设计和性能评估直,之字形,和翼型鳍配置在100千瓦超临界CO2 PCHE增强预冷却器的应用

IF 7.6 Q1 ENERGY & FUELS
Md Maruf Ahmed, M. Monjurul Ehsan
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引用次数: 0

摘要

印制电路换热器(PCHE)预冷器翅片的设计对超临界二氧化碳(sCO2)再压缩循环的效率和成本有重要影响。本研究采用一种新颖的迭代离散节点方法来评估直线型、锯齿形和翼型翅片PCHE在不同进气条件下的性能,这是一种创新的努力,以解决目前对翅片配置对PCHE性能影响的理解中的关键空白。该分析采用了基于python的尖端设计代码和用于工作流体性质(RGP)的CoolProp。翅片的几何形状对PCHE的sCO2侧的压降和传热率有显著影响。直翅片的热性能最低,但压降最小。相比之下,锯齿形和翼型翼(AFF)实现更高的传热由于增强湍流从他们的受限流动路径。直翼、之字形翼和翼型翼在所有进口条件下保持sCO2压降的比例约为1:7:2。尽管如此,与翼型相比,锯齿形通道的传热率提高了约3%,并且在较高的sCO2进口压力下,这一增益进一步降低。因此,翼型翅片结构提供了最好的平衡,提供传热性能相当于锯齿翼与边缘压力增加超过直鳍。对于非设计性能分析,sCO2进口压力(7.5 MPa-11 MPa)、进口温度(65°C-110°C)和流量(0.4 g/s-1.4 g/s)是关键参数,表明对于任何翅片布置,随着进气压力、温度和流量的增加,换热效果都有所改善。随着进口压力和温度的升高,两种流体的压降减小。进口压力超过9mpa时,压降收益每MPa降低10%,这意味着两种流体的收益递减。较高的流量降低了水侧压降,但使sco侧压降增加了大约7倍,使得超过0.6 g/s的操作变得不可行,并抵消了传热收益。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Design and performance Assessment of Straight, Zigzag, and airfoil fin configurations in 100 kW supercritical CO2 PCHE for enhanced Pre-Cooler application
The design of the fins of the Printed Circuit Heat Exchanger (PCHE) pre-cooler significantly impacts the efficacy and cost of supercritical carbon dioxide (sCO2) Recompression cycles. This study uses a novel iterative discrete nodal approach to assess the performance of straight, zigzag, and airfoil-finned PCHEs under varying intake conditions in an innovative effort to address critical voids in the current understanding of fin configurations’ impact on PCHE performance. The analysis employs a cutting-edge Python-based design code and CoolProp for working fluid properties (RGP). The fins’ geometry significantly affects the pressure drop and heat transmission rate on the sCO2 side of the PCHE. Straight fins exhibit the lowest thermal performance but the smallest pressure drop. In contrast, Zigzag and Airfoil fins (AFF) achieve higher heat transfer due to enhanced turbulence from their confined flow paths. The straight, zigzag, and airfoil fins maintain a ratio of sCO2 pressure drop of approximately 1:7:2 across all inlet conditions. Nonetheless, Zigzag channels show an improvement in heat transfer rate over Airfoils of roughly 3 %, and this gain decreases further at higher sCO2 inlet pressures. Thus, the Airfoil fin structure offers the best balance, providing heat transfer performance equivalent to Zigzag fins with a marginal pressure increase over straight fins. For the off-design performance analysis, sCO2 inlet pressure (7.5 MPa-11 MPa), inlet temperature (65 °C-110 °C), and flow rates (0.4 g/s-1.4 g/s) are the key parameters, suggesting that heat transfer improves with increasing intake pressure, temperature, and flow rate for any fin arrangement. As the inlet pressure and temperature rise, the pressure drop of both fluids reduces. Inlet pressure exceeding 9 MPa reduces pressure drop gains at a rate of 10 % per MPa, signifying diminishing benefits for both fluids. Higher flow rates lower water-side pressure drop but increase sCO-side pressure drop by roughly sevenfold, making operation beyond 0.6 g/s unfeasible and negating heat transfer gains.
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来源期刊
CiteScore
8.80
自引率
3.20%
发文量
180
审稿时长
58 days
期刊介绍: Energy Conversion and Management: X is the open access extension of the reputable journal Energy Conversion and Management, serving as a platform for interdisciplinary research on a wide array of critical energy subjects. The journal is dedicated to publishing original contributions and in-depth technical review articles that present groundbreaking research on topics spanning energy generation, utilization, conversion, storage, transmission, conservation, management, and sustainability. The scope of Energy Conversion and Management: X encompasses various forms of energy, including mechanical, thermal, nuclear, chemical, electromagnetic, magnetic, and electric energy. It addresses all known energy resources, highlighting both conventional sources like fossil fuels and nuclear power, as well as renewable resources such as solar, biomass, hydro, wind, geothermal, and ocean energy.
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