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Flash boiling effect on swirled injector spray angle

机译:闪蒸对旋流喷射器喷射角的影响

摘要

AbstractudA swirled injector for gasoline direct injection was used to investigate the effect of fuel flash boiling on the initial angle of the spray. udThe hollow cone spray was injected into a constant pressure bomb filled with quiescent air. The fuel was fed at 7 MPa constant pressure to the injector. Three parameters were changed to study the effect of the injection conditions on the spray angle: fuel composition, fuel temperature and air pressure in the test bomb.udThe injector tip was heated up to 150°C to keep the fuel to be injected at the desired temperature. Different blends of iso-octane and n-pentane were used to obtain fuels with different bubble temperature at the same air pressure.udIn a reduced set of experiments, only with pure fuels, the ambient pressure was varied to change the bubble temperature independently from the fuel temperature. It was observed that, when the fuel conditions exceed the bubble point, the spray angle, measured close to the injector, becomes wider. This angle was chosen as an indicator of the flash boiling intensity. The experimental results show that the angle value is well fitted by a unique correlation if it is expressed as a function of the ratio P=Pb/ Pair between the fuel bubble pressure and the bomb pressure
机译:摘要 ud使用涡流喷射器直接喷射汽油,以研究燃料闪蒸对喷射初始角度的影响。 ud将空心锥形喷雾喷入充满静态空气的恒压炸弹中。燃料以7 MPa恒定压力进料到喷油器。更改了三个参数以研究喷射条件对喷雾角度的影响:燃料成分,燃料温度和测试炸弹中的气压。 ud将喷射器尖端加热至150°C,以将要喷射的燃料保持在所需温度。在相同的气压下,异辛烷和正戊烷的不同混合物用于获得具有不同气泡温度的燃料。 ud在一组简化的实验中,仅对于纯燃料,改变环境压力以独立于改变气泡温度燃油温度。观察到,当燃料条件超过起泡点时,靠近喷射器测量的喷射角变宽。选择该角度作为闪蒸强度的指标。实验结果表明,如果将角度值表示为燃料气泡压力与炸弹压力之间的比率P = Pb / Pair的函数,则该角度值很好地符合唯一相关性。

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