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Effects of Rounding-off Inlet Hole in Fuel Nozzle on Spray and Combustion Characteristics under High-Pressure and High-Temperature

机译:燃料喷嘴圆排入口孔对高压高温喷射特性的影响

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Experiments were performed to clarify the effects of rounding-off inlet hole of nozzles on spray and combustion characteristics for six pieces, two types injection nozzles with and without rounding-off. Marine diesel fuel oil was used in every test, the matrix of experimental conditions included ambient temperature from 470K to 1000K, ambient pressure from 3MPa to 7MPa, fuel pump revolution was set at two fixed value of 150rpm and 250rpm and position of fuel pump rack of 10, 20 and 30 notches. High resolution, high speed video camera possible to take up to 12000 frame per seconds with extension trigger was adopted, with available software, imagine pictures were analyzed synchronized on the same screen, it revealed that with rounding off nozzle at low pressure and low temperature of ambient condition ignition starts early than without rounding-off nozzles. At supposed conditions of two-phase (liquid and gases) flow inside the nozzle, a commercial CFD engine simulation software program was also adopted to calculate and visualize cavitations. Turbulence phenomena occurred at Inlet hole area of fuel injector nozzle and calculated velocity distribution along axis of nozzle for two typed of nozzle with and without rounding-off was obtained by turbulence and injection spray output. The geometry of two nozzles is symmetrical and exactly the same except the radius of curvature of inlet hole. Inlet and outlet boundary condition were defined for three cases 120MPa, 72 MPa and 36MPa corresponding to condition of the experiments. It is found that the velocity distribution along the axis of rounding-off nozzle was higher than without rounding-off ones. The difference in the higher velocity distribution can be explained by term of the cavitation generated In without rounding-off Injection nozzle. Experiment results validated, the effects of rounding-off inlet hole nozzle not only to reduces cavitations, turbulence, increase effective flow area, but also potentially improve combustion process at low ambient temperature that corresponding to low load condition of diesel engine. In contrary, at condition of high temperature and fuel pump rack of 20 and 30 notches, ignition delay of two type nozzle were similar.
机译:进行实验以阐明喷嘴的圆角入口孔对六件的喷雾和燃烧特性的影响,两种类型的注射喷嘴,无舍入。在每个测试中使用船用柴油燃料油,实验条件的基质包括470k至1000K的环境温度,环境压力从3MPa到7MPa,燃油泵旋转设定为250rpm和250rpm的两个固定值和燃料泵架的位置10,20和30个缺口。高分辨率,高速摄像机可以采用高速摄像机,每秒占用扩展触发器最多可容纳12000帧,采用可用软件,拍摄图像在同一屏幕上同步分析,透露,在低压下舍入喷嘴,低压和低温环境条件点火早期开始于没有舍入喷嘴。在喷嘴内部的两相(液体和气体)流动的假设条件下,还采用了一种商业CFD发动机仿真软件程序来计算和可视化空化。通过湍流和注射喷射输出获得燃料喷射器喷嘴的入口孔区域发生在燃料喷射器喷嘴的入口孔面积上,沿喷嘴轴的速度分布,通过湍流和注射喷射输出获得。除了入口孔的曲率半径之外,两个喷嘴的几何形状是对称的,完全相同。入口和出口边界条件被定义为40MPa,72MPa和36MPa对应于实验条件的3例。发现沿舍入喷嘴的轴的速度分布高于无舍入距离的速度分布。可以通过在没有舍入的注射喷嘴的情况下产生的空化术语来解释较高速度分布的差异。实验结果验证,圆形脱水入口孔喷嘴的影响不仅可以减少空化,湍流,增加有效流动面积,还可以在低环境温度下进行燃烧过程,对应于柴油发动机的低负载条件。相反,在20和30凹口的高温和燃料泵架的条件下,两种喷嘴的点火延迟相似。

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