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Optimization of critical angle, distance and flow rate of secondary fuel injection in DI diesel engine using computational fluid dynamics

机译:使用计算流体动力学优化DI柴油机中辅助燃料喷射的临界角度,距离和流速

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This study presents the optimization of the intake manifold and the optimized flow rate of the acetylene gas which actsas a low reactivity fuel to achieve the superior performance and emission characteristics used in the Reactivity controlledcompression ignition (RCCI) engine. Intake manifold is one of the engine components which are an important factorin determining the quality of combustion. A very recent evolution of the RCCI engine using the low temperature combustiontechnique requires a low reactivity fuel which is injected through the secondary fuel injector. The secondaryfuel injector must be designed and optimized to allow the acetylene gas to maximize the engine performance and theamount of acetylene gas in liters per minute required for better combustion. If the secondary fuel injector is mountedapart from the critical point, then the performance of the RCCI engine may be poor and also if the acetylene gas is notsupplied properly, there is a risk of poor combustion and also if the acetylene gas is supplied excessively, there is a riskof knocking along with the backfire due to the excess fuel charge accumulation during the combustion process. Physicaltesting of the secondary fuel injector in the intake manifold with different angles, distance and flow rate of supply ofacetylene gas is time and cost consuming process. To mitigate this issue optimization is done through computationalfluid dynamics principles comes in handy to minimize time and money. In our study, ANSYS-FLUENT software is used forsimulation purposes. Optimization of acetylene gas injector distance is carried out by analyzing the pressure contours atthe entrance of the combustion chamber. The optimized flow rate of acetylene gas and the injector inclination is foundby analyzing the flow contours of turbulent kinetic energy and turbulent dissipation rate.
机译:本研究提出了用于乙炔气的进气歧管的优化和作用的乙炔气体的优化流速作为低反应性燃料,实现了对照控制的优越性和发射特性压缩点火(RCCI)发动机。进气歧管是一种是一个重要因素的发动机组件之一在确定燃烧质量方面。使用低温燃烧的RCCI发动机最近的进展技术需要一种低反应性燃料,其通过次级燃料喷射器注入。中学必须设计和优化燃料喷射器,以允许乙炔气体最大化发动机性能和需要更好的燃烧所需的乙炔气体的量。如果安装二次燃料喷射器除了临界点外,RCCI发动机的性能可能差,如果乙炔气不是正常供应,燃烧不良,如果乙炔气体过度供应,则存在风险由于燃烧过程中的过剩燃料电荷积累而导致的燃料电荷延长。身体的用不同角度,距离和流速的进气歧管中的次级燃料喷射器测试乙炔气是时间和成本耗费过程。为了减轻这个问题,优化是通过计算完成的流体动力学原理方便,以尽量减少时间和金钱。在我们的研究中,ANSYS-FLUENT软件用于模拟目的。通过分析压力轮廓进行乙炔气体喷射器距离的优化燃烧室的入口。发现了乙炔气体的优化流速和喷射器倾斜度通过分析湍流动能和湍流耗散速率的流量轮廓。

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