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Physics Based Control Oriented Model for HCCI Combustion Timing

机译:HCCI燃烧正时的基于物理的控制导向模型

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Incorporating homogeneous charge compression ignition (HCCI) into combustion engines for better fuel economy and lower emission requires understanding the dynamics influencing the combustion timing in HCCI engines. A control oriented model to dynamically predict cycle-to-cycle combustion timing of a HCCI engine is developed. The model is designed to work with parameters that are easy to measure and to have low computation time with sufficient accuracy for control applications. The model is a full-cycle model and consists of a residual gas model, a modified knock integral model, fuel burn rate model, and thermodynamic models. In addition, semi-empirical correlations are used to predict the gas exchange process, generated work and completeness of combustion. The developed model incorporates the thermal coupling dynamics caused by the residual gases from one cycle to the next cycle. The model is parameterized by over 5700 simulations from a detailed thermokinetic model and experimental data obtained from a single-cylinder engine. Cross-validation of the model with both steady-state and transient HCCI experiments for four different primary reference fuel blends is detailed. With seven model inputs, the combustion timing of over 150 different HCCI points is predicted to within an average error of less than 1.5 deg of crank angle. A narrow window of combustion timing is found to provide stable and efficient HCCI operation. ©2010 American Society of Mechanical Engineers
机译:将均质充量压缩点火(HCCI)集成到内燃机中以提高燃油经济性和降低排放要求了解影响HCCI发动机燃烧正时的动力学。开发了一种用于动态预测HCCI发动机的逐周期燃烧正时的面向控制模型。该模型旨在使用易于测量的参数进行工作,并具有较短的计算时间,并且对于控制应用具有足够的精度。该模型是一个全周期模型,由残余气体模型,改进的爆震积分模型,燃料燃烧率模型和热力学模型组成。此外,半经验相关性可用于预测气体交换过程,产生的功和燃烧的完整性。开发的模型结合了由一个循环到下一循环的残留气体引起的热耦合动力学。该模型通过详细的热动力学模型和从单缸发动机获得的实验数据进行了5700多次仿真,进行了参数设置。详细介绍了针对四种不同的主要参考燃料混合物的稳态和瞬态HCCI实验对模型的交叉验证。通过七个模型输入,可以预测超过150个不同HCCI点的燃烧正时,其平均误差在小于曲柄角1.5度的范围内。发现燃烧定时的狭窄窗口可提供稳定且有效的HCCI操作。 ©2010美国机械工程师学会

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