首页> 美国卫生研究院文献>Heliyon >Analysis of diesel engine injector nozzle spray characteristics fueled with residual fuel oil
【2h】

Analysis of diesel engine injector nozzle spray characteristics fueled with residual fuel oil

机译:柴油发动机喷射器喷嘴喷射特性的分析用剩余燃料油燃料

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

Experimental analysis on the spray characteristics of a diesel engine injector nozzle fueled with Residual Fuel Oil (RFO) was carried out in this study. To achieve this, the fuel was characterized to determine its physicochemical properties, and an experimental set up was designed to visualize and capture the spray pattern of the fuel. The images obtained were processed and analysed using Image J software to determine the spray length, spray cone angle, spray area, spray volume, and spray velocity values of the fuel. Experimental results obtained agree with validation models and reveal that spray parameter values of RFO are higher than those of diesel fuel. The values of spray parameters of RFO such as 456mm spray length, 2.85mm Sauter Mean Diameter (SMD) and the low spray cone angle of 12.69°, led to a higher spray volume causing the engine to run on a rich mixture after initial start-up conditions. This would create such challenges as reduction in power and clogging of injector nozzle tip due to an increase in carbon deposits. Regression models generated reveal that these challenges could be eliminated when the spray parameters run on optimal values of 256mm, 6.41cm , 16.18cm , 0.96 mm/s and 13.59° for the spray length, spray area, spray volume, spray velocity and the spray angle respectively. These optimal values were obtained when the engine fuel injection time was set to 500μs while running on fuel of viscosity 4.305 mPa.s and temperature of 48 °C.
机译:本研究开展了用残余燃料油(RFO)燃料柴油发动机喷射器喷嘴喷射特性的实验分析。为此,燃料的特征在于确定其物理化学性质,设计实验组设计以可视化和捕获燃料的喷雾模式。使用图像J软件处理并分析所获得的图像,以确定燃料的喷雾长度,喷雾锥角,喷射面积,喷雾体积和喷射速度值。获得的实验结果与验证模型一致,并揭示RFO的喷射参数值高于柴油燃料。 RFO的喷涂参数值如456mm喷雾长度,2.85mm落刀平均直径(SMD)和12.69°的低喷雾锥角,导致更高的喷雾体积,导致发动机在初始启动后在丰富的混合物上运行条件。这将产生这种挑战,因为由于碳沉积物的增加,喷射器喷嘴尖端的功率和堵塞的挑战。生成的回归模型揭示了当喷射参数在256mm,6.41cm,16.18cm,0.96 mm / s和13.59°的最佳值上运行时可以消除这些挑战,用于喷射长度,喷雾面积,喷雾体积,喷雾速度和喷雾剂分别的角度。当发动机燃料喷射时间设定为500μs时,获得了这些最佳值,同时在粘度的燃料上运行4.305MPa.s和48℃的温度。

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号