High-Fuel Loading Ignition Delay Time Characterization of Hydrogen/Natural Gas/Ammonia at Gas Turbine-Relevant Conditions Inside a High-Pressure Shock Tube

Michael Pierro, Justin J Urso, Cory Kinney, Shubham Kesharwani, Jonathan McGaunn, Christopher W. Dennis, Subith S. Vasu
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Abstract

This study explores the combustion characterization of high-fuel percentage, air-diluted mixtures of H2 mixed with natural gas (NG) as well as mixtures of H2 and NH3 at temperatures and pressures relevant to turbine operating conditions (20–30 bar, 1000–1500 K). Lower temperatures (below 1070 K) exhibit preignition characteristics due to non-homogeneity. An attempt to mitigate these occurrences at high pressures is investigated using the constrained reaction volume (CRV) stage-filling technique. Due to the need to further refine the facility CRV stage-filling uncertainty, only higher temperature data will be interpreted at this time. The test conditions in this study closely replicate the temperatures, pressures, and mixtures that would be seen in hydrogen-powered gas turbines, making it the first to explore such conditions. The experimental IDTs were compared against the current state-of-the-art chemical kinetic models for mechanism validation. The current work will advance H2-powered turbines and aims to determine the optimum molecular ratio of H2 when mixed with natural gas.
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高压激波管内氢气/天然气/氨在燃气轮机相关条件下的高燃料负荷点火延迟时间表征
本研究探讨了高燃料百分比、空气稀释的H2与天然气(NG)混合混合物以及H2和NH3混合物在与涡轮工作条件相关的温度和压力(20-30 bar, 1000-1500 K)下的燃烧特性。由于非均匀性,较低温度(低于1070 K)表现出预燃特性。为了在高压下减轻这些情况的发生,研究人员使用了受限反应体积(CRV)分段填充技术。由于需要进一步完善设施CRV级填充的不确定性,此时只能解释更高温度的数据。这项研究的测试条件与氢动力燃气轮机的温度、压力和混合物非常接近,这是第一次探索这种条件。实验IDTs与目前最先进的化学动力学模型进行了比较,以验证机理。目前的工作将推进H2动力涡轮机,并旨在确定H2与天然气混合时的最佳分子比。
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