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DESIGN AND INVESTIGATIONS OF A MICRO-TURBINE FLOW PART

机译:微型透平流部件的设计与研究

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The co-generative micro-power plant with the HFE7100 as a working medium was designed and built for experimental investigations. The heat output of the plant was assumed equal to 20 kW, while the electric output amounted to about 3kW. In the paper a multi-stage micro-turbine with partial admission of all the stages is described in detail and the results of the particular experimental investigations and numerical calculations are shown, followed by an appropriate discussion and conclusions. The flow calculations were performed using ANSYS package and finally the axial multistage turbine was chosen. This allowed to apply typical nozzle and blade profiles. The turbine consists of 5 similar (almost identical) stages with constant section blades, the only difference being the increase of the admission arc (number of nozzles) in the successive stages. The rotor speed was assumed equal to 8000 rpm, mean rotor diameter -100 mm and blade height -10 mm. The stream lines, pressure and temperature distribution in the nominal and off-design conditions are presented and discussed in the paper. The micro-turbine was built and tested experimentally. The turbine performance was calculated for HFE7100 but also for air and nitrogen as a working medium for testing purposes. In the first stage of experiments the turbine behaviour was checked using these gases and the results were compared with the calculation data. The results of the experiments correspond very well with the appropriate CFD calculation data.
机译:设计并建造了以HFE7100为工作介质的热电联产微型发电厂,用于实验研究。假设该工厂的热输出等于20 kW,而电输出则约为3 kW。在本文中,详细描述了多级微型涡轮机,其中所有级均被部分接纳,并显示了特定实验研究和数值计算的结果,随后进行了适当的讨论和结论。使用ANSYS软件包进行了流量计算,最后选择了轴向多级涡轮机。这允许应用典型的喷嘴和叶片轮廓。涡轮机由5个具有恒定截面叶片的相似(几乎相同)的级组成,唯一的不同是连续级中进气弧(喷嘴数量)的增加。假定转子速度等于8000 rpm,平均转子直径为-100 mm,叶片高度为-10 mm。本文介绍并讨论了标称和非设计条件下的流线,压力和温度分布。微型涡轮机的建造和实验进行了测试。涡轮机性能是针对HFE7100进行计算的,还针对作为测试目的的空气和氮气作为工作介质进行了计算。在实验的第一阶段,使用这些气体检查了涡轮的性能,并将结果与​​计算数据进行了比较。实验结果与适当的CFD计算数据非常吻合。

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