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Near-nozzle spray dynamics of 6-hole GDI injector under subcooled and superheated conditions

机译:过冷和过热条件下6孔GDI喷射器的近喷嘴喷雾动力学

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摘要

The flash boiling of fuel sprays can occur in engines when the fuel is injected into the ambient gas which pressure is lower than the saturation vapor pressure of the fuel. Recently, the flash boiling has attracted many engine researchers' interest due to its superior spray atomization performance. It has been discussed that the formation of the flash boiling sprays is governed by the bubble dynamics in the fuel such as bubble nucleation, growth, and burst. However, the detailed bubble dynamics and its effects on near-nozzle spray dynamics have remained a mystery due to great difficulties in the observation of flow characteristics inside and near the nozzle. The current study investigates the near-nozzle dynamics of flash boiling sprays from a 6-hole gasoline-direct-injection injector using an X-ray imaging technique. Various Rp (ratio of saturated vapor pressure to ambient gas pressure) conditions were applied by altering the ambient pressure under the fixed fuel temperature. The results showed that the flash boiling did not alter significantly the emerging flow velocity at the nozzle exit. The center of flash-boiling sprays did not decelerate in the near-nozzle region while that of the subcooled spray showed a gradual deceleration. The radial velocity of the flash boiling sprays increased at the edge of the spray as Rp increased while that in the spray center was near zero regardless of Rp condition. The radial velocity of the flash boiling spray was solely governed by Rp regardless of injection pressure while that of the subcooled sprays was altered by the injection pressure. Based on the results, the initial formation mechanism of the flash boiling sprays and the associated bubble dynamics were thoroughly discussed.
机译:当将燃料喷射到压力低于燃料的饱和蒸汽压的环境气体中时,燃料喷雾的闪蒸会在发动机中发生。近来,闪蒸由于其卓越的喷雾雾化性能而吸引了许多发动机研究人员的兴趣。已经讨论了闪蒸喷雾的形成是由燃料中的气泡动力学决定的,例如气泡成核,生长和破裂。然而,由于在观察喷嘴内部和附近的流动特性方面有很大的困难,详细的气泡动力学及其对近喷嘴喷雾动力学的影响仍然是一个谜。当前的研究使用X射线成像技术研究了6孔汽油直接喷射式喷射器的闪蒸沸腾喷雾的近喷嘴动力学。通过在固定燃料温度下改变环境压力来施加各种Rp(饱和蒸气压与环境气压的比)条件。结果表明,闪蒸没有明显改变喷嘴出口处出现的流速。沸腾喷雾的中心在近喷嘴区域没有减速,而过冷喷雾的中心则显示逐渐减速。随Rp的增加,快速沸腾喷雾的径向速度在喷雾的边缘随径向速度的增加而增大,而在喷雾中心的径向速度几乎与零无关。不论喷射压力如何,闪蒸沸腾喷雾的径向速度仅由Rp控制,而过冷喷射的径向速度则由喷射压力改变。根据结果​​,彻底讨论了闪蒸喷雾的初始形成机理和相关的气泡动力学。

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