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Optimizing the Shape of a Compression-Ignition Engine Combustion Chamber by Using Simulation Tests

机译:通过使用仿真试验优化压缩点火发动机燃烧室的形状

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Modern solutions used in compression-ignition internal combustion engines are quite similar to each other. The use of high-pressure, direct fuel injection results in high combustion rates with controlled exhaust emissions. One of the combustion system quality criteria is to obtain adequately high thermodynamic indicators of the combustion process, which are obtained through, among others, the right combustion chamber geometry. Its shape influences the fuel atomization process, turbulence of fuel dose, evaporation and the combustion process. Optimizing the combustion chamber shape is one of the decisive factors proving the correct execution of the combustion process. This article presents the methodology of choosing the combustion chamber shape (changes of three selected combustion chamber dimensions) by using the optimization methods. Generating multidimensional data while maintaining the correlation structure was performed by using the Latin hypercube method. Chamber optimization was carried out by using the Nelder-Mead method. The combustion chamber shape was optimized for three engine load values (determined by the average indicated pressure) at selected engine operating conditions. The presented method of engine combustion chamber optimization can be used in low and high speed diesel propulsion engines (especially in maritime transport applications).
机译:压缩点火内燃机中使用的现代解决方案彼此非常相似。使用高压,直接燃油喷射导致高燃烧速率与受控排放。其中一种燃烧系统质量标准是通过右燃烧室几何形状获得通过燃烧过程的充分高热力学指示器。其形状影响燃料雾化过程,燃料剂量的湍流,蒸发和燃烧过程。优化燃烧室形状是证明燃烧过程正确执行的决定性因素之一。本文介绍了选择燃烧室形状的方法(三种选定燃烧室尺寸的变化)通过使用优化方法。通过使用拉丁超立体方法执行在保持相关性的同时产生多维数据。通过使用Nelder-Mead方法进行室优化。在所选择的发动机操作条件下针对三个发动机负载值(由平均指示的压力决定)进行了优化的燃烧室形状。发动机燃烧室优化的呈现方法可用于低速和高速柴油推进发动机(特别是在海运应用中)。

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