10mwe超临界CO2涡轮在1mwe流动回路中的开发与测试

J. Moore, Stefan D. Cich, Meera Day-Towler, J. Mortzheim
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引用次数: 1

摘要

与传统的蒸汽朗肯循环相比,sCO2动力循环提高了循环效率。然而,支持这种循环所需的涡轮机械在商业规模上不存在,需要开发。本文介绍了一种新型10 MWe规模的sCO2涡轮机,并在sCO2闭环再压缩布雷顿循环中进行了演示。由于该涡轮机是为聚光太阳能发电(CSP)应用而开发的,因此在美国能源部SunShot计划和行业合作伙伴的资助下,选择了超过700°C的目标入口温度。然而,它可以应用于传统的热源,如天然气、煤炭和核能。传统的朗肯蒸汽循环热效率通常在35-40%的范围内,但对于先进的超超临界蒸汽循环,热效率可高达45%。使用外部燃烧的热源,sCO2循环可以接近50%的热效率。此外,这种循环也非常适合底部循环废热回收应用,通常在较低的温度下运行。sCO2循环的高功率密度和低热质量导致了紧凑,高效的电源模块,可以快速响应瞬态环境变化和瞬态操作,这对于太阳能,废热和船舶应用具有特别的优势。涡轮的功率密度明显大于传统的蒸汽涡轮,可与液体火箭发动机涡轮泵相媲美。本文描述了涡轮机的设计和构造,并提供了在1mwe测试设施中对10mwe涡轮机的额外测试,包括转子动力学,热管理,转子航空和机械设计,轴端和套管密封,轴承和联轴器的描述。涡轮的测试数据包括在内,因为它达到了715°C, 250 bara和27,000 rpm的运行目标。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development and Testing of a 10 MWe Supercritical CO2 Turbine in a 1 MWe Flow Loop
sCO2 power cycles offer improved cycle efficiencies compared with traditional steam Rankine cycles. However, the turbomachinery required to support such a cycle does not exist at a commercial scale and requires development. This paper describes a new 10 MWe scale sCO2 turbine was developed and demonstrated in an sCO2 closed-loop recompression Brayton cycle. Since this turbine was developed for Concentrating Solar Power (CSP) applications, a target inlet temperature of over 700°C was chosen using funding from the US DOE SunShot initiative and industry partners. However, it can be applied to traditional heat sources such as natural gas, coal, and nuclear power. Traditional Rankine steam cycle thermal efficiencies are typically in the 35–40% range, but can be as high as 45% for advanced ultra-supercritical steam cycles. The sCO2 cycle can approach 50% thermal efficiency using externally fired heat sources. Furthermore, this cycle is also well suited for bottoming cycle waste heat recovery applications, which typically operate at lower temperatures. The high-power density and lower thermal mass of the sCO2 cycle results in compact, high-efficiency power blocks that can respond quickly to transient environmental changes and transient operation, a particular advantage for solar, waste heat, and ship-board applications. The power density of the turbine is significantly greater than traditional steam turbines and is comparable to liquid rocket engine turbo pumps. This paper describes the design and construction of the turbine and provides additional testing of the 10 MWe turbine in a 1 MWe test facility including a description of rotordynamics, thermal management, rotor aero and mechanical design, shaft-end and casing seals, bearings, and couplings. Test data for the turbine is included, as it achieves its operational goal of 715°C, 250 bara, and 27,000 rpm.
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