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Experimental study of radial low specific speed turbocompressor running in reverse as turboexpander

机译:径向低比速涡轮压缩机逆转涡轮升降机的试验研究

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This paper includes small market research in the field of turboexpanders. The market research includes list of applications as well as list of some of major manufacturers of turboexpander. During the course of this research numbers of experiments were carried out to assess the performance of a small turboexpander with 65mm diameter rotor operating at relatively low speeds in comparison to standard radial turbines. The output power of the turboexpander was calculated based on the electrical output of the loading generator. The turbine rotor comprised of a TurboClaw compressor operating in reverse with two set of experiments for the following nozzles; as expander with single nozzle and a set of six nozzles. It was found that even for a non optimised geometry (rotor is a compressor not a turbine) the system efficiency for micro turboexpander is excellent.
机译:本文包括涡轮增压器领域的小市场研究。 市场研究包括申请清单以及涡轮增压器的一些主要制造商名单。 在该研究期间,进行了实验的数量,以评估小涡轮机的性能,与标准径向涡轮机相比,以相对低的速度以相对低的速度运行的65mm直径转子的性能。 基于装载发生器的电气输出来计算TurboExpander的输出功率。 涡轮机转子包括涡轮爪式压缩机,其用两组用于以下喷嘴的两组实验; 用单个喷嘴和一组六个喷嘴的膨胀机。 发现即使对于非优化的几何形状(转子是压缩机而不是涡轮机),Micro TurboExpander的系统效率优异。

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