海拔高度对电动涡轮复合发动机废气能量回收影响的热力学分析

L. Leng, Jianghua Cheng, Lei Shi, K. Deng
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引用次数: 0

摘要

涡轮增压发动机的燃油经济性随着海拔高度的升高而下降,这是一个亟待解决的问题。涡轮复合技术是一种在非设计海拔高度充分回收废气能量、降低发动机油耗的有前途的技术,但它会受到海拔高度造成的环境边界的影响。本研究通过热力学分析,揭示了海拔高度对涡轮复合式发动机排气能量回收的影响和机理。结果表明,在不同海拔高度下,涡轮复合式发动机的系统总输出功率均高于基础发动机,最大提高比例可达 4.3%;且随着海拔高度的增加,总输出功率劣化程度降低。当海拔升至 4 千米时,涡轮复合发动机的排气能量利用系数仅下降约 2%。根据能量和放能分析,废气能量的充分回收和利用有助于提高涡轮增压发动机的海拔适应性。在发动机转速为 1800 r/min 时,涡轮复合式发动机在保持发动机功率不变的情况下的最大飞行高度为 4.66 km。因此,涡轮复合式柴油发动机可高效运行的海拔范围扩大了。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Thermodynamic analysis on the effect of altitude on the exhaust energy recovery of electric turbocompound engines
The deterioration of fuel economy for turbocharged engines with altitude is an urgent problem. Turbocompounding is a promising technology to fully recover exhaust energy and reduce engine fuel consumption at off-design altitudes, but it is affected by the environmental boundary caused by altitude. In this study, the effect and mechanism of altitude on the exhaust energy recovery of turbocompound engines were revealed via thermodynamic analysis. The results show that the total system power output of the turbocompound engine is higher than that of the base engine at different altitudes, the maximum improvement percentage of which reaches up to 4.3%; and the total power output deteriorates less with increasing altitude. When the altitude increases to 4 km, the exhaust energy utilization coefficient of turbocompound engine decreases by only about 2%. Based on energy and exergy analysis, full recovery and utilization of exhaust energy contribute to improving the altitude adaptability of turbocharged engines. The maximum altitude while maintaining the engine power constant for the turbocompound engine is 4.66 km under an engine speed of 1800 r/min. Thus, the altitude range over which turbocompound diesel engines can operate efficiently is widened.
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