Hydrogen and Ammonia Blending with Natural Gas: Ignition Delay Times and Chemical Kinetic Model Validation At Gas Turbine Relevant Conditions

IF 1.4 4区 工程技术 Q3 ENGINEERING, MECHANICAL Journal of Engineering for Gas Turbines and Power-transactions of The Asme Pub Date : 2023-10-17 DOI:10.1115/1.4063789
Michael Pierro, Justin Urso, Ramees K. Rahman, Christopher W Dennis, Marley Albright, Jonathan McGaunn, Cory Kinney, Subith Vasu
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Abstract

Abstract Ignition delay times from undiluted mixtures of natural gas (NG)/H2/Air and NG/NH3/Air were measured using a high-pressure shock tube at the University of Central Florida. The combustion temperatures were experimentally tested between 1000-1500 K near a constant pressure of 25 bar. As mentioned, mixtures were kept undiluted to replicate the same chemistry pathways seen in gas turbine combustion chambers. Recorded combustion pressures exceeded 200 bar due to the large energy release, hence why these were performed at the high-pressure shock tube facility. The data is compared to the predictions of the NUIGMech 1.1 mechanism for chemical kinetic model validation and refinement. An exceptional agreement was shown for stoichiometric conditions in all cases but strayed at lean and rich equivalence ratios, especially in the lower temperature regime of H2 addition and all temperature ranges of the baseline NG mixture. Hydrogen addition also decreased ignition delay times by nearly 90%, while NH3 fuel addition made no noticeable difference in ignition time. NG/NH3 exhibited similar chemistry to pure NG under the same conditions, which is shown in a sensitivity analysis. The reaction CH3 + O2 = CH3O + O is identified and suggested as a possible modification target to improve model performance. Increasing the robustness of chemical kinetic models via experimental validation will directly aid in designing next-generation combustion chambers for use in gas turbines, which in turn will greatly lower global emissions and reduce greenhouse effects.
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天然气与氢、氨混合:燃气轮机相关条件下的点火延迟时间和化学动力学模型验证
利用中佛罗里达大学的高压激波管测量了未稀释的天然气/H2/空气和天然气/NH3/空气混合物的点火延迟时间。实验测试了燃烧温度在1000-1500 K之间,接近25 bar的恒定压力。如上所述,混合物保持未稀释,以复制在燃气轮机燃烧室中看到的相同化学途径。由于大量的能量释放,记录的燃烧压力超过200巴,因此为什么这些是在高压激波管设施中进行的。将数据与NUIGMech 1.1机制的预测结果进行对比,对化学动力学模型进行验证和改进。在所有情况下,化学计量条件下的结果都非常一致,但在贫当量比和富当量比下,特别是在H2添加的较低温度范围和基线NG混合物的所有温度范围内,结果却不一致。氢气的加入也使点火延迟时间减少了近90%,而NH3燃料的加入对点火延迟时间没有显著影响。在相同条件下,NG/NH3表现出与纯NG相似的化学性质,这在灵敏度分析中得到了证明。确定了反应CH3 + O2 = ch30 + O,并提出了可能的修改目标,以提高模型的性能。通过实验验证提高化学动力学模型的稳健性将直接有助于设计用于燃气轮机的下一代燃烧室,从而大大降低全球排放并减少温室效应。
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来源期刊
CiteScore
3.80
自引率
20.00%
发文量
292
审稿时长
2.0 months
期刊介绍: The ASME Journal of Engineering for Gas Turbines and Power publishes archival-quality papers in the areas of gas and steam turbine technology, nuclear engineering, internal combustion engines, and fossil power generation. It covers a broad spectrum of practical topics of interest to industry. Subject areas covered include: thermodynamics; fluid mechanics; heat transfer; and modeling; propulsion and power generation components and systems; combustion, fuels, and emissions; nuclear reactor systems and components; thermal hydraulics; heat exchangers; nuclear fuel technology and waste management; I. C. engines for marine, rail, and power generation; steam and hydro power generation; advanced cycles for fossil energy generation; pollution control and environmental effects.
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