用于超临界CO2动力循环的创新弹性流体动力密封概念

S. Cesmeci, Rubayet Hassan, M. Hassan, Ikenna Ejiogu, Matthew DeMond, Hanping Xu, Jing Tang
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引用次数: 1

摘要

超临界CO2 (sCO2)动力循环是一种很有前途的下一代动力技术,在化石燃料发电厂、核能发电、太阳能发电、地热发电和船舶推进方面具有巨大的潜力。为了释放sCO2电力循环的潜力,必须在10-600 MWe的规模上,在sCO2温度和压力350-700°C和20-30 MPa的核工业中证明技术准备就绪。在组件层面的许多挑战中,缺乏适合sCO2运行条件的轴封是下一代核涡轮机和压缩机开发需要解决的问题。在这项研究中,我们提出了一种新型的弹性流体动力(EHD)高压、高温、可伸缩的sCO2涡轮机械轴密封,它具有低泄漏、最小磨损、低成本和无应力集中的特点。本文的重点是借助基于物理的计算机模拟进行概念验证研究。结果表明,概念验证研究是成功的,值得进一步研究。特别值得注意的是,泄漏率的二次型,在Pin = 15 MPa时达到m˙= 0.075 kg/s的峰值,然后在Pin = 30 MPa时衰减到小于m˙= 0.040 kg/s,这表明所提出的密封设计可以进一步定制,成为sCO2涡轮机械轴封问题的潜在候选。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
An Innovative Elasto-Hydrodynamic Seal Concept for Supercritical CO2 Power Cycles
Supercritical CO2 (sCO2) power cycles are promising next generation power technologies, holding a great potential in fossil fuel power plants, nuclear power production, solar power, geothermal power, and ship propulsion. To unlock the potential of sCO2 power cycles, technology readiness must be demonstrated on the scale of 10–600 MWe and at sCO2 temperatures and pressures of 350–700 °C and 20–30 MPa for nuclear industries. Amongst many challenges at the component level, the lack of suitable shaft seals for sCO2 operating conditions needs to be addressed for the next generation nuclear turbine and compressor development. In this study, we propose a novel Elasto-Hydrodynamic (EHD) high-pressure, high temperature, and scalable shaft seal for sCO2 turbomachinery that offers low leakage, minimal wear, low cost, and no stress concentration. The focus in this paper was to conduct a proof-of-concept study with the help of physics-based computer simulations. The results showed that the proof-of-concept study was successfully demonstrated, warranting further investigation. Particularly, it was interesting to note the quadratic form of the leakage rate, making its peak of m ˙ = 0.075 kg/s at Pin = 15 MPa and then decaying to less than m ˙ = 0.040 kg/s at Pin = 30 MPa, suggesting that the proposed seal design could be tailored further to become a potential candidate for the shaft seal problems in sCO2 turbomachinery.
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