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Development and calibration of an enhanced quasi-dimensional combustion model for HSDI diesel engines

机译:HSDI柴油机的增强准尺寸燃烧模型的开发和校准

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摘要

The paper describes the development and validation of a quasi-dimensional combustion model, applicable to any type of high-speed direct-injection (HSDI) diesel engines. In this model, the fundamental in-cylinder processes are taken into account, including turbulence, fuel injection, spray dynamics, ignition, and combustion. In comparison with similar models presented in the literature, a more physical description of average in-cylinder turbulence properties and their interaction with spray dynamics is introduced, as well as a detailed modelling of fuel jet wall impingement. Some experimental measures available in the literature and three-dimensional computational fluid dynamics simulations were considered to calibrate the modelling parameters. These improved sub-models make results accuracy less dependent on the calibration carried out on each engine, so that the same parameter setting can be successfully applied to different combustion chamber configurations. The model was first applied to a small HSDI turbocharged diesel engine. The specific calibration was supported by both experimental and simulation results, the latest being obtained from the three-dimensional computational fluid dynamics analyses. Then, a different diesel engine was simulated, adopting the same set-up of the model parameters. For both engines, the comparison between experiments and simulation showed a very good agreement in terms of in-cylinder pressures and heat release rates, as well as of average in-cylinder turbulence properties. It is worth mentioning that the two engines had a quite different unit displacement, i.e. 312 and 697 cm3, respectively. As a conclusion, this model was demonstrated to be a reliable tool for addressing the optimization of the main engine design parameters, such as injection rates and timings, combustion chamber base geometry, and so forth.
机译:本文介绍了准尺寸燃烧模型的开发和验证,该模型适用于任何类型的高速直接喷射(HSDI)柴油发动机。在该模型中,考虑了基本的缸内过程,包括湍流,燃料喷射,喷雾动力学,点火和燃烧。与文献中提供的类似模型相比,介绍了平均缸内湍流特性及其与喷雾动力学的相互作用的更多物理描述,以及燃油喷射壁撞击的详细模型。考虑了一些文献和三维计算流体动力学模拟中可用的实验方法来校准建模参数。这些改进的子模型使结果精度不再依赖于在每个发动机上执行的校准,因此相同的参数设置可以成功地应用于不同的燃烧室配置。该模型首先应用于小型HSDI涡轮增压柴油发动机。实验和仿真结果都支持特定的校准,最新的校准是通过三维计算流体动力学分析获得的。然后,采用相同的模型参数设置,模拟了另一台柴油机。对于这两种发动机,实验和仿真之间的比较表明,在缸内压力和放热率以及平均缸内湍流特性方面,都有很好的一致性。值得一提的是,两个引擎的单位排量相差很大,分别为312和697 cm 3 。结论是,该模型被证明是用于解决主机设计参数优化问题的可靠工具,例如喷射速率和正时,燃烧室基础几何形状等。

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  • 来源
    《International Journal of Engine Research》 |2011年第4期|p.311-335|共25页
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  • 作者单位

    Department of Mechanical and Civil Engineering (DIMeC), University of Modena and Reggio Emilia, Modena, Italy;

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