Design and structure optimization of small-scale radial inflow turbine for organic Rankine cycle system

被引:20
|
作者
Wu, Tan [1 ,2 ]
Shao, Long [3 ]
Wei, Xinli [1 ,2 ]
Ma, Xinling [1 ,2 ]
Zhang, Guojie [1 ,2 ]
机构
[1] Zhengzhou Univ, Sch Chem Engn & Energy, Zhengzhou 450001, Henan, Peoples R China
[2] MOE, Engn Res Ctr Energy Saving Technol & Equipments T, Zhengzhou 450001, Henan, Peoples R China
[3] Henan Agr Univ, Coll Mech & Elect Engn, Zhengzhou 450002, Henan, Peoples R China
关键词
Waste heat recovery; Organic Rankine cycle; Radial inflow turbine; Turbine design and optimization; WASTE HEAT-RECOVERY; PERFORMANCE ANALYSIS; WORKING FLUID; ORC SYSTEM; EXPANDER; IMPACT; SIMULATION; PREDICTION; SELECTIONS; DRIVEN;
D O I
10.1016/j.enconman.2019.111940
中图分类号
O414.1 [热力学];
学科分类号
摘要
The ORC (organic Rankine cycle) system has the advantages of simple structure, environmental friendliness, reliability and low capital cost. The expander is the key device of energy conversion in the ORC system, and its performance has a direct influence on that of the ORC. In this paper, a self-designed and manufactured radial inflow turbine is applied to low temperature waste heat power generation. The numerical model for the internal flow of the radial inflow turbine is established, and the numerical results show a better agreement with the experimental data. Firstly, the influence of blade stagger angles on nozzle performance is studied. The study finds that with the decrement of stagger angles under specific angle ranges, the velocity coefficient increases. However, the efficiency of the nozzle decreases sharply when the stagger angle exceeds 30. Secondly, the influence of the blade profile on the efficiency of the rotor is investigated. The results indicate that with t increasing, the efficiency of the rotor firstly increases, then decreases quickly. It increases by 1% compared with that of the original rotor, when the t = 1.95. At last, the performance of the turbine is researched numerically. This paper discovers that total-to-static efficiency of the turbine increases by 1.7% compared with that of the original turbine. This research provides orientation and basis for the improvement of aerodynamic design and performance of radial inflow turbine. As for practical application, the study can provide certain reference for the structure and blade profile design of nozzles and rotors to further improve the performance, and to offer some data for the operational control and tests.
引用
收藏
页数:12
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