氨氢燃料激光点火特性实验和模型研究

Experimental and Model Study on Laser Ignition Characteristics of Ammonia-Hydrogen Fuel

来源:中文会议(科协)
中文摘要英文摘要

基于定容燃烧平台,对不同掺氢比(0~20%)、不同当量比(0.6~1.4)及不同初始压力(0.1~0.4MPa)的氨氢混合气进行了激光点火实验,对不同条件下的火焰发展状态、点火成功率及最小点火能量的变化进行了分析,同时提出了能直接预测不同工况混合气的最小点火能量优化模型。结果表明:提高掺氢比和初始压力均能明显提高火焰稳定性及降低最小点火能量,在掺氢比为10%或初始压力为0.2MPa时,降低效果最明显,但继续提高掺氢比或压力,降低幅度会逐渐减小;当量比对火焰稳定性和最小点火能量的影响均呈现非单调变化,当量比为0.8时,最小点火能量达到最小值;优化后的模型在各工况下,均能较好地预测最小点火能量,但其预测结果的精确性仍然受函数性质的影响。

Based on the constant volume combustion chamber, laser ignition experiments were carried out on ammonia-hydrogen mixture with different hydrogen mixing ratio (0~20%), different equivalence ratio (0.6~1.4) and different initial pressure (0.1~0.4MPa). The flame development morphology, probability of ignition and minimum ignition energy changes under different conditions were analyzed. At the same time, a minimum ignition energy optimization model is proposed which can directly predict the energy under different working conditions. The results show that increasing the hydrogen ratio and initial pressure can significantly improve the flame stability and reduce the minimum ignition energy. The reduction effect is most obvious when the hydrogen ratio is 10% or the initial pressure is 0.2MPa, but the reduction range will gradually decrease with increasing the hydrogen ratio or pressure. The effect of equivalence ratio on flame stability and minimum ignition energy is non-monotonic. When equivalence ratio is 0.8, the minimum ignition energy reaches the minimum value. The optimized model can predict the minimum ignition energy well under all working conditions, but the accuracy of the prediction results is still affected by the function properties.

张俊杰;胡二江;江鑫;刘昀洋;黄佐华;

西安交通大学动力工程多相流国家重点实验室,西安 710049;西安交通大学动力工程多相流国家重点实验室,西安 710049;西安交通大学动力工程多相流国家重点实验室,西安 710049;西安交通大学动力工程多相流国家重点实验室,西安 710049;西安交通大学动力工程多相流国家重点实验室,西安 710049;

2023交通能源与智能动力大会

V233.3;TK401

激光点火 氨氢燃料 最小点火能量 点火概率模型 定容燃烧弹

laser ignition ammonia-hydrogen fuel minimum ignition energy ignition probability model constant volume combustion chamber

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