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Influence Of Fuel Injection Techniques On CombustionudPerformance Of Multi-Jet Shear Layer Combustionud

机译:燃油喷射技术对燃烧的影响 ud多喷嘴剪切层燃烧的性能 ud

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摘要

Experimental work was carried out to study the effect of fuel injection techniques on the high intensity non-swirl multi-jet shear layer combustion performance of a fourhole conical burner. Two modes of gas oil fuel injection were investigated using a simple type atomiser with four holes positioned 45o to the horizontal axis and can be manually aligned either offset or inline with the hole centre. This enables the fuel to be radially injected either straight into or between the jet shear layers. The test results show that the fuel injection techniques had strong influence on the fuel atomisation and the fuel/air mixing and hence the combustion performance. The NOx results of the offset fuel injection showed a typical NOx profile of an aerodynamic lean/rich combustion. The inline fuel injection produced better combustion performance as compared to the offset injection but was limited by a narrower stability. However, the relatively high combustion inefficiency , as indicated by high CO and UHC emissions, with the inline injection mode even though at high pressure losses indicate the problems of inadequate atomisation and mixing which were attributed mainly to the aerodynamic features of the system concerned.
机译:进行实验工作以研究燃料喷射技术对四孔锥形燃烧器的高强度非旋流多喷嘴剪切层燃烧性能的影响。使用简单的雾化器研究了两种模式的燃油喷射方式,该雾化器具有四个与水平轴成45o位置的孔,并且可以手动对准孔中心偏移或成一直线。这使得燃料能够被径向地直接喷射到射流剪切层中或射流剪切层之间。测试结果表明,燃油喷射技术对燃油雾化,燃油/空气混合以及燃烧性能有很大影响。补偿燃料喷射的NOx结果显示出典型的NOx浓淡的空气动力学特性。与偏置喷射相比,直列燃料喷射产生了更好的燃烧性能,但受到狭窄稳定性的限制。但是,即使是在高压损失下,即使在高压下也存在较高的燃烧效率,如高CO和UHC排放所指示的直列喷射模式,这表明雾化和混合不充分的问题主要归因于相关系统的空气动力学特性。

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  • 作者

    Mustafa A.; Andrews G. E.;

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  • 年度 2003
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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