首页> 外文会议>ASME Turbo Expo: Turbomachinery Technical Conference and Exposition >EFFECTS OF VARYING LIQUID FUEL AND AIR CO-FLOW RATES ON SPRAY CHARACTERISATION OF AN ANNULAR CO-FLOW SPRAY BURNER
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EFFECTS OF VARYING LIQUID FUEL AND AIR CO-FLOW RATES ON SPRAY CHARACTERISATION OF AN ANNULAR CO-FLOW SPRAY BURNER

机译:液体燃料和空气共流速率的变化对环形共流喷雾燃烧器喷雾特性的影响

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Development of efficient and clean combustion systems requires the understanding of all the processes experienced by a complex liquid fuel in IC engines, such as atomization, vaporization, turbulent mixing, and combustion. Many of these processes are interconnected; the atomization process, which leads to various droplet sizes can enhance or diminish the vaporization rate of the liquid fuel and consequently impact the energy conversion process. Furthermore, the combustion/flame stability of liquid-fueled gas turbine can be influenced by the fuel and the air co-flow rates delivered in the engine. Increasing the fuel and/or air flow rates can enhance droplet breakup and the turbulence of the flow, and as a result sway the droplet size distribution of the spray. This work focuses on investigating the impact of varying the fuel and air flow rates on the spray atomization (e.g. droplet size distribution) of an Annular Co-Flow Spray Burner. This was explored by measuring droplet sizes and velocities of the spray at different radial and axial positions of n-heptane fuel under nonreacting conditions. In addition, the turbulence intensity and the liquid spray droplet distribution were quantified for different fuel and air flow rate conditions. The measurements were obtained by using a Phase Doppler Particle Analyzer/Laser Doppler Velocimeter (PDPA/LDV) at P = 1 atm and T = 298 K. Moreover, the Sauter Mean Diameters for different flow conditions are predicted, using an established correlations, and compared to PDPA/LDV measurements. The results provided a fair understanding of the influence of varying the fuel and air flow rates on the droplet sizes, velocity, and turbulent intensity. Furthermore, the results presented here will support future work that will focus on unraveling the role of phase change on flame stability.
机译:要开发高效,清洁的燃烧系统,需要了解IC发动机中复杂液体燃料所经历的所有过程,例如雾化,汽化,湍流混合和燃烧。这些过程中有许多是相互联系的。导致各种液滴尺寸的雾化过程会提高或降低液体燃料的蒸发速率,从而影响能量转换过程。此外,液体燃料燃气涡轮机的燃烧/火焰稳定性会受到在发动机中输送的燃料和空气同流率的影响。增加燃料和/或空气流速可以增强液滴的破裂和流动的湍流,并因此摇摆喷雾的液滴尺寸分布。这项工作的重点是研究改变燃料和空气流速对环形同流喷雾燃烧器的喷雾雾化(例如液滴尺寸分布)的影响。通过在非反应条件下测量正庚烷燃料在不同径向和轴向位置的喷雾液滴尺寸和速度来探索这一点。另外,针对不同的燃料和空气流速条件,对湍流强度和液体雾滴分布进行了定量。通过使用相位多普勒粒子分析仪/激光多普勒测速仪(PDPA / LDV)在P = 1 atm和T = 298 K时获得测量结果。此外,使用已建立的相关性,可以预测不同流量条件下的索特平均直径,以及与PDPA / LDV测量结果相比。结果提供了对改变燃料和空气流速对液滴尺寸,速度和湍流强度的影响的公正理解。此外,此处给出的结果将支持未来的工作,该工作将集中于阐明相变对火焰稳定性的作用。

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