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Multi-objective optimization investigation of natural gas engine operating parameters using model-based methodologies

机译:基于模型的方法的自然燃气发动机运行参数的多目标优化研究

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In order to improve the comprehensive performance of a heavy-duty natural gas engine, the paper developed a strategy to efficiently optimize operating parameters. An approximate mathematical model, which the input control variables were air-fuel ratio and ignition advance angle while the output response were a set of eight core indicators of characterizing the whole performance of engine, was established using response surface method and further validated by test results. A multi-objective and multi-variable optimization function was built with a compromise consideration between the power, economy, emission and thermal load of the engine. The optimal operating parameters under all conditions were obtained by the global optimization with multi-island genetic algorithm. The comparison results showed that, with optimal operating parameters, the engine maintained its original power, but with the drop in gas consumption rate (1.11%), maximum combustion temperature (1.46%) and NO_x emission (97.45%).
机译:为了提高重型天然气发动机的综合性能,本文开发了一种有效优化操作参数的策略。一个近似数学模型,输入控制变量是空燃比和点火前进角,而输出响应是一组八个核心指示器,其表征发动机的整体性能,是使用响应表面方法建立的,并通过测试结果进一步验证。在发动机的电力,经济,排放和热负荷之间令人妥协的考虑,建立了多目标和多变量优化功能。所有条件下的最佳操作参数是通过与多岛遗传算法的全局优化获得。比较结果表明,通过最佳操作参数,发动机保持其原始功率,但随着气体消耗率下降(1.11%),最大燃烧温度(1.46%)和NO_X排放(97.45%)。

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