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500 kW supercritical CO2 power generation system for waste heat recovery: System design and compressor performance test results

机译:500 KW超临界CO2发电系统,用于废热回收:系统设计和压缩机性能测试结果

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摘要

The supercritical CO2 Brayton cycle has received attention as a next generation power conversion system. However, technical challenges that relate to the design and operation of the system remain to be overcome. In particular, achieving turbomachinery operation with design points is imperative to demonstrate the feasibility of the technology. This study aims to provide the current research status of the supercritical CO2 power generation system in KAERI, with a focus on the detailed design of the system and operation of the compressor. In this study, cycle design (a simple recuperated cycle layout) of the system was developed using an in-house code for the optimization of a pilot plant of a 500 kW supercritical CO2 power generation system for waste heat recovery. A thermal efficiency of 16.5% of the proposed cycle was achieved. In addition, the detailed design of key components, such as turbomachines and heat exchangers, was developed. Furthermore, the first-step configuration, a compressor performance test loop, of the supercritical CO2 power generation system pilot plant was accomplished. The compressor was designed and manufactured as a hermetic system for the supercritical CO2 power generation system. A compressor performance test was conducted to verify the target performance of the compressor. The operation of the compressor at the design point was achieved during the test; the compressor inlet was 33 degrees C at 7.68 MPa, and the compressor rotational speed was 34200 rpm; its efficiency was 83.7%, and the pressure ratio was 1.756.
机译:超临界CO2布雷顿循环作为下一代的能量转换系统受到了广泛关注。然而,与该系统的设计和运行有关的技术挑战仍有待克服。特别是,为了证明该技术的可行性,必须实现涡轮机械的设计点运行。本研究旨在提供卡里超临界CO2发电系统的研究现状,重点是系统的详细设计和压缩机的运行。在本研究中,系统的循环设计(简单的回热循环布局)是使用内部代码开发的,用于优化500 kW超临界CO2发电系统的余热回收中试装置。该循环的热效率为16.5%。此外,还开发了关键部件的详细设计,如涡轮机械和热交换器。此外,还完成了超临界CO2发电系统中试装置的第一步配置,即压缩机性能测试回路。压缩机是作为超临界CO2发电系统的密封系统设计和制造的。进行压缩机性能测试,以验证压缩机的目标性能。试验期间,压缩机在设计点运行;压缩机入口温度为33℃,压力为7.68 MPa,压缩机转速为34200 rpm;其效率为83.7%,压力比为1.756。

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