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首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >Supersonic Virtual Valve Design for Numerical Simulation of a Large-Bore Natural Gas Engine
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Supersonic Virtual Valve Design for Numerical Simulation of a Large-Bore Natural Gas Engine

机译:大型天然气发动机数值模拟的超音速虚拟气门设计

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In many applications of supersonic injection devices, three-dimensional computation that can model a complex supersonic jet has become critical. However, in spite of its increasing necessity, it is computationally costly to capture the details of supersonic structures in intricate three-dimensional geometries with moving boundaries. In large-bore stationary natural gas fueled engine research, one of the most promising mixing enhancement technologies currently used for natural gas engines is high-pressure fuel injection. Consequently, this creates considerable interest in three-dimensional computational simulations that can examine the entire injection and mixing process in engines using high-pressure injection and can determine the impact of injector design on engine performance. However, the cost of three-dimensional engine simulations—including a moving piston and the kinetics of combustion and pollutant production—quickly becomes considerable in terms of simulation time requirements. One limiting factor is the modeling of the small length scales of the poppet valve flow. Such length scales can be three orders of magnitude smaller than cylinder length scales. The objective of this paper is to describe the development of a methodology for the design of a simple geometry supersonic virtual valve that can be substituted in three-dimensional numerical models for the complex shrouded poppet valve injection system actually installed in the engine to be simulated. Downstream flow characteristics of the jets from an actual valve and various virtual valves are compared. Relevant mixing parameters, such as local equivalent ratio and turbulence kinetic energy, are evaluated in full-scale moving piston simulations that include the effect of the jet-piston interaction. A comparison of the results has indicated that it is possible to design a simple converging-diverging fuel nozzle that will produce the same jet and, subsequently, the same large-scale and turbulent-scale mixing patterns in the engine cylinder as a real poppet valve.
机译:在超音速喷射装置的许多应用中,能够模拟复杂的超音速射流的三维计算已变得至关重要。然而,尽管其日益增加的必要性,但是在具有移动边界的复杂的三维几何形状中捕获超音速结构的细节在计算上是昂贵的。在大口径固定式天然气燃料发动机的研究中,高压燃料喷射是当前用于天然气发动机的最有前途的混合增强技术之一。因此,这引起了对三维计算仿真的极大兴趣,这些三维计算仿真可以检查使用高压喷射的发动机的整个喷射和混合过程,并可以确定喷射器设计对发动机性能的影响。然而,就仿真时间要求而言,三维发动机仿真的成本(包括活动的活塞以及燃烧动力学和污染物产生的动力学)很快变得相当可观。一个限制因素是提动阀流的小长度比例模型。这样的长度标尺可以比圆柱体长度标尺小三个数量级。本文的目的是描述一种简单几何超音速虚拟气门设计方法的开发,该方法可在三维数值模型中代替实际安装在要模拟的发动机中的复杂带罩提升气门喷射系统。比较了实际阀和各种虚拟阀的射流的下游流动特性。相关的混合参数,例如局部当量比和湍流动能,在包括活塞-活塞相互作用影响的满量程移动活塞模拟中进行评估。结果的比较表明,可以设计一个简单的会聚-发散燃料喷嘴,该喷嘴将在发动机气缸中产生与真实的提升阀相同的喷射流,并随后产生相同的大比例和湍流比例混合模式。 。

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