直喷式氢发动机氢射流性能评价及局部热流密度降低冷却损失评价研究

Yoshihisa Kojiya, Ryota Sato, Hiromi Saito, Daijiro Ishii, Masakuni Oikawa, Y. Takagi, Y. Mihara
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引用次数: 0

摘要

作者提出了一种新的燃烧过程,称为羽流点火燃烧概念(PCC),在该燃烧过程中,氢射流的羽流在注入氢后被火花点燃,以完成羽流的燃烧。通过对喷射正时、点火正时和射流几何形状控制的优化组合,该燃烧过程显著提高了热效率,减少了冷却损失,这是提高氢发动机热效率的关键因素。为了评估氢能发动机的冷却损失,本研究通过测量燃烧室中前置和尾尾两个位置的热流密度来评估PCC燃烧的局部冷却损失特征。结果表明,在PCC燃烧的15°喷油角下,喷油前向的局部冷却热流比后向和燃烧室的空间平均冷却损失要高得多。将喷注角扩大到25°后,热效率得到提高,且前缘局部热流密度减小。结果表明,捕获局部热流密度,特别是在喷射射流导向方向上的热流密度是提高热效率的关键。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Research on evaluation of hydrogen jet behavior and assessment of cooling loss reduction by measuring local heat flux in direct injection hydrogen engines
The authors have proposed a new combustion process called the Plume Ignition Combustion Concept (PCC), in which a plume of the hydrogen jet is spark-ignited just after hydrogen is injected to accomplish combustion of a plume of rich mixture. With an optimal combination of injection timing, ignition timing and controlled jet geometry, this combustion process markedly improved thermal efficiency by reducing cooling loss which is an essential element to be reduced for improving thermal efficiency in hydrogen engine. In this study, in order to evaluate the cooling loss in hydrogen engine, characteristics of local cooling loss of PCC combustion are evaluated by measuring heat flux in two locations, one in the leading location and the others in the trailing location in the combustion chamber. As a result, it was found that local cooling heat flux in the leading direction of the jet injected showed extremely high level compare to trailing direction and spatially averaged cooling loss of the combustion chamber in injection angle of 15° of PCC combustion. By enlarging injection angle to 25°, thermal efficiency was improved and local heat flux in the leading direction is also mitigated. This result indicated that capturing local heat flux, especially in the leading direction of the injected jet, is a key to improve thermal efficiency.
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