Potential and Evolution of Miniatures Compressed Air Energy Storage Plants Based on Impulse Turbine

Ayad Al Jubori, Laith A. Al-Sadawi, T. Biedermann, S. Alfarawi
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Abstract

This paper describes the work carried out to develop an impulse turbine for miniatures compressed air system. This study hypothesizes the question; what is the effect of combining an impulse turbine loss model into a compressed air energy storage system analysis? The miniatures power system has lower mass flow rates which lead to a small turbine size. The miniature impulse turbine has relatively low efficiency and is highly sensitive to operating conditions at a low mass flow rate due to all losses in terms of passage, trailing edge, incidence, and clearance becoming higher amounts compared to the total losses of the percentage foundation. The development of a novel impulse turbine configuration is presented based on one-dimensional design and three-dimensional simulations. The impulse turbine in single-stage configuration was designed and analyzed for a range of operating conditions in terms of pressures, temperatures, mass flow rate, and rotational speeds. The simulations results showed that the maximum efficiency and power were 65.93% and 4.019 kW respectively with a mass flow rate of 0.2 kg/s. The energy analysis revealed that the system efficiency was 10.3%. The miniature compressed air energy storage system driven by an impulse turbine can be used to generate electricity for small power applications.
基于脉冲涡轮的微型压缩空气储能装置的潜力与发展
本文介绍了微型压缩空气系统脉冲涡轮的研制工作。这项研究假设了这个问题;将脉冲涡轮损失模型结合到压缩空气储能系统分析中,效果如何?微型动力系统具有较低的质量流量,从而导致涡轮尺寸较小。由于在通道、尾缘、入射和间隙方面的所有损失与百分比基础的总损失相比变得更高,因此微型脉冲涡轮的效率相对较低,并且对低质量流量下的运行条件非常敏感。提出了一种基于一维设计和三维仿真的新型脉冲涡轮结构。在压力、温度、质量流量和转速等工况条件下,对单级冲击涡轮进行了设计和分析。仿真结果表明,在质量流量为0.2 kg/s时,最大效率为65.93%,最大功率为4.019 kW。能量分析表明,系统效率为10.3%。由脉冲涡轮驱动的微型压缩空气储能系统可用于小功率发电。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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