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Exploring the Role of Physical and Chemical Properties on the Ignition and Flame Stability of Liquid Fuels with a Spray Burner and Fuel Ignition Tester (FIT)

机译:使用喷雾燃烧器和燃料点火测试仪(FIT)探索物理和化学性质对液体燃料的点火和火焰稳定性的作用

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Liquid fuels have different physical and chemical properties which can affect the atomization, evaporation and mixing processes inside heat engines, including turbine and reciprocating internal combustion engines. In this work, the relationship between the fuel's properties and its ignition/flame stability is investigated. A spray burner was designed and manufactured to simulate the mixing dynamics experienced in a turbine engine combustor capable of delivering high fuel and air co-flow rates. The flame behavior and stability have been studied by measuring the flame liftoff heights and blowout limits for different single component fuels at different fuel and air flow conditions. In addition, a Fuel Ignition Tester (FIT) was used to investigate the impact of volatility and local enrichment on ignition delay. Results indicate a strong influence of fuel volatility and atomization on the flame stability. The less volatile/heavier fuels have higher liftoff heights, while the fuels with smaller droplet sizes and higher volatility blowout easier than less volatile fuels and those which atomize into larger droplets. In the FIT, it was noticed that the local equivalence ratio defined by the fuels volatility has more effect on the ignition delay than the global air fuel ratio. As a result, n-dodecane ignites faster than n-heptane, despite the having a lower measured global equivalence ratio.
机译:液体燃料具有不同的物理和化学特性,这些特性会影响热机(包括涡轮机和往复式内燃机)内的雾化,蒸发和混合过程。在这项工作中,研究了燃料性质与其点火/火焰稳定性之间的关系。喷雾燃烧器的设计和制造可模拟涡轮发动机燃烧器中能够提供高燃料和空气同流速率的混合动力。通过在不同的燃料和空气流动条件下测量不同的单组分燃料的火焰升空高度和喷出极限,研究了火焰行为和稳定性。此外,还使用了燃油点火测试仪(FIT)来研究挥发度和局部浓化对点火延迟的影响。结果表明燃料挥发性和雾化对火焰稳定性有很大影响。挥发性较低/较重的燃料具有较高的升空高度,而液滴尺寸较小且挥发度较高的燃料比挥发性较低的燃料和雾化成较大液滴的燃料更容易。在FIT中,应注意的是,由燃油挥发性定义的局部当量比对点火延迟的影响要大于总的空燃比。结果,尽管测得的整体当量比较低,但正十二烷的点燃速度快于正庚烷。

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