Ignition Delay Times of Syngas and Methane in sCO2 Diluted Mixtures for Direct-Fired Cycles

Samuel Barak, Owen M. Pryor, Erik M. Ninnemann, Sneha Neupane, Xijia Lu, B. Forrest, Subith S. Vasu
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引用次数: 4

Abstract

In this study, a shock tube is used to investigate combustion tendencies of several fuel mixtures under high carbon dioxide dilution and high fuel loading. Individual mixtures of oxy-syngas and oxy-methane fuels were added to CO2 bath gas environments and ignition delay time data was recorded. Reflected shock pressures maxed around 100 atm, which is above the critical pressure of carbon dioxide in to the supercritical regime. In total, five mixtures were investigated within a temperature range of 1050–1350K. Ignition delay times of all mixtures were compared with predictions of two leading chemical kinetic computer mechanisms for accuracy. The mixtures included four oxy-syngas and one oxy-methane combinations. The experimental data tended to show good agreement with the predictions of literature models for the methane mixture. For all syngas mixtures though the models performed reasonably well at some conditions, predictions were not able to accurately capture the overall behavior. For this reason, there is a need to further investigate the discrepancies in predictions. Additionally, more data must be collected at high pressures to fully understand the chemical kinetic behavior of these mixtures to enable the supercritical CO2 power cycle development.
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合成气和甲烷在sCO2稀释混合物中直接燃烧循环的点火延迟时间
在本研究中,用激波管研究了几种燃料混合物在高二氧化碳稀释和高燃料负荷下的燃烧趋势。将氧-合成气和氧-甲烷燃料的单独混合物添加到CO2浴气环境中,并记录了点火延迟时间数据。反射的冲击压力在100大气压左右达到最大值,高于二氧化碳进入超临界状态的临界压力。总共在1050-1350K的温度范围内研究了五种混合物。所有混合物的点火延迟时间与两种领先的化学动力学计算机机制的预测进行了准确性比较。混合物包括四种氧-合成气和一种氧-甲烷混合物。实验数据与文献模型对甲烷混合物的预测结果趋于一致。对于所有的合成气混合物,虽然模型在某些条件下表现得相当好,但预测不能准确地捕捉到整体行为。因此,有必要进一步调查预测中的差异。此外,必须在高压下收集更多数据,以充分了解这些混合物的化学动力学行为,从而实现超临界CO2动力循环的开发。
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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