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OPTIMIZING THE SHAPE OF A COMPRESSION-IGNITION ENGINE COMBUSTION CHAMBER BY USING SIMULATION TESTS

机译:通过模拟测试优化压燃式发动机燃烧室的形状

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摘要

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:压燃式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可提高燃烧速率,并控制废气排放。燃烧系统质量标准之一是获得足够高的燃烧过程热力学指标,这些指标是通过正确的燃烧室几何形状获得的。它的形状会影响燃料雾化过程,燃料剂量的湍流,蒸发和燃烧过程。优化燃烧室的形状是证明正确执行燃烧过程的决定性因素之一。本文介绍了通过使用优化方法选择燃烧室形状(三个选定的燃烧室尺寸的变化)的方法。使用拉丁超立方体方法在保持相关结构的同时生​​成多维数据。通过使用Nelder-Mead方法进行腔室优化。在选定的发动机工况下,针对三个发动机负荷值(由平均指示压力确定)优化了燃烧室的形状。提出的发动机燃烧室优化方法可用于低速和高速柴油推进发动机(特别是在海上运输应用中)。

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