction to study the effect of anti-cavitation edge thickness on the turbine internal flow patterns and the flow characteristics of tip leakage vortex under different conditions. The results show that the high-altitude bubble concentrated area on the blade suction surface is reduced after installing the anti-cavitation edges. Meanwhile, the leakage volume decreases by 13.28% under the optimal condition, and the maximum leakage decreases by 37.72% under the off-design condition. The raised structure of the anti-cavitation edge can effectively push the tip leakage vortex (TLV) away from the blade suction surface and destroy the original vortex structure; the strength of tip separation vortex (TSV) is obviously reduced. The energy loss increasingly reduces with the increase of anti-cavitation edge thickness, and the loss reduction value is greater in the off-design condition. The small negative helicity vortex at the draft tube wall surface disappears. The above research results provide a certain reference for the performance optimization of tubular turbine.
引用
收藏
页数:11
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