Assessment of altitude effects based on the consumption behavior of a piston-prop engine by entropy approach

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE Aircraft Engineering and Aerospace Technology Pub Date : 2024-08-05 DOI:10.1108/aeat-02-2024-0028
Mehmet Ziya Sogut
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Abstract

Purpose

The altitude and weather conditions affect directly fuel consumption and engine efficiency of the aircraft engines. The thermo-physical properties of the weather of altitude play a significant role in this process. Unfortunately, engine performance based on altitude conditions also causes waste heat and environmental pollution due to engine entropy generation. However, environmental impact assessment is needed to improve environmental sustainability. This study aimed to analyse the energy and environmental performance of a piston engine based on altitude conditions.

Design/methodology/approach

This study is based on the entropy approach, and it aims to assess the environmental impact of the engine. Exergy analysis with together two new indices to evaluate the environmental effects caused by the engine under altitude conditions was used.

Findings

The analysis reveals that the exergy efficiency of the piston engine is 23.9% on average for the three referenced altitudes, while the exergy efficiency difference between altitude boundary conditions is 11%. In addition, the entropy production of the engine is on average 10.55 kW/K. In this case, the environmental pollution potential resulting from the entropy production of the engine is on average 3.29 times higher due to reversible conditions, while the improvement rate was found to be 58%.

Originality/value

This analysis shows that engine efficiency increases as altitude increases. Similarly, it can also be said that the environmental impacts are reduced and the improvement of the engine has opportunities for operational processes. Besides, in the study, some suggestions for motor performance impact analysis were presented.

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用熵法评估基于活塞螺旋桨发动机消耗行为的高度效应
目的 高度和天气条件直接影响飞机发动机的燃料消耗和效率。在这一过程中,海拔天气的热物理性质起着重要作用。遗憾的是,基于高度条件的发动机性能也会因发动机熵的产生而造成废热和环境污染。然而,为了提高环境的可持续性,需要进行环境影响评估。本研究旨在分析基于海拔条件的活塞式发动机的能源和环境性能。设计/方法/途径本研究基于熵方法,旨在评估发动机对环境的影响。结果分析表明,活塞发动机在三个参考海拔高度下的平均放能效率为 23.9%,而不同海拔高度边界条件下的放能效率差异为 11%。此外,发动机产生的熵平均为 10.55 kW/K。在这种情况下,由于可逆条件,发动机的熵产生所造成的环境污染潜力平均高出 3.29 倍,而改善率为 58%。同样,也可以说对环境的影响减少了,发动机的改进也为运行过程带来了机会。此外,研究还提出了一些关于发动机性能影响分析的建议。
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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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