提高低氮氧化物微混合火焰燃料灵活性的新型喷油器几何结构

D. Kroniger, Atsushi Horikawa, Kunio Okada, Yuji Ashida
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摘要

为提高干式微混合燃烧原理的燃油柔韧性,设计了一种新型喷油器。微混合燃烧最初是为纯氢燃料而开发的,它基于非预混型交叉流射流混合,具有固有的抗闪回安全性,以及火焰小型化和增殖以抑制NOx排放。本研究探讨了新型几何结构在高天然气含量燃料作业中的潜力。在常压条件下的实验表明,新的喷油器将燃料的柔韧性降低到60 - 80 vol.% H2之间。利用详细的化学模型,在发动机压力条件下进行了RANS数值模拟,验证了相应的流动现象。基于OH化学发光分布的大气条件下数值方法的实验验证表明,非定常LES模型比定常RANS模型能更准确地预测微混合火焰的着火点,尽管两种模型都低估了反应过程,与更拉伸火焰的实验结果相比。
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Novel Fuel Injector Geometry for Enhancing the Fuel Flexibility of a Dry Low NOx MicroMix Flame
A novel fuel injector is presented for enhancing the fuel flexibility of the dry micromix (MMX) combustion principle. Originally having been developed for pure hydrogen fueling, the micromix combustion is based on a non-premixed type jet-in-crossflow mixing for inherent safety against flashback, as well as flame miniaturization and multiplication for suppressing NOx emissions. This study investigates the potential of the novel geometry regarding the operation with higher natural gas content fuels. In experiments at atmospheric pressure conditions it could be shown that the new injector extends the fuel flexibility down to between 60 and 80 vol.% H2. The responsible flow phenomena are verified with numerical RANS simulations at engine pressure conditions using a detailed chemistry model. An experimental validation of numerical methods at atmospheric conditions based on OH chemiluminescence distributions showed that the unsteady LES model can predict the micromix flame more accurately regarding to its ignition point than the steady RANS model, although the reaction progress is underestimated by both models, which in comparison to the experiment results in a more stretched flame.
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