Performance analysis and multi-objective optimization of irreversible Diesel cycle with non-ideal gas working fluid

IF 3 3区 工程技术 Q2 CHEMISTRY, ANALYTICAL
Di Wu, Yanlin Ge, Lingen Chen, Shuangshuang Shi, Huijun Feng
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引用次数: 0

Abstract

In the early research process, the ideal gas was taken as the research object, but in practice, the working fluid was all non-ideal gas, so it is of great significance to study performance of actual internal combustion engine with non-ideal gas. This study utilizes an irreversible Diesel cycle model, which has been established in the previous literature, and considers various irreversible loss terms and specific heat model of non-ideal gas working fluid, to perform cycle performance analysis and multi-objective optimization. Compression ratio (\(\gamma\)) is taken as optimization variable to optimize efficiency (\(\eta\)), dimensionless power (\(\overline{P}\)), dimensionless power density (\(\overline{{P_{{\text{d}}} }}\)) and dimensionless ecological function (\(\overline{E}\)). The results show that there are optimal \(\gamma\) s to maximize the four-objective functions (\(\eta_{\max }\), \(\overline{P}_{\max }\), \(\overline{{P_{{\text{d}}} }}_{\max }\) and \(\overline{E}_{\max }\)); with the rises of irreversible loss terms, the \(\eta_{\max }\), \(\overline{P}_{\max }\), \(\overline{{P_{{\text{d}}} }}_{\max }\) and \(\overline{E}_{\max }\) all drop. As freedom degree of monatomic gas changes from 1 to 3, only \(\eta_{\max }\) drops and the other three-objective functions rise. When \(\overline{P} - \eta - \overline{E} - \overline{P}_{{\text{d}}}\) is optimized and \(\gamma_{{{\text{opt}}}}\) is mainly concentrated between 3.6 and 5.3, the calculation results of \(\overline{P}_{{}}\) are distributed between 0.85 and 1. The calculation results of \(\eta\) are distributed between 0.46 and 0.52. The calculation results of \(\overline{E}\) are distributed between 0.6 and 1. The calculation results of \(\overline{{P_{{\text{d}}} }}\) are distributed between 0.9 and 1. When \(\overline{P} - \eta - \overline{E} - \overline{P}_{{\text{d}}}\) and \(\overline{P} - \overline{E} - \overline{P}_{{\text{d}}}\) are optimized, deviation indexes obtained by using LINMAP decision-making are the smallest and the best among all optimization results. Multi-objective optimization algorithm is an optimization method to solve multiple conflicting objectives by simulating the competition mechanism in nature. It can find a balance point among multiple objective extremes and thus improve comprehensive performance of Diesel cycle.

Abstract Image

使用非理想气体工作流体的不可逆柴油机循环的性能分析和多目标优化
在早期的研究过程中,以理想气体为研究对象,但在实际应用中,工作流体均为非理想气体,因此研究实际内燃机的非理想气体性能具有重要意义。本研究利用以往文献中已建立的不可逆柴油机循环模型,考虑各种不可逆损失项和非理想气体工作流体的比热模型,进行循环性能分析和多目标优化。以压缩比(\(\gamma\))为优化变量,优化效率(\(\eeta\))、无量纲功率(\(\overline{P}\))、无量纲功率密度(\(\overline{P_{\text{d}}}})和无量纲生态函数(\(\overline{E}\))。结果表明,存在最优的(gamma)s 来最大化四个目标函数(\(eta_{\max }\), (\overline{P}_{max }\), (\overline{P_{text{d}}}}})和(\overline{E}_{\max }\) );随着不可逆损耗项的上升,\(\eta_{\max }\),\(\overline{P}_{\max }\),\(\overline{P_{{\text{d}}} }}_{\max }\) 和\(\overline{E}_{\max }\) 都会下降。当单原子气体的自由度从 1 变为 3 时,只有 \(\eta_{\max }\) 下降,其他三个目标函数上升。当 \(\overline{P} - \eta - \overline{E} - \overline{P}_{{text\{d}}}\) 被优化,并且 \(\gamma_{{text\{opt}}}}\) 主要集中在 3.6 和 5 之间时,计算结果为: \(\overline{P} - \eta - \overline{E} - \overline{P}_{{text\{d}}}\) 被优化。3、 \(overline{P}_{{}}\) 的计算结果分布在 0.85 和 1 之间。\(\overline{E}\) 的计算结果分布在 0.6 和 1 之间。 \(\overline{P}_{{text{d}} }}\) 的计算结果分布在 0.9 和 1 之间。当(\overline{P} - \eta - \overline{E} - \overline{P}_{{text/{d}}})和(\overline{P} - \overline{E} - \overline{P}_{text/{d}}})被优化时,使用LINMAP决策得到的偏差指数是所有优化结果中最小和最好的。多目标优化算法是通过模拟自然界的竞争机制来解决多目标冲突的一种优化方法。它可以在多个目标极值之间找到平衡点,从而提高柴油机循环的综合性能。
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来源期刊
CiteScore
8.50
自引率
9.10%
发文量
577
审稿时长
3.8 months
期刊介绍: Journal of Thermal Analysis and Calorimetry is a fully peer reviewed journal publishing high quality papers covering all aspects of thermal analysis, calorimetry, and experimental thermodynamics. The journal publishes regular and special issues in twelve issues every year. The following types of papers are published: Original Research Papers, Short Communications, Reviews, Modern Instruments, Events and Book reviews. The subjects covered are: thermogravimetry, derivative thermogravimetry, differential thermal analysis, thermodilatometry, differential scanning calorimetry of all types, non-scanning calorimetry of all types, thermometry, evolved gas analysis, thermomechanical analysis, emanation thermal analysis, thermal conductivity, multiple techniques, and miscellaneous thermal methods (including the combination of the thermal method with various instrumental techniques), theory and instrumentation for thermal analysis and calorimetry.
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