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A three-zone heat-release rate model for dual-fuel combustion

机译:双燃料燃烧的三区放热率模型

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摘要

Dual-fuel engines are modified compression ignition engines, where the primary source of fuel is a gaseous fuel, and ignition is provided by a ‘pilot’ injection of a reduced quantity of diesel. The generally accepted understanding of the dual-fuel engine describes its combustion process as proceeding in three stages. Initially, around half of the pilot will burn and entrain some gaseous fuel into an overall fuel-rich process. Subsequently, the remaining pilot fuel burns and entrains an increasing amount of the primary fuel into its reaction zone. In the final stage, a flame propagation process engulfs the remaining gaseous fuel. In this article, a three-zone model for the analysis of heat-release rate during the dual-fuel combustion process will be derived. This model will be tested against data obtained for diesel combustion and then applied to experimental data from a dual-fuel test program. It will be shown that there is little evidence to support the generally accepted description of the dual-fuel combustion process in a direct injection engine. The conclusion of this work is that dual-fuel combustion may be better considered as a diesel combustion process, where the gaseous fuel modifies the reaction zone surrounding each igniting droplet of the pilot fuel.
机译:双燃料发动机是改进的压燃式发动机,其主要燃料来源是气体燃料,并且通过“先导”喷射减少量的柴油来提供点火。对双燃料发动机的普遍接受的理解将其燃烧过程描述为分三个阶段进行。最初,约有一半的飞行员将燃烧并夹带一些气态燃料进入整个燃料丰富的过程。随后,剩余的引燃燃料燃烧并带走越来越多的一次燃料进入其反应区。在最后阶段,火焰传播过程将剩余的气态燃料吞没。在本文中,将得出一个用于分析双燃料燃烧过程中放热率的三区模型。将针对柴油燃烧获得的数据对该模型进行测试,然后将其应用于双燃料测试程序的实验数据。将会显示,几乎没有证据支持直喷式发动机中双燃料燃烧过程的普遍接受的描述。这项工作的结论是,最好将双燃料燃烧视为柴油机燃烧过程,其中,气体燃料会改变围绕引燃燃料每个点燃液滴的反应区。

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